Gas turbine engine component having vascular engineered lattice structure
US10221694B2 · kind B2 · utility
10Cited by
64References
17Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Feb 17, 2016 |
| Grant date | Mar 5, 2019 |
| Priority date | — |
| Expiry date | Mar 5, 2037 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02P10/25
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A flowpath component for a gas turbine engine includes a first platform including a vascular engineered lattice structure, a body extending from, and supported by the first platform. The body is configured to at least partially span a flowpath in an installed position and the vascular engineered lattice structure including at least one purge air inlet, and at least one spent air outlet.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.