Invention Grant
- Patent Title: Gas turbine engine rapid response clearance control system with variable volume turbine case
-
Application No.: US14781179Application Date: 2014-02-06
-
Publication No.: US10557368B2Publication Date: 2020-02-11
- Inventor: Ken F. Blaney , Todd M. LaPierre
- 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: Getz Balich LLC
- International Application: PCT/US2014/015080 WO 20140206
- International Announcement: WO2014/018603 WO 20141120
- Main IPC: F01D11/22
- IPC: F01D11/22 ; F01D25/24 ; F02C7/28

Abstract:
An active clearance control system of a gas turbine engine includes a radially adjustable blade outer air seal system movable between a radially contracted Blade Outer Air Seal (BOAS) position that defines a first air volume and a radially expanded Blade Outer Air Seal (BOAS) position that defines a second air volume, the second air volume different than the first air volume. An accumulator system accommodate a difference in air volume between the first air volume and the second air volume.
Public/Granted literature
- US20160305269A1 GAS TURBINE ENGINE RAPID RESPONSE CLEARANCE CONTROL SYSTEM WITH VARIABLE VOLUME TURBINE CASE Public/Granted day:2016-10-20
Information query
IPC分类: