JP4361329B2 - デュアルチャネル電子マルチファンクションプローブおよび異なりかつ独立したエアデータ出力を実現する方法 - Google Patents

デュアルチャネル電子マルチファンクションプローブおよび異なりかつ独立したエアデータ出力を実現する方法 Download PDF

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JP4361329B2
JP4361329B2 JP2003292255A JP2003292255A JP4361329B2 JP 4361329 B2 JP4361329 B2 JP 4361329B2 JP 2003292255 A JP2003292255 A JP 2003292255A JP 2003292255 A JP2003292255 A JP 2003292255A JP 4361329 B2 JP4361329 B2 JP 4361329B2
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aircraft
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JP2004075060A5 (https=
JP2004075060A (ja
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フロイド アルウィン スティーブ
ジェイムス クローニン デニス
チャールズ スカローリド マーク
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ローズマウント エアロスペース インコーポレイテッド
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    • 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
    • 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
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B9/00—Safety arrangements
    • G05B9/02—Safety arrangements electric
    • G05B9/03—Safety arrangements electric with multiple-channel loop, i.e. redundant control systems
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0077—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements using redundant signals or controls

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Measuring Fluid Pressure (AREA)
JP2003292255A 2002-08-12 2003-08-12 デュアルチャネル電子マルチファンクションプローブおよび異なりかつ独立したエアデータ出力を実現する方法 Expired - Lifetime JP4361329B2 (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/217,060 US6668640B1 (en) 2002-08-12 2002-08-12 Dual-channel electronic multi-function probes and methods for realizing dissimilar and independent air data outputs

Publications (3)

Publication Number Publication Date
JP2004075060A JP2004075060A (ja) 2004-03-11
JP2004075060A5 JP2004075060A5 (https=) 2006-07-06
JP4361329B2 true JP4361329B2 (ja) 2009-11-11

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JP2003292255A Expired - Lifetime JP4361329B2 (ja) 2002-08-12 2003-08-12 デュアルチャネル電子マルチファンクションプローブおよび異なりかつ独立したエアデータ出力を実現する方法

Country Status (3)

Country Link
US (1) US6668640B1 (https=)
EP (1) EP1391736B1 (https=)
JP (1) JP4361329B2 (https=)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20200053857A (ko) * 2018-11-09 2020-05-19 (주) 에어로매스터 항공기의 통합 대기 자료 시스템

Families Citing this family (39)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2833709B1 (fr) * 2001-12-14 2004-04-02 Thales Sa Sonde multifonction a fleche variable
US7379839B2 (en) * 2002-12-23 2008-05-27 Rosemount Aerospace, Inc. Multi-function air data probes employing neural networks for determining local air data parameters
US7257470B2 (en) * 2004-10-29 2007-08-14 Rosemount Aerospace Inc. Fault isolation method and apparatus in artificial intelligence based air data systems
FR2882141B1 (fr) * 2005-02-14 2007-05-04 Airbus France Sas Procede et dispositif pour detecter au sol l'obstruction d'une prise de pression d'un capteur de pression statique d'un aeronef
US7178394B2 (en) * 2005-02-17 2007-02-20 The Boeing Company Pressure testing assemblies for use in flow bodies and methods of testing flow bodies
US20060212181A1 (en) * 2005-03-16 2006-09-21 Rosemount Aerospace Inc. Method and apparatus for extending useful range of air data parameter calculation in flush air data systems
US7213454B2 (en) * 2005-04-06 2007-05-08 Rosemount Aerospace Inc. Method and apparatus for obtaining improved accuracy and range for air data parameters inferred from independent measurements of interdependent pressures
FR2891368B1 (fr) * 2005-09-27 2007-11-30 Airbus France Sas Systeme de surveillance de parametres anemobaroclinometriques pour aeronefs
US20070130096A1 (en) * 2005-12-01 2007-06-07 Rosemount Aerospace, Inc. Fault detection in artificial intelligence based air data systems
US7658100B2 (en) * 2006-03-16 2010-02-09 Roy Geoffrey Werbin Device and method for measuring air movement
US8182143B2 (en) * 2006-08-09 2012-05-22 Spectrasensors, Inc. Mobile temperature sensor
FR2905006B1 (fr) * 2006-08-21 2008-10-17 Airbus France Sas Procede de surveillance de l'integrite d'une position avion calculee a bord
FR2908882B1 (fr) * 2006-11-17 2008-12-26 Thales Sa Dispositif de mesure de la pression totale d'un ecoulement et procede mettant en oeuvre le dispositif
US8620495B2 (en) * 2006-12-19 2013-12-31 Rosemount Aerospace Inc. Air data stall protection system
ES2374996T3 (es) * 2006-12-19 2012-02-23 Rosemount Aerospace Inc. Sonda de temperatura total del aire y electrónica integradas.
US7597018B2 (en) 2007-04-11 2009-10-06 Rosemount Aerospace Inc. Pneumatic line isolation and heating for air data probes
US8761970B2 (en) * 2008-10-21 2014-06-24 The Boeing Company Alternative method to determine the air mass state of an aircraft and to validate and augment the primary method
US8527233B2 (en) * 2010-09-27 2013-09-03 The Boeing Company Airspeed sensing system for an aircraft
US8479581B2 (en) 2011-05-03 2013-07-09 General Electric Company Device and method for measuring pressure on wind turbine components
FR2999293B1 (fr) * 2012-12-11 2015-01-16 Thales Sa Systeme pour la fourniture d'estimations de parametres de vol d'un aeronef independantes et dissimilaires et aeronef associe
US9383381B2 (en) 2014-03-13 2016-07-05 The Boeing Company Airspeed calculation system for an aircraft
JP6450108B2 (ja) * 2014-08-08 2019-01-09 三菱航空機株式会社 航空機、および航空機の機外に設置される装置を機体に取り付けるための方法
US9927480B2 (en) 2014-11-06 2018-03-27 Rosemount Aerospace, Inc. System and method for probe heater health indication
FR3033403B1 (fr) * 2015-03-06 2017-03-31 Thales Sa Systeme de fourniture et de surveillance de parametres de vol d'un aeronef
US9841304B2 (en) 2015-04-17 2017-12-12 Rosemount Aerospace Inc. Air data system
US20160370236A1 (en) * 2015-06-22 2016-12-22 Rosemount Aerospace Inc. Aircraft total air temperature anomaly detection
US10179654B2 (en) 2015-10-20 2019-01-15 Honeywell International Inc. Architecture for air data probe power supply control
US10012668B1 (en) 2016-12-09 2018-07-03 Rosemount Aerospace Inc. Triple-redundant air data system architecture
US20190064198A1 (en) * 2017-08-24 2019-02-28 Rosemount Aerospace Inc. Air data system architectures using integrated pressure probes
US10822109B2 (en) 2018-01-05 2020-11-03 The Boeing Company Methods and systems for determining airspeed of an aircraft
US20190346278A1 (en) * 2018-05-09 2019-11-14 Rosemount Aerospace Inc. Multi-function probe air data system architecture including acoustic sensors
US10852316B2 (en) 2018-06-15 2020-12-01 Rosemount Aerospace Inc. Advanced air data system architecture with air data computer incorporating enhanced compensation functionality
US10913545B2 (en) 2018-06-15 2021-02-09 Rosemount Aerospace Inc. Architecture for providing enhanced altitude functionality to aircraft air data system
US11015955B2 (en) * 2018-06-15 2021-05-25 Rosemount Aerospace Inc. Dual channel air data system with inertially compensated backup channel
US11740109B2 (en) * 2019-03-25 2023-08-29 Rosemount Aerospace Inc. Digital air data systems and methods
US11639954B2 (en) 2019-05-29 2023-05-02 Rosemount Aerospace Inc. Differential leakage current measurement for heater health monitoring
US11472562B2 (en) * 2019-06-14 2022-10-18 Rosemount Aerospace Inc. Health monitoring of an electrical heater of an air data probe
US11627014B2 (en) 2019-08-06 2023-04-11 Rosemount Aerospace Inc. Distributed electric air data module system
US11930563B2 (en) 2019-09-16 2024-03-12 Rosemount Aerospace Inc. Monitoring and extending heater life through power supply polarity switching

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3318146A (en) 1966-02-14 1967-05-09 Rosemount Eng Co Ltd Pressure sensing instrument for aircraft
US4378696A (en) 1981-02-23 1983-04-05 Rosemount Inc. Pressure sensor for determining airspeed altitude and angle of attack
US4378697A (en) 1981-07-06 1983-04-05 Rosemount Inc. Strut mounted multiple static tube
FR2569848B1 (fr) 1984-09-03 1986-09-05 Crouzet Badin Sa Sonde de pression multifonction pur aeronef
US5001638A (en) * 1989-04-18 1991-03-19 The Boeing Company Integrated aircraft air data system
US5297052A (en) * 1989-10-16 1994-03-22 The Boeing Company Integrated fault-tolerant air data inertial reference system
BR9107293A (pt) 1991-03-22 1994-05-17 Rosemount Inc Sonda sensora de pressao para montagem sobre uma superficie de uma aeronave, sensor de dados aéreos, e, sonda sensora de dados aéreos
US5205169A (en) 1991-08-08 1993-04-27 Rosemount Inc. Angle of attack sensor using inverted ratio of pressure differentials
US5550736A (en) * 1993-04-27 1996-08-27 Honeywell Inc. Fail-operational fault tolerant flight critical computer architecture and monitoring method
US5369993A (en) 1993-06-30 1994-12-06 The B. F. Goodrich Company Three axis air data system for air vehicles
US5731507A (en) 1993-09-17 1998-03-24 Rosemount Aerospace, Inc. Integral airfoil total temperature sensor
FI96260C (fi) 1993-10-29 1996-05-27 Rautaruukki Oy Suodatusmenetelmä ja suodatin
US5585557A (en) * 1995-05-12 1996-12-17 Lockheed Corporation Air data system for measuring fluid flow direction and velocity
US5653538A (en) 1995-06-07 1997-08-05 Rosemount Aerospace Inc. Total temperature probe
US6012331A (en) 1998-07-02 2000-01-11 Avionics Specialties, Inc. Multifunction aircraft probes
US6076963A (en) 1998-10-20 2000-06-20 Avionics Specialties, Inc. Aircraft probe with integral air temperature sensor
EP1349759A1 (de) * 2001-01-12 2003-10-08 DaimlerChrysler AG Vorrichtung zur überwachung von in einem fahrzeug angeordneten sensormitteln

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20200053857A (ko) * 2018-11-09 2020-05-19 (주) 에어로매스터 항공기의 통합 대기 자료 시스템
KR102156339B1 (ko) * 2018-11-09 2020-09-15 (주)에어로매스터 항공기의 통합 대기 자료 시스템

Also Published As

Publication number Publication date
US6668640B1 (en) 2003-12-30
EP1391736A1 (en) 2004-02-25
EP1391736B1 (en) 2012-03-14
JP2004075060A (ja) 2004-03-11

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