Invention Grant
- Patent Title: Pressure activated seals for a gas turbine engine
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Application No.: US15159163Application Date: 2016-05-19
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Publication No.: US10370994B2Publication Date: 2019-08-06
- Inventor: David J. Thomas , Joseph P. Lamusga , Ted J. Freeman , Aaron D. Sippel
- Applicant: Rolls-Royce Corporation , Rolls-Royce North American Technologies, Inc.
- Applicant Address: US IN Indianapolis US IN Indianapolis
- Assignee: Rolls-Royce North American Technologies Inc.,Rolls-Royce Corporation
- Current Assignee: Rolls-Royce North American Technologies Inc.,Rolls-Royce Corporation
- Current Assignee Address: US IN Indianapolis US IN Indianapolis
- Agency: Barnes & Thornburg LLP
- Main IPC: F01D11/00
- IPC: F01D11/00 ; F01D9/02
Abstract:
An assembly for use in a gas turbine engine is disclosed. The assembly includes a first component arranged adjacent to a second component to form a gap therebetween and a pressure activated seal that resists flow through the gap.
Public/Granted literature
- US20160348523A1 PRESSURE ACTIVATED SEALS FOR A GAS TURBINE ENGINE Public/Granted day:2016-12-01
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