Invention Grant
- Patent Title: Isolation seals for gas turbine engines
-
Application No.: US16424562Application Date: 2019-05-29
-
Publication No.: US11098652B2Publication Date: 2021-08-24
- Inventor: Brandon T. Slaney
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Cantor Colburn LLP
- Main IPC: F02C7/28
- IPC: F02C7/28 ; F01D11/00 ; F01D25/26

Abstract:
Isolation seals for gas turbine engines are described. The isolation seals include a first interface member configured to be fixedly attached to a first case structure, the first interface member being a full-hoop structure, a housing configured to be mounted to a second case structure, a connector pin arranged within the housing and moveable relative to the housing, and a second interface member located on an end of the connector pin, the second interface member being a full-hoop structure. The first interface member and the second interface member are engageable to form a seal therebetween.
Public/Granted literature
- US20200378308A1 ISOLATION SEALS FOR GAS TURBINE ENGINES Public/Granted day:2020-12-03
Information query
IPC分类: