GB601236A - Improvements in fuel tanks for airplanes and similar applications - Google Patents
Improvements in fuel tanks for airplanes and similar applicationsInfo
- Publication number
- GB601236A GB601236A GB11574/45A GB1157445A GB601236A GB 601236 A GB601236 A GB 601236A GB 11574/45 A GB11574/45 A GB 11574/45A GB 1157445 A GB1157445 A GB 1157445A GB 601236 A GB601236 A GB 601236A
- Authority
- GB
- United Kingdom
- Prior art keywords
- partitions
- elements
- stiffeners
- welded
- fuel tanks
- 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
- 238000005192 partition Methods 0.000 abstract 7
- 239000003351 stiffener Substances 0.000 abstract 3
- JHIVVAPYMSGYDF-UHFFFAOYSA-N cyclohexanone Chemical compound O=C1CCCCC1 JHIVVAPYMSGYDF-UHFFFAOYSA-N 0.000 abstract 1
- 238000007689 inspection Methods 0.000 abstract 1
- 239000007788 liquid Substances 0.000 abstract 1
- 230000002093 peripheral effect Effects 0.000 abstract 1
- 230000003014 reinforcing effect Effects 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
601,236. Liquid-fuel tanks. SOC. ANON. DES USINES CHAUSSON. May 7, 1945, No. 11574. Convention date, Nov. 7, 1944. [Class 69 (i)] A liquid fuel tank comprises two elements, each having a reinforcing structure formed of partitions 11, 12, 30 transversely spaced to channel-shaped stiffeners 5, 27, the stiffeners and partitions being welded to each other and to the walls of the tank. The partitions are provided with recesses 18 and 31 and lightening holes 20. When the two elements are assembled, the two sets of partitions adjoin each other, the lower partitions carrying securing members 23, each having an internally-threaded member holding a screw which passes through the surface 24 of the upper element to secure the two elements together, the peripheral joint being welded. The Specification as open to inspection under Sect, 91 states also that the channel-shaped stiffeners may be replaced by partitions, and in assembling the two elements a pin may be passed through interlocking hinge portions formed on aligned partitions. This subjectmatter does not appear in the Specification as accepted.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR601236X | 1944-11-07 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB601236A true GB601236A (en) | 1948-04-30 |
Family
ID=8971101
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB11574/45A Expired GB601236A (en) | 1944-11-07 | 1945-05-07 | Improvements in fuel tanks for airplanes and similar applications |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB601236A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7748661B2 (en) | 2005-12-21 | 2010-07-06 | Airbus Uk Limited | Aircraft structure and a fastener for use therewith |
-
1945
- 1945-05-07 GB GB11574/45A patent/GB601236A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7748661B2 (en) | 2005-12-21 | 2010-07-06 | Airbus Uk Limited | Aircraft structure and a fastener for use therewith |
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