Low-Cost Ball/Air/Magnetic Hybrid Bearing System for Extended-Life Micro Gas Turbine Engines

Award Information
Agency:
Department of Defense
Branch:
Navy
Amount:
$70,000.00
Award Year:
2010
Program:
STTR
Phase:
Phase I
Contract:
N00014-10-M-0281
Agency Tracking Number:
N10A-037-0678
Solicitation Year:
2010
Solicitation Topic Code:
N10A-T037
Solicitation Number:
2010.A
Small Business Information
Nastec, Inc.
5310 W. 161st Street- Suite G, Brookpark, OH, 44142
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
876355207
Principal Investigator
 Robert Fusaro
 Principal Investigator
 (440) 826-1693
 rfusa@sbcglobal.net
Business Contact
 Richard Klein
Title: President
Phone: (216) 464-8388
Email: dickc123@earthlink.net
Research Institution
 University of Toledo
 Abdollah Afjeh
 Nitschke Hall 4005
Toledo, OH, 43606
 (419) 530-8210
 Nonprofit college or university
Abstract
A unique type of air lubricated thrust bearing called a Wave Bearing is proposed to assist a rolling element bearing to carry the thrust load and to improve the bearing’s life when used in a micro gas turbine engine. The Wave Bearing technology will provide improved reliability, safety and life compared to rolling element bearings used alone, as well as to allow simplification of engine design and reduced costs. When compared to its alternatives, the Wave Bearing has distinct advantages. It is much simpler than a Magnetic Bearing and it is less prone to wear than a Foil Bearing. In the proposed Phase I program, computer codes developed by Dr. Dimofte, will be used to adapt the Wave Bearing to the design requirements relevant to the micro gas turbine engines. Test conditions will be thrust loads to 200N, speeds to 100,000 rpm and durations sufficient to prove the demo. The Wave Bearing will be developed and tested in Phase I to assure with reasonable engineering certainty that it is a viable candidate for use in a micro gas turbine engine and the testing will verify that more extensive testing should be conducted in Phase II.

* information listed above is at the time of submission.

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