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특허 상세정보

Method and apparatus for flight parameter monitoring and control

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) G06F-007/70    G06F-007/76   
미국특허분류(USC) 701/014 ; 701/003 ; 701/004 ; 701/010 ; 701/015 ; 701/007 ; 244/158R ; 244/203 ; 340/959 ; 731/78T
출원번호 US-0076376 (1998-05-12)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Wallenstein & Wagner, Ltd.
인용정보 피인용 횟수 : 41  인용 특허 : 45
초록

Methods and apparatus are disclosed for three-dimensional flight control based generally upon measuring and comparing actual air pressures at or near various surfaces of an aircraft during flight. Sensors are provided for measuring air pressure acting on an aircraft surface. The methods and apparatus include those for measuring air pressure differentials between two or more sensors to evaluate certain critical flight parameters, such as the actual lift being produced, the air direction and speed relative to the aircraft, the air density, and the aircraft...

대표
청구항

[ I claim:] [1.]1. Apparatus for measuring air pressure acting on a surface of an aircraft during operation comprising:a port in a skin of the aircraft;a cover positioned over the port, the cover having a plurality of small openings, the openings each sized large enough to permit air flow but small enough to deter water and Type II fluids from passing through the openings;a sensing means for sensing a pressure and providing a signal related to the pressure;a port connecting means for connecting the port to the means for sensing so that an air pressure ac...

이 특허에 인용된 특허 (45)

  1. Tulinius Jan (Huntington Beach CA). Active flexible wing aircraft control system. USP1992015082207.
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이 특허를 인용한 특허 피인용횟수: 41

  1. Ian Amos CA. Apparatus to calculate dynamic values for pressure density in an aircraft. USP2002096449573.
  2. Schoess, Jeffrey N.; Simons, Mark D.. Conformal fluid data sensor. USP2003126662647.
  3. Ryutaro Yoshino JP. Drag control system for flying machine, process for estimating drag of flying machine, boundary layer control system, and boundary layer control process. USP2002056390417.
  4. Malta, Dan. Dynamic limitation of monoblock flight control surfaces inclinations during stall susceptibility conditions. USP2015028958930.
  5. Tanielian, Minas H; Greegor, Robert B.; Fahley, Stephen L.. Environmental sensor system. USP2012028115646.
  6. Artini,Franck; Demortier,Jean Pierre; Bouchet,Christophe. Flight control indicator determining the maximum slope for the flight control of an aircraft by terrain following. USP2006087089090.
  7. Gölling, Burkhard. High lift system for an aircraft. USP2015079090340.
  8. Gölling, Burkhard; Lorkowski, Thomas. High lift system for an aircraft. USP2015069045224.
  9. Gölling, Burkhard. High-lift system for an aircraft. USP2014048690107.
  10. Goto, Kenichi. Ice protection system for aircraft. USP2012088251313.
  11. Conners, Timothy R.; Henne, Preston A.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2016119482155.
  12. Conners, Timothy R.; Howe, Donald C.; Henne, Preston A.. Isentropic compression inlet for supersonic aircraft. USP2012128333076.
  13. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012128327645.
  14. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012108286434.
  15. Meis, Charles Steven. Laser-based supercooled large drop icing condition detection system. USP2015049013332.
  16. Conners, Timothy R.. Low shock strength inlet. USP2013038393158.
  17. Conners, Timothy R.. Low shock strength inlet. USP2015059027583.
  18. Conners, Timothy R.. Low shock strength propulsion system. USP2014068739514.
  19. Conners, Timothy R.. Low shock strength propulsion system. USP2014078783039.
  20. Baillon, Bertrand; Klotz, Julien; Mutuel, Laurence. Method and device for protecting an aircraft. USP2015028965603.
  21. Velázquez López, Angel Gerardo; Alonso Fernández, Diego; Vega de Prada, José Manuel; Lorente Manzanares, Luis Santiago; De Pablo Fouce, Valentin. Method and system for a quick calculation of aerodynamic forces on an aircraft in transonic conditions. USP2014038666715.
  22. Mangalam, Siva M.. Method and system for locating critical flow feature indicators in three dimensional flow regimes. USP2005116963810.
  23. Dellac, Stephane; Jacquet, Arnaud; Esteban, Antoine. Method of managing the braking of an aircraft by predicting its movements on an airport. USP2011077987036.
  24. Artini,Franck; Strongman,Edward. Method to determine and guide aircraft approach trajectory. USP2008027330781.
  25. Papadopoulos, George. Optical coupled sensors for harsh environments. USP2016079391216.
  26. Mayda, Edward A.. Pressure based load measurement. USP2012038137066.
  27. Henze, Chad M.. Propeller deicing system. USP2017059656757.
  28. Kominsky, Daniel. Rotating stall detection using optical measurement of blade untwist. USP2014108854626.
  29. Andrews, Jr.,George A.. Sampling system for moving fluid. USP2006097111521.
  30. Rouse, Gordon F.; Dupuis, Paul B.. Sensor for measuring wind angle. USP2004086772976.
  31. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Supersonic aircraft jet engine installation. USP2016059334801.
  32. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2004036698684.
  33. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2014078789789.
  34. Mangalam,Siva M.. System and method for closed loop control of boundary layer shear stress. USP2007127302838.
  35. Mangalam, Arun S.; Mangalam, Siva M.. System and method for control of aeroelasticity effects. USP2012048155794.
  36. Mangalam, Siva M.. System and method for real time determination of unsteady aerodynamic loads. USP2004116826493.
  37. Feau, Julien. System for selecting data representing an air parameter, process and computer program relating to the same. USP2012048150566.
  38. Elgersma, Michael Ray. Systems and methods for determining air data parameters. USP2012018104339.
  39. Milgram,Judah H.. Tactile side-slip corrective yaw control for aircraft. USP200712H002206.
  40. Dawson, Mark H.; Wallace, Jack. Variable length wind turbine blade having transition area elements. USP2012068206107.
  41. Walton, Vincent M.; Borland, Christopher J.; Siu, Tze L.; Najmabadi, Kioumars; Coleman, Edward E.; Marquis, David P.; McMullin, Dianne L.; Milligan, Kevin H.. Vertical gust suppression system for transport aircraft. USP2014078774987.