Compressor with gas sealing chamber
US5505588A · kind A · utility
Assignee
Inventors
Key dates
| Filing date | Sep 27, 1994 |
| Grant date | Apr 9, 1996 |
| Priority date | — |
| Expiry date | Sep 27, 2014 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF04D29/102
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A compressor for a gas turbine includes a gas seal chamber to seal the space between the guide vanes and the rotor vanes from ambient air. A seal casing is positioned at a radially inner side of the inlet casing adjacent to an inlet duct and the rotor blades with an annular gap between the seal casing and the rotor shaft. The annular gap communicates for air flow with the inlet duct. A plurality of ribs are mounted on the one or both of the seal casing and rotor shaft to extend into the annular gap to provide flow resistance. The seal casing defines therewithin a sealing air chamber is connected to the inlet space and the annular gap to permit air from the inlet space to flow to the annular gap and to the inlet duct.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.