Next Article in Journal / Special Issue
Preparation and Properties of Elastic Mullite Fibrous Porous Materials with Excellent High-Temperature Resistance and Thermal Stability
Previous Article in Journal
Structural and Electrochemical Evolution of Water Hyacinth-Derived Activated Carbon with Gamma Pretreatment for Supercapacitor Applications
Previous Article in Special Issue
Reducing Water Absorption and Improving Flexural Strength of Aluminosilicate Ceramics by MnO2 Doping
 
 
Search for Articles:
Title / Keyword
Author / Affiliation / Email
Journal
Article Type
 
 
Advanced Search
 
Section
Special Issue
Volume
Issue
Number
Page
 
Journals
Materials
Volume 17
Issue 13
10.3390/ma17133234
materials-logo
Submit to this Journal Review for this Journal Propose a Special Issue
► Article Menu

Article Menu

share Share announcement Help format_quote Cite question_answer Discuss in SciProfiles thumb_up
...
Endorse textsms
...
Comment
first_page
settings
Order Article Reprints
Font Type:
Arial Georgia Verdana
Font Size:
Aa Aa Aa
Line Spacing:
Column Width:
Background:
Article

High-Emissivity Double-Layer ZrB2-Modified Coating on Flexible Aluminum Silicate Fiber Fabric with Enhanced Oxidation Resistance and Tensile Strength

by
Wei Li
,
Xueying Zhang
,
Liwen Yan
,
Anran Guo
,
Haiyan Du
and
Jiachen Liu
*
Key Laboratory of Advanced Ceramics and Machining Technology of Ministry of Education, School of Materials Science and Engineering, Tianjin University, Tianjin 300072, China
*
Author to whom correspondence should be addressed.
Materials 2024, 17(13), 3234; https://doi.org/10.3390/ma17133234
Submission received: 28 April 2024 / Revised: 24 June 2024 / Accepted: 26 June 2024 / Published: 1 July 2024
(This article belongs to the Special Issue Advanced Ceramic and Glass Materials: Preparation, Characterization and Applications—2nd Edition)
Browse Figures
Versions Notes

Abstract

:
Fibers crystallize and become brittle at high temperatures for a long time, so the surface coating must maintain long-lasting emission performance, which requires superior antioxidant properties of the high-emissivity fillers. To improve the radiation performance of the coating and the tensile strength of the fiber fabric, a double-layer coating with high emissivity was prepared on the surface of flexible aluminum silicate fiber fabric (ASFF) using MoSi2 and SiC as emissive agents. The incorporation of borosilicate glass into the outer coating during high-temperature oxidation of ZrB2 results in superior encapsulation of emitter particles, effectively filling the pores of the coating and significantly reducing the oxidation rate of MoSi2 and SiC. Furthermore, the addition of an intermediate ZrO2 layer enhances the fiber bundle’s toughness. The obtained double-coated ASFF exhibits an exceptionally high tensile strength of 57.6 MPa and a high bond strength of 156.2 kPa. After being subjected to a 3 h heating process, the emissivity exhibits a minimal decrease of only 0.032, while still maintaining a high value above 0.9. The thermal insulation composites, consisting of a flexible ASFF matrix and a ZrB2-modified double-layer coating, exhibit significant potential for broad applications in the field of thermal protection.

1. Introduction

During near-space flight and re-entry, the compression of the high-speed airflow and high-speed dynamic friction between the hypersonic aircraft and the atmosphere will generate high thermal energy, namely aerodynamic heating [1,2,3,4,5]. Consequently, effective thermal protection is imperative to mitigate inward heat transfer, such as using carbon fiber composite materials and high-temperature-resistant alloy materials, designing cooling systems, or using insulation layers to ensure the safe operation of an aircraft’s internal components [6,7,8]. The thermal protection system (TPS) on the leeward side of the spacecraft usually consists of a flexible felt fiber and a high-emissivity coating that dissipates and isolates heat energy. The felt fiber demonstrates a layered quilted structure comprising two layers of fiber cloth enveloping an internal layer of cotton fiber, which are meticulously stitched together using fiber threads [9,10]. The felt fiber exhibits low thermal conductivity and marvelous flexibility, enabling it to tightly adhere to the fuselage surface. Nonetheless, under prolonged use at high temperature, the fiber undergoes crystallization, inducing functional failure detrimental to application stability. A coating spayed on the surface can effectively improve the temperature resistance of the fiber blanket by radiating the heat, which is important in ensuring the reusability of TPS [11,12].
The key constituents of a high-emissivity coating encompass a filler with high emissivity and the binder. The emissivity depends on the temperature and type of the material, as well as its surface condition, with the material itself being the most direct factor determining the emissivity. MoSi2, TaSi2, SiC, SiB4, and SiB6 are potential options for high-emitter fillers [13,14,15,16,17]. Guo et al. prepared silica-coated MoSi2 powder through a sol–gel process. The theoretical thickness of the cladding shell layer was about 60 nm, and the MoSi2@SiO2 coating showed satisfactory isothermal cyclic oxidation resistance at 400–600 °C for 12 h, with an oxidation weight gain rate of less than 1 wt.% [18]. Gao et al. mixed SiB6 and Si into TaSi2 and SiC powders for modification and then prepared a high-emissivity coating with high antioxidant properties on alumina fiber fabric (AFF). The borosilicate glass phase generated by SiB6 oxidation at high temperatures healed the cracks on the coating and encapsulated the emitter. After calcination at 1200 °C, the tensile strength of the AFF with 2.5% SiB6 increased by 85%, while the average spectral emissivity in the 2–14 μm band reached 0.95 at room temperature (RT) [19]. Shao et al. prepared a multiphase coating of MoSi2–ZrO2–borosilicate glass with SiB6 by slurry impregnation and sintering, and the resulting coating formed a gradient structure. The dense surface layer provided oxidation resistance and a waterproofing effect, while the internal porous layer greatly enhanced the thermal shock resistance and the adhesion of the coating to the substrate. The coating with 3 wt.% SiB6 added had an emissivity of 0.85 in the 0.8–2.5 μm band at RT [20]. Zhang et al. used SiC and ZrO2 as emissive agents to prepare a bilayer coating with high emissivity on the ASFF. Compared with the original fabric, the double-layer coated fabric had 70% higher tensile strength (75 MPa) after calcination at 1100 °C. Phase analysis after heat treatment revealed that the thermal resistance of fiber fabric markedly increased, with the emissivity in the short-wavelength range reaching 0.93 [21]. These studies consider antioxidant measures when using silicide emitters, but in cases where the fiber clusters on the fiber cloth are bent and uneven, it is necessary to consider the density and continuity of the coating shell at high temperatures.
MoSi2 and SiC are emitters commonly used for high-emissivity coatings but are ball-milled to fine powders before being added to the coating. The high specific surface area and reactivity of the resulting powders are therefore susceptible to oxidation [22,23]. To reduce the exposure of MoSi2 and SiC to oxygen, a cladding structure is usually formed by in situ generation or viscous flow phase coverage [24,25]. ZrB2 has been extensively studied in ultra-high-temperature ceramics, especially ZrB2–SiC composites, and the synergistic effect of oxidization revealed a complex process involving the vapor-based transport of SiO and B2O3 gas, liquid B2O3 transport, and the precipitation of dissolved ZrO2 [26,27]. The glassy oxide formed a protective oxide skin, so the incorporation of ZrB2 into MoSi2 and SiC powders may be an effective way to reduce the oxidation rate [28]. Nowadays, coating preparation methods usually utilize multiple emissivity agents, as the synergistic and supplementary effects of the radiation characteristics in the high-emissivity material composite at different temperatures and bands can enhance the overall radiation performance of the composite coating [3,29,30,31].
An overly dense coating is not conducive to the flexibility of fibers, but a less dense coating can easily exacerbate the oxidation of the emitter, so a porous intermediate layer is added in this work [32]. ZrO2 is an oxide with high emissivity in the 8–14 μm band, a high melting point, and low thermal conductivity [33,34]. Monocyclic ZrO2 (m-ZrO2) converts into tetragonal ZrO2 (t-ZrO2) at temperatures above 900 °C. These metastable t-ZrO2 particles can exist stably in the coating and undergo martensitic transformation under pressure to absorb energy and improve the toughness of the material [35,36]. ZrO2 can similarly serve as a network-forming agent and transform the peak of [BO3] to [BO4] in borosilicate glass, improving the network structure and chemical stability of the glass [37,38,39].
Rigid glass is widely employed as a bonding agent for high-temperature insulation coatings due to its excellent thermal stability, mechanical properties, and self-healing ability [40]. However, using glass powder as a binder raw material necessitates high-temperature sintering, which is prone to matrix shrinkage deformation and cristobalite phase precipitation from the glass during cooling [29,41]. Comparatively, the utilization of silica sol as a binder material significantly reduces the required curing temperature while maintaining reliable bonding performance at elevated temperatures. Therefore, it is better suited for collaboration in the context of flexible felt fiber with a relatively limited temperature resistance [42,43].
In this work, two emitters, MoSi2 and SiC, are selected to promote the broad-spectrum radiation performance of the coating. Furthermore, the neutral silica sol as a binder lessens the density of the coating due to the shrinkage of the gel during curing, which leads to cracking. Therefore, ZrB2 is added to form a borosilicate glass phase at elevated temperatures to improve the density and oxidation resistance of the coating. At the same time, the ZrO2 silica sol coating was prepared as an intermediate layer to mitigate glass-to-fiber bonding failure during melting. The effects of coatings containing varying ZrB2 content on the tensile strength, bonding strength between the coatings and fabric, and thermal performance of the ASFF after heat treatment at different temperatures were investigated. The cross-sectional morphology of the double-layer coating was analyzed following high-temperature calcination, while the tensile strength and radiation properties of the single-layer and double-layer fabric coatings were compared.

2. Materials and Methods

2.1. Materials

Aluminum silicate fiber fabric (ASFF; 0.26 ± 0.02 mm thickness, warp and weft density of the plain fabric, 20 × 20 roots/cm2; Hubei Feilihua Quartz Glass Co., Ltd., Jingzhou, China) was used as the matrix for the series of experiments in this study. MoSi2 (3–5 μm, 99%), SiC (3–5 μm, 99%), ZrB2 (3–5 μm, 99.5%), and ZrO2 (0.5 μm, 99.9%) powders were provided by Eno Materials (Cangzhou, China). Octanol and polyacrylamide were provided by Tianjin Xiensi Biochemical Technology Co., Ltd. (Tianjin, China), which were used as defoamer and dispersant agents, respectively. The solid content of neutral silica sol (Zhejiang Zhiti Nawei New Material Co., Ltd., Taizhou, China) was 25%, with a particle size of 10 nm and a pH of 7. All chemicals and raw materials were used as received.

2.2. Preparation of the Double-Layer Coating

The double-layer coatings were prepared as in Figure 1. Polyacrylamide (0.5 wt.%) and octanol (0.5 wt.%) were added to neutral silica sol as dispersing and defoaming agents, respectively, and the sol was mixed evenly by magnetic stirring. MoSi2, SiC, and ZrB2 powders were then mixed at different mass ratios (Table 1), added to the mixed silica sol, and stirred on a ball mill at 300 r/min to obtain a uniform and stable coating mixture. The coating paste was uniformly sprayed on the ASFF at a loading rate of 60–80 g/m2 and dried at RT for 8 h to obtain a single layer of MoSi2–SiC–ZrB2 coated fabric for subsequent study. In addition, a ZrO2 coating slurry was prepared by mixing ZrO2 powder and silica sol at a 1:1 mass ratio. The ZrO2 slurry as an intermediate layer was evenly sprayed on the surface of the ASFF with a load of 50–70 g/m2. After drying at 80 °C for 2 h, the MoSi2–SiC–ZrB2 coating with 5% ZrB2 was sprayed onto the middle layer to obtain a double-layer coating.

2.3. Characterization and Testing

The phase composition of the coating surface was identified by X-ray diffraction (XRD, D/Max-2500, Rigaku, Akishima-shi, Japan) using Cu-Kα radiation in the range of 2θ = 10–60°. The phases from the XRD spectrum were identified by using the Powder Diffraction File (PDF) database of the International Diffraction Data Center (ICDD). Scanning electron microscopy (SEM) coupled with energy dispersive spectrometry (SEM/EDS, Hitachi SU1510, Tokyo, Japan) was used to survey the coating surface morphology and perform elemental analysis. Fourier-transform infrared spectroscopy (FTIR) was recorded on a NEXUS-670 Fourier transform infrared spectrophotometer using KBr pellets. The samples were prepared in 0.2–0.25 mm thick KBr pellets (1 mg in 100 mg of KBr). Based on the GB/T 1447-2005 standard [44], the tensile strength of the coated ASFF was tested using a mechanical testing machine (LD24.204, Lishi Instruments Co., Ltd., Shanghai, China) at a loading speed of 0.5 mm/min. Five specimens from each group were selected to test the mechanical properties, and the average value was calculated. The bonding strength between the coating and substrate was measured using an electronic universal testing machine. The substrate with dimensions of 30 × 30 mm was covered with the coating, and the fabric was adhered to an aluminum plate with 3M double-sided tape to conduct combined strength tests according to the GB/T 5210-2006 standard [45]. The infrared absorption spectra of the specimens were collected at RT on an infrared spectrometer (SR-5000 N, CI Systems, Jerusalem, Israel), with the spectral range of the thermal radiation emitted from the surface ranging from 2 to 14 μm. The thermal insulation properties of the flexible felt fiber were tested using a thermal infrared imager (LT7-P, Zhejiang Dali Technology Co., Ltd., Hangzhou, China).

3. Results and Discussion

3.1. SEM Images and XRD Spectra of MoSi2–SiC–ZrB2 Powders after High-Temperature Heat Treatment

To demonstrate that ZrB2 can generate B2O3 to shape the borosilicate glass phase with molten SiO2 in a high-temperature environment, two sets of MoSi2, SiC powder, and additional ZrB2 powder samples were ball-milled with water, dried, and heat-treated for 1 h at 1200 °C. These two different mixed powders were named MS and MSZ, respectively. The SEM images of the samples at RT and after heat treatment at 1200 °C are shown in Figure 2. There seems to be no significant discrepancy between the two types of particles at RT (Figure 2a,c). The emitter particles of the MoSi2–SiC sample undergo oxidation in large quantities after 1200 °C, and the generated square quartz phase aggregates on the particle surfaces to form larger independent microspheres (Figure 2b) [23]. In comparison, the MSZ sample with added ZrB2 after heat treatment has flowing parts wrapped around and connected with each particle. The main component of these flowing parts is the borosilicate glassy phase (Figure 2d).
The XRD spectra of the samples after heat treatment at 1200 °C are shown in Figure 3. The intensities of the characteristic MoSi2 and SiC peaks in the MS spectrum exhibit a significant reduction compared to those observed for the MSZ sample. The simultaneous emergence of prominent peaks corresponding to SiO2 and Mo5Si3 indicates the extensive oxidation of both emitters. The MSZ sample spectra exhibit novel peaks corresponding to elemental Mo and Mo4.8Si3C0.6, as the oxidation of ZrB2 removes most of the O2 and prevents the complete oxidation of MoSi2. Concurrently, the formation of a glassy phase comprising SiO2 and B2O3 occurs, effectively encapsulating the emitter particles and facilitating the combination of Mo5Si3 with SiC to yield Mo4.8Si3C0.6. The presence of this enclosed glass phase serves as a barrier against further oxidation of the emitter. In addition, the Mo4.8Si3C0.6 compound exhibits a high melting point of 2100 °C and demonstrates excellent chemical compatibility with SiC and MoSi2 at elevated temperatures, enabling it to effectively impede the passage of O2 [46,47].

3.2. Morphology and XRD Spectra of Single-Layer MoSi2–SiC–ZrB2 Coating and Double-Layer Coatings after Heat Treatment at 1200 °C for Different Times

The surface morphologies of the single-layer coatings with different ZrB2 content after curing are similar, therefore they are not presented, and the surface micro-morphologies after heat treatment at 1200 °C for 1 and 3 h are shown in Figure 4. Under the same heating time, the coating surface containing more ZrB2 exhibits denser and fewer pores. The external layer of the MSS (MoSi2–SiC–Silica sol) coating exhibits a non-dense structure, characterized by particle stacking morphology with prominent pores and bulges resulting from the release of volatile by-products (MoO3 and CO2) and volume expansion-induced protrusions (Figure 4a). The further oxidation of MoSi2 and SiC, along with the contraction of silica sol, leads to the explosion of some fibers under the coating [48]. The exposed fibers are directly subjected to the high-temperature environment, rendering them susceptible to crystallization (Figure 4e). Alongside the emergence of ZrB2-induced flow phases, the glass phase generated at high temperatures promotes particle rearrangements, leading to a denser and smoother coating surface (Figure 4b,c). The borosilicate glass phases can envelop the emitter, preventing oxidation and sealing cracks that may arise during coating gel contraction, thereby reducing or inhibiting heat flow to the interior. The surface morphologies of MSS-3Z coating samples burnt for 1 and 3 h were compared. It was observed that there were additional cristobalite phases because the particles were no longer obvious but were encapsulated and connected by the flowing phase. Furthermore, the silicon–boron ratio in the bonding phase gradually increased, leading to an increase in the softening temperature with prolonged heating duration (Figure 4b,f). The presence of these softened glass phases facilitated the densification process of the coating. After being held at 1200 °C for 1 h, holes reappeared on the surface of the MSS-7Z coating (Figure 4d). Excess B2O3 resulting from the oxidation of ZrB2 was readily volatilized, leading to the formation of residual small pores that serve as channels for oxygen diffusion, while internal fillers’ oxidation caused a loss of flatness in the external coating.
Figure 5 shows the infrared spectra of single-layer coatings with different ZrB2 contents after 1 h of heat treatment at 1200 °C. The orange dashed line in the figure corresponds to the chemical bond associated with the characteristic peak of this wavelength band. The peak located around 700 cm−1 corresponds to the stretching vibration mode of the B-O-B unit. The peak at 850–880 cm−1 is believed to be related to the connection of four non-bridging oxygen [SiO4] units. The peak located around 1150 cm−1 belongs to the stretching vibration of Si-O-Si bonds in the silicon oxygen tetrahedral unit. The peak in the 1250–1500 cm−1 region is related to the stretching vibration of the B-O bond in the [BO3] structural unit. The peak located around 1400 cm−1 corresponds to the [BO3] anti-symmetric stretching vibration mode. The absorption band at a wavenumber of 1640 cm−1 is caused by the bending vibration of H-O-H in free water. From Figure 5, it can be seen that as the amount of ZrB2 added increases, the number of [BO3] structural units in the heat-treated coating samples increases, indicating a higher formation of borosilicate glass.
The XRD patterns of single-layer coating with varying ZrB2 content at RT and after heat treatment at 1200 °C for 1 or 3 h in an air atmosphere are shown in Figure 6. In addition to the diffraction peaks of the three raw materials, a diffraction peak corresponding Mo5Si3, which is the oxidation product of MoSi2, is observed in the coating at RT (Figure 6a). The MoSi2 and SiC powders obtained through ball milling exhibit a remarkably reduced particle size, significantly increased specific surface area, and abundant defects, resulting in diminished oxidation resistance. The severe oxidation of SiC leads to a diminished peak intensity observed in the MSS-0Z sample spectrum, whereas MoO3, formed through the complete oxidation of MoSi2 and Mo5Si3, volatilizes and is absent from the XRD pattern (Figure 6b). The ZrB2 undergoes complete oxidation in the MoSi2–SiC–ZrB2 coatings after heat treatment, as evidenced by the detection of diffraction peaks corresponding to ZrO2 rather than ZrB2. The presence of the Mo4.8Si3C0.6 phase in the ZrB2-added coating indicates a reaction between SiC and Mo5Si3, facilitated by the flow of the borosilicate glass phase, which is recognized as the sole stable ternary phase within the Mo–Si–C system. The generation of Mo4.8Si3C0.6 is accompanied by the concurrent reduction of MoSi2, thereby maintaining a high peak strength for MoSi2 in MSS-5Z, while experiencing a decrease in the peak intensity of Mo5Si3 (Figure 6b). The Mo4.8Si3C0.6 crystal exists as a plethora of irregular lattices, which effectively enhance the asymmetry and lattice vibration of the structural unit. Moreover, owing to its favorable chemical compatibility with MoSi2 and SiC, Mo4.8Si3C0.6 can synergistically synergize with the glass phase to form a protective shell around the emitter particles, thereby effectively inhibiting further oxidation. As the content of ZrB2 increases, an excess B2O3 volatilizes, resulting in the formation of surface holes [49]. External heat flow can then intrude into the interior of the coating through these pathways and come into contact with the fiber, resulting in the increase in the mullite phase peak strength in MSS-7Z. After undergoing a 3 h heat treatment, an increased formation of Mo5Si3 was observed in the MSS-0Z sample, indicating enhanced oxidation of the emitter. Furthermore, the excessive presence of ZrO2 in the MSS-7Z coating can serve as nucleation sites within borosilicate glass, resulting in the crystallization of SiO2 [50]. The weak diffraction peak corresponding to SiO2 in the MSS-5Z spectrum suggests that both MoSi2 and SiC maintain their original states even after prolonged heating, thereby exhibiting excellent emissivity performance.
The cross-sectional SEM images of the fiber fabrics with the single-layer coatings after calcination at 1200 °C for 1 h are shown in Figure 7. The two yellow dashed lines above and below in Figure 7 represent the interface between the coating and resin, as well as the interface between the coating and fiber cloth. The yellow dashed line in the middle is the coating, and the area above the coating is the fiber bundle. After sintering and particle rearrangement, obvious large and fine pores inside the MSS-0Z still remained, maintaining a conspicuous granular shape. The surface of the coating is somewhat concave, as the shrinkage of silica sol and the holes induce the collapse of the coating. The internal pores of MSS-3Z are reduced but still not dense, the MSS-5Z coating achieves densification from the viscous flow of the borosilicate glass phase, and the cross-section of the coating looks relatively smooth, with some molten glass liquid penetrating the interior of the fiber bundles. The portion of the MSS-7Z coating connected to the fiber is flat and compact, but large holes caused by the excessive volatilization of B2O3 still exist outside (Figure 7d). The thicknesses of the MSS-3Z and MSS-5Z coatings remained at approximately 50 µm after heat treatment, whereas the thicknesses of the other two decreased, which can be attributed to the volatilization of the oxidation products.
The cross-section and energy spectrum of the double-coated ASFF sample after heat treatment at 1200 °C for 1 h is shown in Figure 8. The range of the upper and lower layers of coating is roughly marked with yellow dashed lines in Figure 8. The components of the sample shown from bottom to top are the fiber bundles, ZrO2 coating, MSS-5Z coating, and resin curing of the sample for the cross-section shot. After heat treatment, the MSS-5Z coating is partially filled with borosilicate glass, which flows at high temperatures to make the outer layer dense without obvious voids. However, clear holes are still visible at the interface of the ZrO2 coating and fiber bundles. Due to the infiltration of the mobile glass phase, the holes at the interface of the ZrO2/MSS-5Z coating are also filled, making the interface indistinct. The layered interface between the coatings can be roughly distinguished by EDS elemental distribution (Figure 8c,d). Zr is mainly distributed in the ZrO2 layer, while the ZrO2 produced by the oxidation of ZrB2 is not clearly visible in the energy spectrum due to its low content.

3.3. Oxidation Reaction and Mechanism of Fillers in Coatings at High Temperatures

The primary cause for the deterioration of the coating performance lies in the oxidation of the emitter. The high-temperature stability of the MoSi2 and SiC emitters in the borosilicate matrix can be analyzed through a combination of reaction kinetics and thermodynamics. Based on the relevant literature and the XRD analysis, it is inferred that the following reactions will occur in the coating at high temperatures.
2/7MoSi2(s) + O2(g) = 2/7MoO3(s) + 4/7SiO2(s)
5/7MoSi2(s) + O2(g) = 1/7Mo5Si3 (s) + SiO2(s)
1/3MoSi2(s) + O2(g) = 1/3MoO2(s) + 2/3SiO2(s)
1/2MoSi2(s) + O2(g) = 1/2Mo(s) + SiO2(s)
2/5ZrB2(s) + O2(g) = 2/5ZrO2(s) + 2/5B2O3(s)
1/2SiC(s) + O2(g) = 1/2SiO2(s) + 1/2CO2(g)
SiC(s) + 12/7Mo5Si3(s) = 35/21Mo4.8Si3C0.6(s) + 4/7MoSi2(s)
The change in the Gibbs free energy (∆G) versus temperature for each reaction is calculated using the FACT program (Figure 9). It is unpractical to accurately calculate the ∆G of reaction (7) without Mo4.8Si3C0.6 data in the database. At 1200 °C, the ∆G of each reaction can be ordered as follows: reaction (1) > reaction (6) > reaction (3) > reaction (5) > reaction (4) > reaction (2). According to thermodynamic calculations, reaction (2), which generates Mo5Si3 as the by-product, has the lowest ∆G and is most likely to occur. Mo3Si5 was prone to further oxidation into MoO3, while MoO3 and MoO2 generated by reactions (1) and (3) volatilize at high temperature. Since the oxidation of MoSi2, SiC, and ZrB2 is a diffusion-controlled process, the reaction kinetics should also be considered. Existing research has confirmed that reaction (5) is susceptible to occur at temperatures above 1100 °C. Therefore, the oxidation of ZrB2 is completed in the initial stage of heating, and the generated B2O3 will form a eutectic mixture with SiO2 to create the borosilicate glass phase. In addition to oxidizing, part of the SiC will react with Mo5Si3 to generate Mo4.8Si3C0.6 and MoSi2.
The oxidation mechanism diagrams of the MSS-0Z, MSS-5Z, and double-layer coatings calcined at 1200 °C are shown in Figure 10. Before heat treatment, the particles within each coating exhibit a strong interconnection facilitated by the adhesive properties of silica sol. However, numerous tiny pores are observed in the gaps between particle-to-particle stacking. Following a 3 h heat treatment, MoSi2 and SiC on the surface of MSS-0Z coating undergo oxidation to form Mo5Si3, MoO3, and SiO2 compounds. Nevertheless, due to inadequate softening at 1200 °C, SiO2 fails to effectively encapsulate the surfaces of emitter particles. The oxidation reaction, accompanied by significant volume expansion, the release of gaseous products, and the contraction of silica sol, includes extensive cracking within the coating. The gray arrows in Figure 10 represent the contact and release of gases such as O2 and CO2 with the coating surface. These cracks facilitate smooth infiltration and further promote the oxidation of internal SiC and MoSi2. In contrast, ZrB2 in the MSS-5Z coating exhibits preferential oxidation to form B2O3, effectively removing oxygen and generating a borosilicate glass phase with SiO2. Under high-temperature flow, the borosilicate glass phase exhibits a reduction in the diffusion rate of oxygen and effectively encapsulates the internal emitters (MoSi2 and SiC). The formation of oxidation products (i.e., Mo5Si3 and SiO2) is effectively reduced, while simultaneously preserving the morphological stability of the coating. Meanwhile, Mo5Si3 reacted with SiC to form the Mo4.8Si3C0.6 phase in the presence of the glass phase flow, instead of undergoing further oxidation to MoO3. The borosilicate glass phase formed in the double-coated sample at elevated temperatures facilitated the closure of voids within the coating under flow conditions, subsequently infiltrating the internal layer of the ZrO2 coating. Consequently, the two coatings were tightly bonded to facilitate interfacial melting and prevent glass-phase intrusion into the fiber bundles, thereby mitigating fiber degradation.

3.4. Analysis of Mechanical Properties of Single-Layer and Double-Layer Coatings after Heat Treatment at Different Temperatures

To investigate the influence of coatings with varying ZrB2 content on the tensile strength of the ASFF, the tensile strengths of the single-layer coated fiber fabrics were measured after calcination at different temperatures for 1 h (Figure 11a). With increasing heat treatment temperature, the mullite phase gradually precipitates, resulting in the formation of defects on the fiber surface and the coating undergoing localized sintering, which impedes the relative sliding between the fibers and produced axial stress. Thus, the overall tensile strength of the coated fiber fabrics decreases as the temperature increases. At RT, the tensile strength of the MSS-0Z coating is higher than that of the ASFF with the ZrB2 coating, reaching 125.5 ± 5 MPa. The decrease in silica sol content will affect the shaping of gel between fiber gaps, which in turn reduces the fracture of the gel layer and energy dissipates from the separation of the fiber–gel interface. Nonetheless, after high-temperature scorching, the mechanical properties of the ASFF with the MSS-0Z coating were relatively stable at 600–1200 °C, and the tensile strength decreased to about 27.5 MPa at 1200 °C. This is principally due to the oxidation of the emitter, which intensified with the increase in the calcination temperature. The oxidation of the emitter reduces the emissivity of the coating, which makes the ASFF surface gather more heat and accelerates the fiber crystallization. Generated SiO2 melts and penetrates the ASFF, and the subsequent brittle fracture of the ASFF leads to more mullite phase precipitation, defects, and damaged fibers. The tensile strength of the MSS-5Z-coated fabric after heat treatment is the highest among the samples and remains at about 46.5 MPa after burning at 1200 °C, which is 69% higher than that of the MSS-0Z-coated ASFF under the same conditions. ZrB2 mingled into the coating is oxidized to ZrO2, improving the toughness of the coating and the high-temperature oxidation resistance of the emitter. In addition, a high emissivity enhances the radiation of heat. Nevertheless, with the increase in ZrB2 content, the tensile strength of the MSS-7Z-coated fabric decreased sharply to about 35.4 ± 3 MPa after heat treatment at 1200 °C. Excess ZrB2 oxidizes the borosilicate glass phase penetrating between the fiber bundles and excessive ZrO2 as the nucleation site causes glass crystallization, which is not conducive to the mutual removal of fibers.
The tensile strength of the double-layer coated ASFFs with an intermediate layer added on the foundation of the single-layer MSS-5Z coating were measured at different temperatures after insulation for 1 h and then were further compared (Figure 11b). The double-layer coated ASFF exhibited consistently higher tensile strength across all measured temperatures. Considering relevant studies, we believe that the transformation from t-ZrO2 to m-ZrO2 occurred under tensile strain. During the phase transition, energy is absorbed, stress at the crack tip diminishes, and crack propagation is inhibited. The tensile strength of the fabric increased by 11.1 MPa (23.9%) from 46.5 to 57.6 MPa at 1200 °C. The intermediate ZrO2 coating, through phase transition toughening, effectively prevents infiltration of molten borosilicate glass between fiber bundles, thereby reducing fiber damage. Additionally, the thickness of the coating has an impact on the fabric’s tensile strength.
The bonding strength between the ASFF and the coating with different ZrB2 contents after calcination at different temperatures for 1 h is shown in Figure 12a. The bonding strength first decreases and then increases roughly with the heat treatment temperature. The oxidation of SiC and MoSi2 after heat treatment at 600 °C or 900 °C is accompanied by the generation of gaseous products and significant volume expansion that allows for voids and defects to appear at the ASFF/coating interface that are not close in proximity. The bonding strength of the ASFF with MSS-0Z coating is 100.2 ± 9 kPa at 900 °C. Silica sol functions as an adhesive to provide robust cohesion at 1200 °C, and the bonding strength increases to 130.5 ± 4kPa. As the ZrB2 content increased, a more fused borosilicate glass phase was generated to further enhance the bonding ability. Moreover, the higher proportion of B/Si in borosilicate glass led to a decrease in viscosity and improved flowability. At 1200 °C, the bonding strength of ASFF/MSS-7Z reached 190.3 kPa, which was 45.8% higher than that of the MSS-0Z sample. Sample photographs of the coated ASFFs after heat treatment at 1200 °C for 1 h following the bond strength test are shown in Figure 12b. The strong bonding effect of borosilicate glass is clearly observed, while the coating is more inaccessibly completely separated from the ASFF after testing with increasing ZrB2 content.
The bonding strengths of the MSS-5Z and double-layer coatings after calcination for 1 h and pull-out tests are shown in Figure 12c. The bond strength of double-layer coating/ASFF below 900 °C is higher than that of the single-layer coating/ASFF, which is 10.7%, 7.1%, and 9.1% higher at RT, 600 °C, and 900 °C, respectively. The contact part is the ZrO2 layer, which will not cause the coating to peel off the oxidative expansion of the MoSi2 powder at elevated temperatures. The borosilicate glass phase produced by the upper layer penetrates downward into the ZrO2 layer and will not reinforce the interfacial connection between the fiber bundle and the coating. Hence, the binding strength of the double-layer coating/ASFF (156.2 ± 5 kPa) is lower than that of the MSS-5Z sample.

3.5. Comparison of Thermal Insulation Performance between Single-Layer and Double-Layer Coatings

Figure 13a shows the spectral emissivity of the ASFF sprayed with the ZrO2, MSS-5Z, and double-layer coatings at RT in the wavelength range of 2–14 μm. The spectral emissivity of the MSS-5Z and the double-layer coatings show similar trends with wavelength, but an obvious distinction is observed with the ZrO2 coating. The ZrO2 coating exhibits a lower average emissivity in the range of 2–6 μm due to several strong reflection peaks, whereas MSS-5Z and double-layer coated ASFFs have an emissivity above 0.92 in this range, meeting the requirement for radiant TPS. In the 7–14 μm band, the emissivity trend is exactly the opposite, and the ZrO2 coating has a higher emissivity. According to Wien’s displacement law, as the temperature increases, blackbody radiation is principally concentrated in the short-wavelength range. The high-emissivity coating should significantly advance the emissivity in the low band, which is of immense significance for its service at high temperatures. In the emissivity tests, the absorption or reflection of electromagnetic waves by the external coating is prioritized before penetrating the interior of the coating. Therefore, the test mainly collects the reflection effect of the surface coating on electromagnetic waves, and the collaborative absorption effect of the internal coating has less impact. In the 10–14 μm wavelength range, the emissivity curve of MSS-5Z is groove-shaped, and the emissivity decreases by approximately 0.1 due to the inherent defects of SiC particles [51]. Figure 13b shows the average spectral emissivity of different samples without heat treatment at RT. The average emissivity of the ZrO2-coated ASFF is only 0.885. The average emissivity of coatings containing the emissivity filler (i.e., MoSi2 and SiC) is above 0.925, among which the average emissivity of the double-layer coating is the highest (0.949), indicating that the emissivity is affected by several factors simultaneously, such as chemical composition and coating thickness.
The average spectral emissivity of the double-coated ASFF treated at 1200 °C for different times is shown in Figure 13c. The emissivity of the coating showed a decreasing trend with the increase in the heat treatment time. When the heat treatment time reaches 3 h, the surface emissivity of the ASFF remains above 0.91, demonstrating its high emissivity property. The surface of the coating with ZrB2 added forms a silicon-based glass layer at high temperatures. This amorphous structure of long-range disorder can form localized states, whose energy provides conditions for electron transition in the bandgap and promotes short-wave infrared absorption [52]. In addition, the glass layer can mend the pores on the surface of the coating, preclude the entry of oxygen, and improve the oxidation resistance of the MoSi2 and SiC emitters.
The thermal insulation ability of the raw and coated fiber fabrics was characterized using an infrared thermal camera to record thermograms of the surface and back of the sample (Figure 14). A layer of ASFF was covered on the cotton fiber core, the size of the fiber cloth was 100 × 80 mm, and the thickness was 10 mm. The flexible felt fiber was placed 120 mm in front of the butane flame spray gun and heated for 5 min until the temperature of the backside had stabilized. After burning the original ASFF under a flame for 1 min, the maximum temperature at the front center of the ASFF remained stable at around 1383.4 °C, while the back maximum temperature was approximately 294.3 °C (Figure 14a,b). When the ignition time reached 5 min, the back maximum temperature remained stable at about 349.6 °C (Figure 14d). When the MSS-0Z coating was sprayed on the ASFF, the front and back temperatures stabilized at about 1140.8 and 317.4 °C after 1 and 5 min of scorching, respectively (Figure 14e,h). The surface temperature of coated ASFF during the heating process is much lower than that without the coating. This is because the high-emissivity coating can disperse part of the heat on the surface. After 5 min of ignition, the front temperature of the MSS-5Z-coated ASFF decreased by 27% compared to the original ASFF, stabilizing at about 998.8 °C (Figure 14i), while the backside temperature stabilized at 280.5 °C (Figure 14l), decreasing by about 19.8%. The borosilicate glass phase can fill the holes, effectively preventing the further oxidation of the emitter. For high-temperature thermal protection composite materials, the radiation heat transfer mechanism plays a more dominant role than heat conduction and heat convection. A high emissivity corresponds to more heat being radiated out at the same temperature, which reduces the surface temperature of the ASFF. The thickness of the coating also affected the thermal insulation performance, with the thicker double-layer coating providing lower maximum front (954.3 °C) and back (266.7 °C) temperatures under a stable butane flame (Figure 14m,p). According to Figure 13b, a higher emissivity could radiate more surface heat, and a thicker coating reduced the efficiency of heat transfer to the back of the insulation felt. Multiple factors collectively determined that double-layer coatings had better thermal insulation performance.

4. Conclusions

In this study, a glass phase that can fill the internal voids of an ASFF coating was formed by the modification of ZrB2 at high temperatures to leverage the synergistic effect of high-emissivity MoSi2 and SiC fillers and promote the oxidation resistance of the emitter. The addition of a ZrO2 intermediate layer between the ASFF and the high-emissivity coating effectively raised the tensile strength of the fiber fabric. Compared with the single-layer MSS-5Z-coated ASFF, the tensile strength of the double-coated fabric is 23.9% higher and its binding strength reached 156.2 kPa. The ZrO2 sol layer can not only absorb the stress in the tensile strain caused by the phase transition toughening mechanism but also prevent the glass phase from penetrating the fiber bundle and is instrumental in interface debonding and fiber pull-out. Moreover, the average spectral emissivity of the double-coated ASFF after heat treatment at 1200 °C for 3 h is still above 0.91, which can meet the high-temperature thermal insulation performance demands of TPS. After butane flame heating for 5 min, the backside temperature of the double-layer coating felt fiber was 83 °C (23%) lower compared with the bare ASFF. The structural design of the ZrB2-doped coating and intermediate layer not only reduces the oxidation rate but also blocks the bonding between the outer coating and fiber bundles, which effectively restrains the strength attenuation of the high-emissivity coating after high-temperature application. Further exploration can be conducted on the introduction of reflective planes in coatings or felt fiber to reduce the diffusion of thermal energy into the interior of the aircraft, which is also an important mechanism of TPS.

Author Contributions

Conceptualization, W.L. and J.L.; methodology, W.L.; software, W.L.; validation, W.L., A.G. and H.D.; formal analysis, W.L.; investigation, W.L.; resources, W.L.; data curation, W.L.; writing—original draft preparation, W.L.; writing—review and editing, W.L., X.Z., and L.Y.; visualization, W.L.; supervision, W.L.; project administration, W.L. and J.L.; funding acquisition, J.L. All authors have read and agreed to the published version of the manuscript.

Funding

This research was funded by the National Key Research and Development Program of China (grant number 2023YFB3711200), the National Natural Science Foundation of China (grant number 52002268), and the Science and Technology Planning Project of Tianjin (grant number 21JCQNJC00560).

Institutional Review Board Statement

Not applicable.

Informed Consent Statement

Not applicable.

Data Availability Statement

Data are contained within the article.

Conflicts of Interest

The authors declare no conflicts of interest.

References

  1. Gong, W.; Wang, T.; Luo, W.; Du, Y.; Ye, L.; Song, R.; Cui, H.; Zhao, T.; Yang, W.; Dai, Z.; et al. Synthesis and Characterization of High-Purity, High-Entropy Diboride Ceramic Powders by a Liquid Phase Method. Materials 2023, 16, 7431. [Google Scholar] [CrossRef] [PubMed]
  2. Wang, M.; Feng, Z.; Zhai, C.; Zhang, J.; Li, Z.; Zhang, H.; Xu, X. Low-temperature in-situ grown mullite whiskers toughened heat-resistant inorganic adhesive. J. Alloys Compd. 2020, 836, 155349. [Google Scholar] [CrossRef]
  3. Yang, N.; Cai, G.; Wan, Y.; Zhang, R.; Li, J.; Zhang, J.; Zhang, H.; Liu, H.; Yu, X.; Wang, M. High anti-ablative epoxy resin-based flame retardant and thermal insulation coating based on spontaneous Ceramization and vitrification. Ceram. Int. 2024, 50, 24233–24251. [Google Scholar] [CrossRef]
  4. Fu, Y.; Zhang, Y.; Yan, H.; Li, J.; Yin, X.; Sun, J.; Fu, Q.; Riedel, R. Microstructure and evolution of hafnium carbide whiskers via polymer-derived ceramics: A novel formation mechanism. J. Adv. Ceram. 2023, 12, 578–586. [Google Scholar] [CrossRef]
  5. Yang, R.; Xu, J.; Guo, J.; Meng, X.; Zhang, P.; Fan, F.; Qu, Y.; Gao, F. High wave transmittance and low thermal conductivity Y–α-SiAlON porous ceramics for high-temperature radome applications. J. Adv. Ceram. 2023, 12, 1273–1287. [Google Scholar] [CrossRef]
  6. Cai, G.; Wan, Y.; Liu, J.; Yang, N.; Guo, J.; Li, J.; Zhou, Y.; Zhang, J.; Zhang, H.; Wang, M. Preparation and performance analysis of methyl-silicone resin-modified epoxy resin-based intumescent flame retardant thermal insulation coating. J. Micromech. Mol. Phys. 2023, 08, 61–82. [Google Scholar] [CrossRef]
  7. Wang, M.; Bu, F.; Zhou, C.; Zhou, Q.; Wei, T.; Liu, J.; Zhai, W. Bonding performance and mechanism of a heat-resistant composite precursor adhesive (RT-1000°C) for TC4 titanium alloy. J. Micromech. Mol. Phys. 2020, 5, 2050016. [Google Scholar] [CrossRef]
  8. Feng, Z.; Wang, M.; Lu, R.; Xu, W.; Zhang, T.; Wei, T.; Zhang, J.; Liao, Y. A composite structural high-temperature-resistant adhesive based on in-situ grown mullite whiskers. Mater. Today Commun. 2020, 23, 100944. [Google Scholar] [CrossRef]
  9. Xue, Y.; Liu, J. Preparation and Elasticity & Thermal Insulation Properties of Flexible Fiber Blankets. Mater. Rev. 2023, 37, 21030042. [Google Scholar] [CrossRef]
  10. Piacquadio, S.; Pridöhl, D.; Henkel, N.; Bergström, R.; Zamprotta, A.; Dafnis, A.; Schröder, K.U. Comprehensive Comparison of Different Integrated Thermal Protection Systems with Ablative Materials for Load-Bearing Components of Reusable Launch Vehicles. Aerospace 2023, 10, 319. [Google Scholar] [CrossRef]
  11. Li, J.F.; Luo, Z.P. Fabrication and performances of preceramic polymer-based high-temperature High emissivity coating. J. Eur. Ceram. Soc. 2020, 40, 5217–5225. [Google Scholar] [CrossRef]
  12. Wang, M.; Liang, Z.; Yan, S.; Tao, X.; Zou, Y.; Li, J.; Zhou, X.; Zhang, H. The preparation and property analysis of B4C modified inorganic amorphous aluminum phosphates-based intumescent flame retardant coating. Constr. Build. Mater. 2022, 359, 129480. [Google Scholar] [CrossRef]
  13. Zhu, M.; Chen, J.; Ran, N.; Zheng, J.Q.; Huang, Z.R.; Liu, X.J.; Chen, Z.M. High infrared emissivity of SiC-AlN ceramics at room temperature. J. Eur. Ceram. Soc. 2020, 40, 3528–3534. [Google Scholar] [CrossRef]
  14. Yang, X.; Wan, Y.; Li, J.; Liu, J.; Wang, M.; Tao, X. High Emissivity MoSi2-SiC-Al2O3 Coating on Rigid Insulation Tiles with Enhanced Thermal Protection Performance. Materials 2024, 17, 220. [Google Scholar] [CrossRef] [PubMed]
  15. Astapov, A.N.; Potanin, A.Y.; Loginov, P.A.; Shvyndina, N.V.; Eganova, E.M.; Tarasova, A.N.; Levashov, E.A. The effect of Ta on the kinetics and mechanisms of high-temperature oxidation of the (Hf,Ta)B2-SiC ceramics. Corros. Sci. 2024, 227, 111721. [Google Scholar] [CrossRef]
  16. Astapov, A.N.; Matulyak, A.I. Reaction Synthesis for Producing MoSi2-Based Coatings. Russ. Metall. 2022, 2022, 1569–1577. [Google Scholar] [CrossRef]
  17. Sajdak, M.; Kornaus, K.; Zientara, D.; Moskala, N.; Komarek, S.; Momot, K.; Golis, E.; Zych, L.; Gubernat, A. Processing, Microstructure and Mechanical Properties of TiB2-MoSi2-C Ceramics. Crystals 2024, 14, 212. [Google Scholar] [CrossRef]
  18. Guo, L.L.; Hu, X.X.; Tao, X.; Du, H.Y.; Guo, A.R.; Liu, J.C. Low-temperature oxidation resistance of the silica-coated MoSi2 powders prepared by sol-gel preoxidation method. Ceram. Int. 2020, 46, 23471–23478. [Google Scholar] [CrossRef]
  19. Gao, Q.C.; Yan, L.W.; Mu, Y.; Xue, Y.J.; Xu, X.J.; Guo, A.R.; Du, H.Y.; Dong, S.; Liu, J.C. TaSi2-SiC high-emissivity coating modified by SiB6 on flexible alumina fibre fabric with enhanced oxidation resistance and high interfacial bonding strength. Ceram. Int. 2023, 49, 12643–12652. [Google Scholar] [CrossRef]
  20. Shao, G.F.; Wu, X.D.; Cui, S.; Shen, X.D.; Kong, Y.; Lu, Y.C.; Jiao, C.R.; Jiao, J. High emissivity MoSi2-ZrO2-borosilicate glass multiphase coating with SiB6 addition for fibrous ZrO2 ceramic. Ceram. Int. 2016, 42, 8140–8150. [Google Scholar] [CrossRef]
  21. Zhang, G.L.; Xue, Y.J.; Liu, P.S.; Guo, A.R.; Du, H.Y.; Yan, L.W.; Liu, J.C. High emissivity double-layer coating on the flexible aluminum silicate fiber fabric with enhanced interfacial bonding strength and high temperature resistance. J. Eur. Ceram. Soc. 2021, 41, 1452–1458. [Google Scholar] [CrossRef]
  22. Grigoriev, O.; Neshpor, I.; Vedel, D.; Mosina, T.; Silvestroni, L. Influence of chromium diboride on the oxidation resistance of ZrB2-MoSi2 and ZrB2-SiC ceramics. J. Eur. Ceram. Soc. 2021, 41, 2207–2214. [Google Scholar] [CrossRef]
  23. Sedighi, A.; Adeli, M.; Soltanieh, M. Investigation of the effect of SiC additions on the high-temperature oxidation behavior of combustion-synthesized MoSi2. J. Mater. Res. Technol. 2024, 30, 187–196. [Google Scholar] [CrossRef]
  24. Grigoriev, O.N.; Vinokurov, V.B.; Silvestroni, L. ZrB2-MoSi2 ceramics: Kinetics of compaction during hot pressing in CO environment, phase interactions at interfaces and static fatigue. J. Eur. Ceram. Soc. 2024, 44, 2811–2820. [Google Scholar] [CrossRef]
  25. Kiryukhantsev-Korneev, P.; Sytchenko, A.; Pogozhev, Y.; Vorotilo, S.; Orekhov, A.; Loginov, P.; Levashov, E. Structure and Properties of Zr-Mo-Si-B-(N) Hard Coatings Obtained by d.c. Magnetron Sputtering of ZrB2-MoSi2 Target. Materials 2021, 14, 1932. [Google Scholar] [CrossRef] [PubMed]
  26. Azzali, N.; Meucci, M.; Di Rosa, D.; Mercatelli, L.; Silvestroni, L.; Sciti, D.; Sani, E. Spectral emittance of ceramics for high temperature solar receivers. Sol. Energy 2021, 222, 74–83. [Google Scholar] [CrossRef]
  27. Pellegrini, C.; Balat-Pichelin, M.; Rapaud, O.; Bêche, E. Oxidation resistance of Zr- and Hf-diboride composites containing SiC in air plasma up to 2600 K for aerospace applications. Ceram. Int. 2022, 48, 2177–2190. [Google Scholar] [CrossRef]
  28. Vedel, D.V.; Grigoriev, O.N.; Mazur, P.V.; Osipov, A.E. Structure, Strength, and Oxidation Resistance of Ultrahigh-Temperature ZrB2-SiC-WC Ceramics. Powder Metall. Met. Ceram. 2021, 60, 60–68. [Google Scholar] [CrossRef]
  29. Li, X.F.; Feng, J.Z.; Jiang, Y.G.; Lin, H.; Feng, J. Preparation and anti-oxidation performance of Al2O3-containing TaSi2-MoSi2-borosilicate glass coating on porous SiCO ceramic composites for thermal protection. RSC Adv. 2018, 8, 13178–13185. [Google Scholar] [CrossRef]
  30. Cai, G.; Wu, J.; Guo, J.; Wan, Y.; Zhou, Q.; Zhang, P.; Yu, X.; Wang, M. A Novel Inorganic Aluminum Phosphate-Based Flame Retardant and Thermal Insulation Coating and Performance Analysis. Materials 2023, 16, 4498. [Google Scholar] [CrossRef]
  31. Yang, X.; Wan, Y.; Yang, N.; Hou, Y.; Chen, D.; Liu, J.; Cai, G.; Wang, M. The Effect of Different Diluents and Curing Agents on the Performance of Epoxy Resin-Based Intumescent Flame-Retardant Coatings. Materials 2024, 17, 348. [Google Scholar] [CrossRef] [PubMed]
  32. Wei, Z.Y.; Meng, G.H.; Chen, L.; Li, G.R.; Liu, M.J.; Zhang, W.X.; Zhao, L.N.; Zhang, Q.; Zhang, X.D.; Wan, C.L.; et al. Progress in ceramic materials and structure design toward advanced thermal barrier coatings. J. Adv. Ceram. 2022, 11, 985–1068. [Google Scholar] [CrossRef]
  33. Wang, T.C.; Zhang, Z.H.; Dai, C.H.; Li, Q.; Li, Y.C.; Kong, J.; Wong, C.P. Amorphous silicon and silicates-stabilized ZrO2 hollow fiber with low thermal conductivity and high phase stability derived from a cogon template. Ceram. Int. 2019, 45, 7120–7126. [Google Scholar] [CrossRef]
  34. Wang, M.C.; Liu, J.X.; Chen, Z.L.; Hu, X.X.; Zhai, W.Z.; Tao, X.; Liu, J.C. Joining zirconia with nickel-based superalloys for extreme applications by using a pressure-free high-temperature resistant adhesive. Ceram. Int. 2022, 48, 8025–8030. [Google Scholar] [CrossRef]
  35. Zhang, T.; Song, X.; Qi, G.; An, B.; Dong, W.; Zhao, Y.; Wang, Z.; Yi, X.; Yuan, Z.; Zhao, Y.; et al. Investigation of High-Temperature Normal Infrared Spectral Emissivity of ZrO2 Thermal Barrier Coating Artefacts by the Modified Integrated Blackbody Method. Materials 2022, 15, 235. [Google Scholar] [CrossRef] [PubMed]
  36. Chen, Z.; Liu, J.; Wu, Y.; Feng, Z.; Li, J.; Feng, Z.; Zhang, Q.; Wang, M. The preparation and properties of an alloying modified ceramic-precursor high-temperature resistant adhesive for joining zirconia ceramics and titanium-based superalloys. Mater. Today Commun. 2022, 33, 104353. [Google Scholar] [CrossRef]
  37. Aribuga, D.; Karaahmet, O.; Balci-Çagiran, Ö.; Çiçek, B. Effect of Al2O3 and ZrO2 Filler Material on the Microstructural, Thermal and Dielectric Properties of Borosilicate Glass-Ceramics. Micromachines 2023, 14, 595. [Google Scholar] [CrossRef] [PubMed]
  38. Ferguson, J.I.; Al Saad, A.; Seren, M.H.; Ko, J.Y.P.; Nygren, K.E.; Trice, R.W.; Sangid, M.D. Residual elastic strain and survivability of stabilized zirconia coated carbon-carbon (C/C) composite. Surf. Coat. Technol. 2023, 470, 129811. [Google Scholar] [CrossRef]
  39. Al Saad, A.; Martinez, C.; Trice, R.W. Ablation performance of rare earth oxide (REO)-stabilized tetragonal and cubic zirconia coatings as a thermal protection system (TPS) for carbon/carbon composites. J. Eur. Ceram. Soc. 2023, 43, 6449–6460. [Google Scholar] [CrossRef]
  40. Zhang, J.; Mei, G.H.; Zhao, S.M.; Meng, H.J.; Xie, Z. A fused glass coating for oxidation protection of Mo-W-ZrO2 cermet. Surf. Coat. Technol. 2015, 261, 189–194. [Google Scholar] [CrossRef]
  41. Ren, Y.; Qian, Y.H.; Xu, J.J.; Jiang, Y.; Zuo, J.; Li, M.S. Oxidation and cracking/spallation resistance of ZrB2-SiC-TaSi2-Si coating on siliconized graphite at 1500 °C in air. Ceram. Int. 2020, 46, 6254–6261. [Google Scholar] [CrossRef]
  42. Mahltig, B.; Haufe, H.; Böttcher, H. Functionalisation of textiles by inorganic sol-gel coatings. J. Mater. Sci. 2005, 15, 4385–4398. [Google Scholar] [CrossRef]
  43. Liu, J.; Wan, Y.; Xiao, B.; Li, J.; Hu, Z.; Zhang, R.; Hu, X.; Liu, J.; Cai, G.; Liu, H.; et al. The preparation and performance analysis of zirconium-modified aluminum phosphate-based high-temperature (RT–1500 °C) resistant adhesive for joining alumina in extreme environment. J. Adv. Ceram. 2024. [Google Scholar] [CrossRef]
  44. GB/T 1447-2005; Fiber-Reinforced Plastics Composites—Determination of Tensile Properties. China Building Materials Federation: Beijing, China, 2005.
  45. GB/T 5210-2006; Paints and Varnishes—Pull-Off Test for Adhesion. China Petroleum and Chemical Industry Federation: Beijing, China, 2006.
  46. Zhu, Q.; Shobu, K.; Tani, E.; Kishi, K.; Umebayashi, S. Oxidation behavior of Mo≤5Si3C≤1 and its composites. J. Mater. Sci. 2000, 35, 863–872. [Google Scholar] [CrossRef]
  47. Guo, W.M.; Xiao, H.N.; Gao, P.Z.; Xie, W.; Li, Q.; Hu, J.L. Investigation of MoSi2 melt infiltrated RSiC and its oxidation behavior. Ceram. Int. 2012, 38, 111–117. [Google Scholar] [CrossRef]
  48. Mao, J.W.; Ding, S.Y.; Li, Y.J.; Li, S.H.; Liu, F.S.; Zeng, X.; Cheng, X.D. Preparation and investigation of MoSi2/SiC coating with high infrared emissivity at high temperature. Surf. Coat. Technol. 2019, 358, 873–878. [Google Scholar] [CrossRef]
  49. Shao, G.F.; Wu, X.D.; Kong, Y.; Shen, X.D.; Cui, S.; Guan, X.; Jiao, C.R.; Jiao, J. Microstructure, radiative property and thermal shock behavior of TaSi2-SiO2-borosilicate glass coating for fibrous ZrO2 ceramic insulation. J. Alloys Compd. 2016, 663, 360–370. [Google Scholar] [CrossRef]
  50. An, Z.; Chunhua, L.U.; Zhongzi, X.U. Research on Chemical Stability of ZrO2-doped Borosilicate Glass and Analysis of Its Structure. Mater. Rev. 2006, 20, 134–136. [Google Scholar] [CrossRef]
  51. Manara, J.; Arduini-Schuster, M.; Keller, M. Infrared-optical characteristics of ceramics at elevated temperatures. Infrared Phys. Technol. 2011, 54, 395–402. [Google Scholar] [CrossRef]
  52. Cheng, X.D.; Min, J.; Zhu, Z.Q.; Ye, W.P. Preparation of high emissivity NiCr2O4 powders with a spinel structure by spray drying. Int. J. Miner. Metall. Mater. 2012, 19, 173–178. [Google Scholar] [CrossRef]
Materials 17 03234 g001
Figure 1. Flow chart of the preparation processes of the double layer on the ASFF surface.
Figure 1. Flow chart of the preparation processes of the double layer on the ASFF surface.
Materials 17 03234 g001
Materials 17 03234 g002
Figure 2. SEM images of the MoSi2–SiC (MS) and MoSi2–SiC–ZrB2 (MSZ) powders after heat treatment at 1200 °C: (a) MS-RT; (b) MS-1200 °C; (c) MSZ-RT; (d) MSZ-1200 °C.
Figure 2. SEM images of the MoSi2–SiC (MS) and MoSi2–SiC–ZrB2 (MSZ) powders after heat treatment at 1200 °C: (a) MS-RT; (b) MS-1200 °C; (c) MSZ-RT; (d) MSZ-1200 °C.
Materials 17 03234 g002
Materials 17 03234 g003
Figure 3. XRD patterns of the MS and MSZ powders after heat treatment for 1 h at 1200 °C.
Figure 3. XRD patterns of the MS and MSZ powders after heat treatment for 1 h at 1200 °C.
Materials 17 03234 g003
Materials 17 03234 g004
Figure 4. SEM images of the single-layer coating surface after heat treatment at 1200 °C for different times: (a,e) MSS-0Z; (b,f) MSS-3Z; (c,g) MSS-5Z; (d,h) MSS-7Z.
Figure 4. SEM images of the single-layer coating surface after heat treatment at 1200 °C for different times: (a,e) MSS-0Z; (b,f) MSS-3Z; (c,g) MSS-5Z; (d,h) MSS-7Z.
Materials 17 03234 g004
Materials 17 03234 g005
Figure 5. FTIR spectra of single-layer coatings with different ZrB2 content after calcination at 1200 °C for 1 h.
Figure 5. FTIR spectra of single-layer coatings with different ZrB2 content after calcination at 1200 °C for 1 h.
Materials 17 03234 g005
Materials 17 03234 g006
Figure 6. XRD patterns of single-layer coatings with different ZrB2 content before (a) and after calcination at 1200 °C for different periods of time: (b) 1 h; (c) 3 h.
Figure 6. XRD patterns of single-layer coatings with different ZrB2 content before (a) and after calcination at 1200 °C for different periods of time: (b) 1 h; (c) 3 h.
Materials 17 03234 g006
Materials 17 03234 g007
Figure 7. Cross-sectional SEM images of the fiber fabrics with the single-layer coatings after calcination at 1200 °C for 1 h: (a) MSS-0Z; (b) MSS-3Z; (c) MSS-5Z; (d) MSS-7Z.
Figure 7. Cross-sectional SEM images of the fiber fabrics with the single-layer coatings after calcination at 1200 °C for 1 h: (a) MSS-0Z; (b) MSS-3Z; (c) MSS-5Z; (d) MSS-7Z.
Materials 17 03234 g007
Materials 17 03234 g008
Figure 8. EDS elemental distribution images of a cross-section of the ASFF with a double-layer coating after calcination at 1200 °C for 1 h: (a) SEM image; (b) Si; (c) Mo; (d) Zr EDS spectra.
Figure 8. EDS elemental distribution images of a cross-section of the ASFF with a double-layer coating after calcination at 1200 °C for 1 h: (a) SEM image; (b) Si; (c) Mo; (d) Zr EDS spectra.
Materials 17 03234 g008
Materials 17 03234 g009
Figure 9. ∆G of reactions (1)–(6) as a function of temperature.
Figure 9. ∆G of reactions (1)–(6) as a function of temperature.
Materials 17 03234 g009
Materials 17 03234 g010
Figure 10. Oxidation mechanism diagram of the MSS-0Z, MSS-5Z, and double-layer coatings calcined at 1200 °C.
Figure 10. Oxidation mechanism diagram of the MSS-0Z, MSS-5Z, and double-layer coatings calcined at 1200 °C.
Materials 17 03234 g010
Materials 17 03234 g011
Figure 11. Tensile strength of the ASFF with coatings before and after calcination at different temperatures: (a) single-layer coatings; (b) MSS-5Z and double-layer coatings.
Figure 11. Tensile strength of the ASFF with coatings before and after calcination at different temperatures: (a) single-layer coatings; (b) MSS-5Z and double-layer coatings.
Materials 17 03234 g011
Materials 17 03234 g012
Figure 12. (a) Bonding strengths of the single-layer coating/ASFF. (b) Photo of samples after pull-out tests. (c) Bonding strengths of MSS-5Z coating/ASFF and double-layer coating/ASFF.
Figure 12. (a) Bonding strengths of the single-layer coating/ASFF. (b) Photo of samples after pull-out tests. (c) Bonding strengths of MSS-5Z coating/ASFF and double-layer coating/ASFF.
Materials 17 03234 g012
Materials 17 03234 g013
Figure 13. (a) Emissivity of the raw ASFF with a ZrO2 coating, ASFF with an MSS-5Z coating, and ASFF with a double-layer coating. (b) Average spectral emissivity of the coated ASFF in the wavelength range of 2~14 μm at RT. (c) Emissivity of the ASFF with a double-layer coating after heat treatment at 1200 °C for different times.
Figure 13. (a) Emissivity of the raw ASFF with a ZrO2 coating, ASFF with an MSS-5Z coating, and ASFF with a double-layer coating. (b) Average spectral emissivity of the coated ASFF in the wavelength range of 2~14 μm at RT. (c) Emissivity of the ASFF with a double-layer coating after heat treatment at 1200 °C for different times.
Materials 17 03234 g013
Materials 17 03234 g014
Figure 14. Infrared thermal image of flexible insulation felt: (a–d) without coating; (e–h) MSS-0Z coating; (i–l) MSS-5Z coating; (m–p) double-layer coating.
Figure 14. Infrared thermal image of flexible insulation felt: (a–d) without coating; (e–h) MSS-0Z coating; (i–l) MSS-5Z coating; (m–p) double-layer coating.
Materials 17 03234 g014
Table 1. Compositions of the MoSi2–SiC–ZrB2 coating and ZrO2 coating.
Table 1. Compositions of the MoSi2–SiC–ZrB2 coating and ZrO2 coating.
Sample Composition (wt.%)
MoSi2SiCZrB2ZrO2SiO2-Sol
MSS-0Z25250050
MSS-3Z25253047
MSS-5Z25255045
MSS-7Z25257043
ZrO2 coating0005050
Disclaimer/Publisher’s Note: The statements, opinions and data contained in all publications are solely those of the individual author(s) and contributor(s) and not of MDPI and/or the editor(s). MDPI and/or the editor(s) disclaim responsibility for any injury to people or property resulting from any ideas, methods, instructions or products referred to in the content.

Share and Cite

MDPI and ACS Style

Li, W.; Zhang, X.; Yan, L.; Guo, A.; Du, H.; Liu, J. High-Emissivity Double-Layer ZrB2-Modified Coating on Flexible Aluminum Silicate Fiber Fabric with Enhanced Oxidation Resistance and Tensile Strength. Materials 2024, 17, 3234. https://doi.org/10.3390/ma17133234

AMA Style

Li W, Zhang X, Yan L, Guo A, Du H, Liu J. High-Emissivity Double-Layer ZrB2-Modified Coating on Flexible Aluminum Silicate Fiber Fabric with Enhanced Oxidation Resistance and Tensile Strength. Materials. 2024; 17(13):3234. https://doi.org/10.3390/ma17133234

Chicago/Turabian Style

Li, Wei, Xueying Zhang, Liwen Yan, Anran Guo, Haiyan Du, and Jiachen Liu. 2024. "High-Emissivity Double-Layer ZrB2-Modified Coating on Flexible Aluminum Silicate Fiber Fabric with Enhanced Oxidation Resistance and Tensile Strength" Materials 17, no. 13: 3234. https://doi.org/10.3390/ma17133234

APA Style

Li, W., Zhang, X., Yan, L., Guo, A., Du, H., & Liu, J. (2024). High-Emissivity Double-Layer ZrB2-Modified Coating on Flexible Aluminum Silicate Fiber Fabric with Enhanced Oxidation Resistance and Tensile Strength. Materials, 17(13), 3234. https://doi.org/10.3390/ma17133234

Note that from the first issue of 2016, this journal uses article numbers instead of page numbers. See further details here.

Article Metrics

Back to TopTop