Invention Application
US20160348512A1 TURBINE COMPONENT HAVING SURFACE COOLING CHANNELS AND METHOD OF FORMING SAME
有权
具有表面冷却通道的涡轮机部件及其形成方法
- Patent Title: TURBINE COMPONENT HAVING SURFACE COOLING CHANNELS AND METHOD OF FORMING SAME
- Patent Title (中): 具有表面冷却通道的涡轮机部件及其形成方法
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Application No.: US14725695Application Date: 2015-05-29
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Publication No.: US20160348512A1Publication Date: 2016-12-01
- Inventor: Carlos Miguel Miranda , Andrew Lee Trimmer , Srikanth Chandrudu Kottilingam , Benjamin Paul Lacy
- Applicant: General Electric Company
- Main IPC: F01D5/18
- IPC: F01D5/18 ; F23R3/00 ; F02C7/18 ; F02C3/04 ; F01D9/04 ; F01D25/12
Abstract:
A component for a turbine engine includes a substrate that includes a first surface, and an insert coupled to the substrate proximate the substrate first surface. The component also includes a channel. The channel is defined by a first channel wall formed in the substrate and a second channel wall formed by at least one coating disposed on the substrate first surface. The component further includes an inlet opening defined in flow communication with the channel. The inlet opening is defined by a first inlet wall formed in the substrate and a second inlet wall defined by the insert.
Public/Granted literature
- US09752440B2 Turbine component having surface cooling channels and method of forming same Public/Granted day:2017-09-05
Information query
