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특허 상세정보

Sideslip correction for a multi-function three probe air data system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) G01W-001/00   
미국특허분류(USC) 073/170.02; 073/180; 073/170.01
출원번호 US-0850796 (2001-05-08)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Westman, Champlin & Kelly, P.A.
인용정보 피인용 횟수 : 12  인용 특허 : 14
초록

A multi-function probe system that provides redundancy for measurements and compensates for effects of sideslip of an aircraft includes at least two probes that are symmetrically located on the opposite sides of the aircraft, and a third probe mounted on the centerline of the aircraft positioned to directly measure local sideslip with ports that are positioned on opposite sides of the center plane of the aircraft. Each of the probes includes self contained instrumentation for providing signals indicating various pressures. The local angle of sideslip sen...

대표
청구항

A multi-function probe system that provides redundancy for measurements and compensates for effects of sideslip of an aircraft includes at least two probes that are symmetrically located on the opposite sides of the aircraft, and a third probe mounted on the centerline of the aircraft positioned to directly measure local sideslip with ports that are positioned on opposite sides of the center plane of the aircraft. Each of the probes includes self contained instrumentation for providing signals indicating various pressures. The local angle of sideslip sen...

이 특허에 인용된 특허 (14)

  1. Muehlhauser Brett A. ; Ranum Brian. Air data probe with heater means within wall. USP2000066070475.
  2. Wandel Hermann,DEX ; Jost Michael,DEX ; Sommer Helmut,DEX ; Fischer-Wilk Robert,DEX. Aircraft pitot and static pressure sensing device and aircraft having the sensing device. USP2000036038932.
  3. Townsend Ray T. (Des Moines IA) Vandewege Orville (Tempe AZ). Airplane angle of attack and direction of flight indicator. USP1980104230290.
  4. Hagen Floyd W. (Eden Prairie MN). Angle of attack sensor using inverted ratio of pressure differentials. USP1993045205169.
  5. Renshaw Kevin J.. Apparatus and method for measuring the side slip of a low observable aircraft. USP1998125852237.
  6. Halliday David P. (Preston GB2) Riley John F. (Preston GB2) Sharrock Barry (Preston GB2). Arrangements for mounting a probe on an aircraft. USP1984014428549.
  7. Baltins Guntis U. (Charlottesville VA) Boyle Russell W. (Earlysville VA) Mason Denis G. (Charlottesville VA) Moore Howard M. (Stanardsville VA) Owen A. DeBow (Charlottesville VA) Sharp Joseph A. (Sta. Combined aircraft angle of attack and dynamic/static pressure sensor assembly. USP1996085544526.
  8. Hagen Floyd W. (Eden Prairie MN). Deployable probe combined with flush static port. USP1995085442958.
  9. Eckert Alfred,DEX. Method for determining an additional yawing moment based on side slip angle velocity. USP1998015710705.
  10. Hagen Floyd W. (Eden Prairie MN) Hohenstein Gregg A. (Bloomington MN) Severson John A. (Eagan MN) Trongard Pennelle J. (Savage MN). Multifunctional air data sensing probes. USP1997055628565.
  11. Whitmore Stephen A. ; Cobleigh Brent R. ; Haering ; Jr. Edward A.. Stable algorithm for estimating airdata from flush surface pressure measurements. USP2001066253166.
  12. Panxika Larramendy FR. System for the yaw control of an aircraft. USP2002036352223.
  13. Hagen Floyd W. (Eden Prairie MN). Three pressure pseudo -D
  14. Ito Ken (Yokohama JPX). Vehicle control system for controlling side slip angle and yaw rate gain. USP1988084767588.

이 특허를 인용한 특허 피인용횟수: 12

  1. Foster, Roger D.; Heine, Paul F.; Moynihan, Patrick J.; Owens, David G.. Aerodynamically shaped static pressure sensing probe. USP2005076915687.
  2. Harris, Christopher A.; Li, Yuan; Westphal, Russell V.; Lawrence, Kris I.; Oo, Htet Htet; Gerhardt, James A.; Cuppoletti, Daniel R.. Directional dynamic absolute pressure sensor shroud and arrangement. USP2018019869570.
  3. Hongerholt,Derrick David; Cronin,Dennis James. Fault isolation method and apparatus in artificial intelligence based air data systems. USP2007087257470.
  4. Toulmay,François. Method and a device for measuring the speed of an aircraft, in particular a rotorcraft at low speed. USP2008127461548.
  5. Schauer,Travis Jon; Hongerholt,Derrick David; Cronin,Dennis James. Method and apparatus for obtaining improved accuracy and range for air data parameters inferred from independent measurements of interdependent pressures. USP2007057213454.
  6. Fontova, Laurent; Freissinet, Sebastien. Method and device for detecting, on the ground, the obstruction of a pressure tap of a static pressure sensor of an aircraft. USP2010037675434.
  7. Choisnet,Joel; Collot,Lionel; Hanson,Nicolas. Method for determining aerodynamic parameters and method for detecting failure of a probe used for determining aerodynamic parameters. USP2006057051586.
  8. Thomas,Steven H.. Methods and system for determining angles of attack and sideslip using flow sensors. USP2008057377159.
  9. Cronin,Dennis J.; Drutowski,Karl G.; Mack,Andrew P.. Multi-function air data probes employing neural networks for determining local air data parameters. USP2008057379839.
  10. Seidel, Greg A.; Cronin, Dennis J.; Mette, John H.; Koosmann, Mark R.; Schmitz, James A.; Fedele, John R.; Kromer, Dana A.. Multi-function air data sensing probe having an angle of attack vane. USP2005096941805.
  11. Collot,Lionel; Hanson,Nicolas. Multifunction probe with variable flexure. USP2007017155968.
  12. Liu, Lin; Lee, Chien-Hsin. Wireless mouse and wireless input device. USP2015028963839.