Invention Grant
US08839625B2 Gas turbine engine diffuser having air flow channels with varying widths
有权
具有不同宽度的气流通道的燃气涡轮发动机扩散器
- Patent Title: Gas turbine engine diffuser having air flow channels with varying widths
- Patent Title (中): 具有不同宽度的气流通道的燃气涡轮发动机扩散器
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Application No.: US12796028Application Date: 2010-06-08
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Publication No.: US08839625B2Publication Date: 2014-09-23
- Inventor: James C. Napier , Anthony C. Jones
- Applicant: James C. Napier , Anthony C. Jones
- Applicant Address: US CT Windsor Locks
- Assignee: Hamilton Sunstrand Corporation
- Current Assignee: Hamilton Sunstrand Corporation
- Current Assignee Address: US CT Windsor Locks
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F04D29/44
- IPC: F04D29/44 ; F04D29/54 ; F02C7/04 ; F01D9/02

Abstract:
An exemplary diffuser includes a plurality of air flow channels defined by a corresponding plurality of vanes. The vanes extend from a first side of the diffuser and define a width of the air flow channel between the corresponding plurality of vanes. The first side has at least one tapered surface extending from an inner radial position to an outer radial position. The distance between a tapered surface and a top side of the plurality of the vanes defines a depth of the air flow channel. The width of the air flow channel varies relative to the depth of the air flow channel along the length of the air flow channel.
Public/Granted literature
- US20110296841A1 GAS TURBINE ENGINE DIFFUSER Public/Granted day:2011-12-08
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