公开(公告)号：US20110100392A1

公开(公告)日：2011-05-05

申请号：US12939379

申请日：2010-11-04

Applicant: Timothy Smith ,  Jocelyn Smith

Inventor： Timothy Smith ,  Jocelyn Smith

IPC: A45D40/26

CPC classification number: A45D44/12

Abstract: A makeup tool includes a body portion with an elongated handle and a pair of arm portions. The pair of arm portions are spaced apart from one another such that an open space exists between the pair of arm portions. At least one collection sheet is removeably secured to each arm and spans the open space between the pair of arm portions. The handle is downwardly angled with respect to the pair of arm portions to allow a user to more easily grab the handle and position an edge of the at least one sheet against or adjacent a face of the user.

Abstract translation: 化妆工具包括具有细长手柄和一对手臂部分的主体部分。 一对臂部彼此间隔开，使得一对臂部之间存在开放空间。 至少一个集合片可移除地固定到每个臂并且跨越所述一对臂部之间的开放空间。 手柄相对于一对臂部分向下成角度，以允许使用者更容易地抓握手柄并将至少一个片材的边缘定位抵靠使用者的脸部或邻近使用者的脸部。

公开(公告)号：US20110066305A1

公开(公告)日：2011-03-17

申请号：US12594533

申请日：2008-03-26

Applicant: Shu Lin ,  Timothy Smith ,  Pierre De Serres

Inventor： Shu Lin ,  Timothy Smith ,  Pierre De Serres

IPC: G05D1/08 ,  G05D1/00

CPC classification number: B64C13/503 ,  B64C13/04 ,  B64C19/00 ,  G05D1/0077

Abstract: A multi-axis serially redundant, single channel, multi-path fly-by-wire control system comprising: serially redundant flight control computers in a single channel where only one “primary” flight control computer is active and controlling at any given time; a matrix of parallel flight control surface controllers including stabilizer motor control units (SMCU) and actuator electronics control modules (AECM) define multiple control paths within the single channel, each implemented with dissimilar hardware and which each control the movement of a distributed set of flight control surfaces on the aircraft in response to flight control surface commands of the primary flight control computer; and a set of (pilot and co-pilot) controls and aircraft surface/reference/navigation sensors and systems which provide input to a primary flight control computer and are used to generate the flight control surface commands to control the aircraft in flight in accordance with the control law algorithms implemented in the flight control computers.

Abstract translation: 多轴串行冗余，单通道，多路径逐线控制系统，其包括：在单个通道中的串行冗余飞行控制计算机，其中只有一个“主要”飞行控制计算机处于活动状态并在任何给定时间进行控制; 包括稳定器电机控制单元（SMCU）和执行机构电子控制模块（AECM）在内的并行飞行控制面控制器矩阵定义了单个通道内的多个控制路径，每个控制路径用不同的硬件实现，每个控制路径分别控制一组分布式飞行 响应于主飞行控制计算机的飞行控制表面命令来控制飞机上的表面; 以及一组（飞行员和副驾驶员）控制和飞机表面/参考/导航传感器和系统，其向主飞行控制计算机提供输入并用于产生飞行控制表面命令以根据 控制算法在飞行控制计算机中实现。

公开(公告)号：US20100267920A1

公开(公告)日：2010-10-21

申请号：US12824435

申请日：2010-06-28

Applicant: Timothy Smith

Inventor： Timothy Smith

IPC: C08G77/14 ,  C08G77/04 ,  C08G77/28 ,  C08G77/18 ,  C08G77/30 ,  C08G77/12 ,  C08G77/24

CPC classification number: G02B26/001

Abstract: A light filter or an array of filters can be either one or two dimensional. The filter or filters use multiple beam interference by varying an optical path length between semi-reflective surfaces. The optical path length between the semi-reflective surfaces is varied by changing a thickness of a polymer film in response to an electric field formed between two semi-transparent electrodes. The filter can be configured in either a transmissive or reflective mode.

Abstract translation: 滤光器或滤光器阵列可以是一维或二维。 过滤器或过滤器通过改变半反射表面之间的光程长度来使用多个光束干涉。 通过根据在两个半透明电极之间形成的电场改变聚合物膜的厚度来改变半反射表面之间的光程长度。 滤波器可以配置为透射或反射模式。

公开(公告)号：US07580777B2

公开(公告)日：2009-08-25

申请号：US11460769

申请日：2006-07-28

Applicant: Timothy Smith ,  James Daas

Inventor： Timothy Smith ,  James Daas

IPC: B64C13/50

CPC classification number: B64D15/22 ,  B64D15/14 ,  H04B3/54 ,  H04B3/548 ,  H04B2203/5458 ,  H04B2203/547

Abstract: An aircraft system for control of the application of power to a plurality of devices in the aircraft comprises a plurality of local control modules. Each local control module controls the application of the power to the group of at least one device. A central control system communicates with and controls the local control modules.

Abstract translation: 用于控制向飞行器中的多个装置施加电力的飞行器系统包括多个本地控制模块。 每个本地控制模块控制对至少一个设备的组的电力的应用。 中央控制系统与本地控制模块进行通信和控制。

公开(公告)号：US20080036472A1

公开(公告)日：2008-02-14

申请号：US11838831

申请日：2007-08-14

Applicant: Edward Collins ,  Timothy Smith ,  Randall Emanuel

Inventor： Edward Collins ,  Timothy Smith ,  Randall Emanuel

IPC: G01R27/16

CPC classification number: G01R27/16 ,  G01R19/2513 ,  G01R31/025

Abstract: Embodiments according to the present invention provide an Impedance-based Arc-Fault Determination Device (IADD) and method that, when attached to an electrical node on the power system and through observations on voltage, current and phase shift with a step load change, determine the effective Thevenin equivalent circuit or Norton equivalent circuit at the point of test. The device and method determine the expected bolted fault current at the test location of interest, which enables calculation of incident energy and the assignment of a flash-hazard risk category.

Abstract translation: 根据本发明的实施例提供了一种基于阻抗的电弧故障确定装置（IADD）和方法，当其连接到电力系统上的电节点上时，并且通过对步进负载变化的电压，电流和相移进行观测，确定 有效的戴维宁等效电路或诺顿等效电路在测试点。 该装置和方法确定感兴趣的测试位置处的预期螺栓故障电流，这使得能够计算入射能量和分配闪电危险风险类别。

公开(公告)号：US20080020480A1

公开(公告)日：2008-01-24

申请号：US11566818

申请日：2006-12-05

Applicant: Bo Lin ,  Gangadhar Jogikalmath ,  Timothy Smith ,  Kurt Albertson ,  Christine Genick ,  Lance Laing

Inventor： Bo Lin ,  Gangadhar Jogikalmath ,  Timothy Smith ,  Kurt Albertson ,  Christine Genick ,  Lance Laing

IPC: G01N21/00 ,  G01N21/01

CPC classification number: G01N21/41 ,  G01N21/253 ,  G01N21/75 ,  G01N2021/7779 ,  Y10S435/81 ,  Y10S436/805 ,  Y10S436/809 ,  Y10S436/815

Abstract: The invention provides compositions and methods of detecting binding of molecules to a biosensor. Compositions of the invention comprise a multiwell plate with an integrated biosensor and a membrane.

Abstract translation: 本发明提供检测分子与生物传感器结合的组合物和方法。 本发明的组合物包括具有集成的生物传感器和膜的多孔板。

公开(公告)号：US20070112480A1

公开(公告)日：2007-05-17

申请号：US11460769

申请日：2006-07-28

Applicant: Timothy Smith ,  James Daas

Inventor： Timothy Smith ,  James Daas

IPC: G06F17/00

CPC classification number: B64D15/22 ,  B64D15/14 ,  H04B3/54 ,  H04B3/548 ,  H04B2203/5458 ,  H04B2203/547

Abstract: An aircraft system for control of the application of power to a plurality of devices in the aircraft comprises a plurality of local control modules. Each local control module controls the application of the power to the group of at least one device. A central control system communicates with and controls the local control modules.

Abstract translation: 用于控制向飞行器中的多个装置施加电力的飞行器系统包括多个本地控制模块。 每个本地控制模块控制对至少一个设备的组的电力的应用。 中央控制系统与本地控制模块进行通信和控制。

公开(公告)号：US07185919B2

公开(公告)日：2007-03-06

申请号：US10754076

申请日：2004-01-07

Applicant: Bruce A. Mather ,  Paul Casimer Arone ,  Wesley J. Blanchard ,  Kenneth Gordon Grant, Jr. ,  Philip Garret Kosarek ,  Richard Lonetto ,  Tom Manley ,  Richard McCulloch ,  Timothy Smith ,  Steven Thompson ,  Michael T. Vecchio ,  John H. Young

Inventor： Bruce A. Mather ,  Paul Casimer Arone ,  Wesley J. Blanchard ,  Kenneth Gordon Grant, Jr. ,  Philip Garret Kosarek ,  Richard Lonetto ,  Tom Manley ,  Richard McCulloch ,  Timothy Smith ,  Steven Thompson ,  Michael T. Vecchio ,  John H. Young

IPC: B60R22/00 ,  A47C15/00

CPC classification number: B60R22/30 ,  B60R22/44 ,  B60R2022/1812 ,  B60R2022/4473 ,  Y10T24/4016 ,  Y10T24/45623 ,  Y10T24/45634

Abstract: In one embodiment, an apparatus for reversibly locking a lap belt portion of a safety belt webbing in a three-point, continuous loop seat belt system which includes a tongue assembly having the belt webbing routed therethrough, includes a cinch body adapted to mount to the tongue assembly, and a cam coupled to the cinch body and adapted to urge the belt webbing against the cinch body.

Abstract translation: 在一个实施例中，一种用于可逆地将安全带织带的腰带部分可逆地锁定在三点连续环形安全带系统中的装置，其包括具有穿过其的带状织带的舌组件，所述舌组件包括适于安装到 舌组件，以及耦合到束带主体并适于将带织带推靠在束带体上的凸轮。

公开(公告)号：US20070019555A1

公开(公告)日：2007-01-25

申请号：US11185282

申请日：2005-07-20

Applicant: Timothy Smith ,  Nina Stewart

Inventor： Timothy Smith ,  Nina Stewart

IPC: H04J3/14 ,  H04L12/56

CPC classification number: H04W40/248 ,  H04L45/126 ,  H04W8/005 ,  H04W84/18

Abstract: According to an embodiment of the invention, a method of dynamically creating a network of a plurality of nodes operable to communicate with objects in operating sectors comprises establishing a first communication link between a first node and a second node of the plurality of nodes. The first communication link is established upon determining that the first communication link between the respective ones of the plurality of nodes would not cross an existing communication link in the network of the plurality of nodes between two of the plurality of nodes or upon determining that the first communication link would be shorter than any existing communication link in the network of the nodes between two of the plurality of nodes that the first communication link would cross. The first communication link has a first communicative line of sight between the first node and the second node.

Abstract translation: 根据本发明的实施例，动态地创建可操作以与操作扇区中的对象通信的多个节点的网络的方法包括建立多个节点中的第一节点和第二节点之间的第一通信链路。 第一通信链路是通过确定多个节点中的相应节点之间的第一通信链路不会跨过多个节点中的两个节点之间的多个节点的网络中的现有通信链路，或者在确定第一通信链路 通信链路将比第一通信链路将跨越的多个节点中的两个之间的节点的网络中的任何现有通信链路短。 第一通信链路在第一节点和第二节点之间具有第一通信视线。

公开(公告)号：US20060067836A1

公开(公告)日：2006-03-30

申请号：US11238834

申请日：2005-09-29

Applicant: Timothy Smith ,  Stephen Vos

Inventor： Timothy Smith ,  Stephen Vos

IPC: F04B53/00

CPC classification number: F04B35/06 ,  F04B41/02

Abstract: An air compressor assembly includes a roll cage assembly which defines a protective volume within the air compressor assembly. The roll cage assembly supports an air storage tank and an air compressor, and at least substantially surrounds the air storage tank and the air compressor. The air compressor assembly includes a shroud mounted to the roll cage assembly. The shroud has a control panel portion including control and output components which are completely contained within the protected volume. The air compressor assembly further includes a handle. The handle is positioned along a vertical axis extending through the center of gravity of the air compressor assembly when the air compressor assembly is oriented to be carried by grasping the handle.

Abstract translation: 空气压缩机组件包括限定空气压缩机组件内的保护体积的滚子保持架组件。 卷笼组件支撑空气储存箱和空气压缩机，并且至少基本上围绕空气储存箱和空气压缩机。 空气压缩机组件包括安装到滚子保持架组件的护罩。 护罩具有控制面板部分，其包括完全包含在受保护体积内的控制和输出部件。 空气压缩机组件还包括手柄。 当空气压缩机组件被定向为通过抓住把手来承载时，手柄沿着延伸穿过空气压缩机组件的重心的垂直轴定位。