-
公开(公告)号：US08274783B2
公开(公告)日：2012-09-25
申请号：US12657196
申请日：2010-01-15
IPC分类号： G06F1/16
CPC分类号： H05K5/0017 , B64D43/00 , G06F1/1626 , G06F2200/1614 , H05K7/1412
摘要： 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.
摘要翻译： 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。
-
公开(公告)号：US20110176267A1
公开(公告)日：2011-07-21
申请号：US12657196
申请日：2010-01-15
CPC分类号： H05K5/0017 , B64D43/00 , G06F1/1626 , G06F2200/1614 , H05K7/1412
摘要： 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.
摘要翻译： 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。
-
公开(公告)号：US20120320512A1
公开(公告)日：2012-12-20
申请号：US13573131
申请日：2012-08-25
CPC分类号： H05K5/0017 , B64D43/00 , G06F1/1626 , G06F2200/1614 , H05K7/1412
摘要： 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.
-
-
搜索结果
3 条记录 (耗时 0.015 秒)
