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    • 9. 发明申请
    • Turbocharger
    • 涡轮增压器
    • US20080260528A1
    • 2008-10-23
    • US12094819
    • 2006-11-24
    • Mathias WeberJochen ZuckDietmar Metz
    • Mathias WeberJochen ZuckDietmar Metz
    • F04D29/54
    • F01D17/165F05D2220/40F05D2250/611F05D2250/70F05D2250/713
    • The invention relates to a turbocharger comprising a turbine casing (2) which has an exhaust-gas inlet opening (3) and an exhaust-gas outlet opening (4); comprising a turbine wheel (5) which is fastened to a shaft (6) and is arranged in the turbine casing (2); comprising a plurality of blades (7; T) which are arranged in the turbine casing (2) between the exhaust-gas inlet opening (3) and the turbine wheel (5), wherein each blade has the following: a profile underside (8; 8′) and a profile top side (9; 9′) which determine the blade thickness, a blade leading edge (10; 10′) at a first intersection of the blade underside (8; 8′) and the blade top side (9; 9′), a blade trailing edge (11; 11′) at a second intersection of the blade underside (8; 8′) and the blade top side (9; 9′), a profile centre line (12; 12′) which is defined by the blade underside (8; 8′) and the blade top side (9; 9′) and runs between them from the blade leading edge (10; 11′) to the blade trailing edge (11; 11′), wherein the profile centre line (12; 12′) runs in a wave-like manner.
    • 本发明涉及一种涡轮增压器,其包括具有排气入口(3)和排气出口(4)的涡轮机壳体(2)。 包括固定到轴(6)并布置在所述涡轮壳体(2)中的涡轮机叶轮(5); 包括多个叶片(7; T),其布置在所述排气入口开口(3)和所述涡轮机叶轮(5)之间的所述涡轮机壳体(2)中,其中每个叶片具有以下:轮廓下侧(8 ; 8')和确定叶片厚度的轮廓顶侧(9; 9'),在叶片下侧(8; 8')和叶片顶侧之间的第一交叉处的叶片前缘(10; 10') (9; 9'),叶片下侧(8; 8')和叶片顶侧(9; 9')的第二交叉处的叶片后缘(11; 11'),轮廓中心线(12; 由叶片下侧(8; 8')和叶片顶侧(9; 9')限定,并从叶片前缘(10; 11')到叶片后缘(11; 11'),其中轮廓中心线(12; 12')以波状方式运行。