Dynamic Camber Control for Helicopter Rotor Blades

Award Information
Agency: Department of Defense
Branch: Army
Contract: W911W6-07-C-0053
Agency Tracking Number: A052-067-2679
Amount: $780,000.00
Phase: Phase II
Program: SBIR
Awards Year: 2007
Solicitation Year: 2005
Solicitation Topic Code: A05-067
Solicitation Number: 2005.2
Small Business Information
11750 Beltsville Drive, 3rd Floor, Beltsville, MD, 20705
DUNS: 061997029
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Peter Chen
 VP, Aerospace
 (240) 790-0600
 chenp@technosci.com
Business Contact
 Amy Hizoune
Title: VP, Finance
Phone: (240) 790-0609
Email: aph@technosci.com
Research Institution
N/A
Abstract
Techno-Sciences, Inc. (TSi), in collaboration with the University of Maryland and Bell Helicopter, proposes to develop and test a pneumatic, on-blade rotor vibration control system. This Phase II project will focus on producing an integrated trailing-edge flap (elevon) system consisting of pneumatic actuators, control electronics, air handling components, and actuator mechanisms for the Bell 407 helicopter. Laboratory and full-scale rotor blade prototypes with integrated flaps will be produced and systematically evaluated in Phase II. The full-scale flap system will be evaluated in a vacuum spin chamber, in a wind tunnel, and on a whirl tower to determine system performance under full-scale loading conditions.

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

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