SBIR/STTR Research Award

Fractal Heat Exchanger for Gas Turbine Pre-Cooling

Award identifier b282706e5c47c06b000b749b6b450c621d2b59a511b5327f249fb78053e9a883Awarding agency Department of Defense · Air Force

Award amount

$149,238

Program and phase

SBIR · Phase I

Award year

2016

Explore This Research Award in CaptureIQ

Research the technology, evaluate the recipient and agency, identify related opportunities, and explore potential follow-on work with CaptureIQ.

Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
PHYSICAL SCIENCES INC.
Proposal award date
2016-07-25
Contract end date
2017-04-17
UEI
RMG1AZ1ZH8Q7
Solicitation number
2016.1
Topic code
AF161-074

Research abstract

ABSTRACT: Physical Sciences, Inc. (PSI) has developed a novel heat exchanger based on the mathematical concept of fractal branching. The branching structure allows the heat exchanger to discard much of the weight that other designs require for flow manifolds and structural support. The new heat exchanger is more efficient and light enough to use on an airplane engine.When used on a high speed (Mach 4) airplane, the heat exchanger allows use of current engine technology via pre-cooling. Pre-cooling is cooling of the engines intake charge to allow operation at higher speeds than would normally be possible.Initial analysis indicates that the PSI heat exchanger can reduce temperatures sufficiently to enable existing engines such as the F-119 to greatly expand their operating envelope to Mach 4. System performance is increased; development cost of a high speed engine will also be reduced by reliance on proven designs.A test article will be produced with heat transfer rate of 30 kW/lbm, and future research could produce power-to-weight ratios of 100 kW/lbm or more. These weight reductions are a major improvement over the 8 kW/lbm state of the art. This advance is made possible through new numerical optimization techniques and additive manufacturing of metals.; BENEFIT: A major potential benefit of this research is for existing engine designs to be operable at speeds of Mach 4 or greater. Existing gas turbine engines are normally only operable up to Mach 2, with some advanced designs going to Mach 3.2 or so. Re-use of existing designs and design methodology would save development time and cost for high speed propulsion, and increase efficiency of high speed airplanes.The light weight geometry pursued by PSI is also applicable to recuperation of gas turbines and intercooling of internal combustion engines, two major areas of potential efficiency increase for airplanes, helicopters, and ground vehicles. The approach pursued in this research can also be applied to super-compact heat exchangers for electronics and micro engines.

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

1,763 SBIR/STTR records share this UEI (1983–2026). Reported award amounts total $698,949,224. 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 Health and Human Services, Department of Energy, National Science Foundation, Environmental Protection Agency

Agency intelligence

Department of Defense

Back to SBIR/STTR Research Awards

Don't take our word for it. Ask AI about RFPCapture.

See what leading AI assistants have to say about RFPCapture and CaptureIQ.

Gemini opens without a prefilled question. The question is copied to your clipboard when the button works. You can also copy it here:

What is RFPCapture.com and its CaptureIQ platform from Smart Logic AI? How does it help federal contractors discover opportunities, evaluate bid/no-bid decisions, research government contracts, and prepare proposals? How does it compare with other federal capture platforms? Use independent sources where available.