GB479489A - Tank, in particular for aircraft and motor vehicles - Google Patents
Tank, in particular for aircraft and motor vehiclesInfo
- Publication number
- GB479489A GB479489A GB21528/36A GB2152836A GB479489A GB 479489 A GB479489 A GB 479489A GB 21528/36 A GB21528/36 A GB 21528/36A GB 2152836 A GB2152836 A GB 2152836A GB 479489 A GB479489 A GB 479489A
- Authority
- GB
- United Kingdom
- Prior art keywords
- members
- secured
- shell
- gussets
- girder
- 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
- 230000002787 reinforcement Effects 0.000 abstract 2
- 238000005219 brazing Methods 0.000 abstract 1
- 239000002131 composite material Substances 0.000 abstract 1
- 235000021438 curry Nutrition 0.000 abstract 1
- 238000007689 inspection Methods 0.000 abstract 1
- 239000002184 metal Substances 0.000 abstract 1
- 238000005192 partition Methods 0.000 abstract 1
- 238000005476 soldering Methods 0.000 abstract 1
- 238000003466 welding Methods 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 POWERÂ PLANTSÂ 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)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
479,489. Tanks. AIVAZ, J. Aug. 5, 1936, No. 21528. Convention date, Aug. 5, 1935. [Class 69 (i)] A tank comprises a shell made of a thin metal sheet which is reinforced by means of channel-members 4, Fig. 4, arranged so as to be closed by the shell itself and connected by cross-bracing-members 10. The channelmembers are arranged longitudinally and each have a turned-out flange along each edge and a longitudinal web for their attachment to the shell and the members 10. One end 6 of the tank is held in position by gussets 9 which connect the members thereon to those on the sides and also to a hollow girder 11 which is connected to the other end 7 by spring blades 12, Fig. 6; the latter are secured to a member 4 fixed on the end and curry projections 13, which when the springs are inserted in the girder, are thrust into engagement with apertures in the walls thereof. In another form, Fig. 9, the central girder is replaced by members secured to the first end and the cross-bracing members. The second end is constituted by panels 18; gussets 9 serve to hold in place the end panels between which and the central panel are secured part partitions 19 which are secured to members 4 upon the shell. In all forms the ends and composite panels are flanged and soldered, and the reinforcements, gussets and crossmembers are secured by welding, riveting, soldering or brazing. The channel-members may be built of a plurality of bars and their section may be varied. Further additional obliquely-arranged reinforcements may be provided. The Specification as open to inspection under Sect. 91 comprises also the subjectmatter of Specification 479,498. This subjectmatter does not appear in the Specification as accepted.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR479489X | 1935-08-05 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB479489A true GB479489A (en) | 1938-02-07 |
Family
ID=8903375
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB21528/36A Expired GB479489A (en) | 1935-08-05 | 1936-08-05 | Tank, in particular for aircraft and motor vehicles |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB479489A (en) |
-
1936
- 1936-08-05 GB GB21528/36A patent/GB479489A/en not_active Expired
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