Invention Grant
- Patent Title: Transition system side seal for gas turbine engines
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Application No.: US16071090Application Date: 2016-01-27
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Publication No.: US11255201B2Publication Date: 2022-02-22
- Inventor: Anthony L. Schiavo
- Applicant: Siemens Energy Global GmbH & Co. KG
- Applicant Address: DE Munich
- Assignee: Siemens Energy Global GmbH & Co. KG
- Current Assignee: Siemens Energy Global GmbH & Co. KG
- Current Assignee Address: DE Munich
- International Application: PCT/US2016/015048 WO 20160127
- International Announcement: WO2017/131650 WO 20170803
- Main IPC: F01D9/02
- IPC: F01D9/02 ; F01D11/00 ; F01D25/12
Abstract:
A gas turbine engine has a transition duct assembly. Between two adjacent transition ducts (20) there is a transition side groove (23) that is formed by transition side rails (22). In this transition side groove (23) is inserted a side seal (30a-30e) that engages transition side grooves (23) that are formed in the transition side rails (22).
Public/Granted literature
- US20210172329A1 TRANSITION SYSTEM SIDE SEAL FOR GAS TURBINE ENGINES Public/Granted day:2021-06-10
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