DE602005021264D1 - Verfahren und Vorrichtung zur Überprüfung eines Temperaturwerts bei einer Zielhöhe eines Flugzeugs - Google Patents

Verfahren und Vorrichtung zur Überprüfung eines Temperaturwerts bei einer Zielhöhe eines Flugzeugs

Info

Publication number
DE602005021264D1
DE602005021264D1 DE602005021264T DE602005021264T DE602005021264D1 DE 602005021264 D1 DE602005021264 D1 DE 602005021264D1 DE 602005021264 T DE602005021264 T DE 602005021264T DE 602005021264 T DE602005021264 T DE 602005021264T DE 602005021264 D1 DE602005021264 D1 DE 602005021264D1
Authority
DE
Germany
Prior art keywords
aircraft
temperature
temperature value
checking
value
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.)
Active
Application number
DE602005021264T
Other languages
English (en)
Inventor
Patrice Rouquette
Vincent Markiton
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.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
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 Airbus Operations SAS filed Critical Airbus Operations SAS
Publication of DE602005021264D1 publication Critical patent/DE602005021264D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C23/00—Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
    • G01K1/00—Details of thermometers not specially adapted for particular types of thermometer
    • G01K1/02—Means for indicating or recording specially adapted for thermometers
    • G01K1/04—Scales
    • 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
    • G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
    • G01K7/00—Measuring temperature based on the use of electric or magnetic elements directly sensitive to heat ; Power supply therefor, e.g. using thermoelectric elements
    • G01K7/42—Circuits effecting compensation of thermal inertia; Circuits for predicting the stationary value of a temperature
DE602005021264T 2004-02-05 2005-01-10 Verfahren und Vorrichtung zur Überprüfung eines Temperaturwerts bei einer Zielhöhe eines Flugzeugs Active DE602005021264D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0401102A FR2866109B1 (fr) 2004-02-05 2004-02-05 Procede et dispositif de verification d'une valeur de temperature a une altitude de destination d'un aeronef.

Publications (1)

Publication Number Publication Date
DE602005021264D1 true DE602005021264D1 (de) 2010-07-01

Family

ID=34673898

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005021264T Active DE602005021264D1 (de) 2004-02-05 2005-01-10 Verfahren und Vorrichtung zur Überprüfung eines Temperaturwerts bei einer Zielhöhe eines Flugzeugs

Country Status (6)

Country Link
US (1) US7334939B2 (de)
EP (1) EP1562023B1 (de)
AT (1) ATE468525T1 (de)
CA (1) CA2493012C (de)
DE (1) DE602005021264D1 (de)
FR (1) FR2866109B1 (de)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2533584A (en) * 2014-12-22 2016-06-29 Airbus Operations Ltd Aircraft fuel tank inerting arrangement, method of inerting one or more aircraft fuel tanks, aircraft and software product
JP6373238B2 (ja) * 2015-08-21 2018-08-15 双葉電子工業株式会社 検出装置、飛行体、操縦装置、気流検出方法
CN112504320B (zh) * 2017-08-01 2022-11-08 广州极飞科技股份有限公司 数据有效性检测的方法及装置

Family Cites Families (45)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2394563A (en) * 1943-05-11 1946-02-12 George H Purcell Altitude correction computer
US2640550A (en) * 1948-07-24 1953-06-02 Curtiss Wright Corp Turbine propeller control system
US3264876A (en) * 1955-11-29 1966-08-09 M Ten Bosch Inc Altitude and vertical velocity meter
US3005607A (en) * 1957-02-18 1961-10-24 Gruen Applied Science Lab Inc Apparatus for cooling of supersonic aircraft
US3212332A (en) * 1963-03-18 1965-10-19 Mike J Pappas Thermometer-altitude unit and method
US3517900A (en) * 1968-06-11 1970-06-30 Philip A Roussel Process and apparatus for detecting ice formation
US3616691A (en) * 1969-03-26 1971-11-02 Bendix Corp Mission capability indicating system
US4212064A (en) * 1977-04-05 1980-07-08 Simmonds Precision Products, Inc. Performance advisory system
US4152938A (en) * 1978-05-19 1979-05-08 Karl Danninger Aircraft temperature probe
US4263804A (en) * 1979-09-10 1981-04-28 Seemann Robert A Apparatus for directly measuring density altitude in an aircraft
US4319487A (en) * 1980-01-25 1982-03-16 Dale J. Thompson Baro data indicator
US4318076A (en) * 1980-08-05 1982-03-02 Dais Corporation Dynamic climatic condition indicating system
US4780838A (en) * 1985-01-03 1988-10-25 The Boeing Company Helicopter weight and torque advisory system
GB2169572B (en) * 1985-01-03 1988-02-10 Boeing Co A helicopter weight and torque advisory system
US5398547A (en) * 1989-01-10 1995-03-21 Innovative Dynamics, Inc. Apparatus for measuring ice distribution profiles
US5070458A (en) * 1989-03-31 1991-12-03 Honeywell Inc. Method of analyzing and predicting both airplane and engine performance characteristics
FR2645828B1 (fr) * 1989-04-17 1991-06-21 Servanty Pierre Rotor apte a developper dans un fluide des efforts sustentateurs et/ou propulsifs, procede de pilotage et aeronef equipe d'un tel rotor
US5001638A (en) * 1989-04-18 1991-03-19 The Boeing Company Integrated aircraft air data system
US5020747A (en) * 1990-01-26 1991-06-04 The Boeing Company Method and apparatus for controlling flare engagement height in automatic landing systems
US5796612A (en) * 1992-11-18 1998-08-18 Aers/Midwest, Inc. Method for flight parameter monitoring and control
US5416728A (en) * 1993-06-01 1995-05-16 Chrysler Corporation System and method for determining ambient temperature outside of a vehicle
JPH08511872A (ja) * 1993-06-22 1996-12-10 ハネウエル・インコーポレーテッド 二重整合電流シンク全温度回路
US5610845A (en) * 1994-08-30 1997-03-11 United Technologies Corporation Multi-parameter air data sensing technique
US5653538A (en) * 1995-06-07 1997-08-05 Rosemount Aerospace Inc. Total temperature probe
US5913158A (en) * 1997-01-17 1999-06-15 Sullivan; William B. Dynamic temperature measurement
US6216064B1 (en) * 1998-02-24 2001-04-10 Alliedsignal Inc. Method and apparatus for determining altitude
US6250149B1 (en) * 1999-04-08 2001-06-26 The Boeing Company System and method for generating aircraft flight data using a flush-mounted air data system
US6209821B1 (en) * 1999-09-14 2001-04-03 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Apparatus and method for measuring air temperature ahead of an aircraft for controlling a variable inlet/engine assembly
US6370450B1 (en) * 1999-12-10 2002-04-09 Rosemount Aerospace Inc. Integrated total temperature probe system
US6263263B1 (en) * 2000-01-12 2001-07-17 Honeywell International Inc. Altitude correction for aircraft under non-ISA temperature conditions
JP2001215162A (ja) * 2000-01-31 2001-08-10 Seiko Instruments Inc 携帯型測定器および表示方法
US6266583B1 (en) * 2000-03-30 2001-07-24 Litton Systems, Inc. System and method for improving the accuracy of pressure altitude determinations in an inertial navigation system
JP3749135B2 (ja) * 2001-03-13 2006-02-22 横河電子機器株式会社 温度測定装置
US6622556B1 (en) * 2001-04-16 2003-09-23 Spectrasensors, Inc. Total temperature probe with complimentary sensor cavity
JP3810669B2 (ja) * 2001-11-19 2006-08-16 セイコーインスツル株式会社 移動検出型高度計
US6778884B2 (en) * 2002-06-11 2004-08-17 Honeywell International, Inc. System and method for generating consolidated gas turbine control tables
US7014357B2 (en) * 2002-11-19 2006-03-21 Rosemount Aerospace Inc. Thermal icing conditions detector
US6809648B1 (en) * 2002-11-26 2004-10-26 University Corporation For Atmospheric Research Aerial sampler system
ES2280940T3 (es) * 2003-02-06 2007-09-16 Flytec Ag Altimetro con correccion de temperatura.
US6864830B1 (en) * 2003-03-03 2005-03-08 Garmin Ltd. Device and method for alert and density altitude features in a transponder
DE10329252A1 (de) * 2003-06-25 2005-01-13 Rolls-Royce Deutschland Ltd & Co Kg Regelsystem für ein Flugtriebwerk
FR2857754B1 (fr) * 2003-07-18 2005-09-23 Airbus France Procede et dispositif de surveillance de la validite d'une information de vitesse d'un aeronef et systeme de generation d'une information de vitesse comportant un tel dispositif
US6837225B1 (en) * 2003-07-29 2005-01-04 Toyota Jidosha Kabushiki Kaisha Fuel supply control device for a turbo-charged diesel aircraft engine
US7031871B2 (en) * 2004-06-04 2006-04-18 Rosemount Aerospace, Inc. Sensor assembly for determining total temperature, static temperature and Mach number
FR2872327B1 (fr) * 2004-06-28 2006-10-06 Avions De Transp Regional Grou Procede et dispositif de detection de degradation de performances d'un aeronef

Also Published As

Publication number Publication date
US7334939B2 (en) 2008-02-26
CA2493012A1 (fr) 2005-08-05
EP1562023B1 (de) 2010-05-19
FR2866109B1 (fr) 2006-04-07
ATE468525T1 (de) 2010-06-15
US20060056482A1 (en) 2006-03-16
EP1562023A1 (de) 2005-08-10
CA2493012C (fr) 2013-04-23
FR2866109A1 (fr) 2005-08-12

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