Invention Grant
- Patent Title: Combustor assembly for a turbine engine
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Application No.: US14842867Application Date: 2015-09-02
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Publication No.: US10168051B2Publication Date: 2019-01-01
- Inventor: Nicholas John Bloom , Michael Alan Stieg , Brian Christopher Towle
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: General Electric Company
- Agent William Andes
- Main IPC: F23R3/00
- IPC: F23R3/00 ; F23R3/60 ; F02C3/04 ; F23R3/50 ; F02C3/14 ; F16C29/02

Abstract:
A combustor assembly for a gas turbine engine is provided. The combustor assembly generally includes an annular dome and a liner. The liner at least partially defines a combustion chamber and includes the forward end received within a slot defined by the annular dome. A mounting assembly attaches the forward end of the liner to the annular dome. The mounting assembly includes a pin extending through the slot and the forward end of the annular dome. The mounting assembly also includes a grommet positioned in an opening in the forward end of the liner. The grommet is also positioned around the pin to protect the liner during operation of the gas turbine engine.
Public/Granted literature
- US20170059166A1 COMBUSTOR ASSEMBLY FOR A TURBINE ENGINE Public/Granted day:2017-03-02
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