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Banked flight stall warning device and method

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • G08B-023/00
출원번호 US-0208828 (1998-12-09)
발명자 / 주소
  • Martin Mack L.
  • Baciak Mark G.
  • Seiler Louis W.
출원인 / 주소
  • Exigent International, Inc.
대리인 / 주소
    Senterfitt
인용정보 피인용 횟수 : 15  인용 특허 : 23

초록

A flight warning system comprises an outside temperature probe for sensing outside temperature, a gyroscope for sensing aircraft bank angle, a static transducer for sensing static pressure, and a dynamic pressure sensor for receiving total pressure from a pitot tube. A computer is responsive to the

대표청구항

[ What is claimed is:] [17.] A flight warning system for an aircraft, comprising:an outside temperature probe for sensing outside temperature;a gyroscope for sensing aircraft bank angle;a static transducer for sensing static pressure; anda dynamic pressure sensor for receiving total pressure from a

이 특허에 인용된 특허 (23)

  1. Stanis John W. (3020 NE. 13th Ave. Pompano Beach FL 33069), Aircraft banking angle indicator.
  2. Miller Harry (Scottsdale AZ) Narveson Parm L. (Phoenix AZ) Hancock William R. (Phoenix AZ) Hsu Joseph P. (Phoenix AZ), Aircraft flight instrument display system.
  3. Bice Gregory W. (Lancaster CA) Skoog Mark A. (Lancaster CA) Howard John D. (Ft. Lauderdale FL), Aircraft ground collision avoidance and autorecovery systems device.
  4. Najmabadi Kioumars ; Evans Monte R. ; Coleman Edward E. ; Bleeg Robert J. ; Breuhaus Richard S. ; Anderson Dorr Marshall ; Nelson Timothy A., Aircraft pitch-axis stability and command augmentation.
  5. Martorella Romeo P. (Dix Hills NY), Aircraft precision approach control system.
  6. Catlin Paul A. (Lowell MI) Ballard Douglas C. (Wayland MI) Watson Gary S. (Ada MI) Worden Alfred M. (Brecksville OH), Aircraft stall warning system.
  7. Clews ; David George ; Sweeting ; David, Airplane instrument with throttle control selectively regulated by air speed or lift.
  8. Orgun Munir (Woodinville WA) Nguyen Dung D. (Edmonds WA), Apparatus and methods for controlling commanded operation of an aircraft within a predetermined flight parameter limit.
  9. Palmer Steven D., Apparatus for measuring lift forces based upon differential pressure between surfaces of an aircraft.
  10. Bateman Charles D. (Bellevue WA), Independent low airspeed alert.
  11. Daly Francis W. ; Kuntman Daryal ; Doerenberg Frank ; McElroy James J., Integrated hazard avoidance system.
  12. Thor Wayne (New Carlisle OH), Low altitude warning system for aircraft.
  13. Smith Joseph A. (Phoenix AZ) Ringnes Erik A. (Glendale AZ) Tarbutton Victor F. (Glendale AZ), Method of airplane performance estimation and prediction.
  14. Maris John M. (E.R.A.U. Box 2188 ; Daytona Beach ; Regional Airport Daytona Beach FL 32014), Method of predicting the approaching stall of an aircraft wing.
  15. Maris John M. (Port Orange FL), Method of predicting the approaching stall of an aircraft wing.
  16. Tuck Edward F. (2412 E. Crescent View Dr. West Covina CA 91790), Methods and apparatus for augmenting satellite broadcast system.
  17. Jones Jerry (202 Albion Ct. Novato CA 94947), Motorcycle headlight aiming device.
  18. De Leo ; Richard V. ; Hagen ; Floyd W., Pressure sensor for determining airspeed, altitude and angle of attack.
  19. Gilson ; Richard D., Semi-automatic aircraft control system.
  20. Wachsmuth Robert H. (Elkins Park PA) Brusch Donald W. (Newtown PA), Spatial disorientation trainer-flight simulator.
  21. Brown Jerry A. (Hazelwood MO), Stall avoidance system for aircraft.
  22. Palmer Steven D. (Burlington IA), System for onboard lift analysis and apparatus therefor.
  23. Vavra George S. (12420 Saddlehorn Trail Scottsdale AZ 85259), Tactile signaling systems for aircraft.

이 특허를 인용한 특허 (15)

  1. Godard, Eric; Chabe, David; Espinasse, Jacques, Display system for an aircraft.
  2. Malta, Dan, Dynamic limitation of monoblock flight control surfaces inclinations during stall susceptibility conditions.
  3. Duerksen, Noel J.; Johnson, John C.; Williams, Justin S., Envelope protection for mechanically-controlled aircraft.
  4. Noice, Lenard E., Head-up display (HUD) stall recovery symbology.
  5. Conner, Kevin J, Low precision temperature sensor for aircraft applications.
  6. Mangalam, Siva M., Method and system for locating critical flow feature indicators in three dimensional flow regimes.
  7. Godard,Eric; Chabe,David; Espinasse,Jacques, Method for displaying flight information.
  8. Godard, Eric; Chabe, David; Espinasse, Jacques, Process and device for aiding the piloting of an aircraft.
  9. Nestico, Brian Francis; Kestner, Brian K.; Miller, Brandon Wayne, Secondary airflow passage for adjusting airflow distortion in gas turbine engine.
  10. Mangalam,Siva M., System and method for closed loop control of boundary layer shear stress.
  11. Mangalam, Arun S.; Mangalam, Siva M., System and method for control of aeroelasticity effects.
  12. Schmidt, R. Kyle, System and method for determining aircraft hard landing events from inertial and aircraft reference frame data.
  13. Schmidt, R. Kyle, System and method for determining aircraft hard landing events from inertial and aircraft reference frame data.
  14. Johnson, Steve; Ishihara, Yasuo; Bateman, Charles Donald, System and method for improved low airspeed warning.
  15. Mangalam, Siva M., System and method for real time determination of unsteady aerodynamic loads.
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