DE2446545C2 - Winkelhebel-Steuerstangenverbindung für eine Flugzeugsteuervorrichtung - Google Patents

Winkelhebel-Steuerstangenverbindung für eine Flugzeugsteuervorrichtung

Info

Publication number
DE2446545C2
DE2446545C2 DE2446545A DE2446545A DE2446545C2 DE 2446545 C2 DE2446545 C2 DE 2446545C2 DE 2446545 A DE2446545 A DE 2446545A DE 2446545 A DE2446545 A DE 2446545A DE 2446545 C2 DE2446545 C2 DE 2446545C2
Authority
DE
Germany
Prior art keywords
angle lever
control rod
connection
pivot pin
control
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
Application number
DE2446545A
Other languages
German (de)
English (en)
Other versions
DE2446545A1 (de
Inventor
John David Newton Conn. Fansler
Stanley Francis Huntington Conn. Okarma
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.)
RTX Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of DE2446545A1 publication Critical patent/DE2446545A1/de
Application granted granted Critical
Publication of DE2446545C2 publication Critical patent/DE2446545C2/de
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24Transmitting means
    • B64C13/26Transmitting means without power amplification or where power amplification is irrelevant
    • B64C13/28Transmitting means without power amplification or where power amplification is irrelevant mechanical
    • B64C13/30Transmitting means without power amplification or where power amplification is irrelevant mechanical using cable, chain, or rod mechanisms
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24Transmitting means
    • B64C13/26Transmitting means without power amplification or where power amplification is irrelevant
    • B64C13/28Transmitting means without power amplification or where power amplification is irrelevant mechanical
    • B64C13/341Transmitting means without power amplification or where power amplification is irrelevant mechanical having duplication or stand-by provisions
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05GCONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
    • G05G7/00Manually-actuated control mechanisms provided with one single controlling member co-operating with one single controlled member; Details thereof
    • G05G7/02Manually-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
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05GCONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
    • G05G2700/00Control mechanisms or elements therefor applying a mechanical movement
    • G05G2700/12Control mechanisms with one controlling member and one controlled member
    • G05G2700/16Mechanisms for conveying motion or signals for or in relation with control mechanisms
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00Joints and connections
    • Y10T403/32Articulated members
    • Y10T403/32549Articulated members including limit means
    • Y10T403/32557Articulated members including limit means for pivotal motion
    • Y10T403/32581Pin and slot
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00Joints and connections
    • Y10T403/32Articulated members
    • Y10T403/32606Pivoted
    • Y10T403/32861T-pivot, e.g., wrist pin, etc.
    • Y10T403/32918T-pivot, e.g., wrist pin, etc. fork and tongue
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00Machine element or mechanism
    • Y10T74/20Control lever and linkage systems
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00Machine element or mechanism
    • Y10T74/20Control lever and linkage systems
    • Y10T74/20576Elements
    • Y10T74/20582Levers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Transmission Devices (AREA)
  • Pivots And Pivotal Connections (AREA)
  • Mechanical Control Devices (AREA)
  • Toys (AREA)
  • Tires In General (AREA)
DE2446545A 1973-12-14 1974-09-28 Winkelhebel-Steuerstangenverbindung für eine Flugzeugsteuervorrichtung Expired DE2446545C2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US00424987A US3842687A (en) 1973-12-14 1973-12-14 Ballistically tolerant bellcrank/rod-end

Publications (2)

Publication Number Publication Date
DE2446545A1 DE2446545A1 (de) 1975-06-19
DE2446545C2 true DE2446545C2 (de) 1985-09-12

Family

ID=23684690

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2446545A Expired DE2446545C2 (de) 1973-12-14 1974-09-28 Winkelhebel-Steuerstangenverbindung für eine Flugzeugsteuervorrichtung

Country Status (9)

Country Link
US (1) US3842687A (enExample)
JP (1) JPS5810278B2 (enExample)
BR (1) BR7409419A (enExample)
CA (1) CA1010344A (enExample)
DE (1) DE2446545C2 (enExample)
FR (1) FR2254480B1 (enExample)
GB (1) GB1479042A (enExample)
IL (1) IL45816A (enExample)
IT (1) IT1026964B (enExample)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4030378A (en) * 1976-03-11 1977-06-21 United Technologies Corporation Redundant pushrod-to-bellcrank connection
US4183687A (en) * 1978-06-15 1980-01-15 United Technologies Corporation Pivotal joint with redundant connecting means between the two pivotally joined parts thereof
JPS6330587Y2 (enExample) * 1980-08-15 1988-08-16
JPH0343453Y2 (enExample) * 1987-02-16 1991-09-11
USD313785S (en) 1988-08-16 1991-01-15 Bombardier, Inc. Vehicle throttle lever
US4899610A (en) * 1988-09-28 1990-02-13 Bombardier Inc. Throttle lever
US20110217111A1 (en) * 2010-03-03 2011-09-08 Sung-Tsun Wu Clamp-proof joint
ITTO20130902A1 (it) * 2013-11-06 2015-05-07 Fiat Group Automobiles Spa Dispositivo di leva ad azionamento manuale per il comando del freno di stazionamento di un autoveicolo
US20190256039A1 (en) * 2018-02-20 2019-08-22 GM Global Technology Operations LLC Systems and methods for a self-aligning restraint system

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3396597A (en) * 1966-01-17 1968-08-13 United Aircraft Corp Flight control linkage for aircraft
US3578267A (en) * 1968-11-21 1971-05-11 Lear Siegler Inc Control system with multiple function capability

Also Published As

Publication number Publication date
AU7399674A (en) 1976-04-08
US3842687A (en) 1974-10-22
BR7409419A (pt) 1976-05-18
DE2446545A1 (de) 1975-06-19
FR2254480B1 (enExample) 1978-06-09
JPS5090100A (enExample) 1975-07-18
GB1479042A (en) 1977-07-06
CA1010344A (en) 1977-05-17
FR2254480A1 (enExample) 1975-07-11
IL45816A (en) 1977-10-31
JPS5810278B2 (ja) 1983-02-24
IT1026964B (it) 1978-10-20
IL45816A0 (en) 1975-05-22

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Legal Events

Date Code Title Description
8110 Request for examination paragraph 44
8127 New person/name/address of the applicant

Owner name: UNITED TECHNOLOGIES CORP., 06101 HARTFORD, CONN.,

D2 Grant after examination
8364 No opposition during term of opposition