Low pressure turbine rotor suspension in a twin hub turbo-engine
US5074109A · kind A · utility
59Cited by
5References
3Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Mar 20, 1990 |
| Grant date | Dec 24, 1991 |
| Priority date | — |
| Expiry date | Mar 20, 2010 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF02C7/06
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
The suspension of the rotor of the low pressure turbine of a twin hub turbo-engine includes a cylindrical support arranged coaxially with the axis of the turbine and firmly attached to the stator by radial spacers at the rear of the turbine, the rotor being carried on a front bearing and a rear bearing both mounted on the cylindrical support.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.