GB192552A - Improvements in joints for structural and other members, suitable for aircraft and other purposes - Google Patents
Improvements in joints for structural and other members, suitable for aircraft and other purposesInfo
- Publication number
- GB192552A GB192552A GB3334021A GB3334021A GB192552A GB 192552 A GB192552 A GB 192552A GB 3334021 A GB3334021 A GB 3334021A GB 3334021 A GB3334021 A GB 3334021A GB 192552 A GB192552 A GB 192552A
- Authority
- GB
- United Kingdom
- Prior art keywords
- members
- structural
- aircraft
- joints
- purposes
- 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
- B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Connection Of Plates (AREA)
Abstract
192,552. Smith, H. T. W. Dec. 12, 1921. Rod couplings.-Structural and other members such as spars for aeroplanes are joined end to end by fish plates 7, 8, which are secured at one end to each spar end and have elongated openings at the other ends adapted to overlap. Circular members 16 with internal wedged or coned surfaces are adapted to fit these openings and to be secured therein by a corresponding member 17 and bolt 19 passing through end grooves in the spars. Fish plates may be used at both top and bottom of the joint. The members 16 may also be formed with stepped shoulders to increase the range of adjustment.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3334021A GB192552A (en) | 1921-12-12 | 1921-12-12 | Improvements in joints for structural and other members, suitable for aircraft and other purposes |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3334021A GB192552A (en) | 1921-12-12 | 1921-12-12 | Improvements in joints for structural and other members, suitable for aircraft and other purposes |
Publications (1)
Publication Number | Publication Date |
---|---|
GB192552A true GB192552A (en) | 1923-02-08 |
Family
ID=10351688
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3334021A Expired GB192552A (en) | 1921-12-12 | 1921-12-12 | Improvements in joints for structural and other members, suitable for aircraft and other purposes |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB192552A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3285633A (en) * | 1963-10-30 | 1966-11-15 | Dow Chemical Co | Fastener |
-
1921
- 1921-12-12 GB GB3334021A patent/GB192552A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3285633A (en) * | 1963-10-30 | 1966-11-15 | Dow Chemical Co | Fastener |
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