GB558313A - Improvements in securing metallic skins to aircraft structures - Google Patents
Improvements in securing metallic skins to aircraft structuresInfo
- Publication number
- GB558313A GB558313A GB13619/42A GB1361942A GB558313A GB 558313 A GB558313 A GB 558313A GB 13619/42 A GB13619/42 A GB 13619/42A GB 1361942 A GB1361942 A GB 1361942A GB 558313 A GB558313 A GB 558313A
- Authority
- GB
- United Kingdom
- Prior art keywords
- per cent
- rubber
- sheets
- skin
- plates
- 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
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
Abstract
558,313. Aircraft. UNITED STATES RUBBER CO. Sept. 28, 1942, No. 13619. Convention date, Dec. 31, 1941. [Class 4] The metal skin of an aircraft wing, fuselage or flooring is secured to the framework by interposing a layer of rubber composition and bonding it to the skin and framework by vulcanizing. A wing is described in which ribbed aluminium or aluminium alloy plates 7 are secured to flanges 9 of ribs 8 so as to present large areas of contact with sheets 11 of rubber composition interposed between the plates 7 and outer skin 10. The plates 7 and skin 10 in contact with the sheets 11 are previously coated with an adhesive known under the Registered Trade Mark "Ty-ply" comprising essentially a rubber hydrochloride, dibutyl pthalate and sulphur. The sheets 11 are of uncured rubber composition such as one containing 36.44 per cent rubber, 54 per cent carbon black, 3 per cent zinc oxide, 4.75 per cent softener, 0.37 per cent accelerator, 0.25 per cent antioxidant and 1.19 per cent sulphur. The sheets are 0.001 to 0.05 of an inch thick. The parts are placed in a moulding press and the layers subjected to vulcanisation. Xylene may be used for softening the 'Ty-ply" if it has become too dry. Neoprene or other synthetic rubber may be used instead of natural rubber.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US558313XA | 1941-12-31 | 1941-12-31 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB558313A true GB558313A (en) | 1943-12-30 |
Family
ID=22000433
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB13619/42A Expired GB558313A (en) | 1941-12-31 | 1942-09-28 | Improvements in securing metallic skins to aircraft structures |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB558313A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2742247A (en) * | 1950-10-31 | 1956-04-17 | Handley Page Ltd | Outer surfaces for craft moving in one fluid |
-
1942
- 1942-09-28 GB GB13619/42A patent/GB558313A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2742247A (en) * | 1950-10-31 | 1956-04-17 | Handley Page Ltd | Outer surfaces for craft moving in one fluid |
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