GB956020A - Improvements in or relating to apparatus for supporting loads on board aircraft - Google Patents
Improvements in or relating to apparatus for supporting loads on board aircraftInfo
- Publication number
- GB956020A GB956020A GB3790361A GB3790361A GB956020A GB 956020 A GB956020 A GB 956020A GB 3790361 A GB3790361 A GB 3790361A GB 3790361 A GB3790361 A GB 3790361A GB 956020 A GB956020 A GB 956020A
- Authority
- GB
- United Kingdom
- Prior art keywords
- frame
- aircraft
- rails
- loads
- secured
- 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
- 241000239290 Araneae Species 0.000 abstract 1
- JHIVVAPYMSGYDF-UHFFFAOYSA-N cyclohexanone Chemical compound O=C1CCCCC1 JHIVVAPYMSGYDF-UHFFFAOYSA-N 0.000 abstract 1
- 238000006073 displacement reaction Methods 0.000 abstract 1
- 230000005484 gravity 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
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/04—Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs
-
- 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)
- Magnetic Bearings And Hydrostatic Bearings (AREA)
Abstract
956,020. Aircraft. SOC. ANON. DES ATELIERS D'AVIATION LOUIS BREQUET. Oct. 23, 1961 [Nov. 17, 1960], No. 37903/61. Headings B7G and B7W. [Also in Division F3] A structure for releasably supporting loads in aircraft comprises one or more frames 4 having means 18 for releasably attaching one or more loads 19, means being provided to displace the frame relatively to the aircraft on longitudinally extending tracks and so shift the load relatively to the centre of gravity of the aircraft, further means being provided to secure the frame in a selected position. Each frame 4 comprises a pair of box girders 5 interconnected by stays and carrying trunnions 6 at each end. On each trunnion is mounted a spider 7 having three radial legs in which rollers 8 are journalled to co-operate with the flanges of channel shaped rails 3 secured to the walls 2 of the stowage compartment in the aircraft. In addition at each end of the frame 4 is mounted a roller 10, which abuts the edge of flange 3a and so prevents lateral displacement of the frame. To lock the frame at a selected position along the rails, at least one trunnion carries a pin 11, Fig. 3, which can be moved by means of a handle 13, sliding in a U-shaped slot 14, into and out of engagement with holes 12 spaced along the rail 3. Preferably additional support means are provided and comprise overhead rails 15 parallel to rails 3 but of smaller section. U-shaped attaching means 16 carried by the girders 5 are secured to the rails 15 by inserting pins 17 into co-operating holes in the members 16 and 15. Loads 19, such as bombs or containers, are suspended from the frame and may be released by remote control. Arcuate arms 18 pivoted on the frame 4 bear against opposing sides of the loads and are simultaneously rotated into and out of position by linkage 21, 23 connected to bevel gearing which is rotated by means of a crank 25. To load the frame 4, a winch 26 is used in conjunction with a pulley 29 on the frame 4.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR844215A FR1280071A (en) | 1960-11-17 | 1960-11-17 | Device for securing loads, which may or may not be dropped, in an aircraft hold |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB956020A true GB956020A (en) | 1964-04-22 |
Family
ID=8742885
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB3790361A Expired GB956020A (en) | 1960-11-17 | 1961-10-23 | Improvements in or relating to apparatus for supporting loads on board aircraft |
Country Status (2)
| Country | Link |
|---|---|
| FR (1) | FR1280071A (en) |
| GB (1) | GB956020A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4168047A (en) * | 1975-07-03 | 1979-09-18 | R. Alkan & Cie | Automatic load carrier and jettisoning system with built-in hoisting means |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108820212B (en) * | 2018-06-11 | 2023-12-22 | 天津航天中为数据系统科技有限公司 | Aircraft with load-transmitting function |
-
1960
- 1960-11-17 FR FR844215A patent/FR1280071A/en not_active Expired
-
1961
- 1961-10-23 GB GB3790361A patent/GB956020A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4168047A (en) * | 1975-07-03 | 1979-09-18 | R. Alkan & Cie | Automatic load carrier and jettisoning system with built-in hoisting means |
Also Published As
| Publication number | Publication date |
|---|---|
| FR1280071A (en) | 1961-12-29 |
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