GB1307769A - Helicopters - Google Patents

Helicopters

Info

Publication number
GB1307769A
GB1307769A GB1307769DA GB1307769A GB 1307769 A GB1307769 A GB 1307769A GB 1307769D A GB1307769D A GB 1307769DA GB 1307769 A GB1307769 A GB 1307769A
Authority
GB
United Kingdom
Prior art keywords
suspension means
damping member
load
helicopter
aperture
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
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.)
Westland Group PLC
Original Assignee
Westland Aircraft 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 Westland Aircraft Ltd filed Critical Westland Aircraft Ltd
Publication of GB1307769A publication Critical patent/GB1307769A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
    • B64D1/22—Taking-up articles from earth's surface

Abstract

1307769 Load suspension from helicopters WESTLAND AIRCRAFT Ltd 23 June 1971 [8 July 1970] 33050/70 Heading B7W [Also in Division F2] A helicopter has load suspension means 11, 15, 16, 17 passing through an aperture 14 in a fuselage floor structure, wherein a damping member 22 is resiliently supported, for example by resilient tubes 20, 21 mounted by pivotal connections on flanges 19, in the aperture 14 for contact by the load suspension means when swinging movements of the suspension means reach a predetermined limit. The suspension means includes a hoist 11 mounted at 12 for swinging longitudinally or laterally and is rotatable through a joint 16, a hook 15 for engaging a load and a snubber ring 17 which engages the damping member 22 in the form of a ring at said predetermined limit. The mount 12 is preferably at the centre of gravity of the helicopter and the resilient support for the damping member may include shock absorbers instead of the tubes 20, 21.
GB1307769D 1970-07-08 1970-07-08 Helicopters Expired GB1307769A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3305070 1970-07-08

Publications (1)

Publication Number Publication Date
GB1307769A true GB1307769A (en) 1973-02-21

Family

ID=10347864

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1307769D Expired GB1307769A (en) 1970-07-08 1970-07-08 Helicopters

Country Status (1)

Country Link
GB (1) GB1307769A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3133015A1 (en) * 2015-08-21 2017-02-22 Marenco Swisshelicopter AG Load hook substructure

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3133015A1 (en) * 2015-08-21 2017-02-22 Marenco Swisshelicopter AG Load hook substructure
CH711440A1 (en) * 2015-08-21 2017-02-28 Marenco Swisshelicopter Ag Loader hook construction for attachment to or in a cabin structure of a helicopter.
CN106467171A (en) * 2015-08-21 2017-03-01 瑞士玛瑞恩克直升机公司 Load hook structures
US10150565B2 (en) 2015-08-21 2018-12-11 Kopter Group Ag Load hook substructure

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Legal Events

Date Code Title Description
PS Patent sealed
PLNP Patent lapsed through nonpayment of renewal fees