Gas turbine engine with attached nosecone
US9540939B2 · kind B2 · utility
8Cited by
15References
20Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Dec 26, 2013 |
| Grant date | Jan 10, 2017 |
| Priority date | — |
| Expiry date | Jun 4, 2035 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY10T29/49321
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A gas turbine engine includes a compressor section and a nosecone assembly. The compressor section includes an inlet guide vane assembly including an inner shroud, an outer shroud, and an inlet guide vane extending from the inner shroud to the outer shroud. The nosecone assembly is attached to the inner shroud.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.