GB126515A - Improvements in the Attachment of the Aerofoils of Aeroplanes. - Google Patents
Improvements in the Attachment of the Aerofoils of Aeroplanes.Info
- Publication number
- GB126515A GB126515A GB9816/18A GB981618A GB126515A GB 126515 A GB126515 A GB 126515A GB 9816/18 A GB9816/18 A GB 9816/18A GB 981618 A GB981618 A GB 981618A GB 126515 A GB126515 A GB 126515A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pin
- block
- jaws
- aerofoils
- joints
- 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
Abstract
126,515. Nieuport & General Aircraft Co., Folland, H. P., and Preston, H. E. June 14, 1918. Hinges and pivots. - Aerofoils are connected to one another or to the fuselage by two or more joints, each consisting of two pairs of jaws a<1>, b<1>, at right angles to each other; the jaws b' carry a rectangular block c and pin d, and the jaws a'carry a pin e passing through the block c and pin d. The pin may be replaced by two pins on the block c, the jaws b<1> being modified to enable the blocks to be assembled. The pin e is secured by a nut e<2>, and has an elongated head e<1> with screw slot, while a cover plate h may be secured to the aerofoils. The block c and pin d are a close fit, but the block may be made shorter, and the pin longer, to correct any inaccurate placing of the joints. The Provisional Specification states also that the pin e may have a tapered end screwing into the lower jaw a<1>, and may pass through the block clear of the pin d.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9816/18A GB126515A (en) | 1918-06-14 | 1918-06-14 | Improvements in the Attachment of the Aerofoils of Aeroplanes. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9816/18A GB126515A (en) | 1918-06-14 | 1918-06-14 | Improvements in the Attachment of the Aerofoils of Aeroplanes. |
Publications (1)
Publication Number | Publication Date |
---|---|
GB126515A true GB126515A (en) | 1919-05-15 |
Family
ID=32670944
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9816/18A Expired GB126515A (en) | 1918-06-14 | 1918-06-14 | Improvements in the Attachment of the Aerofoils of Aeroplanes. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB126515A (en) |
-
1918
- 1918-06-14 GB GB9816/18A patent/GB126515A/en not_active Expired
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