1. Introduction
When the cockpit environmental control system fails, the temperature and humidity conditions in the cabin may rise and exceed the tolerance limit of the pilot, and the pilot may bear a large thermal load and enter different degrees of thermal stress, which may pose a threat to flight safety. Thermal stress is one of the important factors leading to flight accidents [
1]. The high temperature conditions in the cockpit may affect the pilot’s cognitive judgment ability, thus affecting his ability to control the aircraft. Some studies have pointed out that the higher the thermal intensity of the cabin environment, the greater the psychological and physiological load of the operators, and the higher the risk of fatigue and injury [
2,
3].
China has formulated the corresponding airworthiness clause CCAR-25.831(g) according to the FAR25 of the United States. As shown in
Figure 1, the clause stipulates: ‘After any failure with small probability occurs, the duration at a given temperature shall not exceed the specified value, and it is also required to keep the humidity in the aircraft below 27mbar’ [
4]. Using this criterion, Zhou’s study found that after 55 min in a hot and humid environment—where fighter pilots should not operate for more than 55 min—the pilot’s core temperature reached 38 °C [
5].
The purpose of this regulation is to limit the exposure time of the cockpit and cabin to a high-temperature environment, so as to ensure that even if the ventilation system fails, the aircraft can still fly and land safely, and at the same time avoid causing physiological harm to the crew and passengers. However, the manufacturers found that it was difficult or impossible to meet the requirements of 25.831(g), and they could not meet the airworthiness compliance when all gas supply was lost due to the failure of the environmental control system. Therefore, ARAC assigned this task to the Mechanical System Coordination Working Group (MSHWG), and MSHWG released their final report on 31 July 2003, in which a new performance-based standard was formulated to maintain a tolerable environment by limiting crew metabolism and environmental heat load during possible thermal stress exposure.
The final report of MSHWG gives the following equivalent safety rules [
6]: ‘The aircraft design must adapt to any failure situation of the environmental control system that is not indicated to be extremely impossible. The following failure situations apply: (a) the environmental conditions of the cockpit and cabin must not adversely affect the crew’s work, thus leading to dangerous situations; (b) No occupant will suffer permanent physical injury. By verifying the above rules, it can be indirectly proved that the aircraft meets the airworthiness clause CCAR25.831(g). The purpose of this rule is to ensure that the cockpit environment will not affect the crew’s work efficiency, to avoid causing cognitive dysfunction or physical fatigue, and to ensure that they can complete the flight mission safely. It will not cause harm to ordinary sit-in passengers. The acceptable way to comply with this rule is the following: For the cockpit environment when it fails, it is proved through analysis that the crew’s work efficiency will not be affected and the passengers’ health will not be harmed.
For the above proposed regulations, MSHWG proposed the criteria for judging the acceptable high-temperature environment in the cabin based on the core temperature of the human body, requiring the applicant to ensure that when the air-conditioning system is not installed or fails, the core temperature of the human body does not exceed 38 °C (100.4 degrees Fahrenheit) in the steady state; that the temperature does not exceed 38.5 °C (101.3 °C, Fahrenheit) under transient conditions of not more than 20 min; and that the human core temperature of 38.5 °C cannot exceed or last for any length of time [
7]. Studies have shown that when the ambient temperature is too high, the heat storage rate of the human body is greater than zero, and if the residual heat cannot be dissipated in time, then the human body will feel uncomfortable, and when the body temperature reaches 38.2 °C, mild heatstroke may occur [
8]. According to the research results of MSHWG on 25.831(g), the influence of the increase in human core temperature on the crew and passengers is shown in
Table 1.
However, this standard is based on the medical research results of western ethnic groups [
9,
10,
11]. Although some studies related to human functions in a high-temperature environment have been carried out in China [
12,
13], there is a paucity of research findings regarding the applicability of these criteria to the Chinese pilot situation. Therefore, this study takes the general population of different ages as the experimental object, analyzes the core temperature values of the human body in different cabin temperature environments, evaluates the changes in their physiological response and cognitive function, and verifies the accuracy of
Table 1 through statistical data. The purpose of this study is to verify the acceptable high-temperature environment standard in the cabin based on the core temperature of the human body, which can be used as a feasible cockpit environment equivalent safety analysis method and provide strong support for the equivalent safety verification of the airworthiness clause CCAR25.831(g).
2. Subjects and Methods
2.1. Subjects
Members of the general population aged 18–50 years old were selected as experimental subjects, with 10 people in each group. The general population was divided into three groups according to age: group 20 to 30 years old (age 24.00 ± 1.11 years old, BMI index 21.75 ± 2.13), group 30 to 39 years old (age 32.90 ± 2.06 years old, BMI index 24.02 ± 2.12), group 40 years old and above (age 44.63 ± 3.74 years old, BMI index 22.18 ± 2.48). Due to the specific characteristics of pilots, who are predominantly male, the study included only Chinese males who were in good health, had no medical history, had never been to a high-altitude area, had a physical examination within 3 months before the experiment, and had good sleep and diet before the experiment. The present experiment focuses on the relative changes of subjects in the high-temperature environment rather than on the absolute values. Changes in physiological parameters and cognitive abilities before and after the experiment can better reflect the effects of the high-temperature environment on the subjects, rather than relying solely on the initial state. Thus, even if the subjects differ at baseline, the final outcome can still be assessed by relative change. The study was formally reviewed and endorsed by the Ethics Committee of Soochow University on 1 March 2019, affirming that the rights and well-being of the subjects were thoroughly safeguarded throughout the study and that there was no inherent risk to the subjects.
2.2. Experimental Methods
In this study, we measured human heat load in terms of core temperature according to MSHWG regulations and designed three groups with different levels of heat load to systematically explore physiological responses under different conditions. The specific experimental groups were as follows: the first group prior to entering the hot environment (referred to as pre-experiment), the second group after the core body temperature reached 38 °C, and the third group after a duration of 20 min between 38 °C and 38.5 °C.
The high-temperature environment was simulated by a walk-in artificial climate chamber (ESPEC, Osaka, Japan). The core temperature acquisition system (HQinc, Los Angeles, CA, USA) was used in the experiment to monitor the core temperature (Tcore). Metabolism was monitored with a cardiopulmonary function meter (Cortex, Düsseldorf, Germany); a portable heart rate band (Polar, Oulu, Finland) was used to monitor the heart rate (HR), and a wireless oxygen monitoring system (Artinis, Nijmegen, The Netherlands) was used to collect the saturation of arterial blood oxygen (SAO2) and saturation of venous blood oxygen (SVO2); the MSR145WD wireless data logger (MSR, Baar, Switzerland) was used to collect skin temperature (TSK). Neurobehavioral ability indexes (mental arithmetic, visual retention, attention transfer, and selection response) were evaluated by the third edition of the Chinese Neurobehavioral Assessment System (NES-C3, Shanghai, China), and the Neurobehavioral Ability Index (NAI) was calculated. The Brog scale and the Rating of Perceived Exertion (RPE) were used to evaluate the degree of fatigue.
The experimental conditions were set as follows: temperature 40 ± 0.5 °C, relative humidity 40 ± 5% RH, wind speed 0.2 ± 0.1 m/s. The present experiment focuses on the effects of heat load on the body in a hot environment. Provided that the variable of high temperature is effectively controlled, even though barometric pressure and noise may affect the occupants during actual flight, these differences will not affect the main results and conclusions of the experiment. The subjects walked on a treadmill at an incline speed of 5 km/h. The experiment employed subjects walking on a treadmill for two primary purposes. First, this simplified and simulated the workload of the pilot in the event of a ventilation system failure during flight, thereby rendering the experiment more realistic. Secondly, this approach enabled the expeditious attainment of the stipulated conditions for the subjects, thereby facilitating the execution of the experiment. The experimental process is as follows:
- (1)
First, the thermal neutral state was reached in the room temperature environment in advance, and the neurobehavioral ability of the subjects was assessed by an NES-C3 system.
- (2)
The subjects changed the test clothes (ordinary long sleeves and trousers), wore the test equipment of physiological indicators, and then entered the climate chamber with a preset environment to prepare for the test.
- (3)
After the test began, the subjects walked on a treadmill at an incline speed of 5 km/h, recorded their subjective feelings, and measured their metabolic rate 15 min after the test began.
- (4)
The core body temperature of the subjects was monitored. When the core temperature of the subjects reached 38 °C, NES-C3 was used to evaluate the neurobehavioral ability of the subjects.
- (5)
The test was repeated after 20 min, and the core temperature was maintained at 38~38.5 °C during the test.
2.3. Data Processing
SPSS 26.0 statistical software was used to conduct a one-way ANOVA on the data of the four groups under different levels of heat load. All the data were expressed as mean ± standard deviation (x ± s). The significance level of difference was set at p < 0.05 *, and p < 0.01 ** indicates a very significant difference.
4. Discussion
4.1. Physiological Response Variations Under Different Heat Load Environments
The high-temperature environment chosen for this study was set at 40 °C, which falls within the range of 38–40 °C typically observed in the cockpit following a failure of the airplane’s air conditioning system [
14]. This selection reflects a plausible real-world scenario. The safe range of human core temperature is in the range of 36–42 °C, and it is generally believed that if it exceeds 42 °C, there will be symptoms of heatstroke and even risk of death. The skin temperature of human body usually varies in the range of 32–37 °C, and when the skin temperature exceeds this range, it may cause discomfort or health problems. Studies have shown that the physiological tolerance limit of the human heart rate is 172 to 182 beats/min at the effective temperature of 35.4 to 38.5 °C [
15]. After reaching the set temperature conditions, the conclusion of this experiment is consistent with the influence of the existing indoor thermal discomfort environment on human physiological response [
16]. With the increase in temperature, the core temperature, skin temperature, and heart rate of the human body have significantly increased, while blood pressure and oxygen saturation have decreased, but they are all within the safe range. At the same time, a high-temperature operation can reduce the function and adaptability of the cerebral cortex, cause fatigue, and lead to operational errors [
17]. The experimental results show that the fatigue degree of people in all age groups increases significantly with the increase in temperature, and the indexes of neurobehavioral ability change to some extent in a high-temperature environment, but there is no significant difference among various physiological indexes.
The present study revealed that skin temperature and heart rate exhibited a substantial response to heat load in pilots. Skin temperature is influenced by a combination of blood flow and blood temperature. An increase in ambient temperature results in the relaxation of blood vessels and the subsequent rise in blood flow, leading to an elevated skin temperature. Zhou’s experiments on flight simulation demonstrated a substantial increase in the average skin temperature of the human body with rising ambient temperature, accompanied by an increase in fatigue, which is consistent with the findings of the present study [
5]. The rise in mean heart rate in a hot environment is predominantly attributed to cardiac sympathetic excitation. The observed rise in heart rate with core body temperature is designated as thermal cardiac reactivity (TCR). Consequently, skin temperature and heart rate can be regarded as substantial physiological indicators, given their correlation with the physiological demands of pilots. These indicators can serve as a foundation for evaluating cabin temperature control systems.
The experimental results show that the effects of different cabin temperature environments on human physiological response and cognitive function are in line with the expectations in
Table 1, which proves that the core temperature limit given by the Mechanical System Coordination Working Group is also applicable to typical people in China. Therefore, physiological indexes with significant differences can be used as safety indexes to evaluate airworthiness compliance. The results of this experiment prove that we can consider simulating the cabin environment temperature, predicting the changes of human core temperature, and measuring the changes in significant physiological indexes to determine the safety and suitability of the cabin environment, and form a method to verify the airworthiness compliance of the cabin high-temperature environment.
4.2. Advances and Applications of Physiological Sensors
A variety of physiological monitoring tools were utilized in this study to assess the physiological responses of participants under different heat load conditions. In recent years, significant advancements have been made in physiological monitoring technologies, particularly in the domain of wearable devices and sensor technologies. Garcia proposed a non-invasive method to measure heart rate and skin temperature using mobile biosensors in real-world environments and simulate the computation of the human core temperature in a single pass [
18]. Nile designed an Internet of Things (IoT)-based heart rate monitoring system for enhanced flight safety by means of a highly sensitive heartbeat sensor for data input and real-time monitoring at the other end [
19]. Future research endeavors can build on this foundation and utilize larger samples and more advanced physiological monitoring techniques to further explore the effects of heat load on different populations. This will provide a more solid theoretical foundation and practical guidance for research in related fields.
4.3. Limitations
This study is not without its limitations. First, although the experimental conditions were developed in accordance with FAR 23.831(g), the primary subject group targeted was pilots. Given the specificity of the pilot population, which is predominantly male, an all-male sample was selected. This decision may have precluded the exploration of female responses under similar conditions, thereby limiting the generalizability of the findings and their applicability to different gender groups.
Secondly, the limited sample size, with only 10 individuals in each group, totalling 30, may have compromised the statistical validity and reliability of the results. The limited sample size may have led to instability in the results, particularly in the analysis of gender differences and other underlying variables. Consequently, it is imperative for subsequent studies to encompass a more extensive sample size, inclusive of female subjects, in order to achieve a more profound comprehension of the impact of the heat environment on pilots of diverse genders. This approach will enhance the reliability of the findings and provide more instructive conclusions for practice in related fields.
Finally, in this study, we were unable to conduct our experiments in a high-temperature simulation room combined with a flight simulator due to technical limitations. This constraint may have impacted our ability to collect comprehensive data on flight parameters and emergency decision-making. To address this shortcoming, we opted to evaluate several metrics, including memory, attention, and perceptual ability, as alternatives. However, these metrics may not fully capture the emergency decision-making capabilities of pilots in a real flight environment. Therefore, future research should focus on developing more advanced experimental facilities that integrate high-temperature simulation with flight simulation to more comprehensively assess the effects of high temperatures on pilots.