Invention Grant
- Patent Title: Combustor device for a gas turbine engine and gas turbine engine incorporating said combustor device
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Application No.: US15725751Application Date: 2017-10-05
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Publication No.: US10851997B2Publication Date: 2020-12-01
- Inventor: Jost Imfeld , Slawomir Swiatek , Oliver Konradt
- Applicant: ANSALDO ENERGIA SWITZERLAND AG
- Applicant Address: CH Baden
- Assignee: ANSALDO ENERGIA SWITZERLANG AG
- Current Assignee: ANSALDO ENERGIA SWITZERLANG AG
- Current Assignee Address: CH Baden
- Agency: Buchanan Ingersoll & Rooney PC
- Priority: EP16192707 20161006
- Main IPC: F23R3/08
- IPC: F23R3/08 ; F23C6/04 ; F01D9/02 ; F02C3/20 ; F02C7/28 ; F23R3/60

Abstract:
A combustor device for a gas turbines engines includes first and a second tubular members telescopically fitted in axially sliding manner to one another with interposition of annular centering and sealing which include at least a centering annular shoulder and a sealing ring arranged coaxial to one another. The sealing ring is axially spaced apart from the centering annular shoulder so that an axial distance between the centering annular shoulder and the sealing ring is greater than a maximum axial movement allowed between the first and said second tubular members.
Public/Granted literature
- US20180100651A1 COMBUSTOR DEVICE FOR A GAS TURBINE ENGINE AND GAS TURBINE ENGINE INCORPORATING SAID COMBUSTOR DEVICE Public/Granted day:2018-04-12
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