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특허 상세정보

Fuselage nose for controlling aerodynamic vehicles and method of utilizing same

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-010/02    B64C-005/00    B64C-009/00    B64C-009/08   
미국특허분류(USC) 244/003.21 ; 244/003.1 ; 244/003.24 ; 244/003.27 ; 244/075R ; 244/090R
출원번호 US-0377691 (1999-08-20)
우선권정보 DE9837800 (1998-08-20)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Crowell & Moring LLP
인용정보 피인용 횟수 : 27  인용 특허 : 4
초록

A control system for aerodynamic vehicles has a fuselage nose segment and at least one strake. The fuselage nose segment is rotationally adjustable with respect to the aircraft fuselage. The at least one strake is mounted on the fuselage nose segment so that the strake can swing out.

대표
청구항

[ What is claimed is:] [13.]13. A control system for an aerodynamic vehicle which has a fuselage, comprising:a fuselage nose segment rotatable with respect to said fuselage,a strake mounted at the fuselage nose segment,a fuselage nose segment rotating means for rotating the fuselage nose segment with respect to the fuselage, anda strake moving means for moving the strake between an inoperative position inside the fuselage nose segment to an operative position extending outwardly of the fuselage nose segment to apply aerodynamically induced control forces...

이 특허를 인용한 특허 피인용횟수: 27

  1. Geswender,Chris E.; Hinsdale,Andrew J.; Blaha,George A.; Dryer,Richard. 2-D projectile trajectory correction system and method. USP2007017163176.
  2. David J. Hepner ; Michael S. L. Hollis ; Peter C. Muller ; Thomas E. Harkins ; Gary Borgen ; William P. D'Amico ; Bradford S. Davis ; Lawrence W. Burke. Aeroballistic diagnostic system. USP2002026349652.
  3. Marmo, Anthony V.. Aerodynamic strakes for underbody panels of motor vehicles. USP20181210155552.
  4. Prince, Troy; Lisy, Frederick J.; Patel, Mehul P.; DiCocco, Jack M.; Carver, Reed; Schmidt, Robert N.. Aircraft and missile forebody flow control device and method of controlling flow. USP2011077977615.
  5. Prince,Troy; Lisy,Frederick J.; Patel,Mehul P.; DiCocco,Jack M.; Carver,Reed; Schmidt,Robert N.. Aircraft and missile forebody flow control device and method of controlling flow. USP2007067226015.
  6. Harbeck, Michael W.; Quayle, Brian. Aircraft fuselage drag reduction blivet. USP2014078783617.
  7. Jay Lipeles ; R. Glenn Brosch. Guided bullet. USP2002116474593.
  8. Conners, Timothy R.; Henne, Preston A.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2016119482155.
  9. Conners, Timothy R.; Howe, Donald C.; Henne, Preston A.. Isentropic compression inlet for supersonic aircraft. USP2012128333076.
  10. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012128327645.
  11. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012108286434.
  12. Conners, Timothy R.. Low shock strength inlet. USP2013038393158.
  13. Conners, Timothy R.. Low shock strength inlet. USP2015059027583.
  14. Conners, Timothy R.. Low shock strength propulsion system. USP2014068739514.
  15. Conners, Timothy R.. Low shock strength propulsion system. USP2014078783039.
  16. Low, Richard; Deeds, Michael; Jean, Daniel L.; Hovland, Christopher. MEMS control surface for projectile steering. USP2009127628352.
  17. Hakenesch, Peter. Method and apparatus for determining air flow and pressure data of an aircraft or aerodynamic vehicle. USP2003056568260.
  18. Teter, Roger D.; Dunn, Steven; Barczi, Kenneth. Methods and apparatus for varying a trim of a vehicle. USP2013068466397.
  19. Jones, James F.; Kast, Brian A.; Kniskern, Marc W.; Rose, Scott E.; Rohrer, Brandon R.; Woods, James W.; Greene, Ronald W.. Small caliber guided projectile. USP2010087781709.
  20. Olden, Thomas A.; Cavalleri, Robert; Kinsey, Jr., Lloyd E.. Solid-fuel pellet thrust and control actuation system to maneuver a flight vehicle. USP2012068193476.
  21. Luo, Michael Y. H.; Mohr, Harvey O.; Zhang, Lixin; Lambrakos, Kostas Filoktitis. Spar hull belly strake design and installation method. USP2014078783198.
  22. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Supersonic aircraft jet engine installation. USP2016059334801.
  23. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2004036698684.
  24. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2014078789789.
  25. Levine, Mark D.. Toy pen. USP200305D474237.
  26. Morris, Joseph P.; Smith, Douglas L.. Trajectory modification of a spinning projectile. USP2015059040885.
  27. Potvin, Caleb J.; Fahland, Jason D.. Variable-width aerodynamic spoiler assemblies and control logic for motor vehicles. USP20190410246141.