Feasibility Analysis of a Mobile Microgrid Design to Support DoD Energy Resilience Goals
Abstract
:1. Introduction
- Can mobile microgrids (one size fits all) effectively meet an average 10 kW critical load while reducing the reliance on diesel fuel for power generation?
- What are the trade-offs between a mobile microgrid and a single load-specific microgrid (e.g., resilience, time, over or under utilization, load shedding)?
1.1. Motivation and Need
1.2. Specific Contribution
2. Background and Related Research
2.1. DoD Installation Energy Resilience
2.2. Why Does the DoD Care about Energy Resilience?
2.3. DoD Installation Microgrids
2.4. Single Load Microgrids
2.5. Mobile Microgrids
2.6. Related Research/Gap
3. Mission Sets
3.1. Backup Power for DoD Installation Critical Loads
3.2. Contingency Operations
3.3. Large Scale Combat Operations
4. Methodology
4.1. CONOPS and Requirements
4.1.1. Framing Assumptions
- Power outages will likely be accompanied by a fuel-constrained environment such as a natural disaster that restricts fuel transportation due to road damage, damage to nearby supply stores and pipelines, or enemy-targeted SCNs.
- Risk/Reward Relationship: The risk of an outage of both the host domestic grid and installation microgrid does not warrant each individual critical load on the installation having a designated backup power redundancy such as a single load microgrid.
4.1.2. Indentifying Objectives
- Provide an “Off-the-Shelf” solution that allows installation energy managers to treat a mobile microgrid as an equipment purchase rather than going through the design and construction process associated with load-specific implementations for single load microgrids [1].
- Provide a highly mobile design that supports movement with common DoD installation assets (e.g., 10K forklift, flatbed trucks, and trailers).
- Support air transportation using common fixed wing military airlift assets (e.g., C-130 or C-17) and rotary wing airlift assets (e.g., CH-47 or CH-53) to support contingency operations, LSCO, and organic military asset long and short-range air transportation.
- Align with DoD common shipping infrastructure such as flatbed truck, railroad, cargo plane, and cargo ship movement.
- Provide a solution that offers the potential to support DoD installations, contingency operations, and secure rear-echelon power demands in LSCO.
- Restore power to critical loads within 30 min of being collocated with the load.
- Meet an average 10 kW load 12 h a day over 14 days of continuous operation.
- Reduce the need for fossil fuels and resources external to the DoD installation.
4.1.3. Identify Constraints
- The housing for the mobile microgrid in this feasibility study is an International Organization for Standardization (ISO) Triple Container (TriCon).
- -
- The ISO TriCon is a shipping container used heavily by DoD, and is easily transported by both ground and air assets common to DoD and commercial shipping infrastructure. This container constraint was chosen because many DoD forklift assets can move TriCon containers without requiring extensive balancing of the internal load because of the container dimension’s minimal overlap on fork width. This reduces risk in all envisioned operations, requiring only standard training of transportation asset operators.
- The mobile microgrid must be forklift transportable to allow for quicker reaction to emergent power requirements during an outage of the domestic host grid or microgrid.
- -
- The concept is to be able to use internal DoD installation assets to quickly relocate a mobile microgrid to the point of need without the use of special assets which may delay responding to the outage (focused on reducing the “Respond, Adapt” and “Recover” phases of the resilience curve in Figure 2). The forklift-compatible constraint primarily constrains the weight of the mobile microgrid, which for this research, is limited to less than 10,000 lbs (approximately 4535 kg) based on an assumption that DoD installations have Rough Terrain Military Forklifts or similar capabilities.
- The mobile microgrid must be air-transportable.
- -
- For this constraint, both DoD fixed wing and helicopter assets were analyzed. The previous weight restriction of 10,000 lbs (approximately 4535 kg) is more restrictive than the limitations of larger heavy lift rotary wing assets. The other constraint is hazmat considerations associated with the BESS for fixed wing airlift. Helicopter airlift is assumed to be external load only.
4.1.4. Identify Common Load Level (DoD Installations)
4.1.5. Architectural Design
4.2. Modeling and Simulation
4.2.1. Model
- EDG Usage: Calculated as a percent of time compared to running the load only from an EDG.
- Average Load per Day: The load is randomized using a normal distribution and standard deviation around a mean of the threshold average load.
- Load Shed: Calculated as the ratio of the amount of unserved load by the mobile microgrid to the total load demanded.
- Average Sun Hours: The average peak sun hours over the period of operation provides a more widely used and simplified metric to understand the level of conservatism of the model’s renewable power generation.
4.2.2. Simulate
4.3. Analyze Feasibility
4.3.1. Analyze Initial Results
4.3.2. Statistical Analysis of Results
4.3.3. Identify Trade-Offs
5. Preliminary Proposed Design
5.1. Sizing
5.2. Load Analysis
- Average threshold load = 10 kw
- Operating hours per day = 8 h
- Inverter/Charger efficiency = 0.85
- Peak Sun Hours in Worst Month = 3 h/day@1-sun
5.3. PV Sizing
- Rated panel current = 10.92 A
- Nominal panel voltage = 50.01 V
- Coulomb Efficiency = 0.9
- De-rating factor of the panel = 0.9
5.4. BESS Sizing
- Usable days of storage = 1.5 days
- Using Lithium Iron Phosphate (LiFePO4) Batteries with a maximum depth of discharge (MDOD) of 98%
- A temperature correction factor (TCF) at Celcius for LiFePO4 Battery, TCF = 0.90
- Nominal battery voltage = 48 V
- Single battery capacity = 100 Ah
5.5. Generator Sizing
- The system required a charge time of 20 h.
- The charger efficiency is 80%.
6. Mission Engineering Analysis
- The average threshold load is set using a normal distribution with mean of 10 kW and standard deviation of 2 kW.
- The number of PV panel strings in parallel is set using a uniform discreet distribution with minimum of 27 and maximum of 30 panels. This assumes that there may be up to three panels (10% of the proposed PV array) not working in our system at any one time from occurrences such as damage due to transportation, mishandling, or poor connections.
- The Coulomb efficiency for PV panels uses a triangular distribution with a minimum of 0.80, a likeliest of 0.9 and maximum of 0.93. This provided more conservative results from the model’s solar power generation than using a fixed Coulomb efficiency of 0.90 which some simplified solar models recommend [79].
- The panel De-rating Factor, essentially a parameter of panel efficiency, is a triangular distribution with a minimum of 0.85, likeliest of 0.9, and maximum of 0.93. This also provides more conservative results from the model’s solar power generation than using a fixed De-rating Factor of 0.90 which some basic solar models recommend [79].
- The generator set uses a triangular distribution with max at 10 kW and likeliest at 9 kW and minimum at 8.5 kW for short duration run times to correlate to the model timestep of 30 min. This accounts for the generator running at outputs that align with its continuous output power specifications. This ensures the mobile microgrid can support more stressing scenarios where solar irradiance is lower or when work hours are extended outside of normal business hours during contingency and emergency operations.
- Panel rated current uses a uniform distribution from 10 A to 10.88 A to account for variations in panel reliability from panel to panel and other factors such as dust.
6.1. Feasibility Use Case NSA Monterey
6.1.1. January Analysis
6.1.2. July Analysis
6.2. Stressing Scenarios
6.2.1. Stressing Scenario Using January GHI Data
6.2.2. Stressing Scenario Using July GHI Data
7. Discussion and Future Work
7.1. Design Objectives
7.2. Load Size
7.3. Trade-Offs between a Mobile Microgrid and a Static Customized Single Load Microgrid
7.4. Future Work
8. Conclusions
Author Contributions
Funding
Institutional Review Board Statement
Informed Consent Statement
Data Availability Statement
Acknowledgments
Conflicts of Interest
References
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PV Panel Specifications (STC) | Sources | |||||||
---|---|---|---|---|---|---|---|---|
PV Panel Type by Advertised Size | Open Circuit Voltage (Vmp) [V] | Maximum Power Current (Imp) [A] | Rated Maximum Power (Pmax) [W] | Length (Inches) | Width (Inches) | Depth (Inches) | Weight (lbs) | |
450 W | 49.32 | 10.89 | 450 | 82.90 | 41.11 | 1.43 | 53.95 | [54,55,56,57,58] |
320 W | 42.07 | 9.20 | 320 | 67.82 | 39.68 | 1.48 | 43.08 | [59,60,61,62] |
Battery Specifications | ||||||||
Battery Type | Chemistry | Voltage | Storage Capacity [Ah] | Length (Inches) | Width (Inches) | Height (Inches) | Weight (lbs) | |
LiFePO4 | LiFePO4 | 12 | 100 | 12.49 | 6.76 | 8.38 | 27.68 | [63,64,65,66] |
Lead Acid | Lead Acid AGM Deep Cycle | 12 | 100 | 12.75 | 6.74 | 8.51 | 62.9 | [67,68,69,70] |
LiFePO4 | LiFePO4 | 48 | 100 | 26.68 | 14.98 | 9.25 | 135.57 | [71,72,73] |
Generator: DoD Advanced Medium Mobile Power Sources (AMMPS) | ||||||||
Power Rating (kW) | Fuel Consumption: 100% Rated Load 60 Hz (400 Hz) [GPH] | Length (Inches) | Width (Inches) | Height (Inches) | Weight (Wet) [lbs] | |||
10 | 0.75 | 55 | 32 | 36 | 1060 | [74,75] | ||
15 | 1.06 | 65 | 36 | 53 | 1560 | [74] |
Final Design COTS Component Specifications | |||||||||
---|---|---|---|---|---|---|---|---|---|
PV Panel Specifications (STC) | Sources | ||||||||
PV Panel Type by Advertised Size | Quantity | Open Circuit Voltage (Vmp) [V] | Maximum Power Current (Imp) [A] | Rated Maximum Power (Pmax) [W] | Length (Inches) | Width (Inches) | Depth (Inches) | Weight (lbs) | |
450 W | 30 | 49.32 | 10.89 | 450 | 82.90 | 41.11 | 1.43 | 53.95 | [54,55,56,57,58] |
Battery Specifications | |||||||||
Battery Type | Quantity | Chemistry | Voltage | Storage Capacity (Ah) | Length (Inches) | Width (Inches) | Height (Inches) | Weight (lbs) | |
LiFePO4 | 30 | LiFePO4 | 48 | 100 | 26.68 | 14.98 | 9.25 | 135.57 | [71,72,73] |
Generator: DoD Advanced Medium Mobile Power Sources (AMMPS) | |||||||||
Power Rating (kW) | Quantity | Fuel Consumption: 100% Rated Load 60 Hz (400 Hz) [GPH] | Length (Inches) | Width (Inches) | Height (Inches) | Weight (Wet) [lbs] | |||
10 | 1 | 0.75 | 55 | 32 | 36 | 1060 | [74,75] |
Summary of Results from Mission Engineering Analysis | ||||||||
---|---|---|---|---|---|---|---|---|
Use Case | Period of Analysis (Days) | Average Peak Solar/Day (hrs@1-sun/Day) | Average Load Input (kW) [Mean, Std] | Mean Load/Day (kWh/Day as 95% CI) | Mean Generator Usage (has 95% CI) [14 Days = 336 h] | Mean Generator Usage (% of Period of Analysis as 95% CI) | Load Shed (kWh) [Mean, Std] | Load Shed (% of Total Load Demand) [mean, std] |
January at NSA Monterey | 14 | 2.83 | 10, 2 | 135.29 ± 0.53 | 207.03 ± 1.02 | 62 ± 0.29 | 0.49, 11.96 | 0.0, 0.4 |
July at NSA Monterey | 14 | 7.01 | 10, 2 | 135.23 ± 0.54 | 136.65 ± 1.02 | 41 ± 0.31 | 0.00, 0.00 | 0.00, 0.00 |
January Stressing at NSA Monterey | 14 | 2.83 | 17, 2 | 229.34 ± 0.53 | 328.64 ± 0.27 | 98 ± 0.08 | 374.06, 13.74 | 10.69, 8.74 |
July Stressing at NSA Monterey | 14 | 7.01 | 17, 2 | 230.00 ± 0.53 | 297.82 ± 0.72 | 89 ± 0.22 | 72.94, 160.46 | 1.92, 4.09 |
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Varley, D.W.; Van Bossuyt, D.L.; Pollman, A. Feasibility Analysis of a Mobile Microgrid Design to Support DoD Energy Resilience Goals. Systems 2022, 10, 74. https://doi.org/10.3390/systems10030074
Varley DW, Van Bossuyt DL, Pollman A. Feasibility Analysis of a Mobile Microgrid Design to Support DoD Energy Resilience Goals. Systems. 2022; 10(3):74. https://doi.org/10.3390/systems10030074
Chicago/Turabian StyleVarley, Daniel W., Douglas L. Van Bossuyt, and Anthony Pollman. 2022. "Feasibility Analysis of a Mobile Microgrid Design to Support DoD Energy Resilience Goals" Systems 10, no. 3: 74. https://doi.org/10.3390/systems10030074
APA StyleVarley, D. W., Van Bossuyt, D. L., & Pollman, A. (2022). Feasibility Analysis of a Mobile Microgrid Design to Support DoD Energy Resilience Goals. Systems, 10(3), 74. https://doi.org/10.3390/systems10030074