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Light Weight Collective Pitch Control Systems for Swashplateless Rotors

Award Information

Agency:
Department of Defense
Branch:
Army
Award ID:
87087
Program Year/Program:
2009 / SBIR
Agency Tracking Number:
A082-018-0680
Solicitation Year:
N/A
Solicitation Topic Code:
N/A
Solicitation Number:
N/A
Small Business Information
Orbital Research Inc
4415 Euclid Avenue Suite 500 Cleveland, OH 44103-
View profile »
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No
 
Phase 2
Fiscal Year: 2009
Title: Light Weight Collective Pitch Control Systems for Swashplateless Rotors
Agency / Branch: DOD / ARMY
Contract: W911W6-09-C-0046
Award Amount: $730,000.00
 

Abstract:

Orbital Research proposes to design, optimize and demonstrate a light-weight swashplateless helicopter rotor collective control system. Swashplateless rotors are desirable for reasons including increased rotorcraft top speed, reduced vibration, reduced vehicle mass, and reduced rotorhead maintenance. Swashplateless rotor systems utilize on-blade controls (OBC) or individual blade controls (IBC) to adjust the lift created by each rotor blade. However, a limitation of OBC and IBC is that utilizing the OBC/IBC lift authority for collective blade control diminishes the range available for cyclic blade control. Collective control systems that primarily adjust the root blade incidence angle gives increased lift without reducing the authority of the OBC/IBC. To provide reduced complexity and weight, Orbital Research will utilize all-electric, redundant, zero-backlash actuators to drive a single mechanism capable of increasing the root blade incidence. Because the actuators consist of DC motors and a low-volume, high-gear-ratio transmission, the proposed actuators will be extremely reliable. If an actuator fails, the transmission is individually disconnectable, allowing for redundancy to be incorporated into the swashplateless rotor design. Hence, the rotorcraft can maintain normal flight with 2 actuator failures. The resulting design, while aimed at manned single rotor helicopters, will be scalable to a range of rotorcraft including UAVs.

Principal Investigator:

Matthew Birch
Sr. Mechanical Engineer
2166490399
birch@orbitalresearch.com

Business Contact:

Joseph Snyder
Vice President
2166490399
snyder@orbitalresearch.com
Small Business Information at Submission:

ORBITAL RESEARCH, INC.
4415 Euclid Avenue Suite 500 Cleveland, OH 44103

EIN/Tax ID: 341672688
DUNS: N/A
Number of Employees:
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No