Invention Grant
- Patent Title: Shroud for gas turbine engine
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Application No.: US15995076Application Date: 2018-05-31
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Publication No.: US10550710B2Publication Date: 2020-02-04
- Inventor: Brad Wilson VanTassel , Evan Andrew Sewall , Travis J Packer
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: GENERAL ELECTRIC COMPANY
- Current Assignee: GENERAL ELECTRIC COMPANY
- Current Assignee Address: US NY Schenectady
- Agency: Dority & Manning, P.A.
- Main IPC: F01D25/14
- IPC: F01D25/14 ; F01D11/08

Abstract:
A turbine shroud segment including: a target exterior surface and target interior region; and a cooling configuration having first and second channel types. The first channel type includes: an inlet and outlet; a target section extending through the target interior region; lateral ports spaced lengthwise between first and second ends of the target section; and a path within the target interior region offset from the target exterior surface by a minimum offset. The second channel type includes: dead-ends disposed at first and second ends; lateral ports connecting to lateral ports of the first channel type; and a path through the target interior region that is variable between valleys and peaks. The second channel type resides closer to the target exterior surface at the valleys than at the peaks. At each of the valleys, the second channel type resides within the minimum offset.
Public/Granted literature
- US20190368365A1 SHROUD FOR GAS TURBINE ENGINE Public/Granted day:2019-12-05
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