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    • 1. 发明公开
    • Systems and methods for controlling the gas conversion in a fiber-optic gyroscope
    • 在einem faseroptischen Gyroskop系统和Verfahren zur Steuerung der Gasumwandlung
    • EP2896934A1
    • 2015-07-22
    • EP15150544.3
    • 2015-01-08
    • Honeywell International Inc.
    • Chappell, Charles D.Warrensford, Kara L.
    • G01C19/72
    • G01C19/722G01C19/721
    • A fiber optic sensing coil apparatus for a fiber optic gyroscope is provided. In at least one embodiment, the fiber optic sensing coil apparatus comprises a housing providing a hermetically sealed chamber and an optical fiber disposed within the hermetically sealed chamber of the housing, wherein the optical fiber is disposed in a coil. A gas including oxygen is disposed in the hermetically sealed chamber between the coil of the optical fiber and the housing. Moreover, an adhesive is amongst the optical fiber, wherein the adhesive holds the optical fiber together in the coil; and, a layer of oxygen blocking material is disposed on an outer surface of the coil of optical fiber, wherein the oxygen blocking material has an oxygen transmission rate less than 15 cc/m 2 /day.
    • 提供了一种用于光纤陀螺仪的光纤感测线圈装置。 在至少一个实施例中,光纤感测线圈装置包括提供气密密封室的壳体和设置在壳体的气密密封室内的光纤,其中光纤设置在线圈中。 包含氧的气​​体设置在光纤的线圈和壳体之间的气密密封室中。 此外,粘合剂在光纤之间,其中粘合剂将光纤保持在线圈中; 并且在光纤线圈的外表面上设置一层氧阻塞材料,其中氧气阻挡材料的氧气透过率小于15cc / m 2 /天。
    • 5. 发明公开
    • Intertial measurement unit with wireless power transfer gap control
    • Intertialmesseinheit mit DrahtloserLeistungsübertragungslückensteuerung
    • EP2019289A2
    • 2009-01-28
    • EP08160119.7
    • 2008-07-10
    • Honeywell International Inc.
    • Chappell, Charles D.Johnson, Robert E.Bowen, David A.
    • G01C21/16G01C19/16G01C19/20
    • G01C19/16G01C19/20G01C21/16H02J5/005H02J7/025H02J50/10H02J50/90
    • An inertial measurement unit comprises an outer case assembly including an upper gas plenum and a lower gas plenum, with upper and lower support shells surrounded by the upper and lower gas plenums. A sensor assembly includes a sensor shell, with the sensor assembly surrounded by the upper and lower support shells. A plurality of gas bearing pads extend through apertures in the upper and lower support shells and are configured to inject a first pressurized gas into a gap that separates the gas bearing pads and the sensor shell. This produces a first gas bearing that allows the sensor assembly to be freely suspended and rotated. A wireless power transfer transformer includes a power transmitting core mounted to the outer case assembly, and a power receiving core mounted in an opening of the sensor shell. The receiving core is configured to be aligned with the transmitting core for wireless power transfer. The transmitting core is configured to inject a second pressurized gas into a gap between the transmitting core and the receiving core. This produces a second gas bearing that maintains a predetermined separation distance between the transmitting core and the receiving core during the wireless power transfer.
    • 惯性测量单元包括外壳组件,其包括上气室和下气室,其中上和下支撑壳被上和下气室围绕。 传感器组件包括传感器外壳,传感器组件由上和下支撑壳包围。 多个气体支承垫通过上和下支撑壳中的孔延伸,并且被配置为将第一加压气体注入到分离气体轴承垫和传感器壳的间隙中。 这产生允许传感器组件自由地悬挂和旋转的第一气体轴承。 无线电力传输变压器包括安装在外壳组件上的动力传递芯和安装在传感器壳的开口中的受电芯。 接收核心被配置为与用于无线电力传输的发射核心对准。 发射芯构造成将第二加压气体注入发射芯和接收芯之间的间隙中。 这产生第二气体轴承,其在无线电力传输期间在发射芯和接收芯之间保持预定的间隔距离。
    • 6. 发明公开
    • Method and apparatus for joining together portions of a geometric assembly
    • 一种用于连接几何布置的部分的方法和装置
    • EP2207013A2
    • 2010-07-14
    • EP09172262.9
    • 2009-10-05
    • Honeywell International, Inc.
    • Chappell, Charles D.Burroughs, Edward
    • G01C21/16
    • G01C21/16G01C25/00Y10T29/49826
    • A housing comprises at least first and second portions. The first and second portions mate with each other at respective joining regions. The first and second portions each comprise a respective tapered flange along the joining region. The first and second portions of the housing are connected to each other by placing a plurality of collars over the tapered flanges of the first and second portions of the housing. Each of the collars has a respective groove formed therein. The grooves of the plurality of collars are placed over the tapered flanges of the first and second portions of the housing. A plurality of fasteners causes the plurality of collars to press the first and second portions of the housing together. In one embodiment, the housing is used in a sensor block assembly that is part of an inertial measurement unit.
    • 壳体包括至少第一和第二部分。 所述第一和第二部分与海誓山盟在respectivement接合区域配合。 每个第一和第二部分包括沿所述连接区的respectivement锥形凸缘。 所述壳体的第一部分和第二部分通过将套环上的多个壳体的第一和第二部分的锥形凸缘彼此连接。 每个衣领的在其中形成的凹槽respectivement。 套环的所述多个凹槽被放置在所述壳体的第一和第二部分的锥形凸缘。 紧固件将多个使衣领的多元性到所述壳体的第一和第二部分按压在一起。 在一个,实施例的壳体中的传感器块组件中使用所做的是惯性测量单元的一部分。
    • 7. 发明公开
    • Inertial measurement unit with gas plenums
    • Trägheitsmesseinheitmit Gasplena
    • EP2017575A2
    • 2009-01-21
    • EP08160131.2
    • 2008-07-10
    • Honeywell International Inc.
    • Chappell, Charles D.Bowen, David A.
    • G01C19/16G01C19/20G01C21/16
    • G01C21/16F16C32/0622F16C32/0666F16C2370/00G01C19/20G01P1/023G01P15/08
    • An inertial measurement unit comprises a mounting plate with an opening therethrough, and a sensor assembly disposed in the opening of the mounting plate. Upper and lower support shells having shell flanges are attached to upper and lower surfaces of the mounting plate. The upper and lower support shells surround the sensor assembly. A plurality of gas bearing pads each extends through apertures in the upper and lower support shells. Upper and lower gas plenums have plenum flanges attached to the shell flanges of the upper and lower support shells, with the upper and lower gas plenums surrounding the upper and lower support shells. Pressure relief valves are coupled to the plenum flanges of the upper and lower gas plenums. The gas bearing pads and the sensor assembly are separated by a gap when pressurized gas is fed into the upper and lower gas plenums, thereby creating a gas bearing that allows the sensor assembly to be freely suspended and rotated in all directions.
    • 惯性测量单元包括具有穿过其的开口的安装板和设置在安装板的开口中的传感器组件。 具有壳体凸缘的上和下支撑壳体附接到安装板的上表面和下表面。 上和下支撑壳围绕传感器组件。 多个气体支承垫各自延伸穿过上部和下部支撑壳体中的孔。 上部和下部气体增压室具有附接到上部和下部支撑壳体的壳体凸缘的增压室凸缘,上部和下部气体增压室围绕上部和下部支撑壳体。 减压阀联接到上部和下部气体充气室的增压室凸缘。 当加压气体被供给到上部和下部气体增压室中时,气体轴承瓦块和传感器组件被间隔开,从而形成允许传感器组件在所有方向上自由地悬挂和旋转的气体轴承。