GB1272803A - Cable control system - Google Patents

Cable control system

Info

Publication number
GB1272803A
GB1272803A GB4022269A GB4022269A GB1272803A GB 1272803 A GB1272803 A GB 1272803A GB 4022269 A GB4022269 A GB 4022269A GB 4022269 A GB4022269 A GB 4022269A GB 1272803 A GB1272803 A GB 1272803A
Authority
GB
United Kingdom
Prior art keywords
cable
winch
tension
actual
accumulator
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
GB4022269A
Inventor
Joseph Clair Callaghan
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.)
Minister of National Defence of Canada
UK Secretary of State for Defence
Original Assignee
Minister of National Defence of Canada
UK Secretary of State for Defence
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 Minister of National Defence of Canada, UK Secretary of State for Defence filed Critical Minister of National Defence of Canada
Priority to GB4022269A priority Critical patent/GB1272803A/en
Publication of GB1272803A publication Critical patent/GB1272803A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00Ground or aircraft-carrier-deck installations
    • B64F1/12Ground or aircraft-carrier-deck installations for anchoring aircraft
    • B64F1/125Mooring or ground handling devices for helicopters
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B66HOISTING; LIFTING; HAULING
    • B66DCAPSTANS; WINCHES; TACKLES, e.g. PULLEY BLOCKS; HOISTS
    • B66D1/00Rope, cable, or chain winding mechanisms; Capstans
    • B66D1/28Other constructional details
    • B66D1/40Control devices
    • B66D1/48Control devices automatic
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B66HOISTING; LIFTING; HAULING
    • B66DCAPSTANS; WINCHES; TACKLES, e.g. PULLEY BLOCKS; HOISTS
    • B66D2700/00Capstans, winches or hoists
    • B66D2700/01Winches, capstans or pivots
    • B66D2700/0108Winches, capstans or pivots with devices for paying out or automatically tightening the cable

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tension Adjustment In Filamentary Materials (AREA)

Abstract

1,272,803. Constant tension winches. CANADA, MINISTER OF NATIONAL DEFENCE. 12 Aug., 1969, No. 40222/69. Heading B8B. [Also in Division F2] Apparatus for maintaining a desired tension in a length of cable 5A by which a helicopter is hauled down on to a ship's deck 3 comprises a cable tensioning winch 19 driven by a reversible hydraulic motor 15, and an accumulator 23 arranged to store a variable length loop of cable 5 between the winch and the said length of cable, the direction and speed of the winch driving motor being controlled by signals representative of the actual and desired cable tension, the actual winch speed and the actual speed of the length of cable 5A. The cable 5 extends from the drum 19, around biased apart sets of pulleys 23A, 23C, 23E and 23B, 23D of the accumulator 23 and over guide sheaves 31,33, 35 prior to passing up through the deck 3 to the helicopter. The sheave 35 is supported via a load cell 37 which produces a signal representative of the actual tension in the cable portion 5A and this is compared with a resistor setting variable by a handle 53, which is representative of the desired cable tension, any difference between the signals causing energization of an operating coil 67 of an hydraulic amplifier 47 which actuates a servo valve controlling a variable displacement pump 13 for the winch motor 15. A second operating coil 46 of the amplifier 47 is energizable by a signal representative of a difference in cable velocity at opposite sides of the accumulator, i.e. at the winch drum 19 and at the guide sheave 31, as registered by tachogenerators 41, 43, this controlling the winch motor pump as a result of sudden changes in cable tension which are absorbed by the accumulator 23. The motor 15 may alternatively drive a winch drum 21 for traversing the helicopter once on the deck, a switch 63 being provided for selecting connection between the coil 67 and the haul down circuit including the handle 53, or the traverse circuit including a handle 51. A piston rod of the servo valve is connected to a potentiometer 103 in the transverse circuit to provide a signal indicative of the winch motor pump setting and thus of the actual traverse speed.
GB4022269A 1969-08-12 1969-08-12 Cable control system Expired GB1272803A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB4022269A GB1272803A (en) 1969-08-12 1969-08-12 Cable control system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4022269A GB1272803A (en) 1969-08-12 1969-08-12 Cable control system

Publications (1)

Publication Number Publication Date
GB1272803A true GB1272803A (en) 1972-05-03

Family

ID=10413832

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4022269A Expired GB1272803A (en) 1969-08-12 1969-08-12 Cable control system

Country Status (1)

Country Link
GB (1) GB1272803A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2140752A (en) * 1982-06-23 1984-12-05 Mactaggart Scott Apparatus for controlling the movement of aircraft or the like on a landing surface
EP2975208A3 (en) * 2014-07-15 2016-04-27 BAUER Maschinen GmbH Construction machine and method for controlling a construction machine
WO2019048874A1 (en) * 2017-09-08 2019-03-14 Mactaggart Scott (Holdings) Limited Aircraft handling system

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2140752A (en) * 1982-06-23 1984-12-05 Mactaggart Scott Apparatus for controlling the movement of aircraft or the like on a landing surface
EP2975208A3 (en) * 2014-07-15 2016-04-27 BAUER Maschinen GmbH Construction machine and method for controlling a construction machine
WO2019048874A1 (en) * 2017-09-08 2019-03-14 Mactaggart Scott (Holdings) Limited Aircraft handling system
US10351260B2 (en) 2017-09-08 2019-07-16 Mactaggart Scott (Holdings) Limited Aircraft handling system
US10577127B2 (en) 2017-09-08 2020-03-03 Mactaggart Scott (Holdings) Limited Aircraft handling system

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee