Invention Grant
- Patent Title: Split line flow path seals
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Application No.: US15672991Application Date: 2017-08-09
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Publication No.: US10584605B2Publication Date: 2020-03-10
- Inventor: Aaron D. Sippel , Ted J. Freeman , David J. Thomas , Joseph P. Lamusga , Brian J. Shoemaker , Steven Hillier
- Applicant: Rolls-Royce Corporation , Rolls-Royce North American Technologies Inc. , Rolls-Royce High Temperature Composites Inc. , Rolls-Royce plc
- Applicant Address: US IN Indianapolis US IN Indianapolis US CA Cypress GB
- Assignee: Rolls-Royce Corporation,Rolls-Royce North American Technologies Inc.,Rolls-Royce High Temperature Composites Inc.,Rolls-Royce plc
- Current Assignee: Rolls-Royce Corporation,Rolls-Royce North American Technologies Inc.,Rolls-Royce High Temperature Composites Inc.,Rolls-Royce plc
- Current Assignee Address: US IN Indianapolis US IN Indianapolis US CA Cypress GB
- Agency: Barnes & Thornburg LLP
- Main IPC: F01D11/00
- IPC: F01D11/00 ; F01D25/26 ; F01D5/22 ; F01D5/24 ; F01D9/04 ; F01D25/24
Abstract:
A gas turbine engine assembly adapted to separate a high pressure zone from a low pressure zone includes a seal assembly configured to block gasses from passing through the interface of two adjacent components. The seal assembly includes a rod.
Public/Granted literature
- US20170370240A1 SPLIT LINE FLOW PATH SEALS Public/Granted day:2017-12-28
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