Nozzle guide vane with composite heat shield
US10329950B2 · kind B2 · utility
6Cited by
11References
20Claims
0Family size
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Key dates
| Filing date | Mar 23, 2016 |
| Grant date | Jun 25, 2019 |
| Priority date | — |
| Expiry date | Aug 28, 2037 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A nozzle guide vane for a gas turbine engine is disclosed herein. The nozzle guide vane includes an inner endcap, an outer endcap, and at least one airfoil that extends from the inner endcap to the outer endcap. The nozzle guide vane further includes at least one composite heat shield component adapted to shield metallic components from high temperature gasses.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.