Invention Grant
- Patent Title: Blade outer air seal for a gas turbine engine
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Application No.: US13559901Application Date: 2012-07-27
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Publication No.: US09617866B2Publication Date: 2017-04-11
- Inventor: Nicholas R. Leslie , Fadi S. Maalouf , Georg Zotz , Werner Humhauser
- Applicant: Nicholas R. Leslie , Fadi S. Maalouf , Georg Zotz , Werner Humhauser
- Applicant Address: US CT Hartford DE Munich
- Assignee: United Technologies Corporation,MTU Aero Engines AG
- Current Assignee: United Technologies Corporation,MTU Aero Engines AG
- Current Assignee Address: US CT Hartford DE Munich
- Agency: Carlson, Gaskey & Olds
- Main IPC: F01D11/12
- IPC: F01D11/12

Abstract:
A blade outer air seal (BOAS) for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a seal body having a radially inner face and a radially outer face that axially extend between a leading edge portion and a trailing edge portion. The BOAS includes a trough disposed on the radially inner face and an abradable seal received within the trough. The trough is open to expose a leading edge of the abradable seal to a core flow path of the gas turbine engine.
Public/Granted literature
- US20140030071A1 BLADE OUTER AIR SEAL FOR A GAS TURBINE ENGINE Public/Granted day:2014-01-30
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