发明名称 Seal for a high-pressure turbomachine
摘要 An annular seal is provided for use in a turbomachine. The annular seal may form a generally rectangular cross-section and may include an outer radial surface forming an outer sealing surface and defining at least one annular groove and a plurality of slots spaced circumferentially about the outer radial surface. Each slot may have an end terminating in the at least one annular groove. The annular seal may also include a first axial sidewall forming a sidewall sealing surface and a recessed portion and a second axial sidewall opposing the first axial sidewall. At least one annular groove and the plurality of slots may be configured to maintain a low pressure environment across at least a portion of the outer radial surface. The second axial sidewall, the recessed portion, and the inner radial surface may be configured to maintain a high pressure environment there across during operation of the turbomachine.
申请公布号 US9303655(B2) 申请公布日期 2016.04.05
申请号 US201414317283 申请日期 2014.06.27
申请人 Dresser-Rand Company 发明人 Griffin Daniel J.
分类号 F04D29/16;F04D29/42;F04D17/12 主分类号 F04D29/16
代理机构 Edmonds & Nolte, PC 代理人 Edmonds & Nolte, PC
主权项 1. A compressor comprising: a housing; a shaft rotatably mounted with respect to the housing; a compressor bundle arranged around the shaft and disposed at least partially within the housing; and an annular seal mounted about a portion of the compressor bundle, such that the annular seal is disposed between the housing and the compressor bundle, the annular seal comprising: an inner radial surface defining an inner diameter of the annular seal;an outer radial surface opposing the inner radial surface and defining an outer diameter of the annular seal, the outer radial surface forming an outer sealing surface and the outer radial surface further defining at least one annular groove and a plurality of slots spaced circumferentially about the outer radial surface, each slot having an end terminating in the at least one annular groove;a first axial sidewall forming a sidewall sealing surface and a recessed portion; anda second axial sidewall opposing the first axial sidewall, wherein the annular seal forms a generally rectangular cross-section; wherein the at least one annular groove and the plurality of slots are configured to maintain a low pressure environment across at least a portion of the outer radial surface disposed adjacent an inner surface of the housing; and wherein the second axial sidewall, the recessed portion, and the inner radial surface are configured to maintain a high pressure environment there across during operation of the compressor.
地址 Olean NY US