WO2009013326A3 - Induktiver böensensor - Google Patents

Induktiver böensensor Download PDF

Info

Publication number
WO2009013326A3
WO2009013326A3 PCT/EP2008/059676 EP2008059676W WO2009013326A3 WO 2009013326 A3 WO2009013326 A3 WO 2009013326A3 EP 2008059676 W EP2008059676 W EP 2008059676W WO 2009013326 A3 WO2009013326 A3 WO 2009013326A3
Authority
WO
WIPO (PCT)
Prior art keywords
inductive
wind vane
gust sensor
sensor
rotation angle
Prior art date
Application number
PCT/EP2008/059676
Other languages
English (en)
French (fr)
Other versions
WO2009013326A2 (de
Inventor
Josef Steigenberger
Andreas Wildschek
Original Assignee
Eads Deutschland Gmbh
Josef Steigenberger
Andreas Wildschek
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, Josef Steigenberger, Andreas Wildschek filed Critical Eads Deutschland Gmbh
Publication of WO2009013326A2 publication Critical patent/WO2009013326A2/de
Publication of WO2009013326A3 publication Critical patent/WO2009013326A3/de

Links

Classifications

    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02—Initiating means
    • B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
    • 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
    • G01D—MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
    • G01D5/00—Mechanical means for transferring the output of a sensing member; Means for converting the output of a sensing member to another variable where the form or nature of the sensing member does not constrain the means for converting; Transducers not specially adapted for a specific variable
    • G01D5/12—Mechanical means for transferring the output of a sensing member; Means for converting the output of a sensing member to another variable where the form or nature of the sensing member does not constrain the means for converting; Transducers not specially adapted for a specific variable using electric or magnetic means
    • G01D5/14—Mechanical means for transferring the output of a sensing member; Means for converting the output of a sensing member to another variable where the form or nature of the sensing member does not constrain the means for converting; Transducers not specially adapted for a specific variable using electric or magnetic means influencing the magnitude of a current or voltage
    • G01D5/20—Mechanical means for transferring the output of a sensing member; Means for converting the output of a sensing member to another variable where the form or nature of the sensing member does not constrain the means for converting; Transducers not specially adapted for a specific variable using electric or magnetic means influencing the magnitude of a current or voltage by varying inductance, e.g. by a movable armature
    • G01D5/2006—Mechanical means for transferring the output of a sensing member; Means for converting the output of a sensing member to another variable where the form or nature of the sensing member does not constrain the means for converting; Transducers not specially adapted for a specific variable using electric or magnetic means influencing the magnitude of a current or voltage by varying inductance, e.g. by a movable armature by influencing the self-induction of one or more coils
    • G01D5/2013—Mechanical means for transferring the output of a sensing member; Means for converting the output of a sensing member to another variable where the form or nature of the sensing member does not constrain the means for converting; Transducers not specially adapted for a specific variable using electric or magnetic means influencing the magnitude of a current or voltage by varying inductance, e.g. by a movable armature by influencing the self-induction of one or more coils by a movable ferromagnetic element, e.g. a core
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Vibration Prevention Devices (AREA)
  • Indicating Or Recording The Presence, Absence, Or Direction Of Movement (AREA)
  • Measurement Of Length, Angles, Or The Like Using Electric Or Magnetic Means (AREA)

Abstract

Die Erfindung betrifft ein Windfahnenelement (10) mit einer Windfahne (12), das sich nach der Windrichtung ausrichtet, mit einem Drehwinkelaufnehmer (18), der eine Winkelstellung der Windfahne (12) als Messsignal bereitstellt, wobei der Drehwinkelaufnehmer (18) berührungslos arbeitet.
PCT/EP2008/059676 2007-07-26 2008-07-23 Induktiver böensensor WO2009013326A2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102007035461.6A DE102007035461B4 (de) 2007-07-26 2007-07-26 Verfahren zur Messung von Anstellwinkel und Böengeschwindigkeit an einem Luftfahrzeug oder Flugkörper
DE102007035461.6 2007-07-26

Publications (2)

Publication Number Publication Date
WO2009013326A2 WO2009013326A2 (de) 2009-01-29
WO2009013326A3 true WO2009013326A3 (de) 2009-04-30

Family

ID=40157366

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2008/059676 WO2009013326A2 (de) 2007-07-26 2008-07-23 Induktiver böensensor

Country Status (2)

Country Link
DE (1) DE102007035461B4 (de)
WO (1) WO2009013326A2 (de)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008014236B4 (de) * 2008-03-14 2013-09-05 Eads Deutschland Gmbh Schwingungsreduktionsvorrichtung

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2621873A (en) * 1947-03-31 1952-12-16 North American Aviation Inc Aircraft control
US2962243A (en) * 1956-05-07 1960-11-29 Franklin Institute Gust sensing apparatus for aircraft
US3665760A (en) * 1969-12-15 1972-05-30 Ferranti Ltd Airflow direction indicators
WO2001077622A2 (en) * 2000-04-05 2001-10-18 Rosemount Aerospace Inc. Magnetic angle of attack sensor
WO2009013318A2 (de) * 2007-07-26 2009-01-29 Eads Deutschland Gmbh Versuchsanordnung mit einem wenigstens ein steuerelement umfassenden versuchsmodell sowie ein zugehöriges verfahren
WO2009013322A1 (de) * 2007-07-26 2009-01-29 Eads Deutschland Gmbh Kombinierte rückführ- und vorsteuerregelung zur aktiven verminderung von schwingungen bei luftfahrzeugen

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3077773A (en) 1955-05-09 1963-02-19 North American Aviation Inc Vane angle computer
US3105382A (en) 1960-12-30 1963-10-01 Servomechanisms Inc High altitude transducers
US3260108A (en) 1963-05-06 1966-07-12 Giannini Controls Corp System for representing angle of attack and the like
US6612166B2 (en) 2001-12-13 2003-09-02 Rosemount Aerospace Inc. Variable viscosity damper for vane type angle of attack sensor
EP1814006B1 (de) 2006-01-25 2016-09-21 Airbus Opérations SAS Minimierung der dynamischen strukturellen Lasten eines Flugzeuges

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2621873A (en) * 1947-03-31 1952-12-16 North American Aviation Inc Aircraft control
US2962243A (en) * 1956-05-07 1960-11-29 Franklin Institute Gust sensing apparatus for aircraft
US3665760A (en) * 1969-12-15 1972-05-30 Ferranti Ltd Airflow direction indicators
WO2001077622A2 (en) * 2000-04-05 2001-10-18 Rosemount Aerospace Inc. Magnetic angle of attack sensor
WO2009013318A2 (de) * 2007-07-26 2009-01-29 Eads Deutschland Gmbh Versuchsanordnung mit einem wenigstens ein steuerelement umfassenden versuchsmodell sowie ein zugehöriges verfahren
WO2009013322A1 (de) * 2007-07-26 2009-01-29 Eads Deutschland Gmbh Kombinierte rückführ- und vorsteuerregelung zur aktiven verminderung von schwingungen bei luftfahrzeugen

Also Published As

Publication number Publication date
WO2009013326A2 (de) 2009-01-29
DE102007035461A1 (de) 2009-01-29
DE102007035461B4 (de) 2017-03-30

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