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    • 1. 发明申请
    • Avionics instrument and mounting bracket
    • 航空电子仪器和安装支架
    • US20110176267A1
    • 2011-07-21
    • US12657196
    • 2010-01-15
    • Joseph PolizzottoMarc PolizzottoLawrence E. Elbert
    • Joseph PolizzottoMarc PolizzottoLawrence E. Elbert
    • G06F1/16H05K7/00G12B9/00
    • H05K5/0017B64D43/00G06F1/1626G06F2200/1614H05K7/1412
    • The present invention is an avionics instrument and mounting bracket. In particular, the present invention is directed to an avionics instrument that can be mounted in a variety of positions on an aircraft instrument panel. The mounting bracket preferably comprises a cylindrical interior and an exterior with squared sides and rounded corners. The bracket has an adjustment gap with first and second ports on opposing sides and an adjustment screw spanning the adjustment gap to adjust the tightness of the bracket. The front of the bracket preferably has four panel screw ports. The avionics instrument has a display panel mounted to a cylindrical electronics housing where the diameter of the housing is less than the length of the display panel. The display panel preferably has four positional modes of display and a control button for switching between the display modes. The cylindrical electronics housing is inserted into the bracket.
    • 本发明是一种航空电子仪器和安装支架。 特别地,本发明涉及可以安装在飞机仪表板上的各种位置的航空电子仪器。 安装支架优选地包括圆柱形内部和具有正方形和圆角的外部。 支架具有与相对侧上的第一和第二端口的调节间隙,以及跨越调节间隙的调节螺钉,以调节支架的紧固度。 支架的前部优选具有四个面板螺钉端口。 航空电子仪器具有安装到圆柱形电子器件壳体上的显示面板,其中壳体的直径小于显示面板的长度。 显示面板优选具有四种显示位置模式和用于在显示模式之间切换的控制按钮。 圆柱形电子设备外壳插入支架。
    • 6. 发明授权
    • Ultrasonic horn assembly
    • 超声波喇叭组件
    • US4607185A
    • 1986-08-19
    • US697277
    • 1985-02-01
    • Lawrence E. ElbertCharles S. Irwin
    • Lawrence E. ElbertCharles S. Irwin
    • B06B1/06B06B3/00H01L41/08
    • B06B3/00
    • An ultrasonic horn assembly, particularly suitable for dissolving reagent tablets in a liquid solution in a cuvette which is moved along a path next to the front end face of the horn, includes a generally cylindrical converter fixed to a rear end face of the horn body substantially medial of the length of the rear end face. A pair of elongate resonating members are each fixed at one end to a different side end region of the rear end face on the horn body, and extend perpendicularly from the rear end face. The resonating members cause acoustic waves to propagate from the front end face of the horn body at substantially uniform amplitude along the length of the front end face, so that objects such as cuvettes moving parallel to the front end face are continuously subjected to uniform acoustic waves to insure a thorough dissolving or mixing operation.
    • 一种超声波喇叭组件,特别适用于将试剂片剂溶解在沿着喇叭的前端面旁边的路径移动的比色皿中的液体溶液中,包括大致圆柱形的转换器,其基本上固定到喇叭主体的后端面 内侧的后端面的长度。 一对细长的谐振构件的一端分别固定在喇叭体的后端面的不同的侧端区域,并且从后端面垂直地延伸。 谐振构件使声波从前端面的长度以大致均匀的振幅从喇叭体的前端面传播,使得平行于前端面移动的比色杯等物体连续地经受均匀的声波 以确保彻底的溶解或混合操作。
    • 7. 发明授权
    • Avionics instrument and mounting bracket
    • 航空电子仪器和安装支架
    • US08274783B2
    • 2012-09-25
    • US12657196
    • 2010-01-15
    • Joseph PolizzottoMarc PolizzottoLawrence E. Elbert
    • Joseph PolizzottoMarc PolizzottoLawrence E. Elbert
    • G06F1/16
    • H05K5/0017B64D43/00G06F1/1626G06F2200/1614H05K7/1412
    • The present invention is an avionics instrument and mounting bracket. In particular, the present invention is directed to an avionics instrument that can be mounted in a variety of positions on an aircraft instrument panel. The mounting bracket preferably comprises a cylindrical interior and an exterior with squared sides and rounded corners. The bracket has an adjustment gap with first and second ports on opposing sides and an adjustment screw spanning the adjustment gap to adjust the tightness of the bracket. The front of the bracket preferably has four panel screw ports. The avionics instrument has a display panel mounted to a cylindrical electronics housing where the diameter of the housing is less than the length of the display panel. The display panel preferably has four positional modes of display and a control button for switching between the display modes. The cylindrical electronics housing is inserted into the bracket.
    • 本发明是一种航空电子仪器和安装支架。 特别地,本发明涉及可以安装在飞机仪表板上的各种位置的航空电子仪器。 安装支架优选地包括圆柱形内部和具有正方形和圆角的外部。 支架具有与相对侧上的第一和第二端口的调节间隙,以及跨越调节间隙的调节螺钉,以调节支架的紧固度。 支架的前部优选具有四个面板螺钉端口。 航空电子仪器具有安装到圆柱形电子器件壳体上的显示面板,其中壳体的直径小于显示面板的长度。 显示面板优选具有四种显示位置模式和用于在显示模式之间切换的控制按钮。 圆柱形电子设备外壳插入支架。