NASA GL-10 Greased Lightning

GL-10 Greased Lightning
GL-10 Greased Lightning 50% Scale Prototype
Role Hybrid UAV
National origin United States
First flight 19 August 2014 (tethered)
Introduction 2014
Status In development
Number built 1


The GL-10 Greased Lightning is a hybrid diesel-electric tiltwing aircraft.

Development

The full-scale GL-10 will be a diesel-electric tilt-wing. Currently, NASA has built a 50% scale 10-foot wing span all electric battery powered demonstrator. The wings and horizontal stabilizer rotate with fixed motor pods to facilitate vertical flight. The wing has eight electric motor driven propellers while the horizontal stabilizer has two. In the future full-scale version, power will be generated by two 6 kW (8 hp) diesel engines which will charge lithium ion batteries. The propellers on the leading edge of the wing provide high speed flow, and thus lift, on the wing even in low forward velocity flight allowing pitch, roll, and yaw control authority during the critical transition phase from hover to forward flight.

The VTOL capability of this new class of UAV eliminates the requirement for additional ground support equipment like launch catapults and landing catch mechanisms. In addition, the propellers are designed for a relatively low tip speed resulting in a marked reduction in noise.[1][2][3] The aircraft is designed to complete several vertical take-off and landings during its mission with a loiter endurance of 24 hours in the forward flight mode.[4][5][6] The GL-10 performed transitions between vertical and horizontal flight in 2015.[7]


Full scale specifications (GL-10)

Data from NASA

General characteristics

Performance

References

  1. ↑ "NASA's Greased Lightning Tests Vertical Takeoff But is it systematic, hydromatic, ultramatic". Retrieved 25 August 2014.
  2. ↑ "NASA Flies Hybrid Electric VTOL". Retrieved 25 August 2014.
  3. ↑ "Testing Electric Propulsion". Retrieved 25 August 2014.
  4. ↑ Fredericks, W. J., Moore, M. D., & Busan, R. C. (2013). Benefits of Hybrid-Electric Propulsion to Achieve 4x Increase in Cruise Efficiency for a VTOL Aircraft.
  5. ↑ Rothhaar, P. M., Murphy, P. C., Bacon B. J., Gregory, I. M., Grauer, J. A., Busan, R. C., & Croom, M. A. (2014, June). NASA Langley Distributed Propulsion VTOL Tilt-Wing Aircraft Testing, Modeling, Simulation, Control, and Flight Test Development. In 14th AIAA Aviation Technology, Integration, and Operations Conference, Atlanta, GA.
  6. ↑ Busan, R. C., Rothhaar, P. M., Croom, M. A., Murphy, P. C., Grafton, S. B., & O-Neal, A. W. Enabling Advanced Wind-Tunnel Research Methods Using the NASA Langley 12-Foot Low Speed Tunnel.
  7. ↑ Barnstorff, Kathy (4 May 2015). "NASA's Greased Lightning UAV completes successful flight test". Vertical Magazine. Retrieved 5 May 2015.

See also

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