Invention Grant
- Patent Title: Combustor for a gas turbine engine including a liner having a looped feature
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Application No.: US17340816Application Date: 2021-06-07
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Publication No.: US11885495B2Publication Date: 2024-01-30
- Inventor: Ravindra Shankar Ganiger , Hiranya Kumar Nath , Daniel J. Kirtley , Shai Birmaher , Pradeep Naik
- 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: Venable LLP
- Agent Elizabeth C. G. Gitlin; Michele V. Frank
- Main IPC: F23R3/06
- IPC: F23R3/06 ; F23R3/00 ; F02C3/00 ; F02C3/14
Abstract:
A combustor for a gas turbine engine, the gas turbine engine defining a longitudinal centerline extending in a longitudinal direction, a radial direction extending orthogonally outward from the longitudinal centerline, and a circumferential direction extending concentrically around the longitudinal centerline, the combustor including: a liner at least partially defining a combustion chamber of the gas turbine engine, wherein the liner comprises a looped feature.
Public/Granted literature
- US20220390113A1 COMBUSTOR FOR A GAS TURBINE ENGINE Public/Granted day:2022-12-08
Information query
