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특허 상세정보

Apparatus for influencing a boundary layer on the surface of a body moving through a medium

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-023/06   
미국특허분류(USC) 244/130 ; 244/53B ; 244/199
출원번호 US-0058511 (1987-06-05)
우선권정보 DE-3521329 (1985-06-14)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 33  인용 특허 : 3
초록

The pressure drag on the skin of an aircraft is reduced by rigidly securing boundary layer influencing members to the skin of the aircraft, including the wings, the elevantor and fin/rudder assemblies, and the body near the tail end. These members may be vortex generators and boundary layer diverters and are always located in the attached flow. In addition, if the members are placed upstream of any air intakes, especially flush air intakes, the air intake efficiency is also improved. The influencing members have an effective height above the surface corr...

대표
청구항

An apparatus for influencing a boundary layer o nan aircraft surface including wing surfaces, elevator surfaces, fin/rudder surfaces, and body surfaces, comprising boundary layer influencing means rigidly secured to said wing surfaces approximately along the entire wing span in a fully attached boundary layer flow downstream of the largest wing thickness as viewed in the air flow direction but upstream of any boundary layer separation point, said boundary layer influencing means being also secured to said elevator surfaces in a fully attached boundary la...

이 특허를 인용한 특허 피인용횟수: 33

  1. Gemma, Riccardo. Air intake, in particular for an aircraft chaff dispenser. USP2013078485467.
  2. Mark D. Ralston. Aircraft auxiliary air intake with ram and flush opening door. USP2002026349899.
  3. Uluc, Ozan; Kiryaman, Ahmet Kayihan; Frey, Andreas. Aircraft electronics cooling apparatus for an aircraft having a liquid cooling system. USP2012118315053.
  4. Nowak Dieter K.. Aircraft wing flaps. USP1998065772155.
  5. Powell, Arthur G.; Vijgen, Paul M.. Apparatus and method for passive purging of micro-perforated aerodynamic surfaces. USP2012038128037.
  6. Rupp, Peter L.; Parikh, Pradip G.; Ng, Lian L.; Vijgen, Paul M.. Apparatus and methods for extending hybrid laminar flow control. USP2016119487288.
  7. Kreuzer, Peter; Schaber, Sven; Goldhahn, Iris. Arrangement of aerodynamic auxiliary surfaces for an aircraft. USP2015059038950.
  8. Parikh, Pradip G.. Combined cabin air and heat exchanger RAM air inlets for aircraft environmental control systems, and associated methods of use. USP2010127849702.
  9. Michael Campbell. Controllable vortex generator. USP2002086427948.
  10. Burghardt, Sascha; Guemmer, Volker. Device for the extraction of bleed air and aircraft engine with at least one device for the extraction of bleed air. USP20181010113485.
  11. Sakurai, Seiya; Fevergeon, Matthew D.. Door assembly for laminar flow control system. USP2012088245976.
  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. Isotani, Kazuhide; Hayama, Kenji. High-lift device of air vehicle. USP2017079714079.
  15. Isotani, Kazuhide; Hayama, Kenji. High-lift device of air vehicle. USP2017109789955.
  16. Daggett, David Lee; Utendorf, Randy; Lawson, Irwin. Low drag skin heat exchanger. USP20180810059435.
  17. Smith David R. (West Haven CT) Amelio Armand F. (New Milford CT). Low observable engine air inlet system. USP1997125697394.
  18. Dixon, Charles J.; Hughes, Arthur C.. Method and apparatus for inducing controlled vortices to reduce afterbody drag. USP2004046715717.
  19. Gleine Wolfgang,DEX ; Hilbig Reinhard,DEX ; Wendt Hans-Joachim,DEX. Method and apparatus for optimizing the aerodynamic effect of an airfoil. USP1999035875998.
  20. Schroeder Del C. ; Argeropoulos John G. ; Gleason Mark E. ; Zabat Mike ; Forster Rolls F. ; Doolittle ; III William W.. Method and apparatus for reducing lift and drag of a soft top passenger vehicle. USP1999085941595.
  21. Keefe Laurence R.. Method and apparatus for reducing the drag of flows over surfaces. USP1998095803409.
  22. Huenecke, Klaus. Method and apparatus for reducing trailing vortices in the wake of an aircraft. USP2003026513761.
  23. Sakurai, Seiya; Fevergeon, Matthew D.. Method of laminar flow control using a door assembly. USP2013078484894.
  24. Dyer, Richard S.; Kaemming, Thomas A.; Horne, III, Samuel E.. Multi-path inlet for aircraft engine. USP2012078210474.
  25. Ingo Borchers DE; Roger Drobietz DE; Michael Gruenewald DE; Knut Mau DE; Johann Reichenberger DE. Noise reducing vortex generators on aircraft wing control surfaces. USP2002126491260.
  26. Schmid, Martin; Bartels, Christian; Klimpel, Frank; Vehlhaber, Klaus. Ram air channel assembly and method for operating a ram air channel assembly. USP20190210196148.
  27. Schmid, Martin; Bartels, Christian; Klimpel, Frank; Vehlhaber, Klaus. Ram air channel assembly and method for operating a ram air channel assembly. USP20180710035601.
  28. Parikh, Pradip G.; Hastings, E. Dale. Ram air inlets for use with aircraft environmental control systems and other aircraft and non-aircraft systems. USP2009117618006.
  29. Gionta, Matthew; Karkow, Jon; Roncz, John; Koehler, Dieter; Lednicer, David. Spin resistant aircraft configuration. USP2018039926071.
  30. Gionta, Matthew; Karkow, Jon; Roncz, John; Koehler, Dieter; Lednicer, David. Spin resistant aircraft configuration. USP2016059327828.
  31. Farokhi Saeed (Lawrence KS) Taghavi Ray R. (Lawrence KS). Supersonic vortex generator. USP1997025598990.
  32. Parikh, Pradip G; Atkey, Warren A. Tandem air inlet apparatus and method for an airborne mobile platform. USP2009127624944.
  33. Da Silva, Luis Fernando Figueira; Ferreira, Sandro Barros; Perez, Cesar Celis; Oliveira, Guilherme Lara; De Jesus, Antonio Batista. Vortex generators to improve performance of flush air inlets. USP2013108544799.