WO2003050496A3 - Sonde multifonction pour aeronef - Google Patents

Sonde multifonction pour aeronef Download PDF

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Publication number
WO2003050496A3
WO2003050496A3 PCT/FR2002/004261 FR0204261W WO03050496A3 WO 2003050496 A3 WO2003050496 A3 WO 2003050496A3 FR 0204261 W FR0204261 W FR 0204261W WO 03050496 A3 WO03050496 A3 WO 03050496A3
Authority
WO
WIPO (PCT)
Prior art keywords
aircraft
heating wire
mandrel
tube
measuring total
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/FR2002/004261
Other languages
English (en)
Other versions
WO2003050496A2 (fr
Inventor
Nicolas Hanson
Marc Simeon
Jean-Jacques Barbou
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Thales SA
Original Assignee
Thales SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Thales SA filed Critical Thales SA
Priority to US10/493,567 priority Critical patent/US7124630B2/en
Priority to EP02804605A priority patent/EP1454149A2/fr
Publication of WO2003050496A2 publication Critical patent/WO2003050496A2/fr
Publication of WO2003050496A3 publication Critical patent/WO2003050496A3/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
    • G01K13/00—Thermometers specially adapted for specific purposes
    • G01K13/02—Thermometers specially adapted for specific purposes for measuring temperature of moving fluids or granular materials capable of flow
    • G01K13/028—Thermometers specially adapted for specific purposes for measuring temperature of moving fluids or granular materials capable of flow for use in total air temperature [TAT] probes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/12—De-icing or preventing icing on exterior surfaces of aircraft by electric heating
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D43/00—Arrangements or adaptations of instruments
    • B64D43/02—Arrangements or adaptations of instruments for indicating aircraft speed or stalling conditions
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
    • G01K13/00—Thermometers specially adapted for specific purposes
    • G01K13/02—Thermometers specially adapted for specific purposes for measuring temperature of moving fluids or granular materials capable of flow
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P13/00—Indicating or recording presence, absence, or direction, of movement
    • G01P13/02—Indicating direction only, e.g. by weather vane
    • G01P13/025—Indicating direction only, e.g. by weather vane indicating air data, i.e. flight variables of an aircraft, e.g. angle of attack, side slip, shear, yaw
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P5/00—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
    • G01P5/14—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid
    • G01P5/16—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid using Pitot tubes, e.g. Machmeter
    • G01P5/165—Arrangements or constructions of Pitot tubes

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Testing Or Calibration Of Command Recording Devices (AREA)
  • Measuring Fluid Pressure (AREA)
  • Measuring Temperature Or Quantity Of Heat (AREA)
  • Measuring Volume Flow (AREA)

Abstract

L'invention se rapporte à une sonde multifonction pour aéronef. La sonde comporte des moyens pour mesurer la pression totale (Pt) et des moyens pour mesurer la température totale (Tt) d'un écoulement d'air entourant l'aéronef. Les moyens pour mesurer la pression totale (Pt) comportent un premier tube (20) dit tube de Pitot orienté sensiblement suivant l'axe (8) de l'écoulement d'air entourant l'aéronef et les moyens pour mesurer la température totale (Tt) comportent un second tube (25) ouvert sur l'écoulement d'air et orienté sensiblement dans l'axe (8) de l'écoulement d'air. Le premier tube (20) est situé à l'intérieur du second tube (25). L'invention se rapporte également à un procédé de mise en forme d'un fil chauffant (39) formant des moyens de dégivrage de la sonde multifonction. Le procédé consiste à : - enrouler en hélice le fil chauffant (39) autour d'un premier mandrin (40), - insérer le premier mandrin (40) à l'intérieur d'un second mandrin (42) creux, - poursuivre l'enroulement du fil chauffant (39) autour du second mandrin (42) - placer le fil chauffant (39), ainsi formé, à l'intérieur des deux tubes (20 et 25) et y être fixé.
PCT/FR2002/004261 2001-12-11 2002-12-10 Sonde multifonction pour aeronef Ceased WO2003050496A2 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
US10/493,567 US7124630B2 (en) 2001-12-11 2002-12-10 Multipurpose sensor for aircraft
EP02804605A EP1454149A2 (fr) 2001-12-11 2002-12-10 Sonde multifonction pour aeronef

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR01/15991 2001-12-11
FR0115991A FR2833347B1 (fr) 2001-12-11 2001-12-11 Sonde multifonction pour aeronef

Publications (2)

Publication Number Publication Date
WO2003050496A2 WO2003050496A2 (fr) 2003-06-19
WO2003050496A3 true WO2003050496A3 (fr) 2003-12-24

Family

ID=8870335

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/FR2002/004261 Ceased WO2003050496A2 (fr) 2001-12-11 2002-12-10 Sonde multifonction pour aeronef

Country Status (4)

Country Link
US (1) US7124630B2 (fr)
EP (1) EP1454149A2 (fr)
FR (1) FR2833347B1 (fr)
WO (1) WO2003050496A2 (fr)

Families Citing this family (52)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2840985B1 (fr) * 2002-06-14 2004-09-10 Thales Sa Sonde de temperature totale et procede de determination de temperature au moyen d'une telle sonde
US7014357B2 (en) 2002-11-19 2006-03-21 Rosemount Aerospace Inc. Thermal icing conditions detector
FR2859787B1 (fr) * 2003-09-16 2006-01-20 Thales Sa Dispositif et procede de determination de la temperature totale pour aeronef
FR2862383B1 (fr) * 2003-11-18 2006-02-17 Thales Sa Sonde d'incidence
US7549331B1 (en) * 2007-01-23 2009-06-23 Powell Bradley J Nose section for a pitot probe
US7828477B2 (en) * 2007-05-14 2010-11-09 Rosemount Aerospace Inc. Aspirated enhanced total air temperature probe
FR2924498B1 (fr) * 2007-11-30 2009-12-11 Thales Sa Girouette de mesure de l'orientation du vent a rechauffeur integre
US8392141B2 (en) * 2009-11-02 2013-03-05 Rosemount Aerospace Inc. Total air temperature probe and method for reducing de-icing/anti-icing heater error
US20110184701A1 (en) * 2010-01-28 2011-07-28 Analysis And Measurement Services Corporation Pitot Tube Diagnostic System
US8924184B2 (en) 2010-01-28 2014-12-30 Analysis And Measurement Services Corporation Pitot tube diagnostic systems and methods
US8060334B1 (en) 2010-09-03 2011-11-15 Philip Onni Jarvinen Aircraft pitot-static tube with ice detection
FR2978829B1 (fr) 2011-08-04 2014-03-21 Aer Velocimetre insensible aux conditions givrantes et aux fortes pluies
FR2983964B1 (fr) * 2011-12-09 2014-01-10 Thales Sa Sonde de mesure de pression totale d'un ecoulement et procede de mise en oeuvre de la sonde
GB201213576D0 (en) 2012-07-31 2012-09-12 Rolls Royce Plc Total temperature probe
US8857255B2 (en) * 2012-08-22 2014-10-14 Rosemount Aerospace Inc. Moisture resistant air data probes
CN203757114U (zh) * 2012-10-01 2014-08-06 艾默生过程管理调节技术公司 一种流体调节装置
FR3002801B1 (fr) * 2013-03-01 2015-03-20 Thales Sa Sonde de mesure de pression totale d'un ecoulement et procede de mise en oeuvre de la sonde
US9366555B2 (en) * 2013-12-18 2016-06-14 Lockheed Martin Corporation Air data system
US9429482B2 (en) 2014-02-21 2016-08-30 Rosemount Aerospace Inc. Total air temperature probe with low frontal projected area
WO2015159193A1 (fr) 2014-04-14 2015-10-22 National Research Council Of Canada Capteur d'air doté d'une entrée orientée vers l'aval afin de prévenir la condensation
US9541429B2 (en) 2014-06-02 2017-01-10 University Of Kansas Systems, methods, and devices for fluid data sensing
US10585109B2 (en) 2014-06-02 2020-03-10 University Of Kansas Systems, methods, and devices for fluid data sensing
US20160238456A1 (en) * 2015-02-12 2016-08-18 Rosemount Aerospace Inc. Air temperature sensor and fabrication
FR3034753B1 (fr) 2015-04-10 2018-03-30 Thales Rechauffage d'un equipement aeronautique
GB2541356A (en) * 2015-06-08 2017-02-22 Meggitt (Uk) Ltd Moving-vane angle of attack probe
FR3039515B1 (fr) 2015-07-28 2017-09-01 Thales Sa Rechauffage pour equipement aeronautique
FR3039509B1 (fr) 2015-07-28 2017-12-22 Thales Sa Rechauffage pour equipement aeronautique pour un aeronef
FR3039514B1 (fr) 2015-07-28 2017-09-08 Thales Sa Rechauffage pour un equipement aeronautique
FR3039508B1 (fr) * 2015-07-28 2017-09-01 Thales Sa Rechauffage pour equipement d'aeronef
FR3039512B1 (fr) 2015-07-28 2017-12-22 Thales Sa Rechauffage d'un premier equipement aeronautique d'aeronef
FR3039513B1 (fr) 2015-07-28 2017-09-01 Thales Sa Procede de fabrication additive d'un equipement aeronautique
FR3039511B1 (fr) 2015-07-28 2017-09-08 Thales Sa Rechauffage pour equipement aeronautique d'aeronef
US10160548B2 (en) * 2016-01-04 2018-12-25 The Boeing Company Apparatuses and methods for anti-icing of speed measurement probes
US10203253B2 (en) * 2016-02-10 2019-02-12 Rosemount Aerospace Inc. Total air temperature probe with efficient particle pass through
CN107543649B (zh) * 2016-06-26 2023-10-24 成都凯天电子股份有限公司 热气除冰总压受感器
US10422702B2 (en) 2017-06-08 2019-09-24 Rosemount Aerospace Inc. Total air temperature probe with reduced icing sensor flow passage geometry
US10578498B2 (en) * 2017-06-22 2020-03-03 Unison Industries, Llc Air temperature sensor
USD976139S1 (en) * 2018-06-15 2023-01-24 Rosemount Aerospace, Inc. Aircraft temperature probe
US10852203B2 (en) 2018-06-15 2020-12-01 Rosemount Aerospace Inc. Total air temperature probe with concave flow path transitions to outlet
USD976138S1 (en) * 2018-06-15 2023-01-24 Rosemount Aerospace, Inc. Aircraft temperature probe
US11262227B2 (en) 2018-10-05 2022-03-01 Rosemount Aerospace Inc. Pitot tube heater assembly
CN109708778A (zh) * 2018-12-07 2019-05-03 苏州长风航空电子有限公司 一种防冰温度传感器及其制备方法
US11237031B2 (en) 2019-08-20 2022-02-01 Rosemount Aerospace Inc. Additively manufactured heaters for air data probes having a heater layer and a dielectric layer on the air data probe body
US11237183B2 (en) * 2019-12-13 2022-02-01 Rosemount Aerospace Inc. Ceramic probe head for an air data probe with and embedded heater
US11655726B2 (en) * 2020-02-28 2023-05-23 Rosemount Aerospace Inc. Pressure and temperature sensors and related methods
US11879345B2 (en) 2020-02-28 2024-01-23 Rosemount Aerospace Inc. Pressure and temperature sensors and methods of removing ice from pressure and temperature sensors
US11773745B2 (en) 2020-02-28 2023-10-03 Rosemount Aerospace Inc. Pressure and temperature sensors and methods of controlling ice accretion on pressure and temperature sensors
US11021259B1 (en) 2021-01-07 2021-06-01 Philip Onni Jarvinen Aircraft exhaust mitigation system and process
CN114132512B (zh) * 2022-02-07 2022-04-29 中国空气动力研究与发展中心低速空气动力研究所 一种光纤结冰传感器探头及调节方法
US12409939B2 (en) * 2022-07-11 2025-09-09 Rosemount Aerospace Inc. Air data probe electronics housing with thermal isolating features
CN117906902A (zh) * 2024-03-19 2024-04-19 中国航空工业集团公司沈阳空气动力研究所 一种预加热总温探针及高温高马赫数气流总温测量方法
FR3165241A1 (fr) 2024-08-02 2026-02-06 Thales Dispositif de mesure aérodynamique

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2404978A (en) * 1944-02-10 1946-07-30 Westinghouse Electric Corp Fluid speed indicator
US2984107A (en) * 1957-09-16 1961-05-16 Us Industries Inc Pitot static tube
US5025661A (en) * 1989-12-11 1991-06-25 Allied-Signal Inc. Combination air data probe
FR2802647A1 (fr) * 1999-12-17 2001-06-22 Thomson Csf Sextant Sonde pour aeronef

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2370102A (en) * 1944-01-07 1945-02-20 Westinghouse Electric & Mfg Co Pitot-static air-speed indicator
EP0061864B1 (fr) * 1981-03-24 1986-01-29 PENNY & GILES TRANSDUCERS LIMITED Systèmes de détection de vitesse de l'air
US5616861A (en) * 1995-06-07 1997-04-01 Rosemount Aerospace Inc. Three pressure pseudo -Δ-P sensor for use with three pressure air data probe
US6070475A (en) * 1997-10-15 2000-06-06 Rosemont Aerospace Inc. Air data probe with heater means within wall
US6101429A (en) * 1998-04-07 2000-08-08 Tao Of Systems Integration, Inc. Broad-range, multi-directional aircraft airspeed measuring system
US6076963A (en) * 1998-10-20 2000-06-20 Avionics Specialties, Inc. Aircraft probe with integral air temperature sensor
FR2793022B1 (fr) * 1999-04-30 2001-07-13 Sextant Avionique Sonde multifonctions fixe pour aeronef
DE10001813C2 (de) * 2000-01-18 2003-10-30 Eads Deutschland Gmbh Meßsystem zur Ermittlung von Luftdaten eines Luftfahrzeuges sowie ein Verfahren zur Bestimmung der Luftdaten
FR2817044B1 (fr) 2000-11-17 2003-02-14 Thomson Csf Procede de determination de parametres aerodynamiques et procede de detection de panne d'une sonde utilisee pour determiner les parametres aerodynamiques

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2404978A (en) * 1944-02-10 1946-07-30 Westinghouse Electric Corp Fluid speed indicator
US2984107A (en) * 1957-09-16 1961-05-16 Us Industries Inc Pitot static tube
US5025661A (en) * 1989-12-11 1991-06-25 Allied-Signal Inc. Combination air data probe
FR2802647A1 (fr) * 1999-12-17 2001-06-22 Thomson Csf Sextant Sonde pour aeronef

Also Published As

Publication number Publication date
WO2003050496A2 (fr) 2003-06-19
US7124630B2 (en) 2006-10-24
EP1454149A2 (fr) 2004-09-08
FR2833347A1 (fr) 2003-06-13
US20040237641A1 (en) 2004-12-02
FR2833347B1 (fr) 2004-02-27

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