发明名称 Deicing system for a butterfly valve
摘要 Auto-deicing system with a valve having a butterfly plate (5). The spindle (8) of the valve (4) is controlled by a system terminated by a pin (11) coaxial to the spindle (8) and which, like the latter, has slots (13). When the pin (8) is iced up, the control system initiates a movement of the pin (11) so that the slots (12, 13) come into extension with one another, which allows a circulation of the hot gas on one side of the butterfly plate (5) through the spindle (8), which is thus reheated. The opening movement resumes when the ice has melted. The invention is applicable to cold starting systems on aircraft engines. (FIG. 3 )
申请公布号 US5499651(A) 申请公布日期 1996.03.19
申请号 US19940291550 申请日期 1994.08.16
申请人 SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION "SNECMA" 发明人 GALLO, CLAUDE;LECLERCQ, GUY E. O.
分类号 F01D25/02;F02C7/047;F02C7/277;F16K49/00;(IPC1-7):F02G5/00 主分类号 F01D25/02
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