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    • 4. 发明授权
    • Integrated silicon optomechanical gyroscopes (OMGs)
    • 集成硅光机械陀螺仪(OMG)
    • US09482535B2
    • 2016-11-01
    • US13996669
    • 2011-12-23
    • John HeckHaisheng RongRichard Jones
    • John HeckHaisheng RongRichard Jones
    • G01C19/66G01C19/5684
    • G01C19/661G01C19/5684
    • A system having an optomechanical gyroscope device. An optomechanical disk acts as an optical ring resonator and a mechanical disk resonator. A drive laser generates an optical drive signal. A drive channel acts as a waveguide for the optical drive signal and includes drive electrodes in a first proximity with respect to the optomechanical disk. The drive electrodes to excite the ring by evanescent coupling. A drive photodetector is configured to receive an output optical signal from the drive channel. A sense laser generates a optical sense signal. A sense channel acts as a waveguide for the optical sense signal and includes sense electrodes in a second proximity with respect to the optomechanical disk. A sense photodetector is configured to receive an output optical signal from the sense channel.
    • 具有光学陀螺仪装置的系统。 光学机械盘用作光环谐振器和机械盘谐振器。 驱动激光器产生光驱动信号。 驱动通道用作用于光驱动信号的波导,并且包括相对于机电盘第一接近的驱动电极。 驱动电极通过ev逝耦合激发环。 驱动光电检测器被配置为从驱动通道接收输出光信号。 感测激光产生光学感测信号。 感测通道用作光学感测信号的波导,并且包括相对于光学机械盘的第二接近度的感测电极。 感测光电检测器被配置为从感测通道接收输出光信号。
    • 5. 发明申请
    • AIRCRAFT SAFETY DEVICE SYSTEMS
    • 飞机安全装置系统
    • US20160200445A1
    • 2016-07-14
    • US15080300
    • 2016-03-24
    • Richard JonesTerrell Jones
    • Richard JonesTerrell Jones
    • B64D33/02
    • B64D33/02B64D2033/022B64D2033/0286F02C7/055
    • An aircraft system comprising a deflector assembly including, a base having mounting apertures; an inner ring concentrically positioned within an outer ring, the inner ring and the outer ring have an annulus defined therebetween via a base plate, a plurality of rods attached within the annulus and culminating at an apex creating a conical profile; and a forward-mounted cone-shaped deflecting member. The base plate comprises a through hole allowing airflow through the deflector assembly to supply an airplane engine. The aircraft safety device system further comprises at least one locking latch for removably securing the deflector assembly to a housing of the airplane engine. The aircraft safety device is mountable inside a lip of the housing of the airplane engine. Further, the aircraft safety device provides protection for airplane engines from air born animate and inanimate objects.
    • 一种飞行器系统,包括偏转器组件,该偏转器组件包括:具有安装孔的底座; 内圈同心地定位在外圈内,内环和外环具有通过基板在其间限定的环,多个杆附接在环形空间内并且在顶点达到顶点,产生锥形轮廓; 和前置锥形偏转构件。 基板包括通孔,允许气流通过偏转器组件以供应飞机发动机。 飞机安全装置系统还包括至少一个锁定闩锁,用于可拆卸地将偏转器组件固定到飞机发动机的壳体上。 飞机安全装置可安装在飞机发动机壳体的唇部内。 此外,飞机安全装置为空中出生的动画和无生命物体提供对飞机发动机的保护。
    • 6. 发明授权
    • Backside thermal patterning of buried oxide (BOX)
    • 掩埋氧化物背面热图案(BOX)
    • US08716840B2
    • 2014-05-06
    • US12060177
    • 2008-03-31
    • Richard Jones
    • Richard Jones
    • H01L29/02H01L21/311
    • H01L29/02H01L21/311H01L21/7624H01S5/021H01S5/0261
    • The dominant source of thermal resistance for silicon photonic devices patterned on SOI wafers is the buried oxide layer. To ensure efficient thermally driven silicon devices there is a need for a large thermal resistance. This is in contrast to temperature sensitive components need to have low thermal resistance in order to reduce their temperature to ensure good performance. Embodiments comprise etching the back of an SOI wafer to expose the buried oxide layer and depositing an additional layer of silicon oxide to increase the local thermal resistance. Thus, embodiments provide the ability to tailor the thermal resistance across the wafer or die depending on the device being fabricated.
    • 在SOI晶片上图案化的硅光子器件的主要热阻源是掩埋氧化物层。 为了确保有效的热驱动硅器件,需要大的热阻。 这与温度敏感元件相比,需要具有低热阻,以降低其温度以确保良好的性能。 实施例包括蚀刻SOI晶片的背面以暴露掩埋氧化物层并沉积附加的氧化硅层以增加局部热阻。 因此,实施例提供了根据正在制造的器件来跨越晶片或管芯定制热阻的能力。
    • 7. 发明申请
    • INTEGRATED SILICON OPTOMECHANICAL GYROSCOPES (OMGS)
    • 综合硅光电陀螺(OMGS)
    • US20130293898A1
    • 2013-11-07
    • US13996669
    • 2011-12-23
    • John HeckHaisheng RongRichard Jones
    • John HeckHaisheng RongRichard Jones
    • G01C19/66
    • G01C19/661G01C19/5684
    • A system having an optomechanical gyroscope device. An optomechanical disk acts as an optical ring resonator and a mechanical disk resonator. A drive laser generates an optical drive signal. A drive channel acts as a waveguide for the optical drive signal and includes drive electrodes in a first proximity with respect to the optomechanical disk. The drive electrodes to excite the ring by evanescent coupling. A drive photodetector is configured to receive an output optical signal from the drive channel. A sense laser generates a optical sense signal. A sense channel acts as a waveguide for the optical sense signal and includes sense electrodes in a second proximity with respect to the optomechanical disk. A sense photodetector is configured to receive an output optical signal from the sense channel.
    • 具有光学陀螺仪装置的系统。 光学机械盘用作光环谐振器和机械盘谐振器。 驱动激光器产生光驱动信号。 驱动通道用作用于光驱动信号的波导,并且包括相对于机电盘第一接近的驱动电极。 驱动电极通过ev逝耦合激发环。 驱动光电检测器被配置为从驱动通道接收输出光信号。 感测激光产生光学感测信号。 感测通道用作光学感测信号的波导,并且包括相对于光学机械盘的第二接近度的感测电极。 感测光电检测器被配置为从感测通道接收输出光信号。
    • 10. 发明授权
    • Narrow surface corrugated grating
    • 窄表面波纹光栅
    • US08223811B2
    • 2012-07-17
    • US13160277
    • 2011-06-14
    • Richard Jones
    • Richard Jones
    • H01S3/10
    • H01S5/1032G02B6/124G02B6/29325H01S5/021H01S5/0268H01S5/1035H01S5/125H01S5/4087
    • Narrow surface corrugated gratings for integrated optical components and their method of manufacture. An embodiment includes a grating having a width narrower than a width of the waveguide on which the grating is formed. In accordance with certain embodiments of the present invention, masked photolithography is employed to form narrowed gratings having a desired grating strength. In an embodiment, an optical cavity of a laser is formed with a reflector grating having a width narrower than a width of the waveguide. In another embodiment an integrated optical communication system includes one or more narrow surface corrugated gratings.
    • 用于集成光学部件的窄表面波纹光栅及其制造方法。 一个实施例包括具有窄于其上形成有光栅的波导的宽度的宽度的光栅。 根据本发明的某些实施例,采用掩模光刻技术来形成具有所需光栅强度的窄格栅。 在一个实施例中,激光器的光腔形成有具有窄于波导宽度的宽度的反射器光栅。 在另一个实施例中,集成光通信系统包括一个或多个窄波纹光栅。