GB481058A - A new or improved method of covering aircraft wings surfaces and bodies - Google Patents
A new or improved method of covering aircraft wings surfaces and bodiesInfo
- Publication number
- GB481058A GB481058A GB1088937A GB1088937A GB481058A GB 481058 A GB481058 A GB 481058A GB 1088937 A GB1088937 A GB 1088937A GB 1088937 A GB1088937 A GB 1088937A GB 481058 A GB481058 A GB 481058A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fabric
- flat
- covering
- bodies
- trailing
- 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
- 239000004744 fabric Substances 0.000 abstract 4
- 239000002184 metal Substances 0.000 abstract 2
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)
- Treatment Of Fiber Materials (AREA)
Abstract
481,058. Covering aircraft structures. SHORT BROS. (ROCHESTER & BEDFORD), Ltd., and SHEPHERD, P. April 16, 1937, No. 10889. [Class 4] In aircraft wings or other aircraft bodies wherein the leading portion is covered with metal and the trailing portion is covered with fabric, the trailing edge of the leading portion a, Fig. 3, is joggled inwardly at a<1> to form a flat a<2> in which thread holes are formed, provided, if desired, with eyelets a<5>, and a clamping member b is provided having edges adapted to press against the flat a<2>, the clamping strip also having thread holes to correspond with those in flat a<2>, the leading edge of the fabric c covering the trailing part being lapped around the clamping member b and attached by stitching to both band a<2>. A strip of fabric d is clamped between b and a<2>, is bent forwardly during the stitching operation and is then turned back and secured by doping. The depression at the joint between metal and fabric may be filled with dope or other composition.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1088937A GB481058A (en) | 1937-04-16 | 1937-04-16 | A new or improved method of covering aircraft wings surfaces and bodies |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1088937A GB481058A (en) | 1937-04-16 | 1937-04-16 | A new or improved method of covering aircraft wings surfaces and bodies |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB481058A true GB481058A (en) | 1938-03-04 |
Family
ID=9976180
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1088937A Expired GB481058A (en) | 1937-04-16 | 1937-04-16 | A new or improved method of covering aircraft wings surfaces and bodies |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB481058A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9896339B2 (en) | 2014-10-17 | 2018-02-20 | Sabic Global Technologies B.V. | Carbon monoxide production from carbon dioxide reduction by elemental sulfur |
-
1937
- 1937-04-16 GB GB1088937A patent/GB481058A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9896339B2 (en) | 2014-10-17 | 2018-02-20 | Sabic Global Technologies B.V. | Carbon monoxide production from carbon dioxide reduction by elemental sulfur |
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