发明名称 Sealing device for e.g. aircraft engine, has hole brought in support unit and connected with area that is subjected with small pressure, via valve, where valve opens or closes holes based on temperature within area of brush seal
摘要 <p>The device has a brush seal with bristles arranged in a mounting area bounded by a support unit (21). A hole (24) is brought in the unit and connected with an area (11) subjected with a small pressure, via a valve (25). The area (11) is positioned in a partial area of the mounting area in a downstream of the seal. The valve opens or closes the holes based on the temperature within an area of a gap formed between a rotor and a stator.</p>
申请公布号 DE102004047206(A1) 申请公布日期 2006.04.06
申请号 DE20041047206 申请日期 2004.09.29
申请人 MTU AERO ENGINES GMBH 发明人 PROESTLER, STEPHAN
分类号 F01D11/02;F16J15/16 主分类号 F01D11/02
代理机构 代理人
主权项
地址