GB660430A - Improvements in or relating to reduction gear mechanism - Google Patents
Improvements in or relating to reduction gear mechanismInfo
- Publication number
- GB660430A GB660430A GB15696/49A GB1569649A GB660430A GB 660430 A GB660430 A GB 660430A GB 15696/49 A GB15696/49 A GB 15696/49A GB 1569649 A GB1569649 A GB 1569649A GB 660430 A GB660430 A GB 660430A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wheel
- shaft
- halves
- annulus
- june
- 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
- F16H1/28—Toothed gearings for conveying rotary motion with gears having orbital motion
- F16H1/2809—Toothed gearings for conveying rotary motion with gears having orbital motion with means for equalising the distribution of load on the planet gears
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Retarders (AREA)
Abstract
660,430. Toothed gearing. SOC. DE CONSTRUCTIONS ET D'EQUIPEMENTS MECANIQUES POUR L'AVIATION S.O.C.E.M.A. June 13, 1949 [June 12, 1948], No. 15696/49. Class 80 (i) Epicyclic reduction gearing applicable to the drive of an aircraft propeller includes means for individual angular adjustment of each planetary gear 8. A double helical sun wheel 1 mounted on the driving shaft 2 meshes with planetary wheels each comprising two helical halves 3, 4. The two wheel halves are secured to each other and to a shoulder therebetween on the shaft 6 by resiliently mounted axial bolts 7, with the interposition of distance washers 5 so that the wheel halves are relatively axially adjustable. Keyed to each shaft 6 is an axially adjustable spur wheel 8 meshing with an annulus 9 secured to a casing 10 by means of resiliently mounted bolts 11. Axial adjustment of the wheel halves 3, 4 effects angular adjustment of the shaft 6 to bring each gear wheel 8 into correct meshing engagement with the annulus 9.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR660430X | 1948-06-12 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB660430A true GB660430A (en) | 1951-11-07 |
Family
ID=9010263
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB15696/49A Expired GB660430A (en) | 1948-06-12 | 1949-06-13 | Improvements in or relating to reduction gear mechanism |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB660430A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5472386A (en) * | 1994-05-26 | 1995-12-05 | United Technologies Corporation | Stacked compound planetary gear train for an upgraded powertrain system for a helicopter |
-
1949
- 1949-06-13 GB GB15696/49A patent/GB660430A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5472386A (en) * | 1994-05-26 | 1995-12-05 | United Technologies Corporation | Stacked compound planetary gear train for an upgraded powertrain system for a helicopter |
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