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    • 25. 发明授权
    • Measuring apparatus
    • 测量装置
    • US07746448B2
    • 2010-06-29
    • US12173882
    • 2008-07-16
    • Karsten FranitzaBernd FehrmannMatthias HoebelPeter Lang
    • Karsten FranitzaBernd FehrmannMatthias HoebelPeter Lang
    • G01C3/08
    • G01B11/026G01B11/14
    • A measuring apparatus (1) for contactless detection of a distance between a surface (7) of a measurement object (8) and the measuring apparatus (1), and for simultaneous contactless visual detection of the surface (7), has a measuring head (2) holding a distance measuring device (4), a camera apparatus (5) and an illumination device (6), the illumination device (6) illuminating an operating point (9) on the surface (7) of the measurement object (8) that is simultaneously focused by the camera apparatus (5) and the distance measuring device (4). On an optical axis (10), between the illumination device (6) and the operating point (9), a mirror and filter device (11), that has at least one dichroic mirror (12) that transmits or reflects light beams as a function of wavelength, and thereby splits light reflected by the operating point (9) between the distance measuring device (4) and the camera apparatus (5), is provided.
    • 一种用于对测量对象(8)的表面(7)与测量装置(1)之间的距离进行非接触式检测以及用于表面(7)的同时非接触式视觉检测的测量装置(1)具有测量头 (2)保持距离测量装置(4),照相机装置(5)和照明装置(6),照明装置(6)照射测量对象的表面(7)上的工作点(9) 由相机装置(5)和测距装置(4)同时聚焦。 在光轴(10)上,在照明装置(6)和工作点(9)之间,具有透镜或反射光束的至少一个分色镜(12)的反射镜和过滤装置(11) 提供波长的功能,从而在距离测量装置(4)和照相机装置(5)之间分离由工作点(9)反射的光。
    • 29. 发明申请
    • Thermal turbomachine
    • 热涡轮机
    • US20060062664A1
    • 2006-03-23
    • US11249625
    • 2005-10-14
    • Nicolas Campino JohnsonMatthias HoebelJonas HurterChristoph Niederberger
    • Nicolas Campino JohnsonMatthias HoebelJonas HurterChristoph Niederberger
    • F01D5/20
    • F01D11/12F01D11/08F01D21/04
    • The invention discloses a thermal turbomachine having at least one row of rotor blades (1). At least one first rotor blade (1) has a greater radial length than the others and at the blade tip (2) is equipped with a first abrasive layer (72). At least one rotor blade (1) which has a shorter radial length than the first rotor blade (1) is equipped with a second abrasive layer (71) at the blade tip (2). The first abrasive layer (72) has a better cutting capacity and a lower thermal stability than the second abrasive layer (71). During commissioning of the thermal turbomachine, the first abrasive layer (72) is in contact with the abradable layer of the stator (8), and during continuous operation of the thermal turbomachine the second abrasive layer (71) is in contact with the abradable layer of the stator (8).
    • 本发明公开了一种具有至少一排转子叶片(1)的热涡轮机。 至少一个第一转子叶片(1)具有比其它第一转子叶片(1)更大的径向长度,并且在叶片尖端(2)上配备有第一研磨层(7,2N)。 具有比第一转子叶片(1)更短的径向长度的至少一个转子叶片(1)在叶片尖端(2)处装备有第二研磨层(7I 1)。 第一研磨层(7,2N)具有比第二研磨层(7 SUB)更好的切割能力和更低的热稳定性。 在热式涡轮机的调试期间,第一研磨层(7,2N)与定子(8)的可磨损层接触,并且在热涡轮机的连续操作期间,第二研磨层(7 1< 1>)与定子(8)的可磨损层接触。