GB125284A - Improvements in Struts for Aircraft. - Google Patents
Improvements in Struts for Aircraft.Info
- Publication number
- GB125284A GB125284A GB1044218A GB1044218A GB125284A GB 125284 A GB125284 A GB 125284A GB 1044218 A GB1044218 A GB 1044218A GB 1044218 A GB1044218 A GB 1044218A GB 125284 A GB125284 A GB 125284A
- Authority
- GB
- United Kingdom
- Prior art keywords
- flanges
- struts
- plate
- members
- aircraft
- 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
- B64C3/18—Spars; Ribs; Stringers
- B64C3/185—Spars
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
Abstract
125,284. Brown, E. E., and Mooney, D. J. June 25, 1918. Framework.-Struts for aeroplanes are formed by two longitudinally corrugated channel members a, Fig. 4, with .side flanges c riveted together and shaped to receive end fittings, the members a being covered to an approximate stream-like section by material h such as sheet-metal, veneer, doped fabric, or three-ply wood. The front flanges may be bent at p and may be secured to a plate d, Fig. 7. Corrugations e may also be formed on the plate d, or on the rear flanges as shown. The end fitting may have a single or double eye or a socket, and may be formed upon a split tube. Two plates d may be used, and may form the bends p and the rear extension from the cover h.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1044218A GB125284A (en) | 1918-06-25 | 1918-06-25 | Improvements in Struts for Aircraft. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1044218A GB125284A (en) | 1918-06-25 | 1918-06-25 | Improvements in Struts for Aircraft. |
Publications (1)
Publication Number | Publication Date |
---|---|
GB125284A true GB125284A (en) | 1919-04-17 |
Family
ID=32344581
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1044218A Expired GB125284A (en) | 1918-06-25 | 1918-06-25 | Improvements in Struts for Aircraft. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB125284A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108248814A (en) * | 2018-01-10 | 2018-07-06 | 中国商用飞机有限责任公司 | Aircraft bird strike resistant front edge and support for aircraft bird strike resistant front edge |
-
1918
- 1918-06-25 GB GB1044218A patent/GB125284A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108248814A (en) * | 2018-01-10 | 2018-07-06 | 中国商用飞机有限责任公司 | Aircraft bird strike resistant front edge and support for aircraft bird strike resistant front edge |
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