GB285636A - Improvements in the drive transmission of internal combustion engines for aircraft - Google Patents
Improvements in the drive transmission of internal combustion engines for aircraftInfo
- Publication number
- GB285636A GB285636A GB2854/27A GB285427A GB285636A GB 285636 A GB285636 A GB 285636A GB 2854/27 A GB2854/27 A GB 2854/27A GB 285427 A GB285427 A GB 285427A GB 285636 A GB285636 A GB 285636A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shaft
- bearing
- propeller
- crank
- carried
- 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
- 230000005540 biological transmission Effects 0.000 title 1
- 238000002485 combustion reaction Methods 0.000 title 1
- 239000002131 composite material Substances 0.000 abstract 1
- 230000004048 modification Effects 0.000 abstract 1
- 238000012986 modification Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWERÂ PLANTSÂ OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Gear Transmission (AREA)
Abstract
285,636. Sidwell, F. A. Feb. 1, 1927. Propelling.-In driving gear for the propellers of aircraft using a lay shaft, the propeller shaft 8 is concentric with the crank shaft 2, or an attachment thereto, and a bearing 5 is interposed between the toothed wheel on the propeller shaft and the driving wheel 3 on the crank shaft. A second bearing 4 is provided on the inner end of the crank shaft extension and a second bearing 9 together with a bearing near the propeller carries the propeller shaft. The composite wheels 11, 12 forming the lay shaft are carried by two bearings, one 13 supported on a fixed axle 15, the other 14 carried by the gear casing. The parts 1, 6, 10 of the casing are shaped to form spigots and sockets to allow assemblage. In a modification an extra bearing is supplied for the crank shaft and is placed inside the bearing such as 5 between the crank and propeller shafts. In other arrangements the lay shaft wheels are carried by bearings 41, 42, Fig. 4, supported by the hollow axle 43. The crank shaft is carried by a bearing 31 in the casing and by a spigot 37 received in the hollow propeller shaft. The driven wheel on the propeller shaft is supported by a bearing 38 placed under the toothed periphery or by a bearing 44 surrounding the shaft. Fig. 4 showing both arrangements.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2854/27A GB285636A (en) | 1927-02-01 | 1927-02-01 | Improvements in the drive transmission of internal combustion engines for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2854/27A GB285636A (en) | 1927-02-01 | 1927-02-01 | Improvements in the drive transmission of internal combustion engines for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB285636A true GB285636A (en) | 1928-02-23 |
Family
ID=9747210
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2854/27A Expired GB285636A (en) | 1927-02-01 | 1927-02-01 | Improvements in the drive transmission of internal combustion engines for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB285636A (en) |
-
1927
- 1927-02-01 GB GB2854/27A patent/GB285636A/en not_active Expired
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