发明名称 Gas turbine nozzle seals for 2000° F. gas containment
摘要 A seal for containment of fluids or gases during high temperature applications, separating a high pressure area on one side from a low pressure area on an opposite side, and formed to convert axial displacements into radial movements eliminating axial strains, having at least one engaging, conical ring structure with a tapering arcuate side facing radially away from the high pressure side. The conical ring structure has a side opposite the tapering side that is cylindrical, and a cylindrical diameter that is concentric with the arcuate side. The conical ring structure has an axial distal end with a larger diameter than its opposite end for engaging a flat annular surface on an adjacent structural member to form the seal. A heat-destructible wax spacer may be used for insertion within the clearance gap to locate the seal concentrically with the gland for ease of assembly.
申请公布号 US8104772(B2) 申请公布日期 2012.01.31
申请号 US20090490027 申请日期 2009.06.23
申请人 HALLING HORACE P.;SEAL SCIENCE & TECHNOLOGY, LLC 发明人 HALLING HORACE P.
分类号 H02G3/22;F16J15/02;F16L17/06 主分类号 H02G3/22
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