Invention Grant
US07654791B2 Apparatus and method for controlling a blade tip clearance for a compressor
有权
用于控制压缩机的叶片顶端间隙的装置和方法
- Patent Title: Apparatus and method for controlling a blade tip clearance for a compressor
- Patent Title (中): 用于控制压缩机的叶片顶端间隙的装置和方法
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Application No.: US11477294Application Date: 2006-06-29
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Publication No.: US07654791B2Publication Date: 2010-02-02
- Inventor: Andre Werner
- Applicant: Andre Werner
- Applicant Address: DE Munich
- Assignee: MTU Aero Engines GmbH
- Current Assignee: MTU Aero Engines GmbH
- Current Assignee Address: DE Munich
- Agency: Crowell & Moring LLP
- Priority: DE102005030426 20050630
- Main IPC: F01D11/20
- IPC: F01D11/20

Abstract:
An apparatus and method for controlling a blade tip clearance for a compressor of a turbo-engine, in particular of an aircraft engine, is disclosed. A blade tip clearance control device, which has a rotor and a housing surrounding the rotor forming a blade tip clearance, includes a sealing element that is movable into the blade tip clearance and an actuator unit, where the sealing element is designed as a circumferential shroud liner made of a flexible rubbery material in which at least one tubular diaphragm that is also circumferential is arranged. The diaphragm is acted upon with hydraulic fluid via the actuator unit. This makes it possible to counteract degradation that occurs during operation due to erosion, aging, etc. As a result, efficiency is maintained and the pump limit interval is retained.
Public/Granted literature
- US20090317228A1 APPARATUS AND METHOD FOR CONTROLLING A BLADE TIP CLEARANCE FOR A COMPRESSOR Public/Granted day:2009-12-24
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