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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-017/10    B64C-023/00    B64C-030/00    B64D-037/00    B64C-003/38    B64C-003/42    B64C-009/00    B64C-003/18    B64C-003/20   
출원번호 US-0176865 (2014-02-10)
등록번호 US-9561847 (2017-02-07)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Ingrassia, Fisher & Lorenz PC
인용정보 피인용 횟수 : 0  인용 특허 : 12
초록

A system for controlling a magnitude of a sonic boom includes a first sensor configured to detect a first condition of the supersonic aircraft. The system further includes a pair of wings configured to move fore and aft. The system further includes a processor communicatively coupled with the sensor and operatively coupled with the pair of wings. The processor is configured to (1) receive a first information from the first sensor indicative of the first condition, (2) calculate a lift distribution of the supersonic aircraft based on the first information...

대표
청구항

1. A system for controlling a magnitude of a sonic boom of a supersonic aircraft at supersonic speeds, the system comprising: a first sensor configured to detect a first condition of the supersonic aircraft;a pair of wings configured to move; anda processor communicatively coupled with the sensor and operatively coupled with the pair of wings, the processor configured to: receive a first information from the first sensor, the first information indicative of the first condition of the supersonic aircraft,calculate a lift distribution of the supersonic air...

이 특허에 인용된 특허 (12)

  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. Fraser Norman T. L. (4597 Candleberry Ave. Seal Beach CA 90740). Control system for forward wing aircraft. USP1976053954231.
  4. Hagemeister,Corey; Aronstein,David C.; Schueler,Kurt L.. Design methods and configurations for supersonic aircraft. USP2007087252263.
  5. Friebel Gottfried O. (Bellevue WA) Kulfan Robert M. (Kirkland WA). Double parasol, favorable interference airplane. USP1986074598886.
  6. Tracy,Richard R.; Chase,James D.. Lift and twist control using trailing edge control surfaces on supersonic laminar flow wings. USP2006027004428.
  7. Morgenstern John M. Low sonic boom shock control/alleviation surface. USP1998045740984.
  8. Wood Richard M. (Virginia Beach VA). Multi-body aircraft with an all-movable center fuselage actively controlling fuselage pressure drag. USP1988044735381.
  9. Hartmann, Tom. Passive aerodynamic sonic boom suppression for supersonic aircraft. USP2003076588703.
  10. Rouleau, Bruce S.; Graham, David H.; Reynolds, Ross S.; Wainfan, Barnaby S.. Supersonic aircraft. USP200303D471854.
  11. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2004036698684.
  12. 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.