GB190912204A - Improvements in or relating to the Propulsion of Vehicles, Cycles, Ships and the like. - Google Patents
Improvements in or relating to the Propulsion of Vehicles, Cycles, Ships and the like.Info
- Publication number
- GB190912204A GB190912204A GB190912204DA GB190912204A GB 190912204 A GB190912204 A GB 190912204A GB 190912204D A GB190912204D A GB 190912204DA GB 190912204 A GB190912204 A GB 190912204A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aeroplane
- lever
- mast
- springs
- plane
- 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
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/42—Adjusting about chordwise axes
Abstract
12,204. Gaunt, J. May 24. [Addition to 17,014/08.] Sails.-In a device of the type described in the parent Specification, in which an inverted V-shaped aeroplane, mounted on a mast, is used to support part of the weight of a cycle &c. while travelling, the aeroplane is made collapsible and is connected to a lever pivoted to the mast-head by which the aeroplane is adjusted. The aeroplane is formed of two roofplanes 1, 2, Fig. 1, and two floor-planes 3, 4, which are hinged to one another at c<1>, c<2>, c<3>, c'. The side hinges c<3>, c<4> are connected by springs U, and the upper and lower hinges are connected by detachable rods S. The front part of the plane is mounted in a trough 0, Fig. 3, which is pivoted at N to a lever G. Cords A, B connect the front and rear of the plane to the arms Q, D of the lever G, and springs R connect the sides of the plane to the arm D. The lever G is pivoted at K to the mast 5, and is adjusted by a thumb-screw M to vary the inclination of the aeroplane. The cords A, B restrict the veering movement of the aeroplane; the springs R allow the aeroplane to rock slightly in the trough O.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB190817014T | 1908-08-13 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB190912204A true GB190912204A (en) | 1910-05-24 |
Family
ID=32552877
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB190817014D Expired GB190817014A (en) | 1908-08-13 | 1908-08-13 | Improvements in or relating to the Propulsion of Vehicles, Cycles, and Ships. |
GB190912204D Expired GB190912204A (en) | 1908-08-13 | 1909-05-24 | Improvements in or relating to the Propulsion of Vehicles, Cycles, Ships and the like. |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB190817014D Expired GB190817014A (en) | 1908-08-13 | 1908-08-13 | Improvements in or relating to the Propulsion of Vehicles, Cycles, and Ships. |
Country Status (1)
Country | Link |
---|---|
GB (2) | GB190817014A (en) |
-
1908
- 1908-08-13 GB GB190817014D patent/GB190817014A/en not_active Expired
-
1909
- 1909-05-24 GB GB190912204D patent/GB190912204A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB190817014A (en) | 1909-07-29 |
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