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    • 1. 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。
    • 2. 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。
    • 4. 发明申请
    • ASSEMBLY AND METHOD FOR VERIFYING A REAL MODEL USING A VIRTUAL MODEL AND USE IN AIRCRAFT CONSTRUCTION
    • 使用虚拟模型验证实际模型的组装和方法,并在飞机结构中使用
    • US20120303336A1
    • 2012-11-29
    • US13525970
    • 2012-06-18
    • Benjamin BECKERHolger SCHMIDTIlke Oencue CALIS
    • Benjamin BECKERHolger SCHMIDTIlke Oencue CALIS
    • G06F17/50
    • G01B11/03B64F5/00G01B21/04G06F17/5095
    • An arrangement for verifying a real model by using a virtual model is provided. The arrangement comprises a real model which has a real coordinate system, a virtual model which has a virtual coordinate system, a first position determination element, which is applied in/on the real model in a defined manner, and a real tool element, which is arranged in the real model. A position and/or orientation of the real tool element in the real model can be determined relative to the first position determination element. An operation of the real tool element can be triggered in the real model, and the operation of the real tool element can be imaged in the virtual model. The operation of the real tool element in the real model and the imaged operation in the virtual model can be logically or functionally assigned to one another.
    • 提供了一种通过使用虚拟模型验证真实模型的布置。 该装置包括具有真实坐标系的真实模型,具有虚拟坐标系的虚拟模型,以确定的方式应用于实际模型中的第一位置确定元件和实际工具元素,其中 被安排在真实模型中。 可以相对于第一位置确定元件确定真实模型中的真实工具元素的位置和/或取向。 可以在真实模型中触发真正的工具元素的操作,并且可以在虚拟模型中对真正的工具元素的操作进行成像。 实际模型中的真实工具元素的操作和虚拟模型中的成像操作可以在逻辑上或功能上彼此分配。
    • 6. 发明授权
    • Configuration-controlled dynamic generation of product data for complex products
    • 用于复杂产品的配置控制动态生成产品数据
    • US08560287B2
    • 2013-10-15
    • US13414943
    • 2012-03-08
    • Tobias Schmidt-SchäfferMilton AmadorUlrich SeifertUlf SchillerBenjamin Becker
    • Tobias Schmidt-SchäfferMilton AmadorUlrich SeifertUlf SchillerBenjamin Becker
    • G06F9/455
    • G06F17/5095G06F2217/02G06F2217/06G06F2217/46
    • A method and a device for the computer-assisted generation of a construction plan for modular aircraft components on the basis of already validated partial module construction plans for the individual modules wherein at least one element is assigned to a respective partial module construction plan, and in this manner a hierarchy is defined that comprises a higher, module level and a lower, element level, with the method comprising: re-utilizing at least one of the already validated partial module construction plans; depending on user input, re-specifying at the element level one of the at least one element in one of the partial module construction plans to obtain an individualized partial module construction plan; validating, only at the module level, a combination of one of the partial module construction plans with the individualized partial module construction plan; and in the case of successful validation, composing the partial module construction plans of the combination validated in this manner, to obtain the construction plan.
    • 一种用于计算机辅助生成模块化飞机部件的施工计划的方法和装置,其基于已经验证的用于各个模块的部分模块构造计划,其中至少一个元件被分配给相应的部分模块构造计划,并且 这种方式被定义为包括较高的模块级和较低的元素级别的层次结构,该方法包括:重新利用已验证的部分模块构造计划中的至少一个; 取决于用户输入,在部分模块构造计划之一中的至少一个元素的元素级别上重新指定以获得个性化的部分模块构造计划; 仅在模块级验证部分模块构建计划之一与个性化部分模块构建计划的组合; 在成功验证的情况下,组合以这种方式验证的组合部分模块建设计划,以获得施工计划。
    • 7. 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
    • US20130035906A1
    • 2013-02-07
    • US13641234
    • 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, more particularly of an aircraft, wherein the cabin (1) is subdivided into a plurality of zones (A, B, C, D, E) and wherein at least one parameter zone (A, C, E) and one dynamic zone (B, D) are provided, comprising the following steps: —selection of one or more individual modules from a pool of individual modules, —automatic arrangement of the at least one selected individual module in the parameter zone in accordance with at least one predetermined individual module parameter for the complete configuration of the meter zone, —selection of one or more individual components from a pool of individual components, —automatic calculation of an individual component configuration of the dynamic zone in accordance with the arrangement of the individual modules in the parameter zone and automatic arrangement of individual components in the dynamic zone in accordance with the calculated individual component configuration. The invention furthermore relates to a system and a computer program.
    • 本发明涉及一种用于车辆特别是飞机的自动配置和/或设备的方法,其中舱室(1)被细分为多个区域(A,B,C,D,E)和 其中提供至少一个参数区域(A,C,E)和一个动态区域(B,D),包括以下步骤: - 从单个模块池中选择一个或多个单独模块, - 自动排列 根据用于仪表区域的完整配置的至少一个预定的单独模块参数,从参数区域中选择一个或多个单个组件的至少一个选定的单独模块, - 个体组件的自动计算 根据参数区域中各个模块的布置,动态区域的组件配置和动态区域中各个组件的自动排列,根据计算出的 单个组件配置。 本发明还涉及一种系统和计算机程序。