Advanced Large Diameter Air Seals

Award Information
Agency:
Department of Defense
Branch
Air Force
Amount:
$748,547.00
Award Year:
2008
Program:
SBIR
Phase:
Phase II
Contract:
FA8650-08-C-2852
Agency Tracking Number:
F071-187-2681
Solicitation Year:
2007
Solicitation Topic Code:
AF071-187
Solicitation Number:
2007.1
Small Business Information
MOHAWK INNOVATIVE TECHNOLOGY, INC.
1037 Watervliet-Shaker Road, Albany, NY, 12205
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
883926594
Principal Investigator:
Hooshang Heshmat
President/Technical Direc
(518) 862-4290
hheshmat@miti.cc
Business Contact:
James Walton II
V.P. of Program Developme
(518) 862-4290
jwalton@miti.cc
Research Institution:
n/a
Abstract
During Phase I testing, flow factors less than 0.02 for the candidate non-contacting compliant surface axial face seal were measured demonstrating the feasibility of this technology for advanced turbine engines. Under Phase II, the concept design will be enhanced to reduce flow factor to less than .01 and permit axial motions of approximately 0.150 inches. The seal design will then be fabricated and tested under realistic operating conditions of temperature, differential pressure, surface velocity and axial motions to demonstrate performance substantially better than brush, labyrinth and conventional carbon face seals. Initial testing will be conducted with seals sized for smaller engines, but under large-scale engine dynamic conditions. Finally testing of a segment of the complete full-scale seal will be tested statically. To ensure realistic engine test conditions and a path for technology transition to product in both military and commercial engines a major gas turbine engine manufacturer has been enlisted to support the effort with the necessary engine and test requirements as well as design reviews.

* information listed above is at the time of submission.

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