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    • 5. 发明授权
    • Automatic programming apparatus and control command generating method
    • 自动编程设备和控制命令生成方法
    • US09523966B2
    • 2016-12-20
    • US14110848
    • 2011-06-23
    • Susumu MatsubaraKenji IriguchiDaisuke FujinoTomonori Sato
    • Susumu MatsubaraKenji IriguchiDaisuke FujinoTomonori Sato
    • G05B11/01G05B19/4093
    • G05B11/01G05B19/40931G05B2219/36336G05B2219/36337Y02P90/265
    • An automatic programming apparatus includes a machining-shape generating unit configured to generate second machining shapes for each of machining processes from each of a plurality of first machining shapes input from outside; a machining-order editing unit configured to receive an input of execution order of the machining processes; a machining-shape adjusting unit configured to extend, among a plurality of the second machining shapes having a same tool direction, which is a direction that a tool pierces, one of the second machining shapes in a direction opposite to the tool direction, delete, from the other machining shape that overlaps the one second machining shape because of the extension of the one second machining shape, a portion of the overlap, and generate a third machining shape; and a control-command generating unit configured to generate, based on the third machining shape and the input execution order, a control command.
    • 一种自动编程设备,包括:加工形状生成单元,被配置为从从外部输入的多个第一加工形状中的每一个生成用于每个加工过程的第二加工形状; 加工订单编辑单元,被配置为接收所述加工处理的执行顺序的输入; 一种加工形状调整单元,被构造成在具有与刀具方向相反的方向上的所述第二加工形状中的一个的刀具方向上具有相同刀具方向的多个第二加工形状中, 由于一个第二加工形状的延伸而与另一个加工形状重叠的另一个加工形状,一部分重叠并产生第三加工形状; 以及控制指令生成单元,被配置为基于所述第三加工形状和所述输入执行顺序来生成控制命令。
    • 6. 发明授权
    • Method for configuration and/or equipment of a vehicle cabin, in particular of an aircraft
    • 用于车辆特别是飞行器的车辆的配置和/或设备的方法
    • US09513622B2
    • 2016-12-06
    • US13641269
    • 2011-04-14
    • Tobias Schmidt-SchäfferBenjamin BeckerUlrich Seifert
    • Tobias Schmidt-SchäfferBenjamin BeckerUlrich Seifert
    • G06G7/48G05B19/4093G06F17/50B64F5/00G05B17/02
    • G05B19/40931B64F5/00G05B17/02G05B2219/35152G05B2219/35155G06F17/50G06F17/5095G06F2217/46Y02P90/265
    • The invention relates to a method for the automatic configuration and/or equipment of a vehicle cabin (1), more particularly of an aircraft, wherein the cabin (1) is subdivided into a plurality of zones (A, B, C, D, E) and the method furthermore comprises the following steps: —selection of a plurality of individual modules (11a, 11b, 11c) from a pool of individual modules, —automatic connection of the selected individual modules (11a, 11b, 11c) to form a desired module package (10a), —automatic calculation of a desired module package configuration value, —automatic comparison of the desired module package configuration value with predefined module package configuration values which respectively correspond to a technically prevalidated module package, —automatic selection of the module package (10b) whose module package configuration value deviates the least from the desired module package configuration value, —arrangement of the selected module package (10b) in a zone (A, B, C, D, E) of the cabin (1). The invention furthermore relates to a system and a computer program.
    • 本发明涉及一种用于车辆舱(1)的自动配置和/或设备的方法,更具体地涉及一种飞行器,其中舱室(1)被细分为多个区域(A,B,C,D, E),并且该方法还包括以下步骤: - 从各个模块池选择多个单独的模块(11a,11b,11c), - 所选择的各个模块(11a,11b,11c)的自动连接以形成 期望的模块封装(10a), - 自动计算期望的模块封装配置值, - 所需模块封装配置值与预定义的模块封装配置值的自动比较,其分别对应于技术上预先验证的模块封装, - 自动选择 模块封装(10b),其模块封装配置值至少与期望的模块封装配置值偏离,所选择的模块封装(10b)在区域(A,B ,C,D,E)。 本发明还涉及一种系统和计算机程序。
    • 8. 发明申请
    • METHOD FOR CONFIGURATION AND/OR EQUIPMENT OF A VEHICLE CABIN, IN PARTICULAR OF AN AIRCRAFT
    • 一种车辆特别是飞机组态和/或设备的方法
    • US20130066602A1
    • 2013-03-14
    • US13641269
    • 2011-04-14
    • Tobias Schmidt-SchäfferBenjamin BeckerUlrich Seifert
    • Tobias Schmidt-SchäfferBenjamin BeckerUlrich Seifert
    • G06F17/50
    • G05B19/40931B64F5/00G05B17/02G05B2219/35152G05B2219/35155G06F17/50G06F17/5095G06F2217/46Y02P90/265
    • The invention relates to a method for the automatic configuration and/or equipment of a vehicle cabin (1), more particularly of an aircraft, wherein the cabin (1) is subdivided into a plurality of zones (A, B, C, D, E) and the method furthermore comprises the following steps: selection of a plurality of individual modules (11a, 11b, 11c) from a pool of individual modules, automatic connection of the selected individual modules (11a, 11b, 11c) to form a desired module package (10a), automatic calculation of a desired module package configuration value, automatic comparison of the desired module package configuration value with predefined module package configuration values which respectively correspond to a technically prevalidated module package, automatic selection of the module package (10b) whose module package configuration value deviates the least from the desired module package configuration value, arrangement of the selected module package (10b) in a zone (A, B, C, D, E) of the cabin (1). The invention furthermore relates to a system and a computer program.
    • 本发明涉及一种用于车辆舱(1)的自动配置和/或设备的方法,更具体地涉及一种飞行器,其中舱室(1)被细分为多个区域(A,B,C,D, E),并且该方法还包括以下步骤:从各个模块池中选择多个单独的模块(11a,11b,11c),自动连接所选择的各个模块(11a,11b,11c)以形成期望的 模块封装(10a),自动计算期望的模块封装配置值,将期望的模块封装配置值与分别对应于技术上预先验证的模块封装的预定模块封装配置值进行自动比较,模块封装(10b)的自动选择 其模块封装配置值至少与期望的模块封装配置值偏离,所选择的模块封装(10b)在区域(A,B,C,D,E)中的布置 客舱(1)。 本发明还涉及一种系统和计算机程序。
    • 10. 发明授权
    • Finding minimum remaining float for a pattern of non-uniform sized features
    • 找到不均匀尺寸特征图案的最小剩余浮动
    • US07979236B2
    • 2011-07-12
    • US12206381
    • 2008-09-08
    • Bruce A. WilsonPaul C. Hollingshead
    • Bruce A. WilsonPaul C. Hollingshead
    • G01B7/14
    • G05B19/40931G05B2219/37441G05B2219/37617Y02P90/265
    • A method for analyzing tolerances for features for an object. A framework may be created from the plurality of features for the object. The framework may be fitted to a plurality of manufactured features for the object based on the plurality of features to form a fit framework. A remaining clearance may be identified between each of a plurality of manufactured sizes associated with the plurality of features and each of plurality of virtual conditions for the plurality of features to form a plurality of remaining clearances. A plurality of remaining clearance geometric shapes may be formed from the plurality of remaining clearances. The plurality of remaining clearance features may be positioned around a single true position. A common region may be identified from between the plurality of remaining clearances. A minimum remaining float may be identified from the common region. A resulting pattern transformation may be determined.
    • 一种用于分析对象特征的公差的方法。 可以从对象的多个特征创建框架。 基于多个特征,框架可以被安装到用于对象的多个制造特征以形成配合框架。 可以在与多个特征相关联的多个制造尺寸中的每一个与用于多个特征的多个虚拟条件中的每一个之间识别剩余间隙,以形成多个剩余间隙。 可以从多个剩余间隙形成多个剩余的间隙几何形状。 多个剩余的间隙特征可以围绕单个真实位置定位。 可以从多个剩余间隙之间识别公共区域。 可以从公共区域识别最小剩余浮动。 可以确定所得到的图案变换。