GB598813A - Improvements in or relating to transport-planes - Google Patents
Improvements in or relating to transport-planesInfo
- Publication number
- GB598813A GB598813A GB23431/45A GB2343145A GB598813A GB 598813 A GB598813 A GB 598813A GB 23431/45 A GB23431/45 A GB 23431/45A GB 2343145 A GB2343145 A GB 2343145A GB 598813 A GB598813 A GB 598813A
- Authority
- GB
- United Kingdom
- Prior art keywords
- hold
- wheels
- wings
- gauge
- road
- 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
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Agricultural Machines (AREA)
Abstract
598,813. Aeroplanes. SOC. NATIONALE DE CONSTRUCTIONS AERONAUTIQUES DU SUD-EST. Sept. 11, 1945, No. 23431. Convention date, Sept. 12, 1944. [Class 4] In transport planes of the type in which the freight-containing portion of the aircraft or hold may be separated from the main structure, - the plane is constructed so as to form with the totality of its essential elements (such as wings, engines, pilot's cock-pit, rear portion of the fuselage, fins and control surfaces) a complete unit 22, to the under-forward portion of which is fixed the detachable hold 12, which may be made to carry parts of the undercarriage as well as the controls thereof. In Fig. 1 is shown the unit 22 (unhatched) to the underforward portion of which the hold 12 (hatched) is connected by members such as 2, 3, 4, 5, 6 and 11 (see Fig. 3). Two main landing wheels 14, 15 are carried by the hold and their gauge is such as to make them fit for road use. Two side wheels 16, 17 (which may be retractable) are fixed to the wings 23 for transverse balancing when running on uneven ground or subjected to a beam wind. Wheels 18 are rigidly mounted on the hold and they may serve for the hold's travel by road or, if of larger gauge, be retractable into hold part 20 for towing the hold on a road by carrier-tractor 21, the side wheels 16, 17 not being then required ; if a narrow-gauge or single-track forward gear is provided, an ordinary tractor can be used. The connecting members for the hold admit of angular movements. When the hold has been detached, the unit 22 may be strengthened by the attachment of struts 26, 27. For attaching or detaching the hold, separate wheeled supports 30 for the wings may be used ; or the wing-tip wheels 16, 17 may be -made adjustable as supports when required.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR598813X | 1944-09-12 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB598813A true GB598813A (en) | 1948-02-26 |
Family
ID=8969161
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB23431/45A Expired GB598813A (en) | 1944-09-12 | 1945-09-11 | Improvements in or relating to transport-planes |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB598813A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2683005A (en) * | 1951-01-18 | 1954-07-06 | Lockheed Aircraft Corp | Airplane with detachable cargo compartment |
FR2989063A1 (en) * | 2012-04-05 | 2013-10-11 | Airbus Operations Sas | DISSOCIABLE COUPLING METHOD BETWEEN A PROPULSION MODULE AND A TRANSPORT MODULE OF AN AIRCRAFT AND MODULAR PLANE OF IMPLEMENTATION |
-
1945
- 1945-09-11 GB GB23431/45A patent/GB598813A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2683005A (en) * | 1951-01-18 | 1954-07-06 | Lockheed Aircraft Corp | Airplane with detachable cargo compartment |
FR2989063A1 (en) * | 2012-04-05 | 2013-10-11 | Airbus Operations Sas | DISSOCIABLE COUPLING METHOD BETWEEN A PROPULSION MODULE AND A TRANSPORT MODULE OF AN AIRCRAFT AND MODULAR PLANE OF IMPLEMENTATION |
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