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    • 2. 发明申请
    • PROJECTION EXPOSURE SYSTEM FOR MICROLITHOGRAPHY AND METHOD OF MONITORING A LATERAL IMAGING STABILITY
    • 用于微观计算的投影曝光系统和监测横向成像稳定性的方法
    • US20160266501A1
    • 2016-09-15
    • US14992702
    • 2016-01-11
    • Carl Zeiss SMT GmbH
    • Matthias MANGERArmin SCHOECHUlrich MUELLER
    • G03F7/20
    • G03F7/70191G03F7/70258G03F7/70591G03F7/7085
    • A projection exposure system (10) for microlithography. The system includes projection optics (12) configured to image mask structures into a substrate plane (16), an input diffraction element (28) which is configured to convert irradiated measurement radiation (21) into at least two test waves (30) directed onto the projection optics (12) with differing propagation directions, a detection diffraction element (34; 28) which is disposed in the optical path of the test waves (30) after the latter have passed through the projection optics (12) and is configured to produce a detection beam (36) from the test waves (30) which has a mixture of radiation portions of both test waves (30), a photo detector (38) disposed in the optical path of the detection beam (36) which is configured to record the radiation intensity of the detection beam (36), time resolved, and an evaluation unit which is configured to determine the lateral imaging stability of the projection optics (12) from the radiation intensity recorded.
    • 一种用于微光刻的投影曝光系统(10)。 该系统包括被配置成将掩模结构成像到衬底平面(16)中的投影光学器件(12),被配置为将照射的测量辐射(21)转换成至少两个测试波(30)的输入衍射元件(28) 具有不同传播方向的投影光学器件(12),检测衍射元件(34; 28),其被布置在经过投影光学器件(12)的测试波(30)的光路中,并被配置为 从具有两个测试波的辐射部分的混合物的测试波(30)产生检测光束(36),设置在检测光束(36)的光路中的光电检测器(38) 记录检测光束(36)的辐射强度,时间分辨率和被配置为根据记录的辐射强度确定投影光学器件(12)的横向成像稳定性的评估单元。
    • 9. 发明申请
    • MEASURING ARRANGEMENT FOR USE WHEN DETERMINING TRAJECTORIES OF FLYING OBJECTS
    • 用于确定飞行物体的轨迹时使用的测量装置
    • US20160350935A1
    • 2016-12-01
    • US15169104
    • 2016-05-31
    • Carl Zeiss SMT GmbH
    • Matthias MANGER
    • G06T7/20H04N5/225H04N7/18G03F7/20H05G2/00
    • G06T7/20G01P3/68G03F7/70033G03F7/7085G06T2207/30241H04N5/2252H04N5/2254H04N7/18H05G2/003H05G2/008
    • A measuring arrangement for use when determining trajectories of flying objects, wherein the measuring arrangement comprises at least one photodetector arrangement (411, 412, 421, 422, 780, 785, 880, 980) comprising a plurality of photodetector cells in a monolithic construction, wherein the photodetector arrangement is assigned exactly one imaging system (700, 750, 800, 900). During the operation of the measuring arrangement, images in each case a flying object situated in an object plane (OP) of the imaging system onto the photodetector arrangement situated in an image plane (IP) of the imaging system, and a time measuring device for measuring transit instants, wherein each of the transit instants corresponds to an instant at which an image of a flying object, generated in the image plane (IP) of the imaging system, respectively crosses a cell boundary between mutually adjacent photodetector cells in the photodetector arrangement.
    • 一种在确定飞行物体的轨迹时使用的测量装置,其中所述测量装置包括至少一个光电检测器装置(411,412,421,422,780,785,880,980),其包括整体结构中的多个光电探测器单元, 其中光电检测器装置被精确地分配一个成像系统(700,700,800,900)。 在测量装置的操作期间,每种情况下的图像是位于成像系统的物体平面(OP)中的飞行物体到位于成像系统的图像平面(IP)中的光电检测器装置上,以及用于 测量传输时刻,其中每个传输瞬间对应于在成像系统的图像平面(IP)中生成的飞行对象的图像分别跨越光电检测器装置中相互相邻的光电检测器单元之间的单元边界的瞬间 。
    • 10. 发明申请
    • METHOD FOR MEASURING AN OPTICAL SYSTEM
    • 测量光学系统的方法
    • US20130271749A1
    • 2013-10-17
    • US13913212
    • 2013-06-07
    • CARL ZEISS SMT GmbH
    • Thomas KORBChristian HETTICHMichael LAYHUlrich WEGMANNKarl-Heinz SCHUSTERMatthias MANGER
    • G01M11/02
    • G01N21/94G01M11/02G01N21/9501G03F7/70483G03F7/708G03F7/7085
    • First test beams (464a-d), after passing through an optical system on optical paths that differ in pairs, impinge on a first measurement region (461) at angles that differ in pairs with respect to the measurement plane. Second test beams (465a-d), after passing through the optical system on optical paths that differ in pairs, impinge on a second measurement region (462) at angles that differ in pairs, wherein the second region differs from the first. A value of a first measurement variable of the test beam at the first region is detected for each of the first test beams, and comparably for a second measurement variable at the second region for the second test beams. Impingement regions (467a-d) on reference surface(s) (466, 471) of the optical system are determined and a spatial diagnosis distribution of a property of the reference surface(s) for each test beam is calculated.
    • 第一测试光束(464a-d)在通过成对不同的光路上的光学系统之后,以相对于测量平面成对不同的角度照射在第一测量区域(461)上。 第二测试光束(465a-d)在穿过成对不同的光路上的光学系统之后,以成对不同的角度撞击第二测量区域(462),其中第二区域与第一区域不同。 对于第一测试光束中的每一个检测第一区域处的测试光束的第一测量变量的值,并且针对第二测试光束的第二测量变量的第二测量变量进行比较。 确定光学系统的参考表面(466,471)上的冲击区域(467a-d),并且计算每个测试光束的参考表面的属性的空间诊断分布。