发明名称 GUIDE VANE FOR VARIABLE TURBINE GEOMETRY
摘要 PROBLEM TO BE SOLVED: To provide an improved guide vane geometry.SOLUTION: A guide vane 10 includes four sections a1-a4, the first section a1 and the second section a2 forming a first region b1, the third section a3 and the fourth section a4 forming a third region b3. A curvature line 12 of the sections a1 and a2 of the first region b1 and a curvature line 12 of the sections a3 and a4 of the third region b3: continuously transit to each other at connection places 22 of the sections a1 and a2 and the sections a3 and a4; and curve in the same direction of upward or downward direction. The second section a2 and the third section a3: form a second region b2 of the guide vane 10; are coupled together; transit to each other in discontinuity at the connection place 22 of the two sections a2 and a3; and form a crease line 24 in a direction opposite to directions of curved extensions of the first region b1 and the third region b3.
申请公布号 JP2013238249(A) 申请公布日期 2013.11.28
申请号 JP20130184103 申请日期 2013.09.05
申请人 CONTINENTAL AUTOMOTIVE GMBH 发明人 BOENING RALF;DETTMANN THBIAS;FAETH HOLGER;KAUFMANN ANDRE
分类号 F01D9/02;F01D17/16;F02B37/24 主分类号 F01D9/02
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