GB128770A - Improved Construction of Wings, Aerofoils and the like for Aeronautical Machines. - Google Patents
Improved Construction of Wings, Aerofoils and the like for Aeronautical Machines.Info
- Publication number
- GB128770A GB128770A GB11666/18A GB1166618A GB128770A GB 128770 A GB128770 A GB 128770A GB 11666/18 A GB11666/18 A GB 11666/18A GB 1166618 A GB1166618 A GB 1166618A GB 128770 A GB128770 A GB 128770A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ribs
- spars
- plates
- secured
- aerofoils
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
128,770. Mayrow, J. J. July 16, 1918. Framework; planes, arrangement and construction of. - The framework of wings, aerofoils, &c. is composed of obliquelyarranged ribs and connected spars forming a series of triangles. The spars are parallel, or nearly so, with the front edge of the wing, and the ribs and spars are secured together by plates 10, Fig. 13, at their crossing or meeting points and have front, rear, and side edge connexions, internal wiring being dispensed with. The ribs may be made from short lengths, Figs. 1 and 2, joined together, the meeting ends 8 being bent and shaped, and the ribs also having recesses 7 for the channel spars. The ribs may be V-shaped with centre portions riveted together, and may consist of channels 20, Fig. 27, and angle-irons 21 with distance-pieces 22, the spars in this case consisting cf U-members 18 and oblique distancepieces 19. The spars may also consist of channelled metal, Fig. 15, apertured at 15 for lightness and at 16 to receive the ribs, and provided with strengthening-plates 17. Stretchers or supports of tape or metal are provided for the fabric at the open parts between the ribs and spars. Attachment to the struts is provided by the plate 25, Fig. 9, formed to fit and secured to the ribs, spars, and rods, the plate also transmitting stresses. Plates 13, Fig. 11, are secured to the aileron and to the wing, and connected by a transverse pin acting as a hinge-pin.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB11666/18A GB128770A (en) | 1918-07-16 | 1918-07-16 | Improved Construction of Wings, Aerofoils and the like for Aeronautical Machines. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB11666/18A GB128770A (en) | 1918-07-16 | 1918-07-16 | Improved Construction of Wings, Aerofoils and the like for Aeronautical Machines. |
Publications (1)
Publication Number | Publication Date |
---|---|
GB128770A true GB128770A (en) | 1919-07-03 |
Family
ID=32408517
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB11666/18A Expired GB128770A (en) | 1918-07-16 | 1918-07-16 | Improved Construction of Wings, Aerofoils and the like for Aeronautical Machines. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB128770A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114104261A (en) * | 2022-01-24 | 2022-03-01 | 中国空气动力研究与发展中心空天技术研究所 | Wing beam of composite wing aircraft |
-
1918
- 1918-07-16 GB GB11666/18A patent/GB128770A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114104261A (en) * | 2022-01-24 | 2022-03-01 | 中国空气动力研究与发展中心空天技术研究所 | Wing beam of composite wing aircraft |
CN114104261B (en) * | 2022-01-24 | 2022-04-12 | 中国空气动力研究与发展中心空天技术研究所 | Wing beam of composite wing aircraft |
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