GB611761A - Improvements in or relating to hydraulic reversing gears - Google Patents
Improvements in or relating to hydraulic reversing gearsInfo
- Publication number
- GB611761A GB611761A GB1377446A GB1377446A GB611761A GB 611761 A GB611761 A GB 611761A GB 1377446 A GB1377446 A GB 1377446A GB 1377446 A GB1377446 A GB 1377446A GB 611761 A GB611761 A GB 611761A
- Authority
- GB
- United Kingdom
- Prior art keywords
- casing
- channel
- blades
- hydraulic reversing
- vanes
- 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
- F16H41/00—Rotary fluid gearing of the hydrokinetic type
- F16H41/24—Details
- F16H41/26—Shape of runner blades or channels with respect to function
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
611,761. Hydraulic reversing gear. PEREGRINE, E. P., and PARSONS & MARINE ENGINEERING TURBINE RESEARCH & DEVELOPMENT ASSOCIATION.. May 7, 1946, No. 13774. [Class 69 (ii)] A hydraulic reversing gear comprises a fixed toroidal casing G, B having a ring member D fixed thereto, forming a toroidal channel. Impeller vanes F carried by a casing 2 mounted on a driving shaft 3, projects into the channel and a duct 4 connects the channel to an inlet 5. Pump diffuser vanes 9 receive liquid from the vanes F, the liquid then passing round the toroidal channel in planes containing the axis of the shaft to turbine nozzle blades 10 on the casing B thence to rotor blades 6 mounted on a driven shaft 8 around the driving shaft 3, and back to the impeller blades F. The blades F, 6 are of twisted aerofoil section. Ducts are provided in the casing to discharge liquid for temperature control.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1377446A GB611761A (en) | 1946-05-07 | 1946-05-07 | Improvements in or relating to hydraulic reversing gears |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1377446A GB611761A (en) | 1946-05-07 | 1946-05-07 | Improvements in or relating to hydraulic reversing gears |
Publications (1)
Publication Number | Publication Date |
---|---|
GB611761A true GB611761A (en) | 1948-11-03 |
Family
ID=10029110
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1377446A Expired GB611761A (en) | 1946-05-07 | 1946-05-07 | Improvements in or relating to hydraulic reversing gears |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB611761A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2163114A5 (en) * | 1971-11-26 | 1973-07-20 | Ustav Pro Vyzkum Motorovych Vo |
-
1946
- 1946-05-07 GB GB1377446A patent/GB611761A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2163114A5 (en) * | 1971-11-26 | 1973-07-20 | Ustav Pro Vyzkum Motorovych Vo |
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