GB481406A - Improvements in fuel tanks for airplanes - Google Patents
Improvements in fuel tanks for airplanesInfo
- Publication number
- GB481406A GB481406A GB21141/37A GB2114137A GB481406A GB 481406 A GB481406 A GB 481406A GB 21141/37 A GB21141/37 A GB 21141/37A GB 2114137 A GB2114137 A GB 2114137A GB 481406 A GB481406 A GB 481406A
- Authority
- GB
- United Kingdom
- Prior art keywords
- partition
- wall
- airplanes
- fuel tanks
- secured
- 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; ARRANGEMENTS 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
- B64D37/08—Internal partitioning
Abstract
481,406. Tanks. BREEZE CORPORATION, Inc. July 30, 1937, No. 21141. Convention date, Feb. 8. [Class 69 (i)] A fuel tank, particularly for aeroplanes, having a partition C secured at its edges to the wall A, is provided with a passage for the liquid past the partition, formed by a plate 5 secured to the outside of the wall and covering apertures 4 in the wall on each side of the partition. The partition and wall are shown connected by an interengaging bent rib and flange as described in Specification 481,329.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US481406XA | 1937-02-08 | 1937-02-08 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB481406A true GB481406A (en) | 1938-03-10 |
Family
ID=21952944
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB21141/37A Expired GB481406A (en) | 1937-02-08 | 1937-07-30 | Improvements in fuel tanks for airplanes |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB481406A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111976999A (en) * | 2020-07-06 | 2020-11-24 | 西安飞机工业(集团)有限责任公司 | Vibration reduction method for airplane soft oil tank |
CN115636094A (en) * | 2022-12-23 | 2023-01-24 | 西安远飞航空技术发展有限公司 | Connecting structure of skin and partition plate, manufacturing method of connecting structure and aircraft oil tank |
-
1937
- 1937-07-30 GB GB21141/37A patent/GB481406A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111976999A (en) * | 2020-07-06 | 2020-11-24 | 西安飞机工业(集团)有限责任公司 | Vibration reduction method for airplane soft oil tank |
CN111976999B (en) * | 2020-07-06 | 2022-08-09 | 西安飞机工业(集团)有限责任公司 | Vibration reduction method for airplane soft oil tank |
CN115636094A (en) * | 2022-12-23 | 2023-01-24 | 西安远飞航空技术发展有限公司 | Connecting structure of skin and partition plate, manufacturing method of connecting structure and aircraft oil tank |
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