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특허 상세정보

Aircraft and missile forebody flow control device and method of controlling flow

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-023/06   
미국특허분류(USC) 244/203; 199/075.R; 199/130
출원번호 US-0336117 (2003-01-03)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Kolkowski, Brian M.
인용정보 피인용 횟수 : 28  인용 특허 : 3
초록

The present invention relates to a forebody flow control system and more particularly to aircraft or missile flow control system for enhanced maneuverability and stabilization at high angles of attack. The present invention further relates to a method of operating the flow control system. In one embodiment, the present invention includes a missile or aircraft comprising an afterbody and a forebody; at least one deployable flow effector on the missile or aircraft forebody; at least one sensors each having a signal, the at least one sensor being positioned...

대표
청구항

The present invention relates to a forebody flow control system and more particularly to aircraft or missile flow control system for enhanced maneuverability and stabilization at high angles of attack. The present invention further relates to a method of operating the flow control system. In one embodiment, the present invention includes a missile or aircraft comprising an afterbody and a forebody; at least one deployable flow effector on the missile or aircraft forebody; at least one sensors each having a signal, the at least one sensor being positioned...

이 특허를 인용한 특허 피인용횟수: 28

  1. Moniz, Thomas Ory; Rose, Joseph George; Orlando, Robert Joseph; Chou, Chenyu Jack. Actuation system utilizing MEMS technology. USP20190210215047.
  2. 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.
  3. Patel, Mehul; Ng, T. Terry; Suchy, Paul. Aircraft, missile, projectile or underwater vehicle with improved control system and method of using. USP2014088809755.
  4. Patel, Mehul P.; Ng, T. Terry; Suchy, Paul. Aircraft, missile, projectile, or underwater vehicle with improved control system and method of using. USP2017059664485.
  5. Clingman, Dan J.. Apparatus and method for generating vortexes in fluid flow adjacent to a surface. USP2011118047233.
  6. Summers, Matthew H.; Koehler, Frederick B.; Danforth, Jeremy C.; Villarreal, James K.. Base drag reduction fairing using shape memory materials. USP20190110184762.
  7. White, Daniel John; Woolley, Clive Charles; Abbey, Jim Maurice; Simpson, David; Driscoll, Christopher Mark. Casing. USP2016059357111.
  8. Wong, Frank; Rabbath, Camille Alain; Lechevin, Nicholas; Boissonneault, Olivier. Control surface actuation system. USP2012108299411.
  9. Hassan, Ahmed A.; Osborne, Bradley A.; Schwimley, Scott; Billman, Garry; Billman, legal representative, Mary. Dynamic bumps for drag reduction at transonic-supersonic speeds. USP2011098016245.
  10. Sowle, Zak; Vasudevan, Srikanth; Stucke, Russell; Lisy, Frederick J.; Schmidt, Robert N.. Flow control device and method for aircraft and missile forebody. USP2016089429400.
  11. Citro, Robert W.; O'Brien, Paul M.; Janke, Patrick J.; Quortrup, Conlee O.. Gun launched munition with strakes. USP2017099759535.
  12. Prince, Troy S; Kolacinski, Richard; Patel, Mehul. Hierarchical closed-loop flow control system for aircraft, missiles and munitions. USP2016049310166.
  13. Prince, Troy S; Kolacinski, Richard; Patel, Mehul. Hierarchical closed-loop flow control system for aircraft, missiles and munitions. USP20181110139209.
  14. Turner, Travis L.; Cano, Roberto J.; Silox, Richard J.; Buehrle, Ralph D.; Cagle, Christopher M.; Cabell, Randolph H.; Hilton, George C.. Jet engine exhaust nozzle flow effector. USP2014048683807.
  15. Low, Richard; Deeds, Michael; Jean, Daniel L.; Hovland, Christopher. MEMS control surface for projectile steering. USP2009127628352.
  16. Deeds, Michael A.; Herman, David. MEMS type flow actuated out-of-plane flap. USP2010067728265.
  17. Kestler, Steven M.; Sundar, Prithvi; Li, Yuan. Method of controlling boundary layer flow. USP2017109789954.
  18. Thomas,Steven H.. Methods and system for determining angles of attack and sideslip using flow sensors. USP2008057377159.
  19. Herman, David; Deeds, Michael. Out-of-plane deflection MEMS actuator for projectile control surfaces. USP2013038405012.
  20. Dwyer, Paul W.. Reducing bias in an accelerometer via a pole piece. USP20181210161956.
  21. Sowle, Zak; Vasudevan, Srikanth; Birch, Matthew C.. Rotational control actuation system. USP20190210203188.
  22. Neitzke, Klaus-Peter; Bauer, Karin; Bolzmacher, Christian; Kupke, Winfried. Switchable vortex generator and array formed therewith, and uses of the same. USP2017059650124.
  23. Neitzke, Klaus-Peter; Bauer, Karin; Bolzmacher, Christian; Kupke, Winfried. Switchable vortex generator and array formed therewith, and uses of the same. USP2013128616494.
  24. Boldrin, Clete M.; Hassan, Ahmed A.. Vernier active flow control effector. USP2012038128036.
  25. Boldrin,Clete M.; Hassan,Ahmed A.. Vernier active flow control effector. USP2007087255309.
  26. Hegenbart, Matthias; Eilken, Wolfgang; Paul, Erich; Stefes, Bruno; Duken, Lena. Vortex generator arrangement. USP20190210202187.
  27. McVeigh, Michael A.; Maciolek, Robert F.. Vortex generators on rotor blades to delay an onset of large oscillatory pitching moments and increase maximum lift. USP2010077748958.
  28. Gieseke, Thomas J.. Vortex-assisted pressure control at inlet of underwater launch system. USP2005086932016.