Invention Grant
- Patent Title: Turbine disk with pinned platforms
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Application No.: US15944095Application Date: 2018-04-03
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Publication No.: US10767498B2Publication Date: 2020-09-08
- Inventor: Stephen Harris
- Applicant: Rolls-Royce High Temperature Composites Inc.
- Applicant Address: US CA Cypress
- Assignee: Rolls-Royce High Temperature Composites Inc.
- Current Assignee: Rolls-Royce High Temperature Composites Inc.
- Current Assignee Address: US CA Cypress
- Agency: Barnes & Thornburg LLP
- Main IPC: F01D5/30
- IPC: F01D5/30 ; F01D5/28 ; F01D5/14
Abstract:
A blade assembly for use in a gas turbine engine. The blade assembly includes a blade, a platform distinct from the blade and configured to extend around the blade, and a pin that couples the platform with the blade.
Public/Granted literature
- US20190301292A1 TURBINE DISK WITH PINNED PLATFORMS Public/Granted day:2019-10-03
Information query
