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Glenn
Research Center
1994 Phase II
Single
Lever Power Control for General Aviation and Unmanned Aircraft
Aurora
Flight Sciences Corporation
Manassas, VA
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INNOVATION
Pilot or Autopilot controls General
Aviation or Unmanned Air Vehicle (UAV) propulsion system via a Single
Lever or a Single Power Command using a FADEC (Full-Authority Digital
Engine Control) with optimal propeller/engine control
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Aurora's Chiron aircraft with full-digital
Single Lever Power Control
Optional Powerpoint
file
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ACCOMPLISHMENTS
- Developed first FADEC with full-digital
Single Lever Power Control (SLPC) for General Aviation (GA)
aircraft with optimal propeller/engine control
- Developed and flight-tested
the SLPC-FADEC system in GA aircraft - showed over 20% fuel
consumption improvement
- Tested FADEC system with UAV
engine in test cell to 68,000 ft altitude
- FADEC-controlled engine propels
the Perseus B high- altitude UAV to 60,000 ft altitude
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COMMERCIALIZATION
- Joint ventures with Athena Technologies
combines SLPC with advanced flight controls and FTC (Fault-tolerant
Control) algorithms
- FADEC-controlled engines operated
in excess of 500 hours in test cells and in flight
- Ideal propulsion control unit
for General Aviation naturally aspirated and turbocharged
singles, twins, turboprops and other transportation propulsion
systems
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GOVERNMENT/SCIENCE
APPLICATIONS
- Currently being used in NASA’s
AGATE (Advanced General Aviation Transport Experiment) for integrated
flight tests with all-digital cockpit technology components
- Potentially used in NASA’s ERAST
(Environmental Research and Atmospheric Science Technology) UAV
program
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