Invention Grant
- Patent Title: Combustor seal for a gas turbine engine combustor
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Application No.: US15334804Application Date: 2016-10-26
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Publication No.: US10669939B2Publication Date: 2020-06-02
- Inventor: Jonathan Jeffery Eastwood , Dennis M. Moura
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: Raytheon Technologies Corporation
- Current Assignee: Raytheon Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Bachman & LaPointe, P.C.
- Main IPC: F02C7/18
- IPC: F02C7/18 ; F01D11/00 ; F01D25/12 ; F23R3/00 ; F01D9/02 ; F01D9/04 ; F02C7/28
Abstract:
A combustor seal for use in a combustor of a gas turbine engine including a seal with a multiple of slots that correspond with a multiple of 1st HPT vanes. A method of cooling within a gas turbine engine including communicating cooling air through combustor seal toward each of a multiple of 1st HPT vanes.
Public/Granted literature
- US20180112597A1 COMBUSTOR SEAL FOR A GAS TURBINE ENGINE COMBUSTOR Public/Granted day:2018-04-26
Information query
IPC分类:
