SBIR-STTR Award

Powerplant development for a miniature tilt-body UAV having long endurance and VTOL capability
Award last edited on: 4/4/2019

Sponsored Program
STTR
Awarding Agency
DOD : Navy
Total Award Amount
$599,912
Award Phase
2
Solicitation Topic Code
N09B-T039
Principal Investigator
Tad McGeer

Company Information

Aerovel Corporation

83 Oak Ridge Road
White Salmon, WA 98672
   (541) 490-4103
   tad@aerovelco.com
   www.aerovelco.com

Research Institution

University of Washington - Seattle

Phase I

Contract Number: N68335-10-C-0154
Start Date: 1/28/2010    Completed: 8/17/2011
Phase I year
2010
Phase I Amount
$99,942
We envision a class of miniature robotic aircraft dubbed Flexrotors which offer range, endurance, and economy at levels associated with wing-borne flight, together with capability for hover and VTOL. Such aircraft would use low-disc-loading rotors which must operate efficiently from zero advance ratio in thrust-borne flight, with rotor axis vertical, to high advance ratio in wing-borne cruise, with rotor axis horizontal. Our proposed Phase I work would advance structural and aerodynamic development of the necessary rotor blades, including wind-tunnel testing. Phase II would include demonstration of long range and endurance with a Flexrotor aircraft.

Benefit:
Miniature VTOL aircraft promise substantially to reduce acquisition and deployment costs for robotic-aircraft systems, while offering unprecedented capability. Consequently they may well make robotic aircraft competitive in multiple new applications for which current designs are uneconomic. Commercial possibilities include ship-based imaging reconnaissance, geomagnetic survey, weather reconnaissance, and atmospheric research.

Keywords:
Tiltrotor, Tiltrotor, OAV, robotic aircraft, MAV, Flexrotor, UAV

Phase II

Contract Number: N68335-11-C-0445
Start Date: 9/27/2011    Completed: 3/28/2013
Phase II year
2011
Phase II Amount
$499,970
We envision a class of miniature robotic aircraft dubbed Flexrotors which offer range, endurance, and economy at levels associated with wing-borne flight, together with capability for hover and VTOL. Such aircraft would use low-disc-loading rotors which must operate efficiently from zero advance ratio in thrust-borne flight, with rotor axis vertical, to high advance ratio in wing-borne cruise, with rotor axis horizontal. As Phase I completed we flew our first prototype in hover. Phase II would develop the rotor and powerplant necessary for demonstration of the full flight envelope, including endurance well over 24 hr.

Benefit:
Miniature VTOL aircraft promise substantially to reduce acquisition and deployment costs for robotic-aircraft systems, while offering unprecedented capability. Consequently they may well make robotic aircraft competitive in multiple new applications for which current designs are uneconomic. Commercial possibilities include ship-based imaging reconnaissance, geomagnetic survey, weather reconnaissance, and atmospheric research.

Keywords:
Flexrotor, UAV, Tiltrotor, MAV, robotic aircraft, OAV