Hybrid compressor
US10480519B2 · kind B2 · utility
1Cited by
10References
17Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Mar 25, 2016 |
| Grant date | Nov 19, 2019 |
| Priority date | — |
| Expiry date | May 30, 2038 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2220/40
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A compressor for a gas turbine engine is disclosed. The compressor includes a first compression stage mounted for rotation about a central axis that includes a plurality of first-stage blades. The compressor also includes a second compression stage mounted along the central axis aft of the first compression stage to receive air compressed by the first compression stage. The second compression stage includes a plurality of second-stage blades.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.