FR2892813B1 - Capteur integrable dans la surface portante d'un aeronef notamment d'un avion ou d'un helicoptere - Google Patents

Capteur integrable dans la surface portante d'un aeronef notamment d'un avion ou d'un helicoptere

Info

Publication number
FR2892813B1
FR2892813B1 FR0654684A FR0654684A FR2892813B1 FR 2892813 B1 FR2892813 B1 FR 2892813B1 FR 0654684 A FR0654684 A FR 0654684A FR 0654684 A FR0654684 A FR 0654684A FR 2892813 B1 FR2892813 B1 FR 2892813B1
Authority
FR
France
Prior art keywords
aircraft
helicopter
integrable
sensor
integrable sensor
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
FR0654684A
Other languages
English (en)
Other versions
FR2892813A1 (fr
Inventor
Alois Frieberger
Christian Grwadolph
Thomas Ziemann
Valentin Kloppel
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 Defence and Space GmbH
Original Assignee
EADS Deutschland GmbH
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 EADS Deutschland GmbH filed Critical EADS Deutschland GmbH
Publication of FR2892813A1 publication Critical patent/FR2892813A1/fr
Application granted granted Critical
Publication of FR2892813B1 publication Critical patent/FR2892813B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L19/00Details of, or accessories for, apparatus for measuring steady or quasi-steady pressure of a fluent medium insofar as such details or accessories are not special to particular types of pressure gauges
    • G01L19/0061Electrical connection means
    • G01L19/0084Electrical connection means to the outside of the housing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D43/00Arrangements or adaptations of instruments
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L19/00Details of, or accessories for, apparatus for measuring steady or quasi-steady pressure of a fluent medium insofar as such details or accessories are not special to particular types of pressure gauges
    • G01L19/0007Fluidic connecting means
    • G01L19/003Fluidic connecting means using a detachable interface or adapter between the process medium and the pressure gauge
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L19/00Details of, or accessories for, apparatus for measuring steady or quasi-steady pressure of a fluent medium insofar as such details or accessories are not special to particular types of pressure gauges
    • G01L19/0007Fluidic connecting means
    • G01L19/0038Fluidic connecting means being part of the housing
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L19/00Details of, or accessories for, apparatus for measuring steady or quasi-steady pressure of a fluent medium insofar as such details or accessories are not special to particular types of pressure gauges
    • G01L19/06Means for preventing overload or deleterious influence of the measured medium on the measuring device or vice versa
    • G01L19/0627Protection against aggressive medium in general
    • G01L19/0636Protection against aggressive medium in general using particle filters
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L19/00Details of, or accessories for, apparatus for measuring steady or quasi-steady pressure of a fluent medium insofar as such details or accessories are not special to particular types of pressure gauges
    • G01L19/14Housings
    • G01L19/147Details about the mounting of the sensor to support or covering means

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Analytical Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Measuring Fluid Pressure (AREA)
FR0654684A 2005-11-03 2006-11-02 Capteur integrable dans la surface portante d'un aeronef notamment d'un avion ou d'un helicoptere Active FR2892813B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102005052929A DE102005052929B4 (de) 2005-11-03 2005-11-03 Sensor für ein Luftfahrzeug, insbesondere ein Flugzeug oder Hubschrauber

Publications (2)

Publication Number Publication Date
FR2892813A1 FR2892813A1 (fr) 2007-05-04
FR2892813B1 true FR2892813B1 (fr) 2015-02-13

Family

ID=37964264

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0654684A Active FR2892813B1 (fr) 2005-11-03 2006-11-02 Capteur integrable dans la surface portante d'un aeronef notamment d'un avion ou d'un helicoptere

Country Status (3)

Country Link
US (1) US7726200B2 (fr)
DE (1) DE102005052929B4 (fr)
FR (1) FR2892813B1 (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008036638B4 (de) * 2008-08-06 2010-08-19 Eads Deutschland Gmbh Verfahren und Vorrichtung zur Ermittlung des Funktionszustandes eines Hubschrauberrotor-Drucksensors
DE102008053072B4 (de) 2008-10-24 2014-10-30 Airbus Defence and Space GmbH Sensor für ein Rotorblatt oder eine Tragfläche
JP2013529524A (ja) * 2010-06-28 2013-07-22 ネステク ソシエテ アノニム カプセル感知システム
US8791375B2 (en) * 2010-12-16 2014-07-29 The Boeing Company Electrically conductive bushing connection to structure for current path
EP2572982B1 (fr) 2011-09-20 2014-06-18 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Profil avec système de contrôle de circulation
US20150143926A1 (en) 2013-11-23 2015-05-28 Silicon Microstructures, Inc. Area-efficient pressure sensing device
US9322685B2 (en) * 2014-06-30 2016-04-26 The Boeing Company MEMS-based conformal air speed sensor
US9573544B1 (en) * 2015-08-24 2017-02-21 Ford Global Technologies, Llc Protective structures for air sensors in a vehicle body structure
CN106915470B (zh) * 2017-03-20 2019-03-01 成都优狼科技有限公司 一种群蜂无人机起吊系统
EP3640612B1 (fr) * 2018-10-16 2023-06-07 Airbus Helicopters Appareil pour détecter une déformation élastique d'un élément creux

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2764646A (en) * 1952-10-21 1956-09-25 Don W Young Sensitive differential pressure capsule switch
US3643510A (en) * 1969-12-17 1972-02-22 Liquidonics Inc Fluid displacement pressure gauges
US3915009A (en) * 1973-05-03 1975-10-28 Ruska Instr Corp Precision pressure gauge
IT1066823B (it) * 1975-12-30 1985-03-12 Sits Soc It Telecom Siemens Trasduttore elettroacustico particolarmente del tipo a lamina piezoceramica
US4288835A (en) * 1979-04-16 1981-09-08 The Bendix Corporation Pressure sensor
US5058430A (en) * 1989-12-29 1991-10-22 Honeywell Inc. Sensor capsule mounting
US5092173A (en) * 1989-12-29 1992-03-03 Honeywell Inc. Secondary accelerometer pickoff
DE19923087B4 (de) 1999-05-20 2004-02-26 Eads Deutschland Gmbh Vorrichtung zur Druck-, Schall- und Vibrationsmessung, sowie Verfahren zur Strömungsanalyse an Bauteiloberflächen
DE10137184B4 (de) * 2001-07-31 2007-09-06 Infineon Technologies Ag Verfahren zur Herstellung eines elektronischen Bauteils mit einem Kuststoffgehäuse und elektronisches Bauteil
US6883380B2 (en) * 2003-05-16 2005-04-26 Rosemount Inc Pressure sensor capsule
DE10326975A1 (de) * 2003-06-12 2005-01-20 Endress + Hauser Gmbh + Co. Kg Drucksensor mit Feuchteschutz

Also Published As

Publication number Publication date
DE102005052929A1 (de) 2007-05-31
US7726200B2 (en) 2010-06-01
DE102005052929B4 (de) 2011-07-21
US20070186672A1 (en) 2007-08-16
FR2892813A1 (fr) 2007-05-04

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