GB131019A - Improvements in Metal Spars, Girders, Longerons and like Structural Members of Aircraft. - Google Patents
Improvements in Metal Spars, Girders, Longerons and like Structural Members of Aircraft.Info
- Publication number
- GB131019A GB131019A GB501218A GB501218A GB131019A GB 131019 A GB131019 A GB 131019A GB 501218 A GB501218 A GB 501218A GB 501218 A GB501218 A GB 501218A GB 131019 A GB131019 A GB 131019A
- Authority
- GB
- United Kingdom
- Prior art keywords
- flanges
- members
- channel
- longerons
- girders
- 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)
- Rod-Shaped Construction Members (AREA)
Abstract
131,019. Mooney, D. J. March 21, 1918. Framework.-Spars, girders, longerons, and like structural members of aircraft are formed from a pair of thin metal channel members having four-sided flanges. The channel members may be arranged in contact as shown in Fig. 7 and stiffened by tubes or channel-pieces i, or the members may be separated by wood or metal distance-pieces. In the construction shown in Fig. 17, the channel members are reversed, the flanges being secured to a box-like distance-member k. The web portions are pierced to reduce weight, and the flanges may be connected by strips longitudinally corrugated or of channel form. Longitudinal stiffening-pieces may be arranged diagonally in the flanges. Specification 8522/12 is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB501218A GB131019A (en) | 1918-03-21 | 1918-03-21 | Improvements in Metal Spars, Girders, Longerons and like Structural Members of Aircraft. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB501218A GB131019A (en) | 1918-03-21 | 1918-03-21 | Improvements in Metal Spars, Girders, Longerons and like Structural Members of Aircraft. |
Publications (1)
Publication Number | Publication Date |
---|---|
GB131019A true GB131019A (en) | 1919-08-21 |
Family
ID=32407694
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB501218A Expired GB131019A (en) | 1918-03-21 | 1918-03-21 | Improvements in Metal Spars, Girders, Longerons and like Structural Members of Aircraft. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB131019A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2828121A (en) * | 1953-01-07 | 1958-03-25 | Edwin H Suess | Pry board for grain doors |
US3131791A (en) * | 1959-05-18 | 1964-05-05 | Davisbilt Steel Joist Inc | Metal joist |
US3190410A (en) * | 1961-03-10 | 1965-06-22 | Malcus Holmquist Ab | Box girders |
EP3623278A1 (en) * | 2018-09-14 | 2020-03-18 | The Boeing Company | Monolithic spar for a wing |
-
1918
- 1918-03-21 GB GB501218A patent/GB131019A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2828121A (en) * | 1953-01-07 | 1958-03-25 | Edwin H Suess | Pry board for grain doors |
US3131791A (en) * | 1959-05-18 | 1964-05-05 | Davisbilt Steel Joist Inc | Metal joist |
US3190410A (en) * | 1961-03-10 | 1965-06-22 | Malcus Holmquist Ab | Box girders |
EP3623278A1 (en) * | 2018-09-14 | 2020-03-18 | The Boeing Company | Monolithic spar for a wing |
CN110901887A (en) * | 2018-09-14 | 2020-03-24 | 波音公司 | Integral spar for a wing |
US11192623B2 (en) | 2018-09-14 | 2021-12-07 | The Boeing Company | Monolithic spar for a wing |
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