Invention Grant
- Patent Title: Combustor for gas turbine engine and method of manufacture
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Application No.: US17178418Application Date: 2021-02-18
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Publication No.: US11549437B2Publication Date: 2023-01-10
- Inventor: Rodolphe Dudebout , Hamdullah Ozogul , Atul Verma , Amy Kujala , Michael Wedig , Ryan Meyer , Bradley Culbertson
- Applicant: HONEYWELL INTERNATIONAL INC.
- Applicant Address: US NC Charlotte
- Assignee: HONEYWELL INTERNATIONAL INC.
- Current Assignee: HONEYWELL INTERNATIONAL INC.
- Current Assignee Address: US NC Charlotte
- Agency: Lorenz & Kopf, LLP
- Main IPC: F02C7/12
- IPC: F02C7/12 ; F23R3/00

Abstract:
A combustor for a gas turbine engine includes an outer liner having a first end interconnected to an opposite second end by an outer liner wall composed of a plurality of outer segments. The inner liner has a first inner end interconnected to an opposite second inner end by an inner liner wall composed of a plurality of inner segments. The outer liner wall and the inner liner wall define a combustion chamber, and each of the outer wall segments extend at an angle of at least 40 degrees relative to a longitudinal axis. The outer wall segments includes a first segment, a second segment that extends at a second angle relative to the first segment, which is less than a third angle defined between the second segment and a third segment and is substantially the same as a fourth angle defined between the third segment and a fourth segment.
Public/Granted literature
- US20220260016A1 COMBUSTOR FOR GAS TURBINE ENGINE AND METHOD OF MANUFACTURE Public/Granted day:2022-08-18
Information query
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