AIRCRAFT WING STRUCTURE AND CONTROL SYSTEM
    1.
    发明申请
    AIRCRAFT WING STRUCTURE AND CONTROL SYSTEM 有权
    飞机结构与控制系统

    公开(公告)号:US20160161949A1

    公开(公告)日:2016-06-09

    申请号:US14907067

    申请日:2014-07-25

    Abstract: An aircraft includes a wing. The wing includes an aileron pivotally connected to a trailing edge of the wing, and a Lam aileron pivotally connected to the trailing edge of the wing. The aircraft includes a motor connected to the Lam aileron and configured to rotate the Lam aileron. The aircraft includes a controller configured to detect a deflection of the aileron from a neutral position, calculate a target deflection for the Lam aileron using the deflection of the aileron, and cause the motor to rotate the Lam aileron to the target deflection.

    Abstract translation: 飞机包括一个机翼。 机翼包括枢转地连接到翼的后缘的副翼和枢转地连接到翼的后缘的Lam副翼。 该飞机包括连接到Lam副翼并配置为旋转Lam副翼的马达。 飞机包括控制器,该控制器被配置为检测来自中立位置的副翼的偏转,使用副翼的偏转来计算Lam副翼的目标偏转,并使马达将Lam副翼旋转到目标偏转。

    Flap panel shuttle system and method therefor
    2.
    发明授权
    Flap panel shuttle system and method therefor 有权
    挡板面板穿梭系统及其方法

    公开(公告)号:US09108723B2

    公开(公告)日:2015-08-18

    申请号:US13702521

    申请日:2011-06-07

    Applicant: Michael Lam

    Inventor: Lawrence Lam

    CPC classification number: B64C13/28 B64C9/02 B64C9/14 B64C9/16

    Abstract: An aircraft control system is presented. The system includes a wing including a flap track, and a shuttle connected to the flap track and configured to slide along a length of the flap track. The system includes a flap panel pivotally attached to the shuttle at a flap pivot. The flap panel is configured to rotate about the flap pivot. When the shuttle is deployed along a length of the flap track, the shuttle is configured to prevent rotation of the flap panel about the flap pivot, and when the shuttle is withdrawn into a stowed position, the shuttle is configured to allow the flap panel to rotate about the flap pivot.

    Abstract translation: 介绍飞机控制系统。 该系统包括翼片,其包括翼片轨道,以及连接到翼片轨道并构造成沿着翼片轨道的长度滑动的梭子。 该系统包括在翼片枢轴处枢转地附接到梭子的翼片板。 翼片板被配置为围绕翼片枢轴旋转。 当梭子沿着翼片轨道的长度展开时,梭子被构造成防止翼片板围绕翼片枢轴旋转,并且当梭子被收回到收起位置时,梭子构造成允许翼片板 围绕襟翼枢轴旋转。

    Mechanical control mixer and method therefor
    3.
    发明授权
    Mechanical control mixer and method therefor 有权
    机械控制搅拌机及其方法

    公开(公告)号:US09004411B2

    公开(公告)日:2015-04-14

    申请号:US13885630

    申请日:2011-11-15

    Applicant: Michael Lam

    Inventor: Lawrence Lam

    CPC classification number: B64C13/04 B64C13/28 B64C13/30 Y10T74/20012

    Abstract: A mechanical control mixer configured to couple to an aircraft is provided. An axle is mounted to a frame of the mechanical control mixer, and a barrel is configured to rotate about the axle. A central rod is disposed within the barrel. The central rod is configured to rotate with respect to the barrel. A roll control input is connected to the central rod. The roll control input is configured to cause the central rod to rotate within the barrel. Output control rods are connected to the central rod. The output control rods are connected to at least one control surface of the aircraft. An air brake input is connected to the barrel. The air brake input is configured to cause the barrel to rotate about the axle to move at least one of the output control rods.

    Abstract translation: 提供了一种配置成耦合到飞行器的机械控制混合器。 轴安装到机械控制混合器的框架上,并且筒构造成围绕轴旋转。 中心杆设置在枪管内。 中心杆构造成相对于筒旋转。 辊控制输入连接到中心杆。 辊控制输入被配置为使得中心杆在筒内旋转。 输出控制杆连接到中心杆。 输出控制杆连接到飞行器的至少一个控制表面。 空气制动器输入端连接到枪管。 空气制动器输入被配置为使得筒绕轴旋转以移动至少一个输出控制杆。

    Data center having expandable or multipurpose configuration
    4.
    发明申请
    Data center having expandable or multipurpose configuration 审中-公开
    数据中心具有可扩展或多用途配置

    公开(公告)号:US20110023388A1

    公开(公告)日:2011-02-03

    申请号:US12805479

    申请日:2010-08-02

    CPC classification number: E04H5/02

    Abstract: A building includes a data center to house computing equipment including computers and servers. The data center stores data. The building also includes a multipurpose center that houses office spaces, conference rooms and meeting rooms. The data center and multipurpose center differ in function but share resources. The data center is expandable using a configuration of a control room, an electrical room and a mechanical room. Additional data center floors adjoin existing structures to increase available space in a linear manner.

    Abstract translation: 建筑物包括一个数据中心,用于容纳包括计算机和服务器在内的计算设备。 数据中心存储数据。 该建筑还包括一个多用途中心,设有办公空间,会议室和会议室。 数据中心和多功能中心功能不同,但共享资源。 数据中心可以使用控制室,电气室和机械室的配置进行扩展。 附加数据中心楼层与现有结构相连,以线性方式增加可用空间。

    MECHANICAL CONTROL MIXER AND METHOD THEREFOR
    6.
    发明申请
    MECHANICAL CONTROL MIXER AND METHOD THEREFOR 有权
    机械控制混合器及其方法

    公开(公告)号:US20140001313A1

    公开(公告)日:2014-01-02

    申请号:US13885630

    申请日:2011-11-15

    Applicant: Michael Lam

    CPC classification number: B64C13/04 B64C13/28 B64C13/30 Y10T74/20012

    Abstract: A mechanical control mixer configured to couple to an aircraft is provided. An axle is mounted to a frame of the mechanical control mixer, and a barrel is configured to rotate about the axle. A central rod is disposed within the barrel. The central rod is configured to rotate with respect to the barrel. A roll control input is connected to the central rod. The roll control input is configured to cause the central rod to rotate within the barrel. Output control rods are connected to the central rod. The output control rods are connected to at least one control surface of the aircraft. An air brake input is connected to the barrel. The air brake input is configured to cause the barrel to rotate about the axle to move at least one of the output control rods

    Abstract translation: 提供了一种配置成耦合到飞行器的机械控制混合器。 轴安装到机械控制混合器的框架上,并且筒构造成围绕轴旋转。 中心杆设置在枪管内。 中心杆构造成相对于筒旋转。 辊控制输入连接到中心杆。 辊控制输入被配置为使得中心杆在筒内旋转。 输出控制杆连接到中心杆。 输出控制杆连接到飞行器的至少一个控制表面。 空气制动器输入端连接到枪管。 空气制动器输入被配置为使得筒绕轴旋转以移动至少一个输出控制杆

    Simulation And Correction Of Mask Shadowing Effect
    7.
    发明申请
    Simulation And Correction Of Mask Shadowing Effect 有权
    面罩遮蔽效果的模拟与校正

    公开(公告)号:US20130080982A1

    公开(公告)日:2013-03-28

    申请号:US13244070

    申请日:2011-09-23

    CPC classification number: G03F1/22 G03F1/70 G03F7/70433

    Abstract: Disclosed are techniques for simulating and correcting the mask shadowing effect using the domain decomposition method (DDM). According to various implementations of the invention, DDM signals for an extreme ultraviolet (EUV) lithography mask are determined for a plurality of azimuthal angles of illumination. Base on the DDM signals, one or more layout designs for making the mask may be analyzed and/or modified.

    Abstract translation: 公开了使用域分解方法(DDM)来模拟和校正掩模阴影效应的技术。 根据本发明的各种实现方式,针对多个方位角的照明来确定用于极紫外(EUV)光刻掩模的DDM信号。 基于DDM信号,可以分析和/或修改用于制作掩模的一个或多个布局设计。

    Data center having heat exchange and transfer configuration
    8.
    发明申请
    Data center having heat exchange and transfer configuration 审中-公开
    数据中心具有热交换和传输配置

    公开(公告)号:US20110024078A1

    公开(公告)日:2011-02-03

    申请号:US12805480

    申请日:2010-08-02

    CPC classification number: E04H5/02

    Abstract: A building includes a data center to house computing equipment including computers and servers. The data center stores data. The building also includes a multipurpose center that houses office spaces, conference rooms and meeting rooms. The data center and multipurpose center differ in function but share resources. Computing equipment in the data center generates a lot of heat energy that is absorbed by the air. An air circulating system transfers the heated air from the data center to the multipurpose center. A fluid circulation system uses fluid to transfer heat energy to locations within the multipurpose center and also outside, such as a parking lot.

    Abstract translation: 建筑物包括一个数据中心,用于容纳包括计算机和服务器在内的计算设备。 数据中心存储数据。 该建筑还包括一个多用途中心,设有办公空间,会议室和会议室。 数据中心和多功能中心功能不同,但共享资源。 数据中心的计算设备产生大量被空气吸收的热能。 空气循环系统将加热的空气从数据中心传送到多功能中心。 流体循环系统使用流体将热能传递到多用途中心内部以及外部的位置,例如停车场。

    SYSTEM AND PROCESS FOR CONCENTRATING HYDROCARBONS IN A BITUMEN FEED
    9.
    发明申请
    SYSTEM AND PROCESS FOR CONCENTRATING HYDROCARBONS IN A BITUMEN FEED 有权
    用于浓缩二氧化碳进料中的碳氢化合物的系统和方法

    公开(公告)号:US20080000810A1

    公开(公告)日:2008-01-03

    申请号:US11759151

    申请日:2007-06-06

    CPC classification number: C10G31/10 C10G1/04

    Abstract: A system and process for concentrating hydrocarbons in a bitumen feed comprising bitumen, water and solids. The system comprises an inclined plate separator, a hydrocarbon cyclone and a centrifuge. The inclined plate separator separates the bitumen feed into a first overflow stream and a first underflow stream, the first overflow stream having a first bitumen concentration greater than that of the first underflow stream. The hydrocarbon cyclone separates the first underflow stream into a second overflow stream and a second underflow stream. The centrifuge separates the second overflow stream into a third overflow stream and a third underflow stream, the third overflow stream having a third bitumen concentration that is greater than that of the third underflow stream.

    Abstract translation: 将沥青浓缩在包含沥青,水和固体的沥青进料中的系统和方法。 该系统包括倾斜板式分离器,烃旋风分离器和离心机。 倾斜板分离器将沥青进料分离成第一溢流和第一下溢流,第一溢流流的第一沥青浓度大于第一下溢流的第一溢流。 烃旋风分离器将第一下溢流分离成第二溢流和第二下溢流。 离心机将第二溢流分离​​成第三溢流和第三下溢流,第三溢流流的第三沥青浓度大于第三下溢流的第三溢流。

    Aileron for fixed wing aircraft
    10.
    发明授权
    Aileron for fixed wing aircraft 有权
    副翼飞机固定翼

    公开(公告)号:US06554229B1

    公开(公告)日:2003-04-29

    申请号:US09581951

    申请日:2000-09-20

    CPC classification number: B64C9/06 B64C9/00 Y02T50/32 Y02T50/44

    Abstract: An aircraft aileron system (10, 10) is comprised of two panels (12, 14, 28, 30, 62, 70) located at the rear portion of the wing (W24, 54), in a spanwise direction and aligned with the wing's trailing edge. The panels are independently hinged at their leading edges and rotate to make angular deflections with respect to the wing. The upper, aileron panel (12, 30, 62) is restricted to upward deflection only from its neutral position and in operation is deployed independently as an aileron. The lower, auxiliary flap panel (14, 28, 70) is capable of both upward and downward deflections from its neutral position, and is deployed independently downward as an auxiliary flap. Both panels are deployed together upwardly only as an aileron. Alternatively, the auxiliary flap panel is capable of downward deployment only, to provide a simpler aileron system. For roll control of an aircraft during cruise, the aileron panel on one side only is deflected up while the aileron panel on the other side remains in its neutral position.

    Abstract translation: 飞机副翼系统(10,10)由位于机翼后部(W24,54)的两个面板(12,14,28,30,62,70)组成,沿翼展方向并与机翼 后缘。 面板在其前缘独立地铰接并旋转以相对于机翼产生角度偏转。 上副翼面板(12,30,62)仅从其中立位置限制向上偏转,并且在操作中作为副翼单独部署。 下辅助翼片板(14,28,70)能够从其中立位置向上和向下偏转,并且作为辅助翼片独立地向下展开。 两个面板仅作为副翼部署在一起。 或者,辅助翼板仅能够向下展开,以提供更简单的副翼系统。 对于巡航期间飞机的滚动控制,一侧的副翼面板仅在另一侧的副翼面板保持在其中立位置时被偏转。

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