Method for producing an optical assembly having at least two optical functional surfaces, an optical device and unit for carrying out the method
    1.
    发明授权
    Method for producing an optical assembly having at least two optical functional surfaces, an optical device and unit for carrying out the method 有权
    用于制造具有至少两个光学功能表面的光学组件的方法,用于执行该方法的光学装置和单元

    公开(公告)号:US09296161B2

    公开(公告)日:2016-03-29

    申请号:US13496089

    申请日:2010-09-13

    摘要: The invention relates to a method for producing an optical assembly, comprising at least two optical functional surfaces arranged in a fixed positional relationship to one another on a common supporting structure, wherein by means of a processing machine, in various process steps, at least two optical functional surfaces and at least one reference structure having a defined and measurable relative position to the optical functional surfaces are produced. The supporting structure remains rigidly connected to the processing machine until said process steps have been completed, and wherein the optical functional surfaces are then measured relative to the at least one reference structure, and any deviation from a target shape and target position is determined, after which said process steps are repeated at least once with modified actuation of the processing machine. The invention further relates to an optical device comprising an optical assembly produced in this way and to a unit for carrying out such a method.

    摘要翻译: 本发明涉及一种用于制造光学组件的方法,所述方法包括至少两个在共同的支撑结构上以彼此固定的位置关系布置的光学功能表面,其中通过加工机器,在各种工艺步骤中,至少两个 产生光学功能表面和至少一个具有与光学功能表面的限定且可测量的相对位置的参考结构。 支撑结构保持刚性地连接到加工机器,直到所述工艺步骤已经完成,并且其中然后相对于至少一个参考结构测量光学功能表面,并且在目标形状和目标位置之间的任何偏差在 其中所述处理步骤通过处理机的修改的致动重复至少一次。 本发明还涉及一种光学装置,其包括以这种方式制造的光学组件和用于执行这种方法的单元。

    Gas turbo set
    2.
    发明授权
    Gas turbo set 有权
    燃气涡轮组

    公开(公告)号:US07013652B2

    公开(公告)日:2006-03-21

    申请号:US10848155

    申请日:2004-05-19

    申请人: Andreas Gebhardt

    发明人: Andreas Gebhardt

    IPC分类号: F02C3/00 F23R3/50

    摘要: A gas turbo set comprises a compressor, combustion chamber and turbine, a common rotor shaft having arranged on it, within the compressor, a plurality of rows of compressor moving blades and, within the turbine, a plurality of rows of turbine moving blades, which alternate with guide vane rows of compressor guide vanes and turbine guide vanes fastened to a carrying structure surrounding the rotor shaft on the outside. Simplified mounting/demounting is achieved with the compressor guide vanes and/or the turbine guide vanes of a guide vane row held in each case in a plurality of separate annular segments together forming a complete ring with at least one guide vane row, and with the annular segments fastened releasably to the carrying structure such that the annular segments, together with the compressor or turbine guide vanes fastened to them, can be removed individually from the carrying structure, while maintaining the carrying structure.

    摘要翻译: 燃气涡轮机组包括压缩机,燃烧室和涡轮机,在其中布置有压缩机内的公共转子轴,多排压缩机活动叶片,以及在涡轮机内的多排涡轮动叶片,其中 与导向叶片排的压缩机导向叶片和涡轮导向叶片交替,固定到围绕外部的转子轴的承载结构。 简化的安装/拆卸是通过压缩机导向叶片和/或导向叶片排的涡轮引导叶片在每个壳体中保持在多个单独的环形段中来实现的,所述多个单独的环形段一起形成具有至少一个导向叶片排的完整的环, 环形段可释放地固定到承载结构上,使得环形段与压缩机或涡轮导向叶片紧固在一起,可以在保持承载结构的同时从承载结构单独移除。

    METHOD FOR PRODUCING AN OPTICAL ASSEMBLY HAVING AT LEAST TWO OPTICAL FUNCTIONAL SURFACES, AN OPTICAL DEVICE AND UNIT FOR CARRYING OUT THE METHOD
    4.
    发明申请
    METHOD FOR PRODUCING AN OPTICAL ASSEMBLY HAVING AT LEAST TWO OPTICAL FUNCTIONAL SURFACES, AN OPTICAL DEVICE AND UNIT FOR CARRYING OUT THE METHOD 有权
    用于生产具有至少两个光学功能表面的光学组件的方法,用于实施该方法的光学装置和装置

    公开(公告)号:US20120236400A1

    公开(公告)日:2012-09-20

    申请号:US13496089

    申请日:2010-09-13

    IPC分类号: G02B23/00 B23B1/00

    摘要: The invention relates to a method for producing an optical assembly, comprising at least two optical functional surfaces arranged in a fixed positional relationship to one another on a common supporting structure, wherein by means of a processing machine, in various process steps, at least two optical functional surfaces and at least one reference structure having a defined and measurable relative position to the optical functional surfaces are produced. The supporting structure remains rigidly connected to the processing machine until said process steps have been completed, and wherein the optical functional surfaces are then measured relative to the at least one reference structure, and any deviation from a target shape and target position is determined, after which said process steps are repeated at least once with modified actuation of the processing machine. The invention further relates to an optical device comprising an optical assembly produced in this way and to a unit for carrying out such a method.

    摘要翻译: 本发明涉及一种用于制造光学组件的方法,所述方法包括至少两个在共同的支撑结构上以彼此固定的位置关系布置的光学功能表面,其中通过加工机器,在各种工艺步骤中,至少两个 产生光学功能表面和至少一个具有与光学功能表面的限定且可测量的相对位置的参考结构。 支撑结构保持刚性地连接到加工机器,直到所述工艺步骤已经完成,并且其中然后相对于至少一个参考结构测量光学功能表面,并且在目标形状和目标位置之间的任何偏差在 其中所述处理步骤通过处理机的修改的致动重复至少一次。 本发明还涉及一种光学装置,其包括以这种方式制造的光学组件和用于执行这种方法的单元。

    Electrostatic deflection system for corpuscular radiation
    5.
    发明授权
    Electrostatic deflection system for corpuscular radiation 失效
    静电偏转系统用于红外辐射

    公开(公告)号:US07491946B2

    公开(公告)日:2009-02-17

    申请号:US11346666

    申请日:2006-02-03

    IPC分类号: H01J37/147

    CPC分类号: G21K1/087

    摘要: The invention is directed to electrostatic deflection systems for corpuscular beams which can be used particularly in microstructured and nanostructured applications in lithography installations or measuring equipment. According to the proposed object of the invention, the individual electrodes of a deflection system of this kind should permanently have and retain a very exact axially symmetric arrangement relative to one another. In the electrostatic deflection system according to the invention, rod-shaped electrodes are held in an axially symmetric arrangement in an inwardly hollow carrier through which a corpuscular beam can be directed. The carrier is formed of at least two, and at most four, carrier members which are connected to one another.

    摘要翻译: 本发明涉及用于微粒束的静电偏转系统,其可以特别用于光刻设备或测量设备中的微结构和纳米结构应用中。 根据本发明的提出的目的,这种偏转系统的各个电极应该永久地保持和保持相对于彼此的精确的轴向对称布置。 在根据本发明的静电偏转系统中,棒状电极被保持在向内空心载体中的轴向对称布置,通过该载体可以引导红细胞束。 载体由彼此连接的至少两个,最多四个载体构件形成。

    METHOD FOR MANUFACTURING A MIRROR COMPRISING AT LEAST ONE CAVITY AND OPTICAL MIRROR
    7.
    发明申请
    METHOD FOR MANUFACTURING A MIRROR COMPRISING AT LEAST ONE CAVITY AND OPTICAL MIRROR 有权
    用于制造包含至少一个孔和光学镜的镜子的方法

    公开(公告)号:US20140247512A1

    公开(公告)日:2014-09-04

    申请号:US14236515

    申请日:2011-08-01

    IPC分类号: G02B5/10

    摘要: The invention relates to a method for manufacturing a light weight optical mirror or a monolithic mirror comprising at least one cooling channel, the method comprising forming a mirror body by iteratively depositing a metallic powder in layers and applying, for each of the layers, heat at least in a subarea of this layer, thereby fusing or sintering the powder in this subarea and bonding it to a previously deposited layer, the powder remaining in an unfused state in at least one region, the method further comprising forming at least one cavity within the carrier by removing the unfused powder from said region and producing a mirror surface at a closed surface of the mirror body. The invention further relates to an optical mirror and to an optical device.

    摘要翻译: 本发明涉及一种用于制造轻质光学镜或包括至少一个冷却通道的单片反射镜的方法,该方法包括通过在层中迭代沉积金属粉末来形成镜体,并且对于每个层施加热量 至少在该层的子区域中,从而使该区域中的粉末熔融或烧结并将其粘合到预先沉积的层上,该粉末在至少一个区域中保持为未熔融状态,该方法还包括在该区域内形成至少一个空腔 通过从所述区域去除未熔融的粉末并在镜体的闭合表面处产生镜面。 本发明还涉及一种光学镜和一种光学装置。

    Gas turbo set
    9.
    发明申请
    Gas turbo set 有权
    燃气涡轮组

    公开(公告)号:US20050132707A1

    公开(公告)日:2005-06-23

    申请号:US10848155

    申请日:2004-05-19

    申请人: Andreas Gebhardt

    发明人: Andreas Gebhardt

    摘要: A gas turbo set comprises a compressor, combustion chamber and turbine, a common rotor shaft having arranged on it, within the compressor, a plurality of rows of compressor moving blades and, within the turbine, a plurality of rows of turbine moving blades, which alternate with guide vane rows of compressor guide vanes and turbine guide vanes fastened to a carrying structure surrounding the rotor shaft on the outside. Simplified mounting/demounting is achieved with the compressor guide vanes and/or the turbine guide vanes of a guide vane row held in each case in a plurality of separate annular segments together forming a complete ring with at least one guide vane row, and with the annular segments fastened releasably to the carrying structure such that the annular segments, together with the compressor or turbine guide vanes fastened to them, can be removed individually from the carrying structure, while maintaining the carrying structure.

    摘要翻译: 燃气涡轮机组包括压缩机,燃烧室和涡轮机,在其中布置有压缩机内的公共转子轴,多排压缩机活动叶片,以及在涡轮机内的多排涡轮动叶片,其中 与导向叶片排的压缩机导向叶片和涡轮导向叶片交替,固定到围绕外部的转子轴的承载结构。 简化的安装/拆卸是通过压缩机导向叶片和/或导向叶片排的涡轮引导叶片在每个壳体中保持在多个单独的环形段中来实现的,所述多个单独的环形段一起形成具有至少一个导向叶片排的完整的环, 环形段可释放地固定到承载结构上,使得环形段与压缩机或涡轮导向叶片紧固在一起,可以在保持承载结构的同时从承载结构单独移除。