GB191224096A - Improvements in and relating to Driving Mechanism for Aeroplanes. - Google Patents
Improvements in and relating to Driving Mechanism for Aeroplanes.Info
- Publication number
- GB191224096A GB191224096A GB191224096DA GB191224096A GB 191224096 A GB191224096 A GB 191224096A GB 191224096D A GB191224096D A GB 191224096DA GB 191224096 A GB191224096 A GB 191224096A
- Authority
- GB
- United Kingdom
- Prior art keywords
- motors
- gear
- driven
- aeroplanes
- relating
- 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
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
- B64D35/08—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions characterised by the transmission being driven by a plurality of power plants
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
Abstract
24,096. Lohner & Co., J. Dec. 2, 1911, [Convention date]. Motor power plant.-Where the propelling unit of an aeroplane (propeller, flapping wings, &c.) is driven by two or more motors a speedreducing gear is introduced between the motors and the propelling-unit so that the latter may be driven at a slower speed when one or more motors break down. The change-speed gear may be arranged partly on the common motordriven shaft 6 and partly on the propeller shaft 9. The reducing-gear 12, 13 is thrown in by a lever 14 and rod 15. The exhaust valves of any motor are opened when it stops working, and the cocks of the two motors may be interconnected.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT191224096X | 1911-12-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB191224096A true GB191224096A (en) | 1913-08-07 |
Family
ID=32513082
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB191224096D Expired GB191224096A (en) | 1911-12-02 | 1911-12-02 | Improvements in and relating to Driving Mechanism for Aeroplanes. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB191224096A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2947014A1 (en) * | 2014-05-23 | 2015-11-25 | Robby Moto Engineering S.r.l. | Propulsion device for helicopters |
-
1911
- 1911-12-02 GB GB191224096D patent/GB191224096A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2947014A1 (en) * | 2014-05-23 | 2015-11-25 | Robby Moto Engineering S.r.l. | Propulsion device for helicopters |
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