$\require{mediawiki-texvc}$
  • 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 configuration for reaction drive rotor system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-027/605    B64C-027/18    B64C-027/02   
미국특허분류(USC) 244/017.25; 244/017.11; 416/090R
출원번호 US-0373433 (2011-11-14)
등록번호 US-9038940 (2015-05-26)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Pate Baird, PLLC
인용정보 피인용 횟수 : 0  인용 특허 : 14
초록

A rotor system is disclosed for a reactive drive rotary wing aircraft. Apparatus and methods are disclosed for maintaining the rigidity of the rotor and eliminating play between flight controls and the rotor by mounting swashplate actuators to a flange rigidly secured to the mast. Methods are disclosed for modulating the temperature of oil pumped over one or more of the mast bearing, swashplate bearing, and spindle bearing. The temperature of air passively or actively drawn through rotor may also be modulated to maintain bearing temperature within a pred...

대표
청구항

1. A rotor system comprising: a mast mounted to an airframe and defining a rotor axis;a hub rotatably mounted to the mast and rotatable with respect to the mast only about the rotor axis, the hub defining a hub cavity; anda plurality of blades mounted to the hub, blade of the plurality of blades defining a duct in fluid communication with the hub cavity, the blade duct being defined by a blade spar of the each blade, the blade spar extending through the hub and into the hub cavity and having a pitch horn secured thereto and positioned within the hub cavi...

이 특허에 인용된 특허 (14)

  1. Pancotti Santino,ITX. Cyclic and collective pitch control device for a helicopter rotor. USP2001126325326.
  2. Leibach ; Heinrich. Device for control of an aircraft. USP1978074099671.
  3. Osder, Stephen S.; Thompson, Thomas L.. Enhanced flight control systems and methods for a jet powered tri-mode aircraft. USP2005046885917.
  4. Flanigan,Kenneth Warren. Gas-powered tip-jet-driven tilt-rotor compound VTOL aircraft. USP2006127147182.
  5. Logan Andrew H. (Rancho Palos Verdes CA) Moore Richard E. (Los Angeles CA). Helicopter antitorque system using circulation control. USP1980044200252.
  6. Wilson John C. (Newport News VA) Crowell Cynthia A. (APO AE NY) Kelley Henry L. (Newport News VA). Helicopter low-speed yaw control. USP1993055209430.
  7. Daniel W. Banks ; Henry L. Kelley. Helicopter tail boom with venting for alleviation and control of tail boom aerodynamic loads and method thereof. USP2002036352220.
  8. Daggett ; Jr. Myron L. (Broomall PA) Douglas Leon L. (Wynnewood PA). Helicopter yaw and propulsion mechanism. USP1976053957226.
  9. Keller Merrill Manson. Keller pressure jet rotor system. USP1999115984635.
  10. De Champeaux, Charles; De Champeaux, Philippe. Rotary seal. USP2013038387910.
  11. Pica, Bret D.. Rotary/fixed wing aircraft. USP2005016845941.
  12. Nyhus Daniel A.. Rotor pitch lock for rotary/wing aircraft. USP2001016170779.
  13. Rampal Etienne,FRX. Swash-plate device for controlling the pitch of rotor blades with non rotating plate stop track and pin. USP2000036033182.
  14. Rampal Etienne Jean,FRX ; Garcin Sylvie,FRX. Swash-plates system for control of the pitch of rotor blades with rotating plate driver. USP2001086280141.