SBIR/STTR Research Award

Micro Fuel Pumps for Small, Heavy Fuel Engines

Award identifier 95bd7669b0fe612273f6390f3e11075d83f0f5b891a21497478aa9f04cc4f7b4Awarding agency Department of Defense · Air Force

Award amount

$99,791

Program and phase

SBIR · Phase I

Award year

2008

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
PRINCEPT RESEARCH GROUP
Proposal award date
2008-06-25
Contract end date
2008-12-25
UEI
Not reported
Solicitation number
2008.1
Topic code
OSD08-UM4

Research abstract

A micro fuel injection system has been proposed to mix fuel and air directly in a combustion chamber quickly and in a controlled fashion to promote efficient and clean combustion. A system constituting of a high pressure fuel pump system, injector(s), distribution lines, injector drivers and control harness would support this micro fuel injection system. A novel pump design (using traditional elements) has been developed to support these fuel injector systems. Miniaturization of traditional fixed clearance pumps sized for the 5-200HP (30lb Thrust Class Inclusive) engine ranges has seen limited efforts. While high performance pumps exist, engine applications have not emphasized the need for miniaturization. Innovative engine technologies coupled with the high performance and small foot print needs of military and aerospace applications are driving the expansion of the technology envelope for optimized lower flow miniaturized pumps. Low flow/high pressure applications define a corner of the pump market that has been met through pump over sizing. This pump design is optimized for the aforementioned low flow applications. Particular attention has been paid to internal sealing, component tolerances, and performance optimization. Specifically, geometry considerations at the pump inlet allow for greater fill pressure and thereby higher altitude operations and performance.

Technology keywords

Not reported

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Agency intelligence

Department of Defense

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