Gas turbine engine combustor liner assembly with convergent hyperbolic profile
US10174949B2 · kind B2 · utility
1Cited by
38References
14Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Feb 5, 2014 |
| Grant date | Jan 8, 2019 |
| Priority date | — |
| Expiry date | Jul 26, 2035 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY10T29/49828
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A heat shield for a combustor of a gas turbine engine includes a first edge with a first set of cantilevered members and a second edge with a second set of cantilevered members.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.