Invention Application
- Patent Title: SPLIT LINE FLOW PATH SEALS
- Patent Title (中): 分流线流路密封
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Application No.: US14723909Application Date: 2015-05-28
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Publication No.: US20160348521A1Publication Date: 2016-12-01
- Inventor: Aaron D. Sippel , Ted J. Freeman , David J. Thomas , Joseph P. Lamusga , Brian J. Shoemaker
- Applicant: Rolls-Royce Corporation , Rolls-Royce North American Technologies, Inc. , Rolls-Royce High Temperature Composites, Inc.
- Main IPC: F01D11/00
- IPC: F01D11/00 ; F01D25/26
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
- US09759079B2 Split line flow path seals Public/Granted day:2017-09-12
Information query
