SBIR/STTR Research Award

Development of a Series Hybrid Propulsion System Using Heavy Fuels

Award identifier 6cfc02a8c76ca8d665b7992f2804a32d136d7b98a12a050374f9e23d09799078Awarding agency Department of Defense · Air Force

Award amount

$148,789

Program and phase

SBIR · Phase I

Award year

2013

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
MAINSTREAM ENGINEERING CORP
Proposal award date
2013-06-12
Contract end date
2014-03-10
UEI
YR8FJBGXWRR1
Solicitation number
2013.1
Topic code
AF131-159

Research abstract

ABSTRACT: The objective of this SBIR topic is to develop a hybrid electric propulsion system to support a Rapid Response Small SUAS (<30lb) capability. This requires fast dash (>150mph) while maintaining extended endurance (>15 hrs) on station and low acoustic noise operation. Full details of the requirements are provided in the solicitation. These UAVs use combustion engines for propulsion and often carry a payload specific to their mission. Currently however, these propulsion systems must be sized for take-off power and are therefore oversized and less efficient for part-load cruise conditions. The proposed engine has much greater efficiency, when compared to a turbine engine, so to reduce overall take-off weight (of engine and fuel) for a 15-25 hour endurance. Furthermore, Mainstream"s patent-pending design that integrates the electrical and mechanical systems also reduces the size of the generator and provides far greater motor starting torque, whenever low-temperature starting is required. MEC is uniquely qualified for this type of work with years of experience in energy conversion and the development of lightweight engines, permanent magnet motor/alternators, and power electronics. In phase I, MEC will also construct and test a bench-top, proof-of-concept hybrid system to confirm simulated component efficiency and fuel savings. BENEFIT: The Phase I effort will provide the proof-of-concept needed by the Air Force and Mainstream to decide whether or not the product is technically and commercially viable. The system-level modeling in Phase I will provide a clear picture of the benefits in terms of flight endurance and operational capability (i.e., silent mode endurance) of the proposed hybrid drivetrain. The engine, alternator, and charge management system will be designed in Phase I. The value proposition for the electric propulsion product is a significant increase in operational capabilities for small UAVs, namely increased flight endurance and the capability for silent mode operation. MEC"s approach is composed of several components that have a high likelihood of being commercialized: 1) a heavy-fuel, high power-density engine, 2) a power dense alternator, 3) a power converter, and 4) a power management system.

Technology keywords

Not reported

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

518 SBIR/STTR records share this UEI (1987–2025). Reported award amounts total $184,860,329. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: Department of Defense, Department of Energy, National Aeronautics and Space Administration, Department of Transportation, Department of Health and Human Services, Environmental Protection Agency

Agency intelligence

Department of Defense

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