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특허 상세정보

Systems and methods for controlling a magnitude of a sonic boom

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-023/00    B64C-030/00    B64C-037/00    B64C-003/38    B64C-003/42    B64C-009/00    B64C-003/18    B64C-003/20    B64C-017/10    B64D-037/00   
출원번호 US-0176879 (2014-02-10)
등록번호 US-9580169 (2017-02-28)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Lorenz & Kopf, LLP (LKGlobal)
인용정보 피인용 횟수 : 0  인용 특허 : 13
초록

A system for controlling a magnitude of a sonic boom caused by off-design operation of a supersonic aircraft includes a sensor configured to detect a condition of the supersonic aircraft. The system further includes a control surface that is mounted to a wing of the supersonic aircraft. The system still further includes a processor communicatively coupled to the sensor and operatively coupled with the control surface. The processor is configured to (1) receive information from the sensor indicative of the condition of the supersonic aircraft, (2) determi...

대표
청구항

1. A system for controlling a magnitude of a sonic boom caused by operation of a supersonic aircraft at supersonic speeds, the system comprising: a sensor configured to detect a condition of the supersonic aircraft;a control surface mounted to a wing of the supersonic aircraft; anda processor communicatively coupled to the sensor and operatively coupled with the control surface, the processor configured to: receive information from the sensor indicative of the condition of the supersonic aircraft,determine that there is a deviation between a lift distrib...

이 특허에 인용된 특허 (13)

  1. Garrett Timothy M.. Aerodynamic body having coplanar joined wings. USP1999055899410.
  2. Lee, Howard; Morgenstern, John M.; Aminpour, Hossein. Aircraft with active center of gravity control. USP2005076913228.
  3. Gerhardt Heinz A. ; Seho Kenneth ; Nolan Joan ; Mrdeza Matthew N.. Aircraft with variable forward-sweep wing. USP1999115984231.
  4. Fraser Norman T. L. (4597 Candleberry Ave. Seal Beach CA 90740). Control system for forward wing aircraft. USP1976053954231.
  5. Hagemeister,Corey; Aronstein,David C.; Schueler,Kurt L.. Design methods and configurations for supersonic aircraft. USP2007087252263.
  6. Friebel Gottfried O. (Bellevue WA) Kulfan Robert M. (Kirkland WA). Double parasol, favorable interference airplane. USP1986074598886.
  7. Tracy,Richard R.; Chase,James D.. Lift and twist control using trailing edge control surfaces on supersonic laminar flow wings. USP2006027004428.
  8. Morgenstern John M. Low sonic boom shock control/alleviation surface. USP1998045740984.
  9. Wood Richard M. (Virginia Beach VA). Multi-body aircraft with an all-movable center fuselage actively controlling fuselage pressure drag. USP1988044735381.
  10. Hartmann, Tom. Passive aerodynamic sonic boom suppression for supersonic aircraft. USP2003076588703.
  11. Rouleau, Bruce S.; Graham, David H.; Reynolds, Ross S.; Wainfan, Barnaby S.. Supersonic aircraft. USP200303D471854.
  12. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2004036698684.
  13. Westre Willard N. ; Allen-Lilly Heather C. ; Ayers Donald J. ; Cregger Samuel E. ; Evans David W. ; Grande Donald L. ; Hoffman Daniel J. ; Rogalski Mark E. ; Rothschilds Robert J.. Titanium-polymer hybrid laminates. USP2000096114050.