Battery and Solar Array Emulator Statement of Work Updated.pdf
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- Attached to
- Intent to Sole Source Notice: DC Bi-Directional Supply for Battery Emulation/Testing and Solar Simulation Federal contract opportunity
- Solicitation number
- 80GRC024PA011
About this file
This document is a Statement of Work for a DC Bi-Directional Supply for Battery Emulation/Testing and Solar Simulation. NASA's Glenn Research Center has a requirement for one multi-purpose battery emulator/tester and solar array simulator to support the Advanced Reconfigurable Electric Aircraft Laboratory (AREAL) and the Revolutionary Vertical Lift Technology (RVLT) project.
The required system must have an AC input of 480Vac, 3-phase, 60Hz and provide a bi-directional DC output of up to 250kW, 1000Vdc, and 1125A. It must emulate lithium-ion and lead-acid battery chemistries, incorporating state-of-charge tracking, irradiance and temperature effects, and the ability to generate programmable sine-wave ripple. The system must also have safety features, local and remote control/telemetry capabilities, and integrated cooling equipment. NASA intends to issue a sole source contract to acquire this commercial item from Anderson Electric Controls, Inc. under the authority of FAR 6.302-1. Interested organizations may submit their qualifications by July 24, 2024 for consideration of a competitive procurement.
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| DC Bi-Directional Supply for Battery Emulation Testing and Solar Simulation SOW.pdf |
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Text version
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
GLENN RESEARCH CENTER
CLEVELAND, OHIO
DC Bi-Directional Supply for Battery Emulation/Testing and Solar Simulation Specifications
Introduction/Background
The Advanced Reconfigurable Electric Aircraft Laboratory (AREAL) is a test facility at Glenn Research Center (GRC) that allows the testing of high- power equipment for eventual use in hybrid-electric aircraft systems. AREAL is part of the Revolutionary Vertical Lift Technology (RVLT) project. The RVLT project is exploring multiple technologies that would enable electric or hybrid-electric aircraft, resulting in quieter, more fuel-efficient, and more environmentally-friendly flight.
Scope of Work NASA GRC needs one multi-purpose battery emulator/tester and solar array simulator for testing and development purposes. The requirements are given below.
System Input Power Requirements:
• Shall have an AC input with the following nominal specifications:
480Vac,LL 60Hz 3 Phase Shall include an appropriately sized transformer to provide galvanic isolation between the unit and the facility
System Output Power Requirements:
• Shall have a DC Output with the following minimum rated specifications:
Fully bi-directional +/- 250kW 1000Vdc +/- 1125A Programmable Current Output (CC Mode) Programmable Voltage Output (CV Mode) Programmable Power Output (CP Mode)
• Shall have a DC Output with the following minimum rated specifications for dynamic performance:
>30 Hz small-signal bandwidth (voltage-mode) 800 Hz small-signal bandwidth (current-mode) Peak voltage slew-rate no less than 100V/ms Peak current slew rate no less than 2kA/ms Output voltage regulation with no greater than 0.1% full-scale error
Emulation Capabilities
• The system shall have the capability to emulate batteries with the following requirements:
Emulate lithium-ion and lead-acid chemistries Emulate using the Partnership of New Generation of Vehicle (PNGV) lumped equivalent battery circuit models Track state-of-charge
• The system shall have the capability to emulate solar arrays with the following requirements:
Incorporate irradiance effects on output performance.
Incorporate temperature effects on output performance.
Contain fully customizable photovoltaic curve capability
• The system shall have the static ability to compensate for voltage drop across on output cable
• The system shall have the dynamic capability to compensate for voltage drop across on output cable
Test Capabilities:
• The system shall have the capability to perform battery cycle testing
• The battery cycle test capabilities shall have integrated watt-hour, amp-hour, and open-circuit voltage measurements.
• The system shall have the capability to generate programmable at least 200 Hz sine-wave ripple on top of the voltage, current or power.
Safety
• The system shall have a hardware interlocked e-stop
• The system shall have a dedicated facility interlock
Control/Telemetry
• The system shall have a local touchscreen for manual control and troubleshooting
• The system shall have remote control capability with the following inputs:
Ethernet (TCP/IP) Input CAN 2.0B Input Analog/digital Input/Hardware-in-the-loop
System to include external air-cooled (natural convection) 275 kVA transformer with 480 VAC L-L Delta primary and 480 VAC L-L Y with floating neutral secondary and 60,000 BTU/HR indoor heat exchanger with dynalene hot-side fluid
Objective Expand capability of the AREAL to include a battery emulator as an additional source for hybrid-electric flight. This will enhance the lab’s ability to emulate different battery chemistries and power levels.
Description of the Work/Contractor Tasks The contractor task consists of providing power supply. No meetings or reviews are expected for this off-the-shelf equipment.
Deliverables The deliverable for this procurement is for one power supply for battery emulation and solar simulation.
File details come from the government source that posted it. Updated .