发明名称 DEVICE PREVENTING ICING OF GAS TURBINE GUIDE WHEEL VANES (VERSIONS), VANE WITH THIS DEVICE AND AIRCRAFT ENGINE EQUIPPED WITH SUCH VANES
摘要 FIELD: engines and pumps. ^ SUBSTANCE: gas turbine engine guide wheel vane deicer comprises a fixed section arranged on the inlet and movable shield fitted at the outlet. The aforesaid fixed section includes a rear U-shape edge, one branch of the said edge being located on the inner outward bend side, while the other branch being arranged on the suction face side. The proposed device comprises, at least, one outlet opening directed towards inlet-outlet and is arranged along only the U-shape edge branch located on the rear edge inner outward bend side. The guide wheel vane is furnished with, at least, one such deicer. The gas turbine engine incorporates, at least, one vane furnished with such deicer. ^ EFFECT: high-efficiency deicer. ^ 18 cl, 10 dwg
申请公布号 RU2347924(C2) 申请公布日期 2009.02.27
申请号 RU20040121996 申请日期 2004.07.16
申请人 SNEKMA MOTER 发明人 KURTO JANNIK ZHAN ROZHE;MARLEN FRANSUA MARI POL';DAN'ELO ZHAN ARMAN FRANSUA
分类号 F02C7/047;F01D5/14;F01D17/16 主分类号 F02C7/047
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