GB137642A - Improvements in the transmission of power - Google Patents
Improvements in the transmission of powerInfo
- Publication number
- GB137642A GB137642A GB371619A GB371619A GB137642A GB 137642 A GB137642 A GB 137642A GB 371619 A GB371619 A GB 371619A GB 371619 A GB371619 A GB 371619A GB 137642 A GB137642 A GB 137642A
- Authority
- GB
- United Kingdom
- Prior art keywords
- engine
- helical
- gearing
- propeller shaft
- wheels
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H1/00—Toothed gearings for conveying rotary motion
- F16H1/02—Toothed gearings for conveying rotary motion without gears having orbital motion
- F16H1/20—Toothed gearings for conveying rotary motion without gears having orbital motion involving more than two intermeshing members
- F16H1/22—Toothed gearings for conveying rotary motion without gears having orbital motion involving more than two intermeshing members with a plurality of driving or driven shafts; with arrangements for dividing torque between two or more intermediate shafts
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Motor Power Transmission Devices (AREA)
Abstract
137,642. Thomas, G. H., and Wilkinson, G. S. Feb. 14, 1919, Motor power plant.-Two internal-combustion engines driving an aircraft propeller are connected to the propeller shaft through helical gearing, in each case with a member capable of sliding under the end thrust of the gearing but normally balanced; if either engine fails to develop a certain minimum of power, the corresponding member slides out of engagement, and the engine ceases to drive. The propeller shaft A carries a sliding hub C with helical wheels C<1>, C<2> gearing with helical wheels D<1>, D<2> on the separate engine shafts. An adjustable resistance to determine the maximum permissible variation is provided by spring buffers F<1>, F<2> and a stirrup-lever E. Notches h<1>, h<2> may be arranged to coact with a spring catch and retain either engine out of action. To prevent damage through the breaking of a tooth, the pairs of helical elements are separated by a partition J.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB371619A GB137642A (en) | 1919-02-14 | 1919-02-14 | Improvements in the transmission of power |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB371619A GB137642A (en) | 1919-02-14 | 1919-02-14 | Improvements in the transmission of power |
Publications (1)
Publication Number | Publication Date |
---|---|
GB137642A true GB137642A (en) | 1920-01-22 |
Family
ID=9763602
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB371619A Expired GB137642A (en) | 1919-02-14 | 1919-02-14 | Improvements in the transmission of power |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB137642A (en) |
-
1919
- 1919-02-14 GB GB371619A patent/GB137642A/en not_active Expired
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