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    • 7. 发明申请
    • Turbocharger
    • 涡轮增压器
    • US20050188694A1
    • 2005-09-01
    • US10653436
    • 2003-09-02
    • Dirk Frankenstein
    • Dirk Frankenstein
    • F02B39/00F01D25/18F16J15/00F02D23/00
    • F01D25/183F05D2220/40F05D2260/6022F16J15/004
    • Turbocharger comprising a rotor shaft (5), a turbine housing (2), a compressor housing (3) connected to the turbine housing (2), and including at least one air supply channel (13′) for supplying air to be compressed and at least one discharge channel (11) for delivering compressed air. One end of the rotor shaft projects into the compressor housing and supports a compressor rotor (21). A bearing (12) in the region of the compressor rotor supports the rotor shaft, and forms a bearing gap. The bearing includes two seals (29,30) axially spaced from one another to seal the bearing gap and to leave an intermediate space (31) between them. A suction channel (33,34) is connected to a vacuum source and sucks gas out of this intermediate space.
    • 涡轮增压器包括转子轴(5),涡轮机壳体(2),连接到涡轮机壳体(2)的压缩机壳体(3),并且包括用于供应被压缩空气的至少一个供气通道(13') 至少一个用于输送压缩空气的排放通道(11)。 转子轴的一端突出到压缩机壳体中并支撑压缩机转子(21)。 压缩机转子区域中的轴承(12)支承转子轴,形成轴承间隙。 轴承包括彼此轴向间隔开的两个密封件(29,30),以密封轴承间隙并在它们之间留下一个中间空间(31)。 抽吸通道(33,34)连接到真空源并将气体从该中间空间吸出。
    • 9. 发明申请
    • TURBOCHARGER
    • 涡轮增压器
    • US20110182717A1
    • 2011-07-28
    • US12295013
    • 2007-03-28
    • Timo TriesRalf BoeningDirk Frankenstein
    • Timo TriesRalf BoeningDirk Frankenstein
    • F04D29/56
    • F01D17/165F05D2220/40F05D2230/64F05D2250/182F05D2250/312F05D2260/50F05D2260/79
    • The invention relates to a turbocharger (1) with variable turbine geometry (VTG), comprising a multiplicity of guide blades (7). Each guide blade (7) has a blade lever (19, 19′), wherein the center plane (Em2) of an intermediate region (24; 24′) of the blade lever (19, 19′) is arranged so as to be offset axially along a blade shaft longitudinal axis (L) at a distance (a) from the center plane (Em1) of a first end region (20; 20′) of the blade lever (19, 19′) and of a second end region (23; 23′) of the blade lever (19, 19′), and wherein a recess (26; 26′) is arranged adjacent to the intermediate region (24; 24′) between the first end region (20; 20′) and the second end region (23; 23′).
    • 本发明涉及具有可变涡轮几何形状(VTG)的涡轮增压器(1),其包括多个导向叶片(7)。 每个引导刀片(7)具有刀片杆(19,19'),其中刀片杆(19,19')的中间区域(24; 24')的中心平面(Em2)被布置成 与叶片杆纵向轴线(L)轴距地偏离与叶片杆(19,19')的第一端部区域(20,20')的中心平面(Em1)的距离(a),第二端 所述刀片杆(19,19')的区域(23; 23'),并且其中在所述第一端部区域(20,20)之间邻近所述中间区域(24; 24')布置有凹部(26; 26' ')和第二端区域(23; 23')。