GB714097A - Improvements in flexible tank installations - Google Patents
Improvements in flexible tank installationsInfo
- Publication number
- GB714097A GB714097A GB277652A GB277652A GB714097A GB 714097 A GB714097 A GB 714097A GB 277652 A GB277652 A GB 277652A GB 277652 A GB277652 A GB 277652A GB 714097 A GB714097 A GB 714097A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gaskets
- tanks
- annular
- walls
- rings
- 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
- 238000009434 installation Methods 0.000 title 1
- 239000011324 bead Substances 0.000 abstract 1
- 239000002828 fuel tank Substances 0.000 abstract 1
- 230000004048 modification Effects 0.000 abstract 1
- 238000012986 modification Methods 0.000 abstract 1
- 230000008719 thickening 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
- B64D37/04—Arrangement thereof in or on aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Gasket Seals (AREA)
Abstract
714,097. Pipe connections. FIREPROOF TANKS, Ltd. Jan. 16, 1953 [Feb. 1, 1952], No. 2776/52. Class 99 (1). Annular gaskets 6 which surround apertures in the walls 5 of flexible fuel tanks are pressed against annular abutments by clamping rings 7 connected by a draw-bolt 11, the rings or gaskets being provided with at least one annular rib 8. The outer periphery of each ring 7 may be turned inwardly to engage the edge of the projecting gasket, and the gaskets may be cemented to the walls of the tanks or moulded as local thickenings of the walls. The abutments may comprise flanges 3 formed on a tube 1 projecting into the tanks. In a modification, the ribs 8 of the gaskets comprise annular beads accommodated in grooves formed in the rings 7, Fig. 5 (not shown). Specification 691,622 is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB277652A GB714097A (en) | 1952-02-01 | 1952-02-01 | Improvements in flexible tank installations |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB277652A GB714097A (en) | 1952-02-01 | 1952-02-01 | Improvements in flexible tank installations |
Publications (1)
Publication Number | Publication Date |
---|---|
GB714097A true GB714097A (en) | 1954-08-25 |
Family
ID=9745684
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB277652A Expired GB714097A (en) | 1952-02-01 | 1952-02-01 | Improvements in flexible tank installations |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB714097A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114148531A (en) * | 2021-11-02 | 2022-03-08 | 湖北航天技术研究院总体设计所 | Aircraft dysmorphism oil tank structure |
-
1952
- 1952-02-01 GB GB277652A patent/GB714097A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114148531A (en) * | 2021-11-02 | 2022-03-08 | 湖北航天技术研究院总体设计所 | Aircraft dysmorphism oil tank structure |
CN114148531B (en) * | 2021-11-02 | 2024-03-12 | 湖北航天技术研究院总体设计所 | Aircraft dysmorphism oil tank structure |
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