GB190915940A - Improvements in Aerial Propellers. - Google Patents
Improvements in Aerial Propellers.Info
- Publication number
- GB190915940A GB190915940A GB190915940DA GB190915940A GB 190915940 A GB190915940 A GB 190915940A GB 190915940D A GB190915940D A GB 190915940DA GB 190915940 A GB190915940 A GB 190915940A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shaft
- propeller
- spindles
- clutches
- blades
- 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
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/006—Paddle wheels
Abstract
15,940. Greenhall, Sir G., Rathmill, J., and Thorley, F. July 8. Propelling.-In a rotary propeller of the kind in which the blades in feathering turn about axes parallel to the propeller shaft, clutches and gearing are provided by which each blade moves parallel to itself during the operative first half of each revolution, and remains stationary on its axis during the inoperative second half of the revolution. The propeller shaft c carries a plate g with spindles h for two toothed wheels i, which are rotated in opposite directions to the shaft c t h r o u g h idle wheels f and a stationary wheel e concentric with the shaft c. The blades a are pivoted on the ends of arms b carried by the shaft c, and are turned or held stationary on their pivots by cranks and connecting-rods from shafts p, according as these shafts are connected with the spindles h by clutches k or are disconnected therefrom. The clutches k are automatically moved into or out of connexion with the spindles h at each halfrevolution of the propeller by a beam n, which is pivoted on the shaft c and is oscillated through links o', o<2> and a bellcrank o from a crank m on the shaft of a toothed wheel gearing with one of the wheels i. The direction of thrust of the propeller may be adjusted by turning the wheel e. The blades a comprise end pieces q connected by adjustable rods or wires r and carrying flexible material s adapted to curve to a radius struck from the propeller axis.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB190915940T | 1909-07-08 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB190915940A true GB190915940A (en) | 1910-07-07 |
Family
ID=32556710
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB190915940D Expired GB190915940A (en) | 1909-07-08 | 1909-07-08 | Improvements in Aerial Propellers. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB190915940A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0213769A1 (en) * | 1985-08-03 | 1987-03-11 | Kabushiki Kaisha Suiden | A ceiling fan |
FR2677952A1 (en) * | 1991-06-24 | 1992-12-24 | Mugnier Georges | Lift and propulsion apparatus using wheels with rotary blades and with active cambering |
-
1909
- 1909-07-08 GB GB190915940D patent/GB190915940A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0213769A1 (en) * | 1985-08-03 | 1987-03-11 | Kabushiki Kaisha Suiden | A ceiling fan |
FR2677952A1 (en) * | 1991-06-24 | 1992-12-24 | Mugnier Georges | Lift and propulsion apparatus using wheels with rotary blades and with active cambering |
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