GB519061A - Improvements in or relating to structural elements and parts of aircraft - Google Patents
Improvements in or relating to structural elements and parts of aircraftInfo
- Publication number
- GB519061A GB519061A GB15668/38A GB1566838A GB519061A GB 519061 A GB519061 A GB 519061A GB 15668/38 A GB15668/38 A GB 15668/38A GB 1566838 A GB1566838 A GB 1566838A GB 519061 A GB519061 A GB 519061A
- Authority
- GB
- United Kingdom
- Prior art keywords
- corrugated sheet
- aircraft
- relating
- parts
- structural elements
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Veneer Processing And Manufacture Of Plywood (AREA)
Abstract
519,061. Plywood. JABLONSKY, E. May 25, 1938, No. 15668. [Class 145 (ii)] [Also in Group XXXIII] A structural element comprising plane sheets 7, 8 and a corrugated sheet 9 is composed of laminated wood sheets, secured together by adhesive and shaped and densified under high pressure to a density of 0À9 or more. Alternatively, one plane and one corrugated sheet may be used, or the corrugated sheet may have angular bends, or may be replaced' by channel members facing alternately in opposite directions. Specification 493,145 is referred to. Reference has been directed by the Comptroller to Specification 493,145, [Group XXXIII].
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB15668/38A GB519061A (en) | 1938-05-25 | 1938-05-25 | Improvements in or relating to structural elements and parts of aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB15668/38A GB519061A (en) | 1938-05-25 | 1938-05-25 | Improvements in or relating to structural elements and parts of aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB519061A true GB519061A (en) | 1940-03-15 |
Family
ID=10063276
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB15668/38A Expired GB519061A (en) | 1938-05-25 | 1938-05-25 | Improvements in or relating to structural elements and parts of aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB519061A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2482798A (en) * | 1946-02-27 | 1949-09-27 | Jr George B Rheinfrank | Aircraft wing and method of manufacture |
| US2540482A (en) * | 1946-10-01 | 1951-02-06 | Hervey Foundation Inc | Wooden structure and method |
| US2563218A (en) * | 1948-04-09 | 1951-08-07 | United Aircraft Corp | Laminated airfoil section and method of making same |
| US2645435A (en) * | 1947-04-09 | 1953-07-14 | Gen Mecanique Appliquee Soc In | Structure for conveying a fluid at high temperature |
-
1938
- 1938-05-25 GB GB15668/38A patent/GB519061A/en not_active Expired
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2482798A (en) * | 1946-02-27 | 1949-09-27 | Jr George B Rheinfrank | Aircraft wing and method of manufacture |
| US2540482A (en) * | 1946-10-01 | 1951-02-06 | Hervey Foundation Inc | Wooden structure and method |
| US2645435A (en) * | 1947-04-09 | 1953-07-14 | Gen Mecanique Appliquee Soc In | Structure for conveying a fluid at high temperature |
| US2563218A (en) * | 1948-04-09 | 1951-08-07 | United Aircraft Corp | Laminated airfoil section and method of making same |
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