Invention Grant
- Patent Title: Strain tolerant combustor panel for gas turbine engine
- Patent Title (中): 用于燃气涡轮发动机的耐应变燃烧器面板
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Application No.: US13168258Application Date: 2011-06-24
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Publication No.: US08997495B2Publication Date: 2015-04-07
- Inventor: James A. Dierberger
- Applicant: James A. Dierberger
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F02C1/00
- IPC: F02C1/00 ; F23R3/00
Abstract:
A combustor component of a gas turbine engine includes a substrate with a cold side, a central core section and a hot side, the cold side and the hot side have a porosity different than the central core section.
Public/Granted literature
- US20120324894A1 STRAIN TOLERANT COMBUSTOR PANEL FOR GAS TURBINE ENGINE Public/Granted day:2012-12-27
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