Invention Grant
- Patent Title: Segmented rim seal spacer for a gas turbine engine
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Application No.: US14730400Application Date: 2015-06-04
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Publication No.: US09719363B2Publication Date: 2017-08-01
- Inventor: David R Pack , Julian Partyka , James D. Hill , Gabriel L Suciu , Gregory M Dolansky , Brian D Merry
- 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: Bachman & LaPointe, P.C.
- Main IPC: F01D5/06
- IPC: F01D5/06 ; F01D11/00
Abstract:
A seal segment for a gas turbine engine includes a first axial span that extends between the first radial span and the second radial span. A second axial span extends between the first radial span and the second radial span, the first radial span, the second radial span, the first axial span and the second axial span forming a torque box.
Public/Granted literature
- US20150354389A1 SEGMENTED RIM SEAL SPACER FOR A GAS TURBINE ENGINE Public/Granted day:2015-12-10
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