发明名称 Attachment for combuster liner.
摘要 <p>The segmented wall of the float-wall combustor liner (16) for a gas turbine engine is retained by a clip (36) secured to a post (20) extending radially from the segmented wall through an opening in the outer combustor shell (12). The clip (36) serves to load the walls radially and has fail-safe features preventing inadvertent dislodging.</p>
申请公布号 EP0157719(A1) 申请公布日期 1985.10.09
申请号 EP19850630037 申请日期 1985.03.27
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 MEMMEN, ROBERT LOUIS
分类号 F16B2/24;F16B21/09;F16B21/18;F23R3/60;(IPC1-7):F16B21/18;F02C7/20;F23R3/00;F23R3/08;F02K1/82 主分类号 F16B2/24
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