GB582704A - Improvements in and relating to fuel tank installations in aircraft - Google Patents
Improvements in and relating to fuel tank installations in aircraftInfo
- Publication number
- GB582704A GB582704A GB14650/45A GB1465045A GB582704A GB 582704 A GB582704 A GB 582704A GB 14650/45 A GB14650/45 A GB 14650/45A GB 1465045 A GB1465045 A GB 1465045A GB 582704 A GB582704 A GB 582704A
- Authority
- GB
- United Kingdom
- Prior art keywords
- tank
- wing
- aircraft
- fuel tank
- section
- 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 3
- 238000009434 installation Methods 0.000 title 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
- B64D37/04—Arrangement thereof in or on aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Abstract
5 8 2 , 7 0 4 . Fuel tanks. BOULTON PAUL AIRCRAFT, Ltd., and NORTH, J. D. June 9, 1945, No. 14650. [Class 4] An aircraft fuel tank 4 is carried in the wing section 1 attached to fuselage 3, the outer wing section 2 being hinged to' the inner section 1 so as to be rotatable upwardly to the position shown in order to allow access to the tank. The wing ribs 15 are apertured to receive the tank, which is provided with spigots 16 received in sockets 19 formed in the inner rib 18 ; the outer end of the tank carries a block 28 pivotally connected to a cover-plate attached to end rib 25. Locking bolts for the two wing parts taking into apertured lugs 8, 9 are operated by a telescoping rod mounted in the outer wing part 2.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB14650/45A GB582704A (en) | 1945-06-09 | 1945-06-09 | Improvements in and relating to fuel tank installations in aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB14650/45A GB582704A (en) | 1945-06-09 | 1945-06-09 | Improvements in and relating to fuel tank installations in aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB582704A true GB582704A (en) | 1946-11-25 |
Family
ID=10045068
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB14650/45A Expired GB582704A (en) | 1945-06-09 | 1945-06-09 | Improvements in and relating to fuel tank installations in aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB582704A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4858778A (en) * | 1988-02-18 | 1989-08-22 | Pats, Inc. | Fuel tank |
GB2604139A (en) * | 2021-02-25 | 2022-08-31 | Airbus Operations Ltd | Wingbox with removable fuel tank |
GB2604140A (en) * | 2021-02-25 | 2022-08-31 | Airbus Operations Ltd | Wingbox with fuel tank attached to ribs |
-
1945
- 1945-06-09 GB GB14650/45A patent/GB582704A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4858778A (en) * | 1988-02-18 | 1989-08-22 | Pats, Inc. | Fuel tank |
GB2604139A (en) * | 2021-02-25 | 2022-08-31 | Airbus Operations Ltd | Wingbox with removable fuel tank |
GB2604140A (en) * | 2021-02-25 | 2022-08-31 | Airbus Operations Ltd | Wingbox with fuel tank attached to ribs |
US11834169B2 (en) | 2021-02-25 | 2023-12-05 | Airbus Operations Limited | Wingbox with removable fuel tank |
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