Gas turbine engine with multiple load outputs
US8853878B1 · kind B1 · utility
22Cited by
7References
20Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | May 14, 2013 |
| Grant date | Oct 7, 2014 |
| Priority date | — |
| Expiry date | May 14, 2033 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02E20/14
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A gas turbine engine includes a compressor, a combustor, a turbine, a power turbine shaft, and a gas producer shaft. The compressor includes a compressor rotor assembly including a plurality of compressor disk assemblies. The turbine includes a turbine rotor assembly including a power turbine section and a gas producer section. The power turbine shaft is coupled to the power turbine section and is configured to couple to a first driven apparatus. The gas producer shaft is coupled to the gas producer section and the compressor rotor assembly, and is configured to couple to a second driven apparatus.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.