GB510383A - An improved fuel tank for aircraft - Google Patents
An improved fuel tank for aircraftInfo
- Publication number
- GB510383A GB510383A GB23145/38A GB2314538A GB510383A GB 510383 A GB510383 A GB 510383A GB 23145/38 A GB23145/38 A GB 23145/38A GB 2314538 A GB2314538 A GB 2314538A GB 510383 A GB510383 A GB 510383A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- fuel tank
- seen
- improved fuel
- substantially elliptical
- 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
- 239000002828 fuel tank Substances 0.000 title abstract 2
- 238000010276 construction Methods 0.000 abstract 1
- 239000000446 fuel Substances 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
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/02—Tanks
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Abstract
510,383. Tanks. BROOKFIELD, E. Aug. 5. 1938, No. 23145. [Class 69 (i)] A fuel tank for aircraft which is made of two flanged halves, 1, 2, bolted together and is substantially elliptical as seen in one direction, and which tapers towards each end or is substantially elliptical as seen in a direction at right angles to the former, is provided with internal baffles 7. In the construction shown the baffles extend diagonally across the tank and extend from side to side and from top to bottom and are formed with corresponding slots 8.,by which they engage one another when assembled, and with waved of serrated edges to permit passage of the fuel around them. The edges of the flanges 3 may be welded together in addition to bolting
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB23145/38A GB510383A (en) | 1938-08-05 | 1938-08-05 | An improved fuel tank for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB23145/38A GB510383A (en) | 1938-08-05 | 1938-08-05 | An improved fuel tank for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB510383A true GB510383A (en) | 1939-08-01 |
Family
ID=10190882
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB23145/38A Expired GB510383A (en) | 1938-08-05 | 1938-08-05 | An improved fuel tank for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB510383A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6293420B1 (en) | 1997-07-25 | 2001-09-25 | Kautex Textron Gmbh & Co., Kg. | Fuel tank |
-
1938
- 1938-08-05 GB GB23145/38A patent/GB510383A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6293420B1 (en) | 1997-07-25 | 2001-09-25 | Kautex Textron Gmbh & Co., Kg. | Fuel tank |
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