GB1307769A - Helicopters - Google Patents
HelicoptersInfo
- 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
Links
- 239000000725 suspension Substances 0.000 abstract 5
- 238000013016 damping Methods 0.000 abstract 3
- 239000006096 absorbing agent Substances 0.000 abstract 1
- 230000005484 gravity Effects 0.000 abstract 1
- 230000035939 shock Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vibration Prevention Devices (AREA)
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.
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)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3133015A1 (en) * | 2015-08-21 | 2017-02-22 | Marenco Swisshelicopter AG | Load hook substructure |
-
1970
- 1970-07-08 GB GB1307769D patent/GB1307769A/en not_active Expired
Cited By (4)
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 |