SBIR/STTR Research Award

Bearings for High-Speed Cruise Missile Engine

Award identifier 8367dbd9e1e406333e7052e0eafc903c57576fd6662cf8d761921ff887efd0eaAwarding agency Department of Defense · Air Force

Award amount

$1,499,467

Program and phase

SBIR · Phase II

Award year

2014

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
MOHAWK INNOVATIVE TECHNOLOGY, INC.
Proposal award date
2014-01-24
Contract end date
2019-03-03
UEI
ZY3GYFN4ELC4
Solicitation number
2012.1
Topic code
AF121-169

Research abstract

ABSTRACT:The overall objective of this proposed effort is to demonstrate bearing technology to meet the requirements for a high performance 1000 lbf thrust gas turbine engine.MiTi and its engine company subcontractor will establish simulator designs of two candidate engines representative of near and longer term applications of the advanced bearings to be demonstrated under this program.The engine subcontractor will establish engine modifications needed for bearing integration.Under Phase II the full scale high temperature bearings will be tested in a relevant environment including expected loads, speeds, temperatures and pressures.Testing will also include non-operating and operating vibration environment.In assessingboth journal and thrust bearing requirements, the limitations of and/or engine modifications needed to make the technology suitable for use in engines will be identified.MiTi will use high temperature bearing alloys in the candidate bearings for operation at relevant high temperatures and will test possible alternative approaches to meeting the requirements.After testing in the test rigs with substantially different load/speed characteristics MiTi will assess the range of scalability possible with the advanced bearing designs.Finally, an updated transition plan for engine integration and testing will be provided, including engine modifications needed to integrate the bearing technology.BENEFIT:This effort will directly support the US Air Force initiative for propulsion systems and components to enhance advanced gas turbine engine performance normalized to cost specifically directed at advanced cruise missile engines.Research performed during this SBIR will result in new design capabilities and methodologies for wide ranging applications such as Integrated Power Units (IPU), gas turbine engines for use in UAVs, missiles, drones and both General and Regional Aviation aircraft.Key markets for the foreseeable future that will be served by foil bearings will include energy and environmental areas, including turbine powered generators as well as waste heat recovery systems and compressors for transportation and delivery of natural or/or hydrogen gas. This technology will also support MiTis current oil-free compressors, blowers for wastewater treatment and high speed drive motors.

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

105 SBIR/STTR records share this UEI (1995–2022). Reported award amounts total $40,033,528. 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 Health and Human Services, National Science Foundation, Department of Commerce

Agency intelligence

Department of Defense

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