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Technology transfer

High performance tilt rotor aircraft in which a nacelle tilt angle and a flaperon angle mechanically interwork with each other

  • Department Administrator
  • Registration Date 2020-02-10
  • Hits 6202
□ Outline of Technology
- In a tilt rotor aircraft, a nacelle and a flaperon are mechanically connected by a power transmission mechanism such as a linkage system, and therefore the flaperon moves in connection with changes of a nacelle angle. The present invention is designed to provide a result in which a lift-to-drag ratio of a flying vehicle increases as an aspect ratio of wings increases so that endurance performance is improved, and also to complement and improve a concept of mounting an extension wing which has previously invented (Korean Patent Document No. 10-0822366).

□ Inventor
- Chief researcher Myeong-gyu LEE

□ Registration (Filing) No.
- US : 8544787

□ Title
- High performance tilt rotor aircraft in which nacelle tilt angle and flaperon angle mechanically interwork with each other

□ TLO of the KARI
- Person-in-charge : Senior Administrator of R&D Performance Diffusion Division Moon-Hee, Cho(moonyxp@kari.re.kr)

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