Invention Grant
- Patent Title: Flexible seal for gas turbine engine system
- Patent Title (中): 燃气轮机发动机系统的柔性密封
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Application No.: US13173954Application Date: 2011-06-30
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Publication No.: US08647048B2Publication Date: 2014-02-11
- Inventor: Steven D. Roberts , Richard W. Monahan , David C. Pimenta
- Applicant: Steven D. Roberts , Richard W. Monahan , David C. Pimenta
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Kinney & Lange, P.A.
- Main IPC: F02C7/28
- IPC: F02C7/28 ; F01D11/00 ; F02K1/80
Abstract:
A system includes a gas turbine engine, a nozzle structure located adjacent to the gas turbine engine, a flexible annular seal linking the gas turbine engine and the nozzle structure, the flexible annular seal having a plurality of corrugate sections, and a reinforcement member positioned between two of the plurality of corrugate sections.
Public/Granted literature
- US20120131929A1 FLEXIBLE SEAL FOR GAS TURBINE ENGINE SYSTEM Public/Granted day:2012-05-31
Information query
IPC分类:
