发明名称 Turbomachine airfoil mounting assembly
摘要 The assembly comprises a plurality of arcuate mounting members 21, 22 each including a central boss 23 having at least one radially extending recess 24 disposed in a radially inner surface (27, 34, Fig. 2 not shown) thereof which contains an elastomeric boot 39 for receiving an end 16 of one of the plurality of airfoils 14. The mounting member further includes integral first and second flanges 25, 26 (32, 33) extending circumferentially outwardly from opposite sides of the boss portion which overlap complementary second and first flanges, respectively, of adjacent mounting members. Fastening means 44 connect the first and second flanges of adjacent mounting members to form a continuous annular shroud. <IMAGE>
申请公布号 GB2115883(A) 申请公布日期 1983.09.14
申请号 GB19830000213 申请日期 1983.01.06
申请人 * GENERAL ELECTRIC COMPANY 发明人 ROBERT HOWARD * ROTH;BRUNO GUSTAV * LAMPSAT;JACK LEE * READNOUR
分类号 F01D5/30;F01D9/02;F01D9/04;(IPC1-7):F01D9/00 主分类号 F01D5/30
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