GB293303A - Improvements in or relating to aeroplanes - Google Patents
Improvements in or relating to aeroplanesInfo
- Publication number
- GB293303A GB293303A GB18352/28A GB1835228A GB293303A GB 293303 A GB293303 A GB 293303A GB 18352/28 A GB18352/28 A GB 18352/28A GB 1835228 A GB1835228 A GB 1835228A GB 293303 A GB293303 A GB 293303A
- Authority
- GB
- United Kingdom
- Prior art keywords
- cabin
- spars
- freight
- fuselage
- detachable
- 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
- 230000000295 complement effect Effects 0.000 abstract 1
- 230000004048 modification Effects 0.000 abstract 1
- 238000012986 modification Methods 0.000 abstract 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 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
- B64D17/00—Parachutes
- B64D17/78—Parachutes in association with other load-retarding apparatus
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Body Structure For Vehicles (AREA)
Abstract
293,303. BlÚriot, L. July 2, 1927, [Convention date]. Aeroplanes; cabins; receptacles, detachable, for mails and freight.-An aeroplane fitted with land wheels is provided with a part adapted to receive passengers or freight or both, which can be detached and navigated as a boat in the event oi descent upon water. A cabin d, provided with an engine or with sails, is normally secured within a recess d<1> in the fuselage and has watertight doors f giving access to and from the main part of the machine. Two recesses h', h<2> fit over the spars g<1>, g<2> of the main wing and the cabin is secured to these spars by removable pins. Plugs are provided to fill the holes in the cabin when the pins are removed. A modification is described in which the detachable cabin is carried in the lower part of the fuselage, the lower booms m, Fig. 5, of the wing spars being divided and the cabin having complementary spar sections l. The abutting ends of the spars m and sections l have flanges o<1>, o<2> which are normally engaged by sliding sockets n.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BE293303X | 1927-07-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB293303A true GB293303A (en) | 1929-01-31 |
Family
ID=3867301
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB18352/28A Expired GB293303A (en) | 1927-07-02 | 1928-06-25 | Improvements in or relating to aeroplanes |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB293303A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19934210A1 (en) * | 1999-07-21 | 2001-02-01 | Robert Srzentic | Transport system with carrier has cargo volume in form of cargo module for replaceable mounting in bay or aperture in fuselage of carrier arrangement, e.g. passenger or transport aircraft |
GB2441613A (en) * | 2007-07-26 | 2008-03-12 | Chao Shu Au | Aircraft storage cell and ejection arrangement |
-
1928
- 1928-06-25 GB GB18352/28A patent/GB293303A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19934210A1 (en) * | 1999-07-21 | 2001-02-01 | Robert Srzentic | Transport system with carrier has cargo volume in form of cargo module for replaceable mounting in bay or aperture in fuselage of carrier arrangement, e.g. passenger or transport aircraft |
DE19934210B4 (en) * | 1999-07-21 | 2018-01-04 | Robert Srzentic | Transport system with a carrier device and method for handling payload in carrier devices |
GB2441613A (en) * | 2007-07-26 | 2008-03-12 | Chao Shu Au | Aircraft storage cell and ejection arrangement |
GB2441613B (en) * | 2007-07-26 | 2008-09-03 | Chao Shu Au | Aircraft storage and ejection arrangement |
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