FR2712867B1 - Control lever apparatus for adjusting thrust in airplanes. - Google Patents

Control lever apparatus for adjusting thrust in airplanes.

Info

Publication number
FR2712867B1
FR2712867B1 FR9411114A FR9411114A FR2712867B1 FR 2712867 B1 FR2712867 B1 FR 2712867B1 FR 9411114 A FR9411114 A FR 9411114A FR 9411114 A FR9411114 A FR 9411114A FR 2712867 B1 FR2712867 B1 FR 2712867B1
Authority
FR
France
Prior art keywords
airplanes
control lever
lever apparatus
adjusting thrust
thrust
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.)
Expired - Lifetime
Application number
FR9411114A
Other languages
French (fr)
Other versions
FR2712867A1 (en
Inventor
Bernd Neudorffer
Klaus Alexander Langner
Wolfgang Kummle
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.)
Bodenseewerk Geratetechnik GmbH
Original Assignee
Bodenseewerk Geratetechnik 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 Bodenseewerk Geratetechnik GmbH filed Critical Bodenseewerk Geratetechnik GmbH
Publication of FR2712867A1 publication Critical patent/FR2712867A1/en
Application granted granted Critical
Publication of FR2712867B1 publication Critical patent/FR2712867B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05G—CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
    • G05G7/00—Manually-actuated control mechanisms provided with one single controlling member co-operating with one single controlled member; Details thereof
    • G05G7/02—Manually-actuated control mechanisms provided with one single controlling member co-operating with one single controlled member; Details thereof characterised by special provisions for conveying or converting motion, or for acting at a distance
    • G05G7/10—Manually-actuated control mechanisms provided with one single controlling member co-operating with one single controlled member; Details thereof characterised by special provisions for conveying or converting motion, or for acting at a distance specially adapted for remote control
    • 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
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • B64D31/02—Initiating means
    • B64D31/04—Initiating means actuated personally
    • 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
    • G01D5/26—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 characterised by optical transfer means, i.e. using infrared, visible, or ultraviolet light
    • G01D5/32—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 characterised by optical transfer means, i.e. using infrared, visible, or ultraviolet light with attenuation or whole or partial obturation of beams of light
    • G01D5/34—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 characterised by optical transfer means, i.e. using infrared, visible, or ultraviolet light with attenuation or whole or partial obturation of beams of light the beams of light being detected by photocells

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Optical Transform (AREA)
  • Transmission And Conversion Of Sensor Element Output (AREA)
  • Mechanical Control Devices (AREA)
FR9411114A 1993-09-15 1994-09-14 Control lever apparatus for adjusting thrust in airplanes. Expired - Lifetime FR2712867B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE4331230A DE4331230B4 (en) 1993-09-15 1993-09-15 Control lever device for adjusting the thrust of airplanes

Publications (2)

Publication Number Publication Date
FR2712867A1 FR2712867A1 (en) 1995-06-02
FR2712867B1 true FR2712867B1 (en) 1997-03-21

Family

ID=6497715

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9411114A Expired - Lifetime FR2712867B1 (en) 1993-09-15 1994-09-14 Control lever apparatus for adjusting thrust in airplanes.

Country Status (5)

Country Link
CA (1) CA2131578C (en)
DE (1) DE4331230B4 (en)
FR (1) FR2712867B1 (en)
GB (1) GB2281882B (en)
IL (1) IL110955A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19961531C2 (en) * 1999-12-20 2003-08-21 Lange Flugzeugbau Gmbh Engine control device for a glider with a folding engine
CN109606704A (en) * 2018-12-11 2019-04-12 四川航空工业川西机器有限责任公司 A kind of fax power control platform

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2080522B (en) * 1979-09-19 1983-10-12 Draper Lab Charles S Improved instrumented remote centre compliance device
DE3822007A1 (en) * 1988-06-30 1990-01-04 Bodenseewerk Geraetetech DIGITAL POSITION SIGNALER
DE3903359A1 (en) * 1989-02-05 1990-08-09 Bayerische Motoren Werke Ag DEVICE FOR DETERMINING THE STEERING WHEEL ANGLE OF A MOTOR VEHICLE
US5029778A (en) * 1989-09-11 1991-07-09 The Boeing Company Throttle control system having real-time-computed thrust vs throttle position function
DE8915839U1 (en) * 1989-11-27 1992-01-16 Bodenseewerk Gerätetechnik GmbH, 7770 Überlingen Position sensor for landing flap levers on aircraft
US5065962A (en) * 1989-12-27 1991-11-19 Rockwell International Corporation Digital power controller

Also Published As

Publication number Publication date
DE4331230A1 (en) 1995-03-16
CA2131578C (en) 2002-07-23
CA2131578A1 (en) 1995-03-16
GB2281882A (en) 1995-03-22
GB2281882B (en) 1997-02-05
GB9418332D0 (en) 1994-11-02
DE4331230B4 (en) 2008-04-17
FR2712867A1 (en) 1995-06-02
IL110955A (en) 1999-08-17
IL110955A0 (en) 1994-11-28

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