Mems element having perpendicular portion formed from substrate
    11.
    发明授权
    Mems element having perpendicular portion formed from substrate 失效
    具有由基板形成的垂直部分的金属元件

    公开(公告)号:US06813412B2

    公开(公告)日:2004-11-02

    申请号:US09915232

    申请日:2001-07-24

    Inventor: Chuang-Chia Lin

    Abstract: A microelectromechanical systems (MEMS) element and a MEMS optical switch are described. The MEMS element comprises a crystalline and moveable element is moveably attached to the substrate. The moveable element includes a perpendicular portion oriented substantially perpendicular to a plane of the substrate. The crystal structure of the perpendicular portion and substrate are substantially similar. The moveable element is capable of motion substantially constrained to a plane oriented substantially perpendicular to a plane of the substrate. In at least one position, a part of a perpendicular portion of the moveable element projects beyond a surface of the substrate. The moveable element may be retained in place by a latch. An array of such structures can be implemented to work as an optical switch. The optical switch may comprise a crystalline substrate and one or more moveable elements moveably attached to the substrate. The various embodiments provide for a robust and reliable MEMS elements that may be simply fabricated and densely packed.

    Abstract translation: 描述了微机电系统(MEMS)元件和MEMS光开关。 MEMS元件包括可移动地附接到基底的结晶和可移动元件。 可移动元件包括垂直于基本垂直于基底平面的垂直部分。 垂直部分和基底的晶体结构基本相似。 可移动元件能够基本上约束到基本上垂直于衬底的平面定向的平面的运动。 在至少一个位置中,可移动元件的垂直部分的一部分突出超过衬底的表面。 可移动元件可以通过闩锁保持在适当的位置。 可以实现这种结构的阵列以用作光学开关。 光学开关可以包括结晶衬底和可移动地附接到衬底的一个或多个可移动元件。 各种实施例提供了可以简单地制造和密集包装的鲁棒且可靠的MEMS元件。

    SURFACE ACOUSTIC WAVE SENSOR ASSEMBLY
    13.
    发明公开

    公开(公告)号:US20240356520A1

    公开(公告)日:2024-10-24

    申请号:US18412243

    申请日:2024-01-12

    Inventor: Chuang-Chia Lin

    CPC classification number: H03H9/02842 H03H9/02543 H10N30/302

    Abstract: A sensor device that includes an integrated sensor assembly having a surface acoustic wave (SAW) sensor disposed on a piezoelectric substrate. The SAW sensor is adapted to measure an environmental condition of an environment in response to an RF signal. The SAW sensor includes an interdigitated transducer (IDT) formed on a substrate having at least a layer of a piezoelectric material. The SAW sensor includes either one or more SAW reflectors of a second IDT formed on the piezoelectric material. The SAW sensor further includes an RF antenna formed on the piezoelectric material. The SAW sensor and the RF antenna are integrated with one another on the piezoelectric material.

    Mechanical latch locking detection sensors

    公开(公告)号:US07843363B2

    公开(公告)日:2010-11-30

    申请号:US11827591

    申请日:2007-07-12

    CPC classification number: E05B39/04 B64D29/06 E05C19/145 Y10T292/0948

    Abstract: The invention provides a sensor for determining when a latch for securing an engine cowl on an aircraft is secured by detecting the proximity of a latch hook and a latch pin. The sensor includes a resonant circuit configured and adapted to transmit a status signal when the latch is in a secured state. The sensor also includes a means for conveying status information of the latch to a location remote from the latch based on the status signal, the conveying means being operably connected to the resonant circuit. The invention also provides a method of determining when a latch is open or secured by detecting the proximity of a latch hook and a latch pin.

    Method of forming protrusions on single crystal silicon structures built on silicon-on-insulator wafers
    16.
    发明授权
    Method of forming protrusions on single crystal silicon structures built on silicon-on-insulator wafers 失效
    在绝缘体上硅晶片上形成的单晶硅结构上形成突起的方法

    公开(公告)号:US06413793B1

    公开(公告)日:2002-07-02

    申请号:US09858469

    申请日:2001-05-17

    CPC classification number: B81B3/001

    Abstract: A semiconductor structure includes a substrate, a sacrificial layer formed on or over the substrate, and a structural layer formed on or over the sacrificial layer. At least one opening is formed in the structural layer. At least one opening is formed in the sacrificial layer below the at least one opening in the structural layer. The at least one opening in the structural layer and the at least one opening in the sacrificial layer are at least partially filled with a filler material. At least one portion of the structural layer is removed to define at least one microstructure. The sacrificial layer is removed such that the at least one microstructure is released from the substrate and the filler material forms one or more protrusions on the at least one microstructure, and/or one or more anchors anchoring the at least one microstructure to the substrate.

    Abstract translation: 半导体结构包括衬底,形成在衬底上或衬底上的牺牲层以及形成在牺牲层上或之上的结构层。 在结构层中形成至少一个开口。 在结构层中的至少一个开口下方的牺牲层中形成至少一个开口。 结构层中的至少一个开口和牺牲层中的至少一个开口至少部分地填充有填充材料。 去除结构层的至少一部分以限定至少一个微结构。 去除牺牲层,使得至少一个微结构从衬底释放并且填充材料在至少一个微结构上形成一个或多个突起,和/或一个或多个将至少一个微结构锚定到衬底的锚固件。

    Systems and methods for mounting landing gear strain sensors
    18.
    发明授权
    Systems and methods for mounting landing gear strain sensors 有权
    安装起落架应变传感器的系统和方法

    公开(公告)号:US08359932B2

    公开(公告)日:2013-01-29

    申请号:US12839170

    申请日:2010-07-19

    CPC classification number: B64C25/001 B64C25/60 B64D2045/008 G01L1/142

    Abstract: A strain sensor device for measuring loads on aircraft landing gear. This is done by measuring strains in the lower end of the strut, by which we infer the loading in the entire landing gear structure. These strains can be very large (as high as 10,000 microstrain) and can be imposed in numerous random directions and levels. The present invention includes a removable sensor assembly. An electromechanical means is presented that can accommodate large strains, be firmly attached to the strut, and provide good accuracy and resolution.

    Abstract translation: 用于测量飞机起落架载荷的应变传感器装置。 这是通过测量支柱下端的应变来进行的,我们推断整个起落架结构的载荷。 这些菌株可以非常大(高达10,000微克),并且可以在许多随机的方向和水平上施加。 本发明包括可拆卸传感器组件。 提出了一种可以容纳大应变的机电装置,牢固地连接到支柱上,并提供良好的精度和分辨率。

    SYSTEMS AND METHODS FOR MOUNTING LANDING GEAR STRAIN SENSORS
    19.
    发明申请
    SYSTEMS AND METHODS FOR MOUNTING LANDING GEAR STRAIN SENSORS 有权
    用于安装接地齿轮传感器的系统和方法

    公开(公告)号:US20120011946A1

    公开(公告)日:2012-01-19

    申请号:US12839170

    申请日:2010-07-19

    CPC classification number: B64C25/001 B64C25/60 B64D2045/008 G01L1/142

    Abstract: A strain sensor device for measuring loads on aircraft landing gear. This is done by measuring strains in the lower end of the strut, by which we infer the loading in the entire landing gear structure. These strains can be very large (as high as 10,000 microstrain) and can be imposed in numerous random directions and levels. The present invention includes a removable sensor assembly. An electromechanical means is presented that can accommodate large strains, be firmly attached to the strut, and provide good accuracy and resolution.

    Abstract translation: 用于测量飞机起落架载荷的应变传感器装置。 这是通过测量支柱下端的应变来进行的,我们推断整个起落架结构的载荷。 这些菌株可以非常大(高达10,000微克),并且可以在许多随机的方向和水平上施加。 本发明包括可拆卸传感器组件。 提出了一种可以容纳大应变的机电装置,牢固地连接到支柱上,并提供良好的精度和分辨率。

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