Invention Application
- Patent Title: TURBINE SHROUD THERMAL DISTORTION CONTROL
- Patent Title (中): 涡轮机热损失控制
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Application No.: US13668733Application Date: 2012-11-05
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Publication No.: US20130094946A1Publication Date: 2013-04-18
- Inventor: Jun Shi , Kevin E. Green , Shaoluo L. Butler , Gajawalli V. Srinivasan , Glenn N. Levasseur
- Applicant: United Technologies Corporation
- Applicant Address: US CT Hartford
- Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Hartford
- Main IPC: F01D11/18
- IPC: F01D11/18
Abstract:
A shroud for a gas turbine engine includes a leading portion having a leading edge and a first set of circumferentially spaced slots at the leading edge that break up the leading portion into circumferentially spaced segments separated by the first set of slots, and a trailing portion adjacent to the leading portion. The trailing portion has a trailing edge.
Public/Granted literature
- US08801372B2 Turbine shroud thermal distortion control Public/Granted day:2014-08-12
Information query
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