GB518178A - Improvements in or relating to aircraft wing construction - Google Patents
Improvements in or relating to aircraft wing constructionInfo
- Publication number
- GB518178A GB518178A GB24178/38A GB2417838A GB518178A GB 518178 A GB518178 A GB 518178A GB 24178/38 A GB24178/38 A GB 24178/38A GB 2417838 A GB2417838 A GB 2417838A GB 518178 A GB518178 A GB 518178A
- Authority
- GB
- United Kingdom
- Prior art keywords
- members
- secured
- intervals
- metal
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Connection Of Plates (AREA)
Abstract
518,178. Aircraft wings. AEROPLASTICS, Ltd. (formerly DEEKAY AIRCRAFT CORPORATION, Ltd.), and STILL, S. C. HART-. Aug. 16, 1938, No. 24178. Addition to 497,623. [Class 4] Aircraft wings as claimed in the parent Specification have the cells divided from one another by a metal box spar or by thin sheet or plate metal members instead of by plates of moulded thermo plastic material. Fig. 2 shows a wing formed with upper and lower stressed members 3 of thermo-hardening plastic material' connected by screws 6, Fig. 5, to semicircular members 5 secured to flanges 4 on metal plate members 2 extending along the span of the wing. Ribs 10 are formed on the members 3 at intermediate positions and fore-and-aft partitions are provided at intervals. The plates 2 are reinforced at intervals. In an alternative construction the members 3 are secured to a single box girder structure.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB24178/38A GB518178A (en) | 1938-08-16 | 1938-08-16 | Improvements in or relating to aircraft wing construction |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB24178/38A GB518178A (en) | 1938-08-16 | 1938-08-16 | Improvements in or relating to aircraft wing construction |
Publications (1)
Publication Number | Publication Date |
---|---|
GB518178A true GB518178A (en) | 1940-02-20 |
Family
ID=10207640
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB24178/38A Expired GB518178A (en) | 1938-08-16 | 1938-08-16 | Improvements in or relating to aircraft wing construction |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB518178A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2202603A (en) * | 1987-03-19 | 1988-09-28 | Sharp Kk | Support structure |
-
1938
- 1938-08-16 GB GB24178/38A patent/GB518178A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2202603A (en) * | 1987-03-19 | 1988-09-28 | Sharp Kk | Support structure |
US4888460A (en) * | 1987-03-19 | 1989-12-19 | Sharp Kabushiki Kaisha | Fixing structure for components of a cooking appliance |
GB2202603B (en) * | 1987-03-19 | 1990-11-14 | Sharp Kk | Appliance |
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