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公开(公告)号：US20160376010A1
公开(公告)日：2016-12-29
申请号：US15165264
申请日：2016-05-26
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： Matthew James-Thomas Gmach , Robert Edward Sable , Scott Wigen , Matthew John Kunkel
IPC: B64D15/04
CPC classification number: B64D15/04 , G01K13/028
Abstract: A device configured to prevent ice accumulation includes at least one wall defining a leading edge and a pneumatic passage configured to receive pressurized fluid. The device also includes at least one ejection port formed in at least one of the leading edge and the at least one wall, the at least one ejection portion fluidly coupled to the pneumatic passage to receive the pressurized fluid therefrom, the at least one ejection port configured to form fluid jets to divert liquid water droplets away from the leading edge of the device.
Abstract translation: 构造成防止积冰的装置包括限定前缘的至少一个壁和构造成接收加压流体的气动通道。 该装置还包括形成在至少一个前缘和至少一个壁中的至少一个喷射口，所述至少一个喷射部分流体地联接到气动通道以从其接收加压流体，所述至少一个喷射口 被配置成形成流体射流以将液体水滴从设备的前缘移开。
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公开(公告)号：US20160374215A1
公开(公告)日：2016-12-22
申请号：US14744330
申请日：2015-06-19
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： Jeffrey P. Danicich , Curtis Wicks
CPC classification number: H05K5/0204 , B60R11/00 , F16B2/185 , F16C11/04 , F16M11/041 , F16M11/08 , F16M13/00 , F16M13/02
Abstract: A mount for holding a display device includes a main support, a plurality of arms, and a locking assembly. The main support includes a front surface and a rear surface. The plurality of arms extends from a periphery of the main support. The main support and the plurality of arms are configured to retain the display device. The locking assembly is connected to the rear surface of the main support, and is configured to secure the display device. The locking assembly includes a locking arm and a locking mechanism. The locking arm is translatable relative to the main support, and is configured to support the display device in a secured position. The locking mechanism is connected to the locking arm. The locking mechanism includes a lever connected to the locking arm for releasing the locking mechanism.
Abstract translation: 用于保持显示装置的支架包括主支撑件，多个臂和锁定组件。 主支架包括前表面和后表面。 多个臂从主支架的周边延伸。 主支撑件和多个臂被构造成保持显示装置。 锁定组件连接到主支架的后表面，并被配置为固定显示装置。 锁定组件包括锁定臂和锁定机构。 锁定臂可相对于主支撑件平移，并且构造成将显示装置支撑在固定位置。 锁定机构连接到锁定臂。 锁定机构包括连接到锁定臂的杆，用于释放锁定机构。
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公开(公告)号：US09488534B2
公开(公告)日：2016-11-08
申请号：US14189885
申请日：2014-02-25
Applicant: Rosemount Aerospace Inc.
Inventor： Scott Wigen , Matthew J. T. Gmach , Robert E. Sable , John T. Otto
CPC classification number: G01K13/028
Abstract: A total air temperature sensor includes a supercritical airfoil body extending from an airfoil base to an opposed airfoil tip along a longitudinal axis. The supercritical airfoil body defines an interior flow passage with an inlet for fluid communication of fluid into the interior flow passage and an outlet for exhausting fluid out from the interior flow passage. A temperature probe is mounted within the interior flow passage for measuring temperature of flow through the interior flow passage to determine total air temperature.
Abstract translation: 总空气温度传感器包括超临界翼型体，其从翼型基部沿着纵向轴线延伸到相对的翼型端头。 超临界翼型体限定了内部流动通道，其具有用于使流体流体连通到内部流动通道中的入口和用于从内部流动通道排出流体的出口。 温度探针安装在内部流动通道内，用于测量通过内部流动通道的流动的温度，以确定总的空气温度。
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公开(公告)号：US20160305802A1
公开(公告)日：2016-10-20
申请号：US14689966
申请日：2015-04-17
Applicant: Rosemount Aerospace Inc.
Inventor： Peter M. Chong , Ronald F. Liffrig
CPC classification number: G01F1/46 , B64D45/00 , G01P5/16 , G01P13/025
Abstract: An air data system includes an avionics system and a plurality of sensors associated with the avionics system, each of the sensors providing a signal indicative of a parameter used by the avionic system to determine the flight status of the aircraft. At least one air data probe is electronically coupled to the avionics system. At least one pitot static probe is coupled to a pressure transducer through pneumatic tubing, the pressure transducer is electronically coupled to the avionics system.
Abstract translation: 空中数据系统包括航空电子系统和与航空电子系统相关联的多个传感器，每个传感器提供指示由航空电子系统使用的参数以确定飞行器的飞行状态的信号。 至少一个空中数据探针电子耦合到航空电子系统。 至少一个皮托静态探头通过气动管连接到压力传感器，压力传感器电耦合到航空电子系统。
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公开(公告)号：US09473710B2
公开(公告)日：2016-10-18
申请号：US14172001
申请日：2014-02-04
Applicant: Rosemount Aerospace Inc.
Inventor： John C. Bartholomew , Nathan D. Evans , James W. Swenson
CPC classification number: H04N5/268 , G06F13/4086 , H04N5/217 , H04N5/77 , H04N9/642
Abstract: A video signal termination detection system includes an input configured to connect to a video driver that produces a video signal, an output configured to connect to a video receiver that operates with a signal type, a detection circuit connected between the input and the output and configured to detect the signal type of the video receiver and to output a detection signal, and a conversion circuit configured to receive the video signal from the video driver and to convert the video signal to the signal type if the video signal is different than the signal type.
Abstract translation: 视频信号终止检测系统包括被配置为连接到产生视频信号的视频驱动器的输入，被配置为连接到以信号类型操作的视频接收器的输出，连接在输入端和输出端之间的检测电路， 以检测视频接收机的信号类型并输出检测信号;以及转换电路，被配置为从视频驱动器接收视频信号，并且如果视频信号不同于信号类型，则将视频信号转换为信号类型 。
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Patent Agency Ranking
公开(公告)号：US09464950B2
公开(公告)日：2016-10-11
申请号：US14185156
申请日：2014-02-20
Applicant: Rosemount Aerospace Inc.
Inventor： Weibin Zhang , Anita Fink , Saeed Fahimi , Kimiko J. Childress
CPC classification number: G01L1/14 , G01L9/0047 , G01L9/0075 , G01L19/0076 , G01L19/0618
Abstract: A capacitive pressure sensor includes a substrate wafer and a diaphragm wafer. The substrate wafer defines a substrate recess with a first recess. The diaphragm wafer defines a diaphragm recess with a second recess. The diaphragm wafer is bonded to the substrate wafer such that the substrate and diaphragm recesses form a height differentiated pressure chamber.
Abstract translation: 电容式压力传感器包括衬底晶片和膜片晶片。 衬底晶片限定具有第一凹部的衬底凹部。 隔膜晶片限定具有第二凹槽的隔膜凹部。 膜片晶片与衬底晶片结合，使得衬底和隔膜凹槽形成高度差异化压力室。
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公开(公告)号：US20160244180A1
公开(公告)日：2016-08-25
申请号：US15145831
申请日：2016-05-04
Applicant: Rosemount Aerospace Inc.
Inventor： William J. Baumgarten , Michael J. Haukom , Thomas J. Horsager , Daniel L. McDowell
CPC classification number: B64D45/00 , G05B23/0216 , G05B2219/23406 , G06F13/4282 , G07C5/006
Abstract: An aircraft interface device is configured to communicate with an aircraft avionics system that includes a plurality of sensors for an aircraft includes a tablet interface module configured to communicate with the aircraft interface device and with one or more tablets. The tablet interface module includes a user interface that is configured to establish, via a wireless transceiver, a communications channel between the tablet interface module and the one or more tablets and an indicator configured to indicate if the tablet interface module is connected to the one or more tablets. The tablet interface module provides the one or more tablets with information received from the aircraft interface device and wherein the tablet interface module comprises a power supply configured to connect to a power system of the aircraft and to provide power to the one or more tablet devices.
Abstract translation: 飞机接口设备被配置为与飞行器航空电子系统通信，该飞行器航空电子系统包括用于飞行器的多个传感器，其包括被配置为与飞行器接口设备和一个或多个平板电脑通信的平板接口模块。 平板电脑接口模块包括用户界面，其被配置为经由无线收发器建立平板接口模块与一个或多个平板电脑之间的通信信道，以及指示器，其被配置为指示平板电脑接口模块是否连接到一个或多个平板电脑 更多片剂 平板电脑接口模块向一个或多个平板电脑提供从飞行器接口设备接收的信息，并且其中平板电脑接口模块包括被配置为连接到飞行器的电力系统并且向一个或多个平板设备提供电力的电源。
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公开(公告)号：US20160209253A1
公开(公告)日：2016-07-21
申请号：US14601768
申请日：2015-01-21
Applicant: Rosemount Aerospace Inc.
Inventor： Michael Robert Daup , Andrew Sherman
IPC: G01F1/46
CPC classification number: G01F1/46 , G01L19/0007 , G01P5/14
Abstract: A tuned sensor system is disclosed. The tuned sensor system may receive an unsteady pressure from an external environment via a pressure inlet port. The pressure may have a first component that is substantially static and a second component that varies at a relatively high frequency. The pressure inlet port may conduct the unsteady pressure to a tuned path. The tuned path may filter the unsteady pressure, blocking the second component and communicating the first component, such as for use by a pressure sensor. The tuned sensor system may be compact and may include one or more turn in the tuned path so that the distance between the pressure inlet port and the sensor is less than the length of the tuned path. The tuned path may be entirely within the supporting structure of the tuned sensor system, easing installation, removal, and maintenance of the compact and modular system.
Abstract translation: 公开了一种调谐传感器系统。 调谐传感器系统可以经由压力入口从外部环境接收不稳定的压力。 压力可以具有基本上静止的第一部件和以较高频率变化的第二部件。 压力入口可以将不稳定的压力导向调谐路径。 调节路径可以过滤不稳定的压力，阻塞第二部件并且连通第一部件，例如由压力传感器使用。 调谐传感器系统可以是紧凑的，并且可以包括调谐路径中的一个或多个转弯，使得压力入口端口和传感器之间的距离小于调谐路径的长度。 调谐路径可以完全在调谐传感器系统的支撑结构内，从而简化了紧凑和模块化系统的安装，拆卸和维护。
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公开(公告)号：US09383249B2
公开(公告)日：2016-07-05
申请号：US14075207
申请日：2013-11-08
Applicant: Rosemount Aerospace Inc.
Inventor： Brian B. Naslund , Jonathan R. Singleton , Robert A. Combs
CPC classification number: G01F25/0007 , G01P13/025 , G01P21/00
Abstract: A method for detecting angle sensor performance degradation in a flow angle measurement device in moving platform, such as aircraft and watercraft, as well as stationary platforms. Sensor dither in a flow angle measurement device is used to detect operational performance degradation of the sensor as a result of dynamic response changes caused by damaged or degraded mechanical components.
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公开(公告)号：US20160124738A1
公开(公告)日：2016-05-05
申请号：US14279691
申请日：2014-05-16
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： Michael James Haukom , Thomas Jay Horsager
Abstract: A method for data loading with a tablet includes receiving one or more software updates published by a ground station and storing the software updates on the tablet. The method also includes establishing communications between the tablet and a tablet interface module of an aircraft and determining if software on the aircraft needs to be updated. Based on determining that the software on the aircraft needs to be updated, the method includes transmitting at least one of the one or more software updates to the tablet interface module for loading into the aircraft and monitoring an installation process of the software updates in the aircraft via the tablet interface module.
Abstract translation: 用于使用平板电脑进行数据加载的方法包括接收地面站发布的一个或多个软件更新并将该软件更新存储在平板电脑上。 该方法还包括在平板电脑和飞行器的平板电脑接口模块之间建立通信并确定飞机上的软件是否需要更新。 基于确定飞机上的软件需要更新，该方法包括将一个或多个软件更新中的至少一个发送到平板接口模块以加载到飞行器中并且监视飞机中的软件更新的安装过程 通过平板电脑接口模块。
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