发明名称 Thermal seal for a gas turbine spacer disc.
摘要 <p>The present invention provides for the removable attachment of sealing segments about the entire circumferential periphery of the rotor spacer discs. To this end, the conventional annular grooves provided in the peripheral surface of each spacer disc (as part of the high/low sealing surface configuration) are reconfigured as dovetail grooves which are designed to receive complimentary or mating portions of the sealing segments. In other words, each adjacent annular groove receives a plurality of sealing segments, the totality of which substantially prevent or at least minimize the impingement of hot gases directly on the peripheral surface of the spacer disc. &lt;IMAGE&gt;</p>
申请公布号 EP0482758(A1) 申请公布日期 1992.04.29
申请号 EP19910308584 申请日期 1991.09.20
申请人 GENERAL ELECTRIC COMPANY 发明人 CARRENO, DIETHER EUSEBIO
分类号 F01D5/06;F01D5/08;F01D11/02;F02C7/24;F16J15/44 主分类号 F01D5/06
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