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Movable nose cap and control strut assembly for supersonic aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-001/38    B64C-001/00    B64C-001/40    B64C-001/52    B64C-003/18    B64C-003/00   
미국특허분류(USC) 244/130; 244/001.A; 244/001.N; 244/171.7; 244/099.1; 244/003.21; 244/037
출원번호 US-0198498 (2005-08-05)
등록번호 US-7278609 (2007-10-09)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Pietragallo Bosick & Gordon, LLP
인용정보 피인용 횟수 : 4  인용 특허 : 11
초록
▼

A nose cap and control strut assembly for supersonic aircraft is disclosed. In one embodiment, the nose cap extends forward from the nose of the aircraft to deflect shock waves and decrease draft during supersonic flight. In another embodiment, control struts extending from the nose of the aircraft have control surfaces which provide yaw and pitch control for the aircraft. The control struts may be rotatable around axes substantially parallel with the longitudinal axis of the aircraft. The control struts may also be retractable into the aircraft. The no...

대표
청구항
▼

The invention claimed is: 1. An aircraft nose cap and control strut assembly comprising: at least two rotatable control struts including control surfaces extending from a nose of the aircraft; and a nose cap mounted at a forward end of the at least two rotatable control struts wherein the control struts are rotatable around different axes which are substantially parallel with each other and the nose cap is coupled to the control struts such that rotation of the control struts does not result in rotation of the nose cap. 2. The assembly of claim 1, wh...

이 특허에 인용된 특허 (11)

  1. Taylor Thomas C. (P.O. Box 1547 Wrightwood CA 92397) Cerna Peter (2815 California ; #4 Dickinson TX 77539). Aerospike for attachment to space vehicle system. USP1987034650139.
  2. Taylor Thomas C. (P.O. Box 1547 Wrightwood CA 92397) Cerna Peter (2815 California ; #4 Dickinson TX 77539). Aerospike for attachment to space vehicle system. USP1988124790499.
  3. Kranz Walter (Taufkirchen DEX). Device for controlling aerodynamic bodies. USP1992015083724.
  4. Peters ; Jr. Spence E. (Fort Worth TX). Flight control device to provide directional control. USP1993045201829.
  5. Kranz Walter (Taufkirchen DEX) Schnbele Werner (Wolfratschausen both of DEX). Missile with adjustable flying controls. USP1990024898342.
  6. Moskovitz Cary A. (Blacksburg VA). Rotatable non-circular forebody flow controller. USP1991095050819.
  7. Ng Tsun-Ming T. (San Pedro CA) Ayers Bert F. (Torrance CA). Rotatable nose and nose boom strakes and methods for aircraft stability and control. USP1993055207397.
  8. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2004036698684.
  9. Cunningham ; Jr. Atlee Marion. Trapped vortex airfoil nose. USP2000126161802.
  10. Kramer Brian (Redondo Beach CA). Vertical nose strake for aircraft stability and control. USP1995095449131.
  11. Rao Dhanvada M. (Hampton VA) Murri Daniel G. (Grafton VA). Yaw and pitch control of air vehicles at high angles of attack. USP1988114786009.

이 특허를 인용한 특허 피인용횟수: 4

  1. Grip, Robert Erik; Brown, John Joseph. Expandable nose cone. USP2015099132908.
  2. Schulein, Erich. Flying object for transonic or supersonic velocities. USP2014028657237.
  3. Mbamalu, Othniel. Space vehicle system. USP20180710023329.
  4. Tyree, Anthony K.. System and method for navigating an object. USP2013088502126.

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