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公开(公告)号：US20070070503A1
公开(公告)日：2007-03-29
申请号：US10578956
申请日：2004-11-12
申请人： David Boswell , Mark Dicker , Steven Winton
发明人： David Boswell , Mark Dicker , Steven Winton
IPC分类号： G02B5/18
CPC分类号： G03H1/028 , B41F11/02 , B41F19/02 , B41M1/04 , B41M1/06 , B41M1/10 , B41M1/12 , B41M1/22 , B41M1/24 , B42D25/328 , G03H1/0011 , G03H1/0244 , G03H2001/185 , G03H2250/40 , G03H2270/12 , G03H2270/23
摘要： There is provided an apparatus and a method of printing a diffraction grating. In particular, the present invention relates to diffraction gratings applied to a substrate (1), such as a hologram.
摘要翻译： 提供了一种印刷衍射光栅的装置和方法。 特别地，本发明涉及应用于诸如全息图等基板（1）的衍射光栅。
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公开(公告)号：US08015919B2
公开(公告)日：2011-09-13
申请号：US10578956
申请日：2004-11-12
申请人： David Boswell , Mark Dicker , Steven Winton
发明人： David Boswell , Mark Dicker , Steven Winton
IPC分类号： B41L35/14
CPC分类号： G03H1/028 , B41F11/02 , B41F19/02 , B41M1/04 , B41M1/06 , B41M1/10 , B41M1/12 , B41M1/22 , B41M1/24 , B42D25/328 , G03H1/0011 , G03H1/0244 , G03H2001/185 , G03H2250/40 , G03H2270/12 , G03H2270/23
摘要： There is provided an apparatus and a method of printing a diffraction grating. In particular, the present invention relates to diffraction gratings applied to a substrate (1), such as a hologram.
摘要翻译： 提供了一种印刷衍射光栅的装置和方法。 特别地，本发明涉及应用于诸如全息图等基板（1）的衍射光栅。
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公开(公告)号：US08453570B2
公开(公告)日：2013-06-04
申请号：US13172921
申请日：2011-06-30
申请人： David Boswell , Mark Dicker , Steven Winton
发明人： David Boswell , Mark Dicker , Steven Winton
IPC分类号： B41F31/00
CPC分类号： G03H1/028 , B41F11/02 , B41F19/02 , B41M1/04 , B41M1/06 , B41M1/10 , B41M1/12 , B41M1/22 , B41M1/24 , B42D25/328 , G03H1/0011 , G03H1/0244 , G03H2001/185 , G03H2250/40 , G03H2270/12 , G03H2270/23
摘要： There is provided an apparatus and a method of printing a diffraction grating. In particular, the present invention relates to diffraction gratings applied to a substrate, such as a hologram.
摘要翻译： 提供了一种印刷衍射光栅的装置和方法。 特别地，本发明涉及应用于诸如全息图等基板的衍射光栅。
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公开(公告)号：US08961139B2
公开(公告)日：2015-02-24
申请号：US12925138
申请日：2010-10-14
申请人： Askari Badre-Alam , David Boswell , Donald Morris , Wayne Winzenz
发明人： Askari Badre-Alam , David Boswell , Donald Morris , Wayne Winzenz
CPC分类号： B64C11/008 , F01D25/04 , Y10S416/50 , Y10T29/4902 , Y10T74/2127
摘要： An aircraft system/method for propeller balancing. The system includes an inboard driver with a first and second inboard electromagnetic coil, the inboard driver and the first counterweight balancing rotor and the second counterweight balancing rotor centered around the aircraft propeller shaft rotating machine member with the first inboard electromagnetic coil proximate the first inboard magnets of the first counterweight balancing rotor, with the inboard electromagnetic coil driver proximate the rotation axis of the aircraft propeller shaft rotating machine member and the first counterweight balancing rotor outboard of the inboard electromagnetic coil driver with the first inboard electromagnetic coil generating a electromagnetic field to electromagnetically step the first inboard magnets of the at least first counterweight balancing rotor to electromagnetically actuate rotational movement of the first counterweight balancing rotor around the rotating machine member and relative to the inboard electromagnetic coil driver to a first rotor held balancing position.
摘要翻译： 一种用于螺旋桨平衡的飞机系统/方法。 该系统包括内部驱动器，其具有第一和第二内侧电磁线圈，内侧驱动器和第一配重平衡转子和第二配重平衡转子以飞行器螺旋桨轴旋转机器构件为中心，第一内侧电磁线圈靠近第一内侧磁体 第一配重平衡转子的内侧电磁线圈驱动器靠近飞机螺旋桨轴旋转机构的旋转轴线，并且内侧电磁线圈驱动器的第一配重平衡转子外侧与第一内侧电磁线圈产生电磁场以电磁 将所述至少第一配重平衡转子的第一内侧磁体逐步地电磁致动所述第一配重平衡转子围绕所述旋转机械构件并相对于所述内侧电磁线圈驱动器到第一r otor保持平衡位置。
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公开(公告)号：US08961140B2
公开(公告)日：2015-02-24
申请号：US13273341
申请日：2011-10-14
CPC分类号： B64C11/008 , F01D25/04 , Y10S416/50 , Y10T29/49332
摘要： An aircraft system and method with a first counterweight rotating balancing rotor mass concentration, and a second counterweight rotating balancing rotor mass concentration to balance a first aircraft propeller. The system includes an inboard electromagnetic coil driver with a first inboard electromagnetic coil, and a second inboard electromagnetic coil, the inboard electromagnetic coil driver and the first counterweight balancing rotor and the second counterweight balancing rotor centered around the aircraft propeller shaft rotating machine member. The system/method utilizes a first control system controller to control the coils and position the mass concentrations to balance the first aircraft propeller. The system/method includes a third counterweight rotating balancing rotor mass concentration, and a fourth counterweight rotating balancing rotor mass concentration to balance a second aircraft propeller which positioned and controlled by a second control system controller.
摘要翻译： 一种具有第一配重旋转平衡转子质量浓度的飞行器系统和方法，以及用于平衡第一飞行器螺旋桨的第二配重旋转平衡转子质量集中。 该系统包括具有第一内侧电磁线圈的内侧电磁线圈驱动器和第二内置电磁线圈，内侧电磁线圈驱动器和第一配重平衡转子和以飞行器传动轴转动机构为中心的第二配重平衡转子。 系统/方法利用第一控制系统控制器来控制线圈并定位质量浓度以平衡第一飞机螺旋桨。 该系统/方法包括第三配重旋转平衡转子质量浓度，以及第四配重旋转平衡转子质量浓度以平衡由第二控制系统控制器定位和控制的第二飞行器螺旋桨。
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公开(公告)号：US20120269626A1
公开(公告)日：2012-10-25
申请号：US13273341
申请日：2011-10-14
CPC分类号： B64C11/008 , F01D25/04 , Y10S416/50 , Y10T29/49332
摘要： An aircraft system and method with a first counterweight rotating balancing rotor mass concentration, and a second counterweight rotating balancing rotor mass concentration to balance a first aircraft propeller. The system includes an inboard electromagnetic coil driver with a first inboard electromagnetic coil, and a second inboard electromagnetic coil, the inboard electromagnetic coil driver and the first counterweight balancing rotor and the second counterweight balancing rotor centered around the aircraft propeller shaft rotating machine member. The system/method utilizes a first control system controller to control the coils and position the mass concentrations to balance the first aircraft propeller. The system/method includes a third counterweight rotating balancing rotor mass concentration, and a fourth counterweight rotating balancing rotor mass concentration to balance a second aircraft propeller which positioned and controlled by a second control system controller.
摘要翻译： 一种具有第一配重旋转平衡转子质量浓度的飞行器系统和方法，以及用于平衡第一飞行器螺旋桨的第二配重旋转平衡转子质量集中。 该系统包括具有第一内侧电磁线圈的内侧电磁线圈驱动器和第二内置电磁线圈，内侧电磁线圈驱动器和第一配重平衡转子和以飞行器传动轴转动机构为中心的第二配重平衡转子。 系统/方法利用第一控制系统控制器来控制线圈并定位质量浓度以平衡第一飞机螺旋桨。 该系统/方法包括第三配重旋转平衡转子质量浓度，以及第四配重旋转平衡转子质量浓度以平衡由第二控制系统控制器定位和控制的第二飞行器螺旋桨。
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公开(公告)号：US20110197703A1
公开(公告)日：2011-08-18
申请号：US12925138
申请日：2010-10-14
申请人： Askari Badre-Alam , David Boswell , Donald Morris , Wayne Winzenz
发明人： Askari Badre-Alam , David Boswell , Donald Morris , Wayne Winzenz
CPC分类号： B64C11/008 , F01D25/04 , Y10S416/50 , Y10T29/4902 , Y10T74/2127
摘要： An aircraft system/method for propeller balancing. The system includes an inboard driver with a first and second inboard electromagnetic coil, the inboard driver and the first counterweight balancing rotor and the second counterweight balancing rotor centered around the aircraft propeller shaft rotating machine member with the first inboard electromagnetic coil proximate the first inboard magnets of the first counterweight balancing rotor, with the inboard electromagnetic coil driver proximate the rotation axis of the aircraft propeller shaft rotating machine member and the first counterweight balancing rotor outboard of the inboard electromagnetic coil driver with the first inboard electromagnetic coil generating a electromagnetic field to electromagnetically step the first inboard magnets of the at least first counterweight balancing rotor to electromagnetically actuate rotational movement of the first counterweight balancing rotor around the rotating machine member and relative to the inboard electromagnetic coil driver to a first rotor held balancing position.
摘要翻译： 一种用于螺旋桨平衡的飞机系统/方法。 该系统包括内部驱动器，其具有第一和第二内侧电磁线圈，内侧驱动器和第一配重平衡转子和第二配重平衡转子以飞行器螺旋桨轴旋转机器构件为中心，第一内侧电磁线圈靠近第一内侧磁体 第一配重平衡转子的内侧电磁线圈驱动器靠近飞机螺旋桨轴旋转机构的旋转轴线，并且内侧电磁线圈驱动器的第一配重平衡转子外侧与第一内侧电磁线圈产生电磁场以电磁 将所述至少第一配重平衡转子的第一内侧磁体逐步地电磁致动所述第一配重平衡转子围绕所述旋转机械构件并相对于所述内侧电磁线圈驱动器到第一r otor保持平衡位置。
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公开(公告)号：USD425071S
公开(公告)日：2000-05-16
申请号：US93523
申请日：1998-09-11
申请人： David Boswell
设计人： David Boswell
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