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Patent Searching and Data


Title:
TURBINE AIR FLOW CONDITIONER
Document Type and Number:
Japanese Patent JP2010261706
Kind Code:
A
Abstract:

To provide an air flow conditioner system for improving air distribution in an air chamber with respect to a turbine engine.

The system includes an air flow conditioner 50 configured to be mounted in the air chamber separated from a combustion chamber of a turbine combustor. The air flow conditioner includes a perforated annular wall 72 configured to direct an air flow in both an axial direction and a radial direction relative to an axis of the turbine combustor. In addition, the air flow conditioner is configured to uniformly supply the air flow into air inlets of one or more fuel nozzles.

COPYRIGHT: (C)2011,JPO&INPIT


Inventors:
BERRY JONATHAN DWIGHT
STEWARD JASON THURMAN
Application Number:
JP2010104701A
Publication Date:
November 18, 2010
Filing Date:
April 30, 2010
Export Citation:
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Assignee:
GEN ELECTRIC
International Classes:
F23R3/16; F23R3/28
Attorney, Agent or Firm:
荒川 聡志
小倉 博
黒川 俊久