Invention Grant
US08646277B2 Combustor liner for a turbine engine with venturi and air deflector
有权
具有文丘里管和空气导流器的涡轮发动机的燃烧器衬套
- Patent Title: Combustor liner for a turbine engine with venturi and air deflector
- Patent Title (中): 具有文丘里管和空气导流器的涡轮发动机的燃烧器衬套
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Application No.: US12708736Application Date: 2010-02-19
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Publication No.: US08646277B2Publication Date: 2014-02-11
- Inventor: Ronald James Chila , Donald Timothy Lemon
- Applicant: Ronald James Chila , Donald Timothy Lemon
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Nixon & Vanderhye P.C.
- Main IPC: F23R3/02
- IPC: F23R3/02 ; F23R3/54

Abstract:
A combustor liner for a combustor of a turbine engine includes a single-walled generally cylindrical liner that extends from a head end to an aft end. A venturi is formed on the combustor liner at a location between the head and aft ends. The venturi is formed by first and second straight portions of the combustor liner that angle inward to form a reduced diameter portion. The combustor liner may also include an air deflector to deflect air down onto the exterior of the reduced diameter portion of the single-walled combustor liner. The combustor liner may also include dilution holes, and turbulator rings.
Public/Granted literature
- US20110203287A1 COMBUSTOR LINER FOR A TURBINE ENGINE Public/Granted day:2011-08-25
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