GB594609A - Improvements in or relating to means for temporarily attaching articles to aircraft - Google Patents
Improvements in or relating to means for temporarily attaching articles to aircraftInfo
- Publication number
- GB594609A GB594609A GB1359045A GB1359045A GB594609A GB 594609 A GB594609 A GB 594609A GB 1359045 A GB1359045 A GB 1359045A GB 1359045 A GB1359045 A GB 1359045A GB 594609 A GB594609 A GB 594609A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pair
- shafts
- aircraft
- shaft
- crutches
- 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
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/04—Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs
- B64D1/06—Bomb releasing; Bomb doors
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
Abstract
594,609. Steadying loads suspended from aircraft. BLACKBURN AIRCRAFT, Ltd., and THARRATT, A. May 30, 1945, No. 13590. [Class 78(iv)] [Also in Group XXI] Mechanism for adjusting a pair 15 and a second pair 24 of retaining crutches for temporarily attaching articles to aircraft comprises an operating shaft 1 which is connected to. a differential gearing 2 which in turn drives two shafts 6, 7, connected to the adjusting means of the crutches. By this means the two shafts may be simultaneously rotated in either direction but when one pair is arrested, as for instance when it engages the load, all the drive is taken to the shaft of the other pair. The crutches 15, 24, shown are constructed as in Specification 594,608, [Group XXI], each consisting of a pair of members which are open and closed by nuts on a threaded shaft 10 or-19. These shafts are geared to the hollow shafts 6, 7, leading to the differential 3. Thus when the shaft 1 is rotated by a handle the shafts 6, 7, will both move but when one is arrested the bevel gears 3 of the differential will rotate and carry all the drive to the other shaft.
Publications (1)
Publication Number | Publication Date |
---|---|
GB594609A true GB594609A (en) | 1947-11-14 |
Family
ID=1729199
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1359045A Expired GB594609A (en) | 1945-05-30 | Improvements in or relating to means for temporarily attaching articles to aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB594609A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3670620A (en) * | 1970-11-23 | 1972-06-20 | Us Navy | Automatic sway brace device |
FR2439131A1 (en) * | 1978-10-17 | 1980-05-16 | Alkan R & Cie | Hooked load suspension underneath aircraft - uses combination of centralised hook suspension control with and mechanism between two suspension points |
EP0016325A1 (en) * | 1979-03-24 | 1980-10-01 | Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung | Device for steadying loads suspended from aircrafts |
FR2454408A2 (en) * | 1979-04-20 | 1980-11-14 | Alkan R & Cie | Hooked load suspension underneath aircraft - uses combination of centralised hook suspension control with and mechanism between two suspension points |
DE3231024A1 (en) * | 1982-08-20 | 1984-02-23 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Release device for aircraft external loads |
US4620680A (en) * | 1983-11-30 | 1986-11-04 | R. Alkan & Cie | Device for carrying and ejecting under aircraft loads, comprising support arms positioned with respect to the diameter of the loads |
-
1945
- 1945-05-30 GB GB1359045A patent/GB594609A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3670620A (en) * | 1970-11-23 | 1972-06-20 | Us Navy | Automatic sway brace device |
FR2439131A1 (en) * | 1978-10-17 | 1980-05-16 | Alkan R & Cie | Hooked load suspension underneath aircraft - uses combination of centralised hook suspension control with and mechanism between two suspension points |
EP0016325A1 (en) * | 1979-03-24 | 1980-10-01 | Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung | Device for steadying loads suspended from aircrafts |
FR2454408A2 (en) * | 1979-04-20 | 1980-11-14 | Alkan R & Cie | Hooked load suspension underneath aircraft - uses combination of centralised hook suspension control with and mechanism between two suspension points |
DE3231024A1 (en) * | 1982-08-20 | 1984-02-23 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Release device for aircraft external loads |
US4620680A (en) * | 1983-11-30 | 1986-11-04 | R. Alkan & Cie | Device for carrying and ejecting under aircraft loads, comprising support arms positioned with respect to the diameter of the loads |
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