GB606088A - Improvements relating to aeroplanes - Google Patents
Improvements relating to aeroplanesInfo
- Publication number
- GB606088A GB606088A GB9999/46A GB999946A GB606088A GB 606088 A GB606088 A GB 606088A GB 9999/46 A GB9999/46 A GB 9999/46A GB 999946 A GB999946 A GB 999946A GB 606088 A GB606088 A GB 606088A
- Authority
- GB
- United Kingdom
- Prior art keywords
- housings
- aeroplanes
- wings
- improvements relating
- aircraft
- 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
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/02—Tanks
- B64D37/06—Constructional adaptations thereof
- B64D37/12—Constructional adaptations thereof jettisonable
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- General Details Of Gearings (AREA)
Abstract
606,088. Propelling aircraft. GOODYEAR AIRCRAFT CORPORATION. April 1, 1946, No. 9999. Convention date, Sept. 8, 1945. (Class 4] An aeroplane is provided with three propulsion units, preferably of the jet type, one of which, 2, is mounted in the fuselage 1, the others 5 being mounted in housings 4 at the tips of the wings 3,. such an arrangement resulting in reduction of the wing tip vortices. To facilitate take-off, aerofoil section drop tanks 6 are attached to the housings, to form extensions to the main wings 3.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US606088XA | 1945-09-08 | 1945-09-08 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB606088A true GB606088A (en) | 1948-08-05 |
Family
ID=22030598
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9999/46A Expired GB606088A (en) | 1945-09-08 | 1946-04-01 | Improvements relating to aeroplanes |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB606088A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2623713A (en) * | 1949-03-19 | 1952-12-30 | Bell Aircraft Corp | Aircraft folding wing and powerplant arrangement |
US2650781A (en) * | 1950-08-11 | 1953-09-01 | United Aircraft Corp | Boundary layer control for aircraft |
US2656136A (en) * | 1951-01-03 | 1953-10-20 | James V Martin | Flying ship |
US2681192A (en) * | 1950-04-07 | 1954-06-15 | Republic Aviat Corp | Wing tip tank construction |
-
1946
- 1946-04-01 GB GB9999/46A patent/GB606088A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2623713A (en) * | 1949-03-19 | 1952-12-30 | Bell Aircraft Corp | Aircraft folding wing and powerplant arrangement |
US2681192A (en) * | 1950-04-07 | 1954-06-15 | Republic Aviat Corp | Wing tip tank construction |
US2650781A (en) * | 1950-08-11 | 1953-09-01 | United Aircraft Corp | Boundary layer control for aircraft |
US2656136A (en) * | 1951-01-03 | 1953-10-20 | James V Martin | Flying ship |
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