Particle separator for a turbine engine
US6698180B2 · kind B2 · utility
Assignee
Inventor
Key dates
| Filing date | Aug 12, 2002 |
| Grant date | Mar 2, 2004 |
| Priority date | — |
| Expiry date | Sep 14, 2022 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY10T137/0536
- WIPO fieldChemical engineering
- WIPO sectorChemistry
Abstract
A particle separator for use with a turbine engine is arranged to divide a flow of air into a radially inner air flow and a radially outer air flow. The particle separator is further arranged to separate inner particles from the inner air flow to allow air from the inner air flow to enter the turbine engine without the inner particles and arranged to separate outer particles from the outer air flow to allow air from the outer air flow to enter the turbine engine without the outer particles.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.