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특허 상세정보

Boundary layer control system for aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-021/04   
미국특허분류(USC) 244/207 ; 244/134B ; 244/214
출원번호 US-0749624 (1976-12-13)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Christensen, O'Connor, Johnson & Kindness
인용정보 피인용 횟수 : 17  인용 특허 : 0
초록

An improved boundary layer control system is particularly useful in applications where controlled air is to be injected into a boundary layer region adjacent to a surface of an aircraft wing. The controlled air is obtained from an air source having a temperature and a pressure which are substantially greater than ambient temperature and pressure, such as that obtained from a jet engine bleed air source. A number of manifolds are located in spanwise arrangement along the wing and serve to conduct the air from the source to a plurality of nozzle penums, ea...

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이 특허를 인용한 특허 피인용횟수: 17

  1. Grove,Graham Bond. Aerofoil arrangement. USP2008127461820.
  2. Paul Laugt FR. Aircraft airfoil leading edge member equipped with a de-icing device. USP2002106467730.
  3. Jeffrey W. Moe. Aircraft wing and method for reducing airframe-generated noise. USP2002096454219.
  4. Giamati, Michael J.. Aircraft wing with electrothermal deicing and/or anti-icing device. USP2009067546980.
  5. Giamati,Michael J.. Aircraft wing with electrothermal deicing and/or anti-icing device. USP2007107278610.
  6. Capuani Alfredo (Torino ITX). Aircraft with jet propulsion. USP1984104478378.
  7. Etling, Keith A.. Anti-icing apparatus for honeycomb structures. USP2011118052089.
  8. Nieman, Ronald J.; Hughes, Jason M.. Anti-icing piccolo tube standoff. USP2012018100364.
  9. Nichols, Davis B.. Detection system and method for ice and other debris. USP2010087784739.
  10. Evulet, Andrei. Fluidic propulsive system and thrust and lift generator for aerial vehicles. USP20190210207812.
  11. Williams Arthur L. (Northridge CA). Leading edge flap for an airfoil. USP1983084398688.
  12. Reckzeh, Daniel; Goelling, Burkhard; Lengers, Matthias. Surface element for an aircraft, aircraft and method for improving high-lift generation on a surface element. USP2016039272772.
  13. Slagle,Jason Corey; Ruehr,William Carl; Ashley,Jared Stephan; Hackler,James Warren; Litter,Jansen James; Li,Meiyun; Blanton,John Clisby. Temperature and/or pressure sensor assembly. USP2008027328623.
  14. Boone, Richard; Gallman, John W.. Thermal insulation barrier for an aircraft de-icing heater. USP2015048998144.
  15. Shmilovich, Arvin; Whalen, Edward Andrew. Thermally controlled active flow control system. USP20181010086927.
  16. Reckzeh, Daniel; Goelling, Burkhard; Lengers, Matthias. Wing for an aircraft, aircraft and method for reducing aerodynamic drag and improving maximum lift. USP2016039278753.
  17. Amorosi, Stephen R.; Santini, Gregory M.; Anderson, Matthew Leroy; Hinrichs, Steve C.; Jarecki, Walter J.; Bennett, Nicholas I.; Pham, Quang Minh; Lai, Paul Hungwai; Rupert, Gregory E.; Osaki, Carl F.. Wing leading edge architecture suitable for laminar flow. USP2018029896190.