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1. 发明授权

US4885714A Calculator having a user-accessible object stack for the uniform application of mathematical functions and logical operations to a multiplicity of object types 失效
标题翻译：计算器具有用户可访问对象堆栈，用于将数学函数和逻辑操作统一应用于多种对象类型
公开(公告)号：US4885714A
公开(公告)日：1989-12-05
申请号：US923933
申请日：1986-10-27
申请人： Gabe L. Eisenstein , Laurence W. Grodd , Paul J. McClellan , Robert M. Miller , Charles M. Patton , William C. Wickes
发明人： Gabe L. Eisenstein , Laurence W. Grodd , Paul J. McClellan , Robert M. Miller , Charles M. Patton , William C. Wickes
IPC分类号： G06F9/44 , G06F15/02
CPC分类号： G06F9/44 , G06F15/02
摘要： A calculator is defined by a user-interface centered around a last in first out stack of mathematical or logical objects, that is both visible and accessible to a user. Objects may be any of a number of different types, each type characterized by specific logical or mathematical rules. Calculator operations are provided that may be applied in a uniform manner to the objects, affecting either or both the internal composition of the objects or the external positions and number of the objects on the stack. Objects of different types are distinguished upon entry on the stack and in visible display by characteristic prefix and postfix symbols, and can be entered from a keyboard or created dynamically as the result of calculator operations.
摘要翻译：计算器由围绕数学或逻辑对象的最后一个堆栈的用户界面定义，这是用户可见和可访问的。对象可以是多种不同类型中的任何一种，每种类型以特定的逻辑或数学规则为特征。提供了可以以均匀的方式应用于对象的计算器操作，影响对象的内部组成或者堆叠上的对象的外部位置和数量。不同类型的对象在堆栈上进入并通过特征前缀和后缀符号进行可见显示时被区分，并且可以从键盘输入或作为计算器操作的结果动态创建。

2. 发明授权

US08844553B2 Passive boundary layer bleed system for nacelle inlet airflow control 有权
标题翻译：被动边界层排气系统，用于机舱入口气流控制
公开(公告)号：US08844553B2
公开(公告)日：2014-09-30
申请号：US12446786
申请日：2006-10-12
申请人： Steven H. Zysman , Wesley K. Lord , Robert M. Miller , Oliver V. Atassi
发明人： Steven H. Zysman , Wesley K. Lord , Robert M. Miller , Oliver V. Atassi
IPC分类号： F02C7/04 , F02C7/045 , F02K3/06 , B64D33/02
CPC分类号： F02C7/04 , B64D33/02 , B64D2033/0226 , F02C7/045 , F05D2250/324 , F05D2250/71 , F05D2270/17 , Y10T137/0536
摘要： A gas turbine engine system includes a nacelle having a pressure side and a suction side. A passage extends between the pressure side and the suction side that permits airflow from the pressure side to the suction side. The passage receives turbulent airflow over the nacelle to produce a laminar airflow over the nacelle aft of the passage to thereby reduce drag on the nacelle.
摘要翻译：燃气涡轮发动机系统包括具有压力侧和吸力侧的机舱。通道在压力侧和吸力侧之间延伸，允许从压力侧到吸力侧的气流。通道在机舱上接收湍流气流，以在通道后面的机舱上方产生层流气流，从而减少机舱上的阻力。

3. 发明授权

US07268901B2 Intelligent printing by a kiosk 有权
标题翻译：通过信息亭进行智能打印
公开(公告)号：US07268901B2
公开(公告)日：2007-09-11
申请号：US09916894
申请日：2001-07-26
申请人： Jon A. Brewster , Kenneth H. Bronstein , Robert M. Miller , Kenneth Oar
发明人： Jon A. Brewster , Kenneth H. Bronstein , Robert M. Miller , Kenneth Oar
IPC分类号： G06F3/12 , G06K15/00
CPC分类号： G07F17/0042 , G07F9/026 , G07F17/26
摘要： A publication is distributed by an automated publication delivery system. Activity around a physical location of the automated publication delivery system is monitored. In response to detection of an increased activity level around the physical location of the automated publication delivery system, additional copies of the publication are printed for distribution. For example, the automated publication delivery system is a kiosk and the publication is a newspaper. Monitoring is performed, for example, using a microphone to monitor noise level, an optical sensor to detect movement near the automated publication delivery system, and/or a motion detector to detect movement near the automated publication delivery system.
摘要翻译：出版物由自动发布系统分发。围绕自动出版物传送系统的实际位置的活动进行监控。响应于检测到自动出版物传送系统的物理位置周围的活动水平增加，印刷出版物的附加副本以进行分发。例如，自动出版物传送系统是一个报亭，出版物是报纸。例如，使用麦克风来监视噪声水平进行监视，用于检测自动发布传送系统附近的移动的光学传感器和/或用于检测自动发布传送系统附近的运动的运动检测器。

4. 发明授权

US07261787B2 Method of making a formable hockey stick blade 有权
标题翻译：制作成形曲棍球棒刀的方法
公开(公告)号：US07261787B2
公开(公告)日：2007-08-28
申请号：US10974828
申请日：2004-10-28
申请人： Alain Bellefleur , Win Fream , Robert M. Miller , Vincent Borbone
发明人： Alain Bellefleur , Win Fream , Robert M. Miller , Vincent Borbone
IPC分类号： A63B59/14 , B32B37/00
CPC分类号： B29C43/18 , B29C70/865 , B29K2105/04 , B29K2105/06 , B29K2105/0827 , B29L2031/52 , B29L2031/5227
摘要： The invention provides a method of making a formable hockey stick blade, the method comprising: (a) providing a core having a blade element with a thickness, the core being made of expandable foam having a Poisson ratio of at least 0.33; (b) forming a preformed stick blade by wrapping the core with a layer of fibers pre-impregnated with a thermoplastic material; (c) placing the preformed stick blade in a mold; (d) applying heat and pressure to the mold for bringing the thermoplastic material to its amorphous form and for compressing the preformed stick blade such that the thickness of the blade element of the core is reduced; (e) cooling the mold such that the thermoplastic material is set; and (f) removing the formable stick blade from the mold.
摘要翻译：本发明提供一种制造可成形曲棍球棒刀的方法，该方法包括：（a）提供具有厚度的刀片元件的芯，该芯由泊松比为至少0.33的可膨胀泡沫制成; （b）通过用预先浸渍有热塑性材料的纤维层包裹芯来形成预成型的棒状刀片; （c）将预成型的棒状刀片放置在模具中; （d）向模具施加热量和压力，以使热塑性材料成为非晶态并压缩预成形的棒状刀片，使得芯部的刀片元件的厚度减小; （e）冷却模具使得热塑性材料被固定; 和（f）从模具中取出可成型的棒状刀片。

5. 发明申请

US20100074739A1 PASSIVE BOUNDARY LAYER BLEED SYSTEM FOR NACELLE INLET AIRFLOW CONTROL 有权
标题翻译：用于空气入口空气流量控制的被动边界层系统
公开(公告)号：US20100074739A1
公开(公告)日：2010-03-25
申请号：US12446786
申请日：2006-10-12
申请人： Steven H. Zysman , Wesley K. Lord , Robert M. Miller , Oliver V. Atassi
发明人： Steven H. Zysman , Wesley K. Lord , Robert M. Miller , Oliver V. Atassi
IPC分类号： F01D25/24
CPC分类号： F02C7/04 , B64D33/02 , B64D2033/0226 , F02C7/045 , F05D2250/324 , F05D2250/71 , F05D2270/17 , Y10T137/0536
摘要： A gas turbine engine system includes a nacelle having a pressure side and a suction side. A passage extends between the pressure side and the suction side that permits airflow from the pressure side to the suction side. The passage receives turbulent airflow over the nacelle to produce a laminar airflow over the nacelle aft of the passage to thereby reduce drag on the nacelle.
摘要翻译：燃气涡轮发动机系统包括具有压力侧和吸力侧的机舱。通道在压力侧和吸力侧之间延伸，允许从压力侧到吸力侧的气流。通道在机舱上接收湍流气流，以在通道后面的机舱上方产生层流气流，从而减少机舱上的阻力。

6. 发明授权

US07611180B1 Robotic end of arm tool method and apparatus 有权
标题翻译：手臂工具方法和装置的机器人末端
公开(公告)号：US07611180B1
公开(公告)日：2009-11-03
申请号：US11493953
申请日：2006-07-27
申请人： Trent P. Fisher , John M Westbeld , Robert M. Miller , Jason R. Heinz
发明人： Trent P. Fisher , John M Westbeld , Robert M. Miller , Jason R. Heinz
IPC分类号： B25J9/00 , B25J15/06
CPC分类号： B25J15/0616 , B25J15/0052 , B25J15/0061
摘要： An end of arm tool has a mounting bracket mounting the end of arm tool to the robot arm for movement therewith and has a plurality of operating mechanisms mounted to the mounting bracket, a plurality of gripping devices each operatively connected to a respective operating mechanism and movable along a path, and a plurality of individual motors each operatively connected to a respective gripping device for moving the respective gripping device along its respective path. At least one programmable controller for operating the motors is provided to adjust the positions of the gripping devices along their respective paths to one of a plurality of predetermined positions established by the controller for gripping the article and to position the end of arm tool adjacent the article so that at least one of the gripping devices grips the article.
摘要翻译：手臂工具的末端具有安装支架，其将手臂工具的端部安装到机器人手臂以与其一起运动，并且具有安装到安装支架的多个操作机构，多个夹紧装置，每个夹紧装置可操作地连接到相应的操作机构并且可移动以及多个单独的电动机，每个电动机可操作地连接到相应的夹持装置，用于沿相应的路径移动相应的夹紧装置。提供用于操作马达的至少一个可编程控制器，用于将夹持装置沿其相应路径的位置调整到由控制器建立的多个预定位置中的一个，用于夹持物品并将手臂工具的末端邻近物品使得握持装置中的至少一个夹持物品。

7. 发明授权

US09001205B2 System and methods for controlling a surveying device 有权
标题翻译：用于控制测量装置的系统和方法
公开(公告)号：US09001205B2
公开(公告)日：2015-04-07
申请号：US13302128
申请日：2011-11-22
申请人： Mikael W. Nordenfelt , Marc A. Howell , Robert M. Miller , Volker Koehler , Omar Soubra , Nico Becke
发明人： Mikael W. Nordenfelt , Marc A. Howell , Robert M. Miller , Volker Koehler , Omar Soubra , Nico Becke
IPC分类号： H04N7/18 , G01C3/08 , G01C9/00 , H04N5/232
CPC分类号： H04N7/183 , H04N5/232 , H04N5/23216 , H04N7/18
摘要： A system and methods are provided for controlling a surveying device. In one embodiment, a method includes displaying a control screen including image data captured by a surveying device, detecting an input associated with the control screen, and determining a control command for the surveying device based on the input associated with the control screen. The method may further include controlling operation of the surveying device based on the control command, wherein the surveying device is configured to rotate in one more of a horizontal and vertical direction based on the control command. The device and methods may advantageously allow for precise pointing of a surveying device and translation of input position to surveying device commands.
摘要翻译：提供了一种用于控制测量装置的系统和方法。在一个实施例中，一种方法包括显示包括由测量装置捕获的图像数据的控制屏幕，检测与控制屏幕相关联的输入，以及基于与控制屏幕相关联的输入来确定测量装置的控制命令。该方法还可以包括基于控制命令来控制测量装置的操作，其中测量装置被配置为基于控制命令沿水平和垂直方向中的多个方向旋转。装置和方法可以有利地允许测量装置的精确指向和输入位置的平移到测量装置命令。

8. 发明授权

US08839805B2 Passive boundary layer bleed system for nacelle inlet airflow control 有权
公开(公告)号：US08839805B2
公开(公告)日：2014-09-23
申请号：US12428582
申请日：2009-04-23
申请人： Steven H. Zysman , Wesley K. Lord , Robert M. Miller , Oliver V. Atassi
发明人： Steven H. Zysman , Wesley K. Lord , Robert M. Miller , Oliver V. Atassi
IPC分类号： F02K3/06 , F02C7/04 , F02C7/045 , B64D33/02
CPC分类号： F02C7/04 , B64D33/02 , B64D2033/0226 , B64D2033/0286 , F05D2240/14 , F05D2260/60 , F05D2270/17 , Y10T137/0536
摘要： A gas turbine engine system includes a nacelle having a pressure side and a suction side. A passage extends between the pressure side and the suction side that permits airflow from the pressure side to the suction side. The passage receives turbulent airflow over the nacelle to produce a laminar airflow over the nacelle aft of the passage to thereby reduce drag on the nacelle.

9. 发明申请

US20120034409A1 FLOOR MAT WITH INTEGRALLY MOLDED CARPETING, AND ASSOCIATED INJECTION MOLD 有权
标题翻译：具有整体成型的地毯和相关的注塑模具
公开(公告)号：US20120034409A1
公开(公告)日：2012-02-09
申请号：US12850931
申请日：2010-08-05
申请人： Robert A. Price , Michael J. Milolla, JR. , David A. Reband , Karl J. Mazur , Robert M. Miller
发明人： Robert A. Price , Michael J. Milolla, JR. , David A. Reband , Karl J. Mazur , Robert M. Miller
IPC分类号： B60N3/04 , B29C45/63
CPC分类号： B60N3/046 , B29C45/14065 , B29C45/14786 , B29C2045/14155 , B29C2045/14934 , B29L2031/7324 , B60N3/044 , B60N3/048 , Y10T428/22
摘要： A method for producing a carpet mat by injection molding, includes providing an injection mold including a cavity and a complementary core, each defining a portion of a mold recess for accommodating the finished carpet mat, providing the cavity with a surface having at least one vacuum opening bordered by a peripheral retaining barrier, applying vacuum to the core, inserting a sheet of carpet into the recess of the cavity and against the surface so that the carpet is in contact with the cavity, so that the carpet is held in the recess by the vacuum. Next, the cavity and core are closed together, thus sealing the recess, and a flowable supply of plastic is injected into the recess. Finally, the mold is opened after a specified period, allowing the plastic to at least partially solidify.
摘要翻译：一种通过注射成型制造地毯垫的方法，包括提供包括空腔和互补芯的注塑模具，每个模具限定用于容纳成品地毯垫的模具凹部的一部分，为空腔提供具有至少一个真空的表面开口由周边保持屏障界定，对芯体施加真空，将一块地毯插入空腔的凹槽中并抵靠表面，使得地毯与空腔接触，使得地毯通过真空。接下来，将空腔和芯体封闭在一起，从而密封凹部，并且将可流动的塑料供应物注入到凹部中。最后，模具在规定的时间后打开，允许塑料至少部分固化。

10. 发明申请

US20090301095A1 PASSIVE BOUNDARY LAYER BLEED SYSTEM FOR NACELLE INLET AIRFLOW CONTROL 有权
标题翻译：用于空气入口空气流量控制的被动边界层系统
公开(公告)号：US20090301095A1
公开(公告)日：2009-12-10
申请号：US12428582
申请日：2009-04-23
申请人： Steven H. Zysman , Wesley K. Lord , Robert M. Miller , Oliver V. Atassi
发明人： Steven H. Zysman , Wesley K. Lord , Robert M. Miller , Oliver V. Atassi
IPC分类号： F02C9/18 , F02C7/00
CPC分类号： F02C7/04 , B64D33/02 , B64D2033/0226 , B64D2033/0286 , F05D2240/14 , F05D2260/60 , F05D2270/17 , Y10T137/0536
摘要： A gas turbine engine system includes a nacelle having a pressure side and a suction side. A passage extends between the pressure side and the suction side that permits airflow from the pressure side to the suction side. The passage receives turbulent airflow over the nacelle to produce a laminar airflow over the nacelle aft of the passage to thereby reduce drag on the nacelle.
摘要翻译：燃气涡轮发动机系统包括具有压力侧和吸力侧的机舱。通道在压力侧和吸力侧之间延伸，允许从压力侧到吸力侧的气流。通道在机舱上接收湍流气流，以在通道后面的机舱上方产生层流气流，从而减少机舱上的阻力。

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