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Unmanned flight vehicle including counter rotating rotors positioned within a toroidal shroud and operable to provide al 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-029/00
  • B64C-039/06
출원번호 US-0526092 (1990-05-18)
발명자 / 주소
  • Cycon James P. (Orange CT) Rosen Kenneth M. (Guilford CT) Whyte Andrew C. (Norwalk CT)
출원인 / 주소
  • United Technologies Corporation (Hartford CT 02)
인용정보 피인용 횟수 : 59  인용 특허 : 0

초록

An unmanned flight vehicle wherein two counter-rotating rotors are positioned within a toroidal fuselage and in which rotor pitch solely is utilized to generate all required lift, pitch, roll, yaw and vibration and stress control for the vehicle.

대표청구항 ▼

A flight vehicle comprising: a. a toroidal fuselage concentric about an axis, b. two counter-rotating bladed rotors located within said toroidal fuselage, c. means to position said rotors for rotation about an axis of rotation which is coincident with the fuselage axis, and d. means to totally contr

이 특허를 인용한 특허 (59)

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