GB706139A - Improvements in continuous, automatically regulating gears - Google Patents
Improvements in continuous, automatically regulating gearsInfo
- Publication number
- GB706139A GB706139A GB23117/51A GB2311751A GB706139A GB 706139 A GB706139 A GB 706139A GB 23117/51 A GB23117/51 A GB 23117/51A GB 2311751 A GB2311751 A GB 2311751A GB 706139 A GB706139 A GB 706139A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shaft
- annulus
- rigid
- impeller
- carrier
- 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
- F16H47/00—Combinations of mechanical gearing with fluid clutches or fluid gearing
- F16H47/06—Combinations of mechanical gearing with fluid clutches or fluid gearing the fluid gearing being of the hydrokinetic type
- F16H47/08—Combinations of mechanical gearing with fluid clutches or fluid gearing the fluid gearing being of the hydrokinetic type the mechanical gearing being of the type with members having orbital motion
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Details Of Gearings (AREA)
Abstract
706,139. Variable-speed gearing. WEINRICH, H. Oct. 4,1951 [Oct. 7, 1950], No. 23117/51. Class 80 (2) In automatically-variable fluid-mechanical gearing, the input member of an epicyclic train is rigid with the driving shaft 1, the output member is rigid with the driven 'shaft 12, the intermediate member is rigid with the impeller 8 of a fluid clutch, and the turbine member 10 is so geared to shaft 12 that the impeller 8 and turbine 10 rotate in opposite directions, the turbine blades being located at the inner periphery of the fluid space. As shown in Fig. 5, the sun 6 is rigid with shaft 1, the carrier 2 with shaft 12, and the annulus 5 with impeller 8, while turbine 10 is geared through planets 14, carried by shaft 12, with fixed annulus 16. Alternatively, however, the annulus 5 may be rigid with shaft 1 and the sun 6 rigid with impeller 8, or carrier 2 may be rigid with shaft 1, annulus 5 with shaft 12, and sun 6 with impeller 8, in which case turbine 10 is geared to annulus 5, through reversing idlers and the shafts 1, 12 are both at the same side of the gear. In Fig. 6, provision is made for reversal of shaft 12, the carrier 18 of planets 14 and the annulus 16 being freely rotatable and adapted to be moved axially in opposite directions through levers 39, 41 under the control of a double cam 37. In the forward - running position shown, annulus 16 is at the left, where it is coupled by teeth 36 to the fixed casing 9, and carrier 18 is at the right, where it is coupled by teeth 33 to a flange 35 of shaft 12. For reverse drive, annulus 16 is moved to the right, so that it is coupled by teeth 40 to flange 25, and carrier 18 to the left, so that it is coupled by teeth 45 to casing 9. An oil pump, driven by shaft 1, may supply oil through bores in the shafts to the bearings and gears and to the clutch. Radial vanes may be formed at 26, Fig. 5, on the hub of the impeller 8 to force oil outwards and prevent cavitation. In Fig. 5, however, air is used as the clutch fluid instead of oil, and this air is continuously renewed, so as to promote cooling, the air escaping through ports 27 at regions of high pressure and entering through ports 32 at regions of low pressure.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE706139X | 1950-10-07 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB706139A true GB706139A (en) | 1954-03-24 |
Family
ID=6617089
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB23117/51A Expired GB706139A (en) | 1950-10-07 | 1951-10-04 | Improvements in continuous, automatically regulating gears |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB706139A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106687665A (en) * | 2014-09-05 | 2017-05-17 | 赛峰飞机发动机公司 | Mechanism for driving members for adjusting the orientation of blades |
-
1951
- 1951-10-04 GB GB23117/51A patent/GB706139A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106687665A (en) * | 2014-09-05 | 2017-05-17 | 赛峰飞机发动机公司 | Mechanism for driving members for adjusting the orientation of blades |
CN106687665B (en) * | 2014-09-05 | 2019-06-14 | 赛峰飞机发动机公司 | Drive the mechanism of the component for adjusting blade orientation |
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