Invention Grant
- Patent Title: Cooled hot section components for a gas turbine engine
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Application No.: US15158782Application Date: 2016-05-19
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Publication No.: US10344611B2Publication Date: 2019-07-09
- Inventor: Nathan K. Galle
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: Cantor Colburn LLP
- Main IPC: F02C3/04
- IPC: F02C3/04 ; F01D11/08 ; F01D25/24
Abstract:
A gas turbine engine includes a turbine section including a plurality of blade outer air seals disposed therein, the blade outer air seals each including a body including a raised material that extends beyond the outer surface of the body and the raised material includes an inlet hole formed through the raised material.
Public/Granted literature
- US20170335707A1 COOLED HOT SECTION COMPONENTS FOR A GAS TURBINE ENGINE Public/Granted day:2017-11-23
Information query
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