Invention Grant
- Patent Title: Turbine tip shroud assembly with plural shroud segments having internal cooling passages
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Application No.: US15899780Application Date: 2018-02-20
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Publication No.: US10900378B2Publication Date: 2021-01-26
- Inventor: Jason Smoke , Kent L. Kime , Blake Petersen , Luke Zurmehly
- Applicant: HONEYWELL INTERNATIONAL INC.
- Applicant Address: US NJ Morris Plains
- Assignee: HONEYWELL INTERNATIONAL INC.
- Current Assignee: HONEYWELL INTERNATIONAL INC.
- Current Assignee Address: US NJ Morris Plains
- Agency: Lorenz & Kopf, LLP
- Main IPC: F01D25/12
- IPC: F01D25/12 ; F01D9/04 ; F01D11/08 ; F01D5/22 ; F01D11/24 ; F01D25/24
Abstract:
A shroud assembly for a gas turbine engine includes a shroud support and a plurality of shroud segments that are attached to the shroud support. The shroud segment includes an internal cooling passage.
Public/Granted literature
- US20180363499A1 TURBINE TIP SHROUD ASSEMBLY WITH PLURAL SHROUD SEGMENTS HAVING INTERNAL COOLING PASSAGES Public/Granted day:2018-12-20
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