$\require{mediawiki-texvc}$
  • 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색연산자 기능 검색시 예
() 우선순위가 가장 높은 연산자 예1) (나노 (기계 | machine))
공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
예2) 나노 장영실
| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
예2) 줄기세포 | 장영실
! NOT 이후에 있는 검색어가 포함된 문서는 제외 예1) (황금 !백금)
예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

Rotor driven auxiliary power apparatus and method

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-027/12    B64C-027/18    B64C-027/02    B64C-027/26    B64C-027/28    B64C-027/82   
미국특허분류(USC) 244/017.11; 244/058; 244/060
출원번호 US-0282938 (2011-10-27)
등록번호 US-8950700 (2015-02-10)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Pate Baird, PLLC
인용정보 피인용 횟수 : 1  인용 특허 : 14
초록

Apparatus and methods is used for controlling yaw of a rotorcraft in the event of one or both of low airspeed and engine failure. A yaw propulsion provides a yaw moment at low speeds. The yaw propulsion device may be an air jet or a fan. A pneumatic fan may be driven by compressed air released into a channel surrounding an outer portion of the fan. The fan may be driven by hydraulic power. Power for the yaw propulsion device and other system may be provided by a hydraulic pump and/or generator engaging the rotor. Low speed yaw control may be provided by ...

대표
청구항

1. A rotorcraft comprising: an airframe;an engine connected to drive the rotorcraft through the air;a rotor rotatably mounted to the airframe and rotatable about an axis of rotation;a power take-off selectively uncoupling from the rotor and coupling to the rotor to be driven by the rotor, the power take-off including a drive wheel; anda power source connected to receive power through the power take-off and comprising at least one of a hydraulic pump and a generator;a mast extending upward;a shroud surrounding the mast and being fastened to the mast;a fla...

이 특허에 인용된 특허 (14)

  1. Darrow, Jr., David A.; D'Anna, Frank P.; Sbabo, Thomas L.. De-rotation system suitable for use with a shaft fairing system. USP2009107607607.
  2. Leibach ; Heinrich. Device for control of an aircraft. USP1978074099671.
  3. Wilson Harold K. (Arlington TX). Drive system for tiltrotor aircraft. USP1991105054716.
  4. Stearns ; Jr. Hoyt A. (4131 E. Cannon Dr. Phoenix AZ 85028). Electric air-driven helicopter. USP1987104702437.
  5. Kirk, Charles T.; Moore, Grover L.; Hodder, legal representative, Virginia L.. Emergency anti-torque thruster system. USP201106E042446.
  6. Kirk,Charles T.; Hodder, legal representative,Virginia L.; Moore, deceased,Grover L.. Emergency anti-torque thruster system. USP2006047032860.
  7. Logan Andrew H. (Rancho Palos Verdes CA) Moore Richard E. (Los Angeles CA). Helicopter antitorque system using circulation control. USP1980044200252.
  8. Ebert Frederick J. (Westport CT) Driscoll Joseph T. (Cheshire CT) Graham ; Jr. Byron (Easton CT) Sweet David H. (Tequesta FL). Helicopter engine control having lateral cyclic pitch anticipation. USP1993115265826.
  9. Wilson John C. (Newport News VA) Crowell Cynthia A. (APO AE NY) Kelley Henry L. (Newport News VA). Helicopter low-speed yaw control. USP1993055209430.
  10. Daniel W. Banks ; Henry L. Kelley. Helicopter tail boom with venting for alleviation and control of tail boom aerodynamic loads and method thereof. USP2002036352220.
  11. Daggett ; Jr. Myron L. (Broomall PA) Douglas Leon L. (Wynnewood PA). Helicopter yaw and propulsion mechanism. USP1976053957226.
  12. Osberger Helmut (A 3491 Strass bei Krems Niederosterreich OE). Helicopters safety drive. USP1977094046335.
  13. De Roche,Mark Stephen. Hybrid drive powered lift platform. USP2007067231997.
  14. Arata,Allen A.. Rechargeable compressed air system and method for supplemental aircraft thrust. USP2006097104499.