公开(公告)号：US20150110154A1

公开(公告)日：2015-04-23

申请号：US14191800

申请日：2014-02-27

Applicant: Rosemount Aerospace Inc.

Inventor： Matthew J. T. Gmach ,  Robert E. Sable ,  John T. Otto ,  Scott Wigen

IPC: G01K13/00

CPC classification number: G01K1/22 ,  G01K13/00 ,  G01K13/028

Abstract: A temperature sensor includes a sensor body and a wedge extension. The sensor body extends from a sensor base to an opposed sensor tip along a longitudinal axis. The sensor body has a leading edge and opposed trailing edge. The sensor body also has 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. The wedge extension is on the sensor body between the sensor tip and the sensor base on the leading edge of the sensor body.

Abstract translation: 温度传感器包括传感器主体和楔形延伸部。 传感器主体沿着纵向轴线从传感器基座延伸到相对的传感器尖端。 传感器主体具有前缘和相对的后缘。 传感器体还具有内部流动通道，其具有用于将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。 楔形延伸部位于传感器顶端与传感器主体前缘的传感器底座之间的传感器本体上。

公开(公告)号：US20150103863A1

公开(公告)日：2015-04-16

申请号：US14184290

申请日：2014-02-19

Applicant: Rosemount Aerospace Inc.

Inventor： Chad J. Herman

IPC: G01K13/02

CPC classification number: G01K13/028

Abstract: A total air temperature probe includes a probe body extending from a probe base to an opposed probe tip along a longitudinal axis defining a leading edge and opposed trailing edge, an interior flow passage aligned with longitudinal axis defined in probe body with an inlet defined on probe tip for fluid communication with interior flow passage, and an outlet for exhausting fluid out from interior flow passage. A sloped surface on probe tip extends from leading edge to trailing edge. A temperature sensor is mounted within interior flow passage for measuring temperature of flow through interior flow passage to determine total air temperature. Sloped surface is flush with leading edge and set in from trailing edge with respect to longitudinal axis to define a lip proximate the trailing edge. The sloped surface and lip are configured to create a high pressure region proximate inlet of interior flow passage.

Abstract translation: 总空气温度探针包括探针主体，其沿着限定前缘和相对后缘的纵向轴线从探针基部延伸到相对的探针尖端，内部流动通道与限定在探针主体中的纵向轴线对准，并具有限定在探针上的入口 用于与内部流动通道流体连通的末端，以及用于从内部流动通道排出流体的出口。 探针尖端上的倾斜表面从前缘延伸到后缘。 温度传感器安装在内部流动通道内，用于测量通过内部流动通道的流量的温度，以确定总空气温度。 倾斜表面与前缘齐平，并相对于纵向轴线从后缘设置，以限定靠近后缘的唇缘。 倾斜表面和唇缘构造成在内部流动通道的入口附近产生高压区域。

公开(公告)号：US20150101414A1

公开(公告)日：2015-04-16

申请号：US14189899

申请日：2014-02-25

Applicant: Rosemount Aerospace Inc.

Inventor： Saeed Fahimi ,  Odd H. Eriksen ,  Charles Little

IPC: G01L13/02 ,  G01D11/24

CPC classification number: G01L13/028 ,  G01D11/245 ,  G01L13/04 ,  G01L15/00 ,  G01L19/0038

Abstract: A transducer baseplate includes a base, a protrusion extending from the base along a longitudinal axis, a pair of opposed transducer receptacles defined within the protrusion, and respective pressure plena. The pressure plena are separated by a plenum wall, each plenum being in fluid connection with an area external to the protrusion through a respective pressure line. The pressure lines provide a direct fluid path to their respective receptacles.

Abstract translation: 传感器基板包括基部，从基部沿着纵向轴线延伸的突起，限定在突出部内的一对相对的换能器插座以及相应的压力斑。 压力斑块由一个增压室隔开，每个气室通过相应的压力管线与突起外部的区域流体连接。 压力线提供了直接流体通向其各自的容器。

公开(公告)号：US08979048B2

公开(公告)日：2015-03-17

申请号：US13899199

申请日：2013-05-21

Applicant: Rosemount Aerospace Inc.

Inventor： Matthew A. Tschann ,  Kenneth J. Freeman

IPC: A47B96/00 ,  B64D43/00 ,  F16M11/04 ,  F16M11/08 ,  F16M13/02

CPC classification number: B64D43/00 ,  F16M11/041 ,  F16M11/08 ,  F16M13/022 ,  F16M2200/024 ,  Y10T403/70

Abstract: An assembly includes an adapter portion configured for attachment to a rear surface of an electronic display device and a base portion configured to be mounted to a fixed structure in the cockpit of an aircraft. The adapter portion has a cylindrical barrel portion having a plurality of circumferentially disposed radially outwardly extending keys, a first radially inwardly extending recess corresponding to a landscape position of the display device and a second radially inwardly extending recess corresponding to a portrait position of the display device. The base portion includes an upper surface with a circular reception port formed therein for receiving the barrel portion of the adapter portion, and the reception port has a plurality of radially outwardly extending circumferentially disposed keyways formed therein for receiving the plurality of keys on the barrel portion of the adapter portion.

Abstract translation: 组件包括配置成附接到电子显示装置的后表面的适配器部分和构造成安装到飞行器驾驶舱中的固定结构的基部。 适配器部分具有圆柱形筒部分，其具有多个周向布置的径向向外延伸的键，对应于显示装置的横向位置的第一径向向内延伸的凹部和对应于显示装置的纵向位置的第二径向向内延伸的凹部 。 基部包括形成在其中的圆形接收端口的上表面，用于容纳适配器部分的筒部，并且接收端口具有形成在其中的多个径向向外延伸的周向设置的键槽，用于容纳筒部分上的多个键 的适配器部分。

公开(公告)号：US20140339385A1

公开(公告)日：2014-11-20

申请号：US13893495

申请日：2013-05-14

Applicant: Rosemount Aerospace Inc.

Inventor： Jonathan L. Boer ,  Kaleb Anderson

IPC: F16M13/02 ,  B64D47/00

CPC classification number: F16M13/02 ,  B60R11/0235 ,  B60R2011/0085 ,  B64D45/00 ,  B64D47/00 ,  B64D2045/0075

Abstract: An assembly is disclosed for mounting an electronic display device to a supporting structure within the cockpit of an aircraft which includes a circular adapter plate configured for attachment to a rear surface of an electronic display device, the adapter plate having a central alignment aperture with an axially extending annular wall that faces away from the rear surface of the display device, and a receiver plate configured for attachment to a supporting structure within the cockpit of an aircraft, the receiver plate having a recessed port for blindly receiving the annular wall of the central alignment aperture of the adapter plate.

Abstract translation: 公开了一种用于将电子显示装置安装到飞行器驾驶舱内的支撑结构的组件，其包括构造成附接到电子显示装置的后表面的圆形适配器板，所述适配器板具有轴向的中心对准孔 面向远离显示装置的后表面的延伸的环形壁以及被配置为附接到飞行器的驾驶舱内的支撑结构的接收板，所述接收板具有用于盲目地接收中心对准的环形壁的凹入端口 适配器板的孔径。

公开(公告)号：US20140327764A1

公开(公告)日：2014-11-06

申请号：US13875888

申请日：2013-05-02

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： Ryan Nelson ,  Alexander Stephens

IPC: H04N5/225 ,  H04N7/18

CPC classification number: H04N5/2252 ,  F16M11/10 ,  F16M11/18 ,  F16M11/2014 ,  F16M13/02 ,  H04N7/18

Abstract: A gimbal assembly including a gimbal housing having opposed first and second yoke portions dimensioned and configured to receive a surveillance device therebetween, the yoke portions defining a gimbal axis about which the surveillance device can rotate relative to the gimbal housing, and a drive assembly disposed within the first yoke portion of the gimbal housing for driving the surveillance device about the gimbal axis, the drive assembly having a connector adapted and configured to mate with and pass electrical signals to and from a corresponding connector on the surveillance device, wherein the second yoke portion is detachable from the gimbal housing to gain access to the surveillance device and the surveillance device is removably connected to the drive assembly.

Abstract translation: 一种万向架组件，包括具有相对的第一和第二磁轭部分的相对的第一和第二磁轭部分的万向架壳体，其尺寸设计成在其间接纳监视装置，所述磁轭部分限定了万向轴线，监视装置可围绕该万向轴线相对于万向节壳体旋转;以及驱动组件， 用于围绕万向轴驱动监视装置的万向架壳体的第一磁轭部分，驱动组件具有适于并配置成与监视装置上的对应连接器配合并将电信号传递到监视装置上的相应连接器的连接器，其中第二磁轭部分 可从万向节壳体拆卸以便进入监视装置，并且监视装置可移除地连接到驱动组件。

公开(公告)号：US20140312161A1

公开(公告)日：2014-10-23

申请号：US13898046

申请日：2013-05-20

Applicant: Rosemount Aerospace Inc.

Inventor： Todd A. Ell

IPC: F41G7/22 ,  G01S3/781

CPC classification number: F41G7/2246 ,  F41G7/008 ,  F41G7/2253 ,  F41G7/226 ,  F41G7/2293 ,  G01S3/781 ,  Y10T29/49002

Abstract: Dual mode SAL/IR imaging seekers are described herein. In some embodiments, a dual-mode SAL/IR imaging seeker described herein includes a focal plane array (FPA), an objective optical assembly providing a common optical path to the FPA for incident laser radiation of a first wavelength band and incident ambient radiation of a second wavelength band non-overlapping with the first wavelength band, a first optical filter operable to selectively pass the incident laser radiation to the FPA in a transmissive mode and selectively block the incident laser radiation from the FPA in a non-transmissive mode and a second optical filter assembly operable to selectively pass the incident ambient radiation to the FPA in a transmissive mode and selectively block the incident ambient radiation from the FPA in a non-transmissive mode.

Abstract translation: 这里描述了双模式SAL / IR成像寻像器。 在一些实施例中，本文所述的双模SAL / IR成像探测器包括焦平面阵列（FPA），物镜光学组件，其提供到FPA的公共光路，用于第一波长带的入射激光辐射和入射环境辐射 与第一波长带不重叠的第二波长带，第一滤光器，其可操作以以透射模式选择性地将入射激光辐射传递到FPA，并以非透射模式选择性地阻挡来自FPA的入射激光辐射，以及 第二光学滤光器组件，其可操作以选择性地将透射模式中的入射环境辐射传递到FPA，并以非透射模式选择性地阻挡来自FPA的入射环境辐射。

公开(公告)号：US20140050247A1

公开(公告)日：2014-02-20

申请号：US13964693

申请日：2013-08-12

Applicant: Rosemount Aerospace Inc.

Inventor： Chad James Herman ,  Howard Earl Larson

IPC: G01K13/02

CPC classification number: G01K1/20 ,  G01K13/028 ,  G01K2013/024

Abstract: A total air temperature probe includes a probe head having an airflow inlet, a main airflow outlet, a main probe head wall extending from the airflow inlet to the main airflow outlet, and a flow separation bend wall positioned between the airflow inlet and the main airflow outlet. The flow separation bend wall is opposite the main probe head wall across a primary flow passage defined through the probe head from the airflow inlet to the main airflow outlet. A flow separation trip feature is defined on an interior surface of the main probe head wall for tripping a boundary layer flow separation in flow in the primary flow passage, e.g., for reduction of deicing heater error.

Abstract translation: 总空气温度探头包括具有气流入口，主气流出口，从气流入口延伸到主气流出口的主探头顶壁的探头和位于气流入口与主气流之间的流动分离弯曲壁 出口。 流动分离弯曲壁与主探头头壁相对，穿过从气流入口到主气流出口通过探头限定的主流道。 流量分离跳闸特征被限定在主探头头壁的内表面上，用于跳过主流道中的流动中的边界层流动分离，例如用于减少除冰加热器误差。

公开(公告)号：US20040024538A1

公开(公告)日：2004-02-05

申请号：US10628551

申请日：2003-07-28

Applicant: Rosemount Aerospace Inc.

Inventor： John A. Severson ,  Kenneth J. Schram

IPC: G06F019/00 ,  G01N031/00

CPC classification number: B64D15/22

Abstract: Ice accretion on a probe is detected with various ice detectors to provide a signal indicating the rate of ice accretion. The rate of change of ice accretion is determined and is combined with parameters including air velocity, air pressure and air temperature for providing a signal that indicates liquid water content in the airflow, as well as ice accretion on the ice detector.

Abstract translation: 用各种冰检测器检测探头上的积冰，以提供指示积冰速率的信号。 确定积冰的变化速率，并与包括空气速度，空气压力和空气温度在内的参数相结合，以提供指示气流中的液态水含量的信号，以及冰检测器上的积冰。

公开(公告)号：US20250130315A1

公开(公告)日：2025-04-24

申请号：US18382970

申请日：2023-10-23

Applicant: Rosemount Aerospace Inc.

Inventor： Gary E. Halama ,  Phillip Acott

IPC: G01S7/481 ,  G01S7/497

Abstract: In accordance with at least one aspect of this disclosure, a method for seeding an optical beam includes, emitting an optical beam from an energy source towards an optical amplifier along an optical axis, and rotating one or more optical elements disposed with in the beam path of the optical beam between the energy source and the optical amplifier about the optical axis to a align the optical beam with a reference beam.