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Innovative Approaches to the Fabrication of Composite Rotary Wing Main Rotor Blade Spars

Award Information
Agency: Department of Defense
Branch: Navy
Contract: N68335-08-C-0196
Agency Tracking Number: N081-026-0969
Amount: $79,968.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: N08-026
Solicitation Number: 2008.1
Solicitation Year: 2008
Award Year: 2008
Award Start Date (Proposal Award Date): 2008-04-01
Award End Date (Contract End Date): 2008-10-01
Small Business Information
407 Front Street
Schenectady, NY 12305
United States
DUNS: 799645916
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Anne Roberts
 Project Engineer
 (518) 377-6471
Business Contact
 Robert Langone
Title: Vice President
Phone: (518) 377-6471
Research Institution

Commonly, composite rotor blade spars are fabricated by hand layups or other non-optimized, not fully automated procedures. These methods are labor intensive and require many de-bulking steps, making them expensive. The results are often inconsistent due to the nature of work done by hand. In our process, continuous graphite fiber reinforced thermoset prepreg tape will be used in conjunction with our automated fiber placement technology to produce high performance composite main rotor blade spars. Since our process is automated, it provides repeatable and accurate results with less labor involvement. The use of continuous fiber reinforced prepreg tape allows us to tailor the lay-up to suit the design criteria at hand. Our automated process provides low cost effective manufacturing methods for the production of high quality composite structures.

* Information listed above is at the time of submission. *

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