Split-torque face gear transmission
AssigneeSikorsky Aircraft Corporation
InventorsYuriy Z. Gmirya, Jules G. Kish
Life of this patent
Estimating the term…
Abstract
A face gear transmission system divides the input torque into multiple kinematic paths. The first kinematic scheme consists of a drive shaft and driven shaft having a plurality of pinions which contact a primary face gear. The second kinematic scheme consists of two independent symmetrical gear paths. One is a first pinion, a first idler and a first idler face gear and the primary face gear. The other independent gear path is a pinion on the second shaft, the idler, and second idler face gear and the primary face gear. The face gear transmission is especially applicable to rotorcraft having one or more input drive shafts to provide a proprotor transmission system which is relatively small in size and light in weight.
Claims8
A face gear transmission comprising:
- an output shaft defining a shaft axis;
- a first face gear coaxially mounted to said output shaft, said face gear having a first set of gear teeth extending from a first surface and a second set of gear teeth extending from a second surface, said first surface opposed from said second surface;
- a first idler face gear coaxially mounted about said shaft axis, said first idler face gear having a third set of gear teeth facing said first set of gear teeth;
- a second idler face gear coaxially mounted about said shaft axis, said second idler face gear having a fourth set of gear teeth facing said second set of gear teeth;
- a first input shaft defining a first input axis;
- a first pinion and a second pinion mounted to said input shaft, said first pinion in contact with both said first set of gear teeth and said third set of gear teeth;
- a second shaft defining a second axis;
- a third pinion and a fourth pinion mounted to said second shaft, said third pinion in contact with both said second set of gear teeth and said fourth set of gear teeth, said fourth pinion in contact with said second pinion;
- a first idler defining a first idler axis, said first idler in contact with both said first set of gear teeth and said third set of gear teeth;
- and
- a second idler defining a second idler axis, said second idler in contact with both said second set of gear teeth and said fourth set of gear teeth.
A helicopter transmission comprising:
- an output shaft defining a shaft axis;
- a first face gear coaxially mounted to said output shaft, said face gear having a first set of gear teeth extending from a first surface and a second set of gear teeth extending from a second surface, said first surface opposed from said second surface;
- a first idler face gear coaxially mounted about said shaft axis, said first idler face gear having a third set of gear teeth facing said first set of gear teeth;
- a second idler face gear coaxially mounted about said shaft axis, said second idler face gear having a fourth set of gear teeth facing said second set of gear teeth;
- a first input shaft defining a first input axis;
- a first pinion and a second pinion mounted to said input shaft, said first pinion in contact with both said first set of gear teeth and said third set of gear teeth;
- a second shaft defining a second axis;
- a third pinion and a fourth pinion mounted to said second shaft, said third pinion in contact with both said second set of gear teeth and said fourth set of gear teeth, said fourth pinion in contact with said second pinion;
- a first idler defining a first idler axis, said first idler in contact with both said first set of gear teeth and said third set of gear teeth;
- and
- a second idler defining a second idler axis, said second idler in contact with both said second set of gear teeth and said fourth set of gear teeth.
Dependencies are inferred from the claim text.