公开(公告)号：EP2945060A2

公开(公告)日：2015-11-18

申请号：EP15168052.7

申请日：2015-05-18

Applicant: Rosemount Aerospace Inc.

Inventor： HAUKOM, Michael James ,  HORSAGER, Thomas Jay

IPC: G06F9/445

CPC classification number: G06F8/65 ,  G06F8/61 ,  G06F8/71 ,  H04L67/12 ,  H04L67/34

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: 用平板电脑加载数据的方法包括接收由地面站发布的一个或多个软件更新并将软件更新存储在平板电脑上。 该方法还包括在平板和飞机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。 基于确定需要更新飞机上的软件，该方法包括将一个或更多个软件更新中的至少一个发送到平板电脑接口模块以加载到飞机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。

公开(公告)号：EP2940366A2

公开(公告)日：2015-11-04

申请号：EP15162856.7

申请日：2015-04-08

Applicant: Rosemount Aerospace Inc.

Inventor： Johnson, Wallace ,  Freeman, Kenneth ,  Danicich, Jeffery P.

IPC: F16M11/04 ,  F16M11/08 ,  F16M11/10 ,  F16M11/16 ,  F16M13/00 ,  B60R11/02

CPC classification number: F16M13/022 ,  B60R11/0235 ,  B60R2011/0085 ,  B64D47/00 ,  F16M11/041 ,  F16M11/08 ,  F16M11/105 ,  F16M11/16 ,  F16M13/00 ,  F16M2200/021

Abstract: In one example, an apparatus (10) for holding a display device (12) includes a back plate (28) and a plurality of engaging members (22) disposed around a periphery of the back plate (28). The back plate includes a rear face (34) and a front face opposite the rear face (34). The plurality of engaging members (22) extend from the back plate (28) in a direction from the rear face (34) to the front face to define an outer boundary of a retention space configured to accept the display device (12). The plurality of engaging members (22) includes a rotatable engaging member (22A) configured to rotate between an engagement position and a disengagement position. The engagement position is configured to secure the display device (12) within the retention space. The disengagement position is configured to allow removal of the display device (12) from the retention space.

Abstract translation: 在一个示例中，用于保持显示装置（12）的装置（10）包括背板（28）和围绕背板（28）的周边设置的多个接合构件（22）。 背板包括后表面（34）和与后表面（34）相对的前表面。 多个接合构件（22）从后板（28）沿着从后表面（34）到前面的方向延伸，以限定配置为接纳显示装置（12）的保持空间的外边界。 多个接合构件（22）包括构造成在接合位置和脱离位置之间旋转的可旋转接合构件（22A）。 接合位置被配置为将显示装置（12）固定在保持空间内。 脱离位置被配置为允许从保持空间移除显示装置（12）。

公开(公告)号：EP2899524A1

公开(公告)日：2015-07-29

申请号：EP14199793.2

申请日：2014-12-22

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： Fahimi, Saeed ,  Eriksen, Odd Harald Steen ,  Little, Charles ,  Fink, Anita

IPC: G01L19/00

CPC classification number: G01L19/0681 ,  B81B2201/0264 ,  G01L19/0069 ,  G01L19/0084

Abstract: A pressure sensor assembly (100) includes a pressure sensor (101) having a pressure sensing transducer connected to a plurality of electrode pins (103) via a plurality of electrode pads (105) disposed on the transducer, an inner casing (107) configured to hold the pressure sensing transducer including a plurality of inner casing electrode pin channels (111) having the electrode pins disposed therein. The pressure sensor further includes an outer casing (115) holding the inner casing therein having a capsule header (117) with a plurality of capsule header electrode pin channels (119) defined therein which can include a ceramic seal (133) disposed therein such that the capsule header electrode pin channels engage the electrode pins in an insulating sealed relationship. The outer casing further includes an isolator plate (127) including an isolator plate fluid port (129) defined therein and a pressure isolator (131) disposed on the isolator plate and configured to deflect in response to a change in ambient pressure. The pressure sensor includes a pressure transmitting fluid disposed in the fluid volume.

Abstract translation: 压力传感器组件（100）包括压力传感器（101），压力传感器（101）具有通过设置在换能器上的多个电极焊盘（105）连接到多个电极引脚（103）的压力感测传感器，内部壳体（107） 以保持包括多个内壳电极引脚通道（111）的压力感测传感器，其中设置有电极引脚。 该压力传感器还包括一个外壳（115），其内部容纳有内壳，该壳体具有胶囊集管（117），胶囊集管（117）具有限定在其中的多个胶囊集管电极销通道（119），其中可包括设置在其中的陶瓷密封件（133） 胶囊头电极针通道以绝缘密封的关系接合电极销。 外壳还包括隔离板（127），隔离板包括限定在其中的隔离板流体端口（129）和设置在隔离板上的压力隔离器（131），并被配置为响应于环境压力的变化而偏转。 压力传感器包括设置在流体体积中的压力传递流体。

公开(公告)号：EP2894666A1

公开(公告)日：2015-07-15

申请号：EP15150254.9

申请日：2015-01-07

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： Wicks, Curtis ,  Lovaasen, Eric ,  Anderson, Kaleb ,  Boer, Jonathan

IPC: H01L23/40 ,  H01L23/427

CPC classification number: H05K7/20418 ,  B23P15/26 ,  B23P2700/10 ,  F28D15/0275 ,  F28D2021/0028 ,  F28F2275/08 ,  F28F2275/20 ,  H01L23/4006 ,  H01L23/427 ,  H01L2924/0002 ,  Y10T29/4935 ,  H01L2924/00

Abstract: A heat exchanger system (10;20) may have a base (30), a mounting apparatus for attaching the base to a device, a gasket shelf (60) for placing a gasket, a dissipation member (70) for dissipating heat, and heat generator attachment sites for absorbing heat. A mounting apparatus may have finger-like extensions which flex and draw the base (30) into contact with an underlying electronic device from which the system conducts heat. A base (30) may also have an integrated heat pipe clamp attachment (100) forming an aperture in the base (30) into which a heat pipe may extend and may be clamped in thermal communication. The dissipation member (70) may be a series of fins and troughs and a fan (130) may direct air over the dissipation member (70) to cool the apparatus.

Abstract translation: 热交换器系统（10; 20）可以具有基座（30），用于将基座附接到设备的安装设备，用于放置垫圈的垫圈架（60），用于散热的散热构件（70），以及 用于吸热的发热器附件。 安装设备可以具有指状的延伸部，其弯曲并拉动基部（30）与系统传导热的下面的电子设备接触。 基座（30）还可以具有在基座（30）中形成孔的集成热管夹附件（100），热管可以延伸到该孔中并且可以热连接夹紧。 散热构件（70）可以是一系列翅片和槽，并且风扇（130）可以将空气引导到散热构件（70）上以冷却设备。

公开(公告)号：EP2881714A1

公开(公告)日：2015-06-10

申请号：EP14196824.8

申请日：2014-12-08

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： Essawy, Magdi A.

IPC: G01D5/20 ,  G01D5/22 ,  B64D45/00

CPC classification number: G01B7/003 ,  B64D45/0005 ,  B64D2045/001 ,  G01B7/30 ,  G01D5/20 ,  G01D5/2266

Abstract: A sensor package (100; 100a; 100b) for sensing rotational positional data includes a stack of separated printed circuit boards that includes a first position target printed board (126), a second printed circuit board (120) having a rotary sensor and a third printed circuit board (140) having power supply components. The sensor package is included in a skew detection system (200) for an aircraft control system, which includes a control surface (210) having opposed first (210a) and second (210b) ends. A first drive mechanism (220a) is operatively connected to the first end of the control surface by a first rack and pinion assembly (230a) and a second drive mechanism (220b) is operatively connected to the second end of the control surface by a second rack and pinion assembly (230b). Each rack and pinion assembly includes a respective sensor package (100a, 100b) operatively connected to the pinion (234a, 234b) thereof. A processing component (240) is operatively connected to both sensor packages to determine presence of skew in the control surface.

公开(公告)号：EP2816311A3

公开(公告)日：2015-03-18

申请号：EP14173511.8

申请日：2014-06-23

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： Ell, Todd ,  Rutkiewicz, Robert

IPC: F41G7/22 ,  G01R23/02 ,  H03K5/26

CPC classification number: F42B15/01 ,  F41G7/226 ,  F41G7/2293 ,  F41G9/00

Abstract: A dual-mode, semi-active, laser-based and passive image-based seeker for projectiles, missiles, and other ordnance that persecute targets by detecting and tracking energy scattered from targets. The disclosed embodiments use a single digital imager having a single focal plane array sensor to sense data in both the image-based and laser-based modes of operation. A shuttering technique allows the relatively low frame-rate of the digital imager to detect, decode and localize in the imager's field-of-view a known pulse repetition frequency (PRF) from a known designator in the presence of ambient light and other confusing target designators, each having a different PRF.

公开(公告)号：EP2420447A3

公开(公告)日：2015-02-25

申请号：EP11250729.8

申请日：2011-08-16

Applicant: Rosemount Aerospace Inc.

Inventor： Eriksen, Odd Harald Steen ,  Spivak, Alexander ,  Sanden, Christopher

IPC: B64D29/06 ,  E05B41/00 ,  E05B51/02 ,  G01L1/14

CPC classification number: B64D29/06 ,  E05B41/00 ,  E05B2047/0069 ,  E05C19/14 ,  G01L1/142 ,  G01L5/0004 ,  Y10T292/0949

Abstract: A sensor (100) for monitoring external loads acting on a pin assembly includes a pin (24) having an axial interior bore defined therein and having a length defined from a first end to an opposed second end thereof. A core pin is mounted axially within the interior bore of the pin spaced radially inwardly from the interior bore for relative displacement with respect to the pin. A capacitor (108) is provided having an inner capacitor plate (118) mounted to the core pin (106), and an outer capacitor plate (114) mounted to the pin (24), such that relative displacement of the core and the pin (24) due to external loading on the pin (24) results in relative displacement of the inner and outer capacitor plates (118,114). The capacitor (108) is configured and adapted to be connected to an electrical circuit (110) to produce signals indicative of external loading on the pin based on relative displacement of the inner and outer capacitor plates (118,114).

公开(公告)号：EP2816312A2

公开(公告)日：2014-12-24

申请号：EP14173554.8

申请日：2014-06-23

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： Ell, Todd ,  Caplan, William

IPC: F41G7/22

Abstract: A method to spread laser photon energy over separate pixels to improve the likelihood that the total sensing time of all the pixels together includes the laser pulse. The optical signal is spread over a number of pixels, N, on a converter array by means of various optical components. The N pixels are read out sequentially in time with each sub-interval short enough that the integration of background photons competing with the laser pulse is reduced. Likewise, the pixel read times may be staggered such that laser pulse energy will be detected by at least one pixel during the required pulse interval. The arrangement of the N pixels may be by converter array column, row, two dimensional array sub-window, or any combination of sub-windows depending on the optical path of the laser signal and the capability of the ROIC control.

公开(公告)号：EP2816311A2

公开(公告)日：2014-12-24

申请号：EP14173511.8

申请日：2014-06-23

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： Ell, Todd ,  Rutkiewicz, Robert

IPC: F41G7/22

CPC classification number: F42B15/01 ,  F41G7/226 ,  F41G7/2293 ,  F41G9/00

Abstract: A dual-mode, semi-active, laser-based and passive image-based seeker for projectiles, missiles, and other ordnance that persecute targets by detecting and tracking energy scattered from targets. The disclosed embodiments use a single digital imager having a single focal plane array sensor to sense data in both the image-based and laser-based modes of operation. A shuttering technique allows the relatively low frame-rate of the digital imager to detect, decode and localize in the imager's field-of-view a known pulse repetition frequency (PRF) from a known designator in the presence of ambient light and other confusing target designators, each having a different PRF.

Abstract translation: 一种双模，半主动，基于激光和被动的图像探测器，用于通过检测和跟踪从目标散射的能量来迫害目标的射弹，导弹和其他武器。 所公开的实施例使用具有单个焦平面阵列传感器的单个数字成像器来检测基于图像和基于激光的操作模式中的数据。 快门技术允许数字成像器的相对较低的帧速率在成像仪的视场中检测，解码和定位已知的脉冲重复频率（PRF），其在存在环境光和其他混乱目标的情况下来自已知的指示符 指示符，每个都有不同的PRF。

公开(公告)号：EP2743896A2

公开(公告)日：2014-06-18

申请号：EP13197270.5

申请日：2013-12-13

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： Swenson, James W.

IPC: G08B13/196 ,  H04N5/225 ,  H04N5/235

CPC classification number: H01L27/15 ,  G08B13/19626 ,  H04N5/2256 ,  H04N7/18

Abstract: A surveillance device (100) includes a circuit card assembly (104) disposed in a housing (102) and a plurality of light emitting diodes (108; 202) disposed on the circuit card assembly (104), each of the plurality of light emitting diodes (108; 202) configured to emit a narrow beam of light. The surveillance device (100) further includes a diffuser (114; 204) disposed in the housing (102), the diffuser (114; 204) configured to spread the narrow beam of light and a Fresnel lens (112; 206) disposed in the housing (102), the Fresnel lens (112; 206) configured to spread and redirect light emitted from the diffuser (114; 204).