GB1233364A - - Google Patents
Info
- Publication number
- GB1233364A GB1233364A GB1233364DA GB1233364A GB 1233364 A GB1233364 A GB 1233364A GB 1233364D A GB1233364D A GB 1233364DA GB 1233364 A GB1233364 A GB 1233364A
- Authority
- GB
- United Kingdom
- Prior art keywords
- winch
- fuselage
- aircraft
- opening
- sept
- 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
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)
- Jib Cranes (AREA)
Abstract
1,233,364. Mounting jib cranes on aircraft. WESTLAND AIRCRAFT Ltd. 29 Aug., 1968 [1 Sept., 1967], No. 40183/67. Heading B7W. [Also in Division B8] A hoisting apparatus installed within an aircraft fuselage comprises a winch 13 rotatable on support structure between positions internal and external of the fuselage and being supported by a variable length member 10. The winch 13 and bottom end of the member 10 are connected by universal joints to the fuselage adjacent the top and bottom of a cargo opening 19, the top of the member 10 being pivoted to the winch 13. A side bracing strut 16 universally jointed at one end to the winch is detachably connected at the other end 17 to the fuselage. The member 10 is telescopically extendable by manual, mechanical, hydraulic, pneumatic or electrical means, to lift the winch 13 above the opening 19 when outside of the fuselage.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4018367 | 1967-09-01 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1233364A true GB1233364A (en) | 1971-05-26 |
Family
ID=10413614
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1233364D Expired GB1233364A (en) | 1967-09-01 | 1967-09-01 |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR1577830A (en) |
GB (1) | GB1233364A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2162469A (en) * | 1984-08-03 | 1986-02-05 | Thomas Balfour | Life saving boom |
US5762297A (en) * | 1996-09-23 | 1998-06-09 | Skyhook Rescue Systems, Inc. | Recovery device for use in an airborne vehicle |
US6059266A (en) * | 1996-09-23 | 2000-05-09 | Ascherin; Terry C. | Recovery device |
EP1405788A1 (en) * | 2002-10-04 | 2004-04-07 | Antar Daouk | Support arm for aircraft |
US10479502B2 (en) | 2016-05-25 | 2019-11-19 | Airbus Helicopters | Aircraft provided with a winch device |
EP3932803A1 (en) * | 2020-06-30 | 2022-01-05 | Airbus Helicopters Deutschland GmbH | Load carrying assembly for a rotary wing aircraft |
-
1967
- 1967-09-01 GB GB1233364D patent/GB1233364A/en not_active Expired
-
1968
- 1968-08-29 FR FR1577830D patent/FR1577830A/fr not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2162469A (en) * | 1984-08-03 | 1986-02-05 | Thomas Balfour | Life saving boom |
US5762297A (en) * | 1996-09-23 | 1998-06-09 | Skyhook Rescue Systems, Inc. | Recovery device for use in an airborne vehicle |
US6059266A (en) * | 1996-09-23 | 2000-05-09 | Ascherin; Terry C. | Recovery device |
EP1405788A1 (en) * | 2002-10-04 | 2004-04-07 | Antar Daouk | Support arm for aircraft |
FR2845349A1 (en) * | 2002-10-04 | 2004-04-09 | Antar Daouk | POTENCY FOR AIRCRAFT |
US10479502B2 (en) | 2016-05-25 | 2019-11-19 | Airbus Helicopters | Aircraft provided with a winch device |
EP3932803A1 (en) * | 2020-06-30 | 2022-01-05 | Airbus Helicopters Deutschland GmbH | Load carrying assembly for a rotary wing aircraft |
Also Published As
Publication number | Publication date |
---|---|
FR1577830A (en) | 1969-08-08 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PLNP | Patent lapsed through nonpayment of renewal fees |