Hybrid Carbon/Aramid Composite Drive Shaft with Captured Titanium End Fittings

Award Information
Agency:
Department of Defense
Branch
Navy
Amount:
$99,858.00
Award Year:
2010
Program:
SBIR
Phase:
Phase I
Contract:
N00014-10-M-0171
Agency Tracking Number:
N101-097-0615
Solicitation Year:
2010
Solicitation Topic Code:
N101-097
Solicitation Number:
2010.1
Small Business Information
Aurora Flight Sciences Corporation
9950 Wakeman Drive, Manassas, VA, 20110
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
604717165
Principal Investigator:
Brandon Pollett
Manufacturing Engineer
(304) 848-5957
bpollett@aurora.aero
Business Contact:
Scott Hart
Financial Analyst
(617) 500-0536
shart@aurora.aero
Research Institution:
n/a
Abstract
Aurora proposes to enhance the CH-53K helicopter drive shaft by reducing the weight and improving its ballistics survivability through the use of advanced composite materials. The new drive shaft will utilize carbon and aramid fibers, an advanced BMI resin system, and captured titanium end fittings in conjunction with existing metal components to reach these improved performance goals. A hybrid composite design also allows for material property tailoring to better meet the structural, dynamic, and environmental requirements imposed on the drive shaft. A composite drive shaft solution that is light weight, low cost, and provides operational performance after incurring ballistic damage would greatly benefit the overall value, performance, and survivability of military rotary wing assets.

* information listed above is at the time of submission.

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