SBIR/STTR Research Award

FADEC Cooling Using High Temperature Loop Heat Pipes

Award identifier 54bd2733445721fd37e9a5c9b4844f68a03da180376d8669bb9d05ccc7c32e36Awarding agency Department of Defense · Air Force

Award amount

$1,097,700

Program and phase

SBIR · Phase II

Award year

2009

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
ADVANCED COOLING TECHNOLOGIES INC
Proposal award date
2009-03-20
Contract end date
2011-07-20
UEI
Z8KVZV3DR7J4
Solicitation number
2007.3
Topic code
AF073-049

Research abstract

The Full Authority Digital Engine Control (FADEC) controls engine operation.  It is historically mounted on the engine case to minimize the routing length of the sensor and actuator wiring.  The FADEC must be maintained below 70°C, while the environment can be as hot as 170°C.  The current design uses fuel to cool the FADEC, however, this often limits the allowable ground or flight idle time before the fuel is too hot to cool the FADEC.  The Phase I program demonstrated that a Loop Heat Pipe (LHP) and heat pipes can be combined into an adaptable thermal management system.  This system will use multiple heat sinks to remove the FADEC heat, passively selecting the best sink at different flight regimes.  Fuel cooling will not longer be required during ground idle.  The goal of the Phase II program will be to design, fabricate, and test a LHP thermal system for passively cooling the FADEC.  The LHP will operate at a higher temperature than conventional aluminum/ammonia LHPs.  The current design will use a titanium LHP, as well as heat pipes incorporated into the FADEC internals. BENEFITS: In addition to the FADEC, the thermal management system that will be developed under this program has the potential to benefit essentially all aircraft electronic systems (power electronics and controls) on both military and commercial platforms.  The first application for a FADEC with advanced thermal management capability is expected to be a future derivative of the F-35 which could realize significant benefit if an alternate heat sink could replace the current fuel heat sink.  The system can also be used for cooling electronic boxes in future military and commercial aircraft, as well as retrofitting current aircraft.  A second military application would be LHP cooling of electrical actuators.  Currently, these actuators require cooling air be ducted to them in the wing, which LHPs could eliminate. As electrical actuators replace hydraulic actuators on commercial aircraft, this concept could also provide cooling.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

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

Research funding history

282 SBIR/STTR records share this UEI (2003–2026). Reported award amounts total $118,415,811. Reported amounts are not federal obligations.

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

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Energy, National Science Foundation, Department of Agriculture, Department of Health and Human Services

Agency intelligence

Department of Defense

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