- Patent Title: Burner seal for gas-turbine combustion chamber head and heat shield
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Application No.: US14264965Application Date: 2014-04-29
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Publication No.: US10041415B2Publication Date: 2018-08-07
- Inventor: Carsten Clemen , Michael Ebel
- Applicant: Rolls-Royce Deutschland Ltd & Co KG
- Applicant Address: DE Blankenfelde-Mahlow
- Assignee: Rolls-Royce Deutschland Ltd & Co KG
- Current Assignee: Rolls-Royce Deutschland Ltd & Co KG
- Current Assignee Address: DE Blankenfelde-Mahlow
- Agency: Shuttleworth & Ingersoll, PLC
- Agent Timothy Klima
- Priority: DE102013007443 20130430
- Main IPC: F02C7/28
- IPC: F02C7/28 ; F02C7/20 ; F23R3/60 ; F23R3/28 ; F23R3/00 ; F01D9/02
Abstract:
The present invention relates to a combustion chamber for a gas turbine with a combustion chamber head and a heat shield which are designed in one piece, with the heat shield being provided with at least one recess, in which is arranged a burner or an annular sleeve enclosing the burner, with a burner seal being provided between the heat shield and the burner, characterized in that the heat shield is provided in the area of the recess with an annular groove, in which is arranged at least one elastic sealing element forming the burner seal.
Public/Granted literature
- US20140318148A1 BURNER SEAL FOR GAS-TURBINE COMBUSTION CHAMBER HEAD AND HEAT SHIELD Public/Granted day:2014-10-30
Information query
IPC分类:
