GB733167A - Improvements relating to systems of controls - Google Patents

Improvements relating to systems of controls

Info

Publication number
GB733167A
GB733167A GB1201552A GB1201552A GB733167A GB 733167 A GB733167 A GB 733167A GB 1201552 A GB1201552 A GB 1201552A GB 1201552 A GB1201552 A GB 1201552A GB 733167 A GB733167 A GB 733167A
Authority
GB
United Kingdom
Prior art keywords
connector
mating parts
projections
recesses
ribs
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
GB1201552A
Inventor
Donald Stanley Pettinger
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.)
Fairey Aviation Co Ltd
Original Assignee
Fairey Aviation Co Ltd
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 Fairey Aviation Co Ltd filed Critical Fairey Aviation Co Ltd
Priority to GB1201552A priority Critical patent/GB733167A/en
Publication of GB733167A publication Critical patent/GB733167A/en
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
    • B64C13/02Initiating means

Abstract

733,167. Fastenings. FAIREY AVIATION CO., Ltd. May 12, 1953 [May 12, 1952]. No. 12015/52. Class 44. [Also in Groups XXVIII and XXXIII] In a system of controls in which each of at least two tension links includes a disengageable connector including two mating parts which lie alongside one another and are held together by a surrounding member, the adjacent surfaces of the mating parts being formed with projections and recesses interengaging to prevent relative longitudinal movement, the distribution of projections and recesses of one connector is different from that of any other so that the controls cannot be interchanged. In part of a control linkage for an aircraft, two oppositely acting tension cables A, B, Fig. 1, are respectively connected by separable connectors A<SP>1</SP>, B<SP>1</SP> to chains A<SP>2</SP>, B<SP>2</SP>. Referring to Fig. 2, the mating parts C, D of each connector are generally semi-cylindrical so that when mated form a substantially cylindrical surface. The interengaging surfaces C<SP>1</SP>, D<SP>1</SP> mate in an axial plane of the connector. Rectangular ribs and grooves formed on one surface mate with corresponding grooves and ribs on the other surface. A shackle E on the part C is pivotally connected to its chain whilst the part D has a bore D<SP>5</SP> to receive its cable which is then secured by a pin locatable in a hole D<SP>6</SP>. A surrounding sleeve F for the connector A<SP>1</SP> is provided with an internal thread H to engage a thread G, Fig. 2. A modified sleeve J for the connector B<SP>1</SP> is slidably mounted on the part D and is urged to its operative position by a spring K. Alternatively the sleeve may be held in place by a spring ball catch or by a pin passing through it and one of the mating parts. The spacing of the ribs and grooves is different for the two connectors so that the part D of one connector cannot be mated with the part C of the other connector and thus interchanging of the control cables is prevented. Other forms of projections and recesses may be provided on the mating parts in lieu of those shown. The connector parts may be swaged to the cables and chains.
GB1201552A 1952-05-12 1952-05-12 Improvements relating to systems of controls Expired GB733167A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1201552A GB733167A (en) 1952-05-12 1952-05-12 Improvements relating to systems of controls

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1201552A GB733167A (en) 1952-05-12 1952-05-12 Improvements relating to systems of controls

Publications (1)

Publication Number Publication Date
GB733167A true GB733167A (en) 1955-07-06

Family

ID=9996868

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1201552A Expired GB733167A (en) 1952-05-12 1952-05-12 Improvements relating to systems of controls

Country Status (1)

Country Link
GB (1) GB733167A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4798098A (en) * 1982-09-09 1989-01-17 Fichtel & Sachs Ag Connection device for gearshift cable
GB2279119A (en) * 1993-06-08 1994-12-21 Halliburton Co Connector assembly for connecting two cylindrical members
GB2291934A (en) * 1994-08-03 1996-02-07 Daimler Benz Ag Coupling fuel injector nozzle needle and piston parts

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4798098A (en) * 1982-09-09 1989-01-17 Fichtel & Sachs Ag Connection device for gearshift cable
GB2279119A (en) * 1993-06-08 1994-12-21 Halliburton Co Connector assembly for connecting two cylindrical members
GB2291934A (en) * 1994-08-03 1996-02-07 Daimler Benz Ag Coupling fuel injector nozzle needle and piston parts
GB2291934B (en) * 1994-08-03 1996-12-11 Daimler Benz Ag Solenoid-valve-controlled injector for direct fuel injection

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