Integration of aerodynamic, thrust bearing and seal running surface
US9261103B1 · kind B1 · utility
0Cited by
15References
30Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | May 18, 2015 |
| Grant date | Feb 16, 2016 |
| Priority date | — |
| Expiry date | May 18, 2035 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF16C2360/24
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A number of variations may include a product for use with a turbocharger system may include a housing with a rotor wheel rotatable relative to the housing. The rotor wheel may have a front face with blades disposed in a gas stream and a back wall facing the housing. The rotor wheel may generate thrust loads. A thrust bearing may be positioned on the housing and may face the back wall. The thrust bearing may be configured to directly absorb the thrust loads from the rotor wheel.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.