Invention Grant
- Patent Title: Combustor liner
- Patent Title (中): 燃烧器衬管
-
Application No.: US12433104Application Date: 2009-04-30
-
Publication No.: US08863527B2Publication Date: 2014-10-21
- Inventor: Marcus Timothy Holcomb , Todd Taylor , Randall E. Yount
- Applicant: Marcus Timothy Holcomb , Todd Taylor , Randall E. Yount
- Applicant Address: US IN Indianapolis
- Assignee: Rolls-Royce Corporation
- Current Assignee: Rolls-Royce Corporation
- Current Assignee Address: US IN Indianapolis
- Agency: Krieg DeVault LLP
- Main IPC: F23R3/42
- IPC: F23R3/42 ; F23R3/28 ; F23R3/00

Abstract:
A combustor liner for a turbine engine is disclosed herein. The combustor liner includes an inner liner surface operable to define at least part of a combustion chamber in a turbine engine. The inner liner surface extends along a portion of a chordal arc on a first side of the chordal arc. The combustor liner also includes a bearing surface operable to support a floating dome panel. At least part of the bearing surface is spaced from the chordal arc on a second side of the chordal arc opposite the first side.
Public/Granted literature
- US20100275606A1 COMBUSTOR LINER Public/Granted day:2010-11-04
Information query