FR2728226A1 - Dispositif d'accouplement-desaccouplement de commandes a bielles - Google Patents

Dispositif d'accouplement-desaccouplement de commandes a bielles Download PDF

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Publication number
FR2728226A1
FR2728226A1 FR9415322A FR9415322A FR2728226A1 FR 2728226 A1 FR2728226 A1 FR 2728226A1 FR 9415322 A FR9415322 A FR 9415322A FR 9415322 A FR9415322 A FR 9415322A FR 2728226 A1 FR2728226 A1 FR 2728226A1
Authority
FR
France
Prior art keywords
arm
input
rod
bearing surfaces
outlet
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.)
Granted
Application number
FR9415322A
Other languages
English (en)
French (fr)
Other versions
FR2728226B1 (da
Inventor
Didier Eric Houssat
Bernard Henri Albert Gemmati
Bras Christophe Guy Nicolas Le
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 Helicopters SAS
Original Assignee
Eurocopter France SA
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 Eurocopter France SA filed Critical Eurocopter France SA
Priority to FR9415322A priority Critical patent/FR2728226A1/fr
Publication of FR2728226A1 publication Critical patent/FR2728226A1/fr
Application granted granted Critical
Publication of FR2728226B1 publication Critical patent/FR2728226B1/fr
Granted legal-status Critical Current

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Classifications

    • 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
    • B64C13/24—Transmitting means
    • B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
    • B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
    • B64C13/30—Transmitting means without power amplification or where power amplification is irrelevant mechanical using cable, chain, or rod mechanisms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061—Frames
    • B64C1/063—Folding or collapsing to reduce overall dimensions, e.g. foldable tail booms

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Transmission Devices (AREA)
FR9415322A 1994-12-20 1994-12-20 Dispositif d'accouplement-desaccouplement de commandes a bielles Granted FR2728226A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR9415322A FR2728226A1 (fr) 1994-12-20 1994-12-20 Dispositif d'accouplement-desaccouplement de commandes a bielles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9415322A FR2728226A1 (fr) 1994-12-20 1994-12-20 Dispositif d'accouplement-desaccouplement de commandes a bielles

Publications (2)

Publication Number Publication Date
FR2728226A1 true FR2728226A1 (fr) 1996-06-21
FR2728226B1 FR2728226B1 (da) 1997-02-21

Family

ID=9469991

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9415322A Granted FR2728226A1 (fr) 1994-12-20 1994-12-20 Dispositif d'accouplement-desaccouplement de commandes a bielles

Country Status (1)

Country Link
FR (1) FR2728226A1 (da)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107600385A (zh) * 2017-10-18 2018-01-19 沈阳旋飞航空技术有限公司 电动无人机的悬臂折叠机构

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB285190A (en) * 1926-11-30 1928-02-16 George Geach Parnall Improvements in or relating to control mechanisms peculiar to aircraft
GB2137943A (en) * 1983-03-15 1984-10-17 Agusta Aeronaut Costr Drive Gear Chain particularly between Disconnectable Parts of an Aircraft

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB285190A (en) * 1926-11-30 1928-02-16 George Geach Parnall Improvements in or relating to control mechanisms peculiar to aircraft
GB2137943A (en) * 1983-03-15 1984-10-17 Agusta Aeronaut Costr Drive Gear Chain particularly between Disconnectable Parts of an Aircraft

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107600385A (zh) * 2017-10-18 2018-01-19 沈阳旋飞航空技术有限公司 电动无人机的悬臂折叠机构
CN107600385B (zh) * 2017-10-18 2023-11-07 沈阳旋飞航空技术有限公司 电动无人机的悬臂折叠机构

Also Published As

Publication number Publication date
FR2728226B1 (da) 1997-02-21

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Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20130830