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1. 发明申请

US20090264168A1 SLIDING MECHANISM AND PORTABLE ELECTRONIC DEVICE USING THE SAME 失效
标题翻译：使用它的滑动机构和便携式电子设备
公开(公告)号：US20090264168A1
公开(公告)日：2009-10-22
申请号：US12327430
申请日：2008-12-03
申请人： JUN WANG , HSIAO-HUA TU , GANG YANG , WEN-WEI SONG , PENG ZHAO
发明人： JUN WANG , HSIAO-HUA TU , GANG YANG , WEN-WEI SONG , PENG ZHAO
IPC分类号： H04M1/00
CPC分类号： H04M1/0237
摘要： A sliding mechanism includes a first plate (32) having a sliding slot (322) and a control slot (325) defined therein. The sliding slot and the control slot having a certain angle therebetween and communicating with each other. A second plate (38) is longitudinally slidably connected to the first plate. The second plate including a sliding member (381) formed on a surface thereof facing the first plate. The sliding member engages with the sliding slot and includes an elastic positioning assembly (389). A control assembly (34) is slidably received in the control slot. A main elastic member (36) has one end thereof being fixed to one end of the sliding slot, the other end thereof being fixed with the sliding member. A portable electronic device (100) using the sliding mechanism is also disclosed.
摘要翻译：滑动机构包括具有滑动槽（322）和限定在其中的控制槽（325）的第一板（32）。滑槽和控制槽在其间具有一定角度并且彼此连通。第二板（38）纵向可滑动地连接到第一板。第二板包括形成在面向第一板的表面上的滑动构件（381）。滑动构件与滑动槽接合并且包括弹性定位组件（389）。控制组件（34）可滑动地容纳在控制槽中。主弹性构件（36）的一端固定在滑动槽的一端，另一端与滑动构件固定。还公开了使用滑动机构的便携式电子设备（100）。

2. 发明申请

US20150284104A1 Rotatable fairing and engine inlet system for high-speed aircraft 审中-公开
标题翻译：用于高速飞机的可旋转整流罩和发动机进气系统
公开(公告)号：US20150284104A1
公开(公告)日：2015-10-08
申请号：US14246021
申请日：2014-04-04
申请人： PENG ZHAO
发明人： PENG ZHAO
IPC分类号： B64D33/02 , B64D29/02 , F02C7/055 , F02C3/10 , F02C7/045
CPC分类号： B64D33/02 , B64D29/02 , B64D2033/0226 , B64D2033/026 , B64D2033/0273 , F02C3/10 , F02C7/045 , F02C7/055 , F02C9/16
摘要： A rotatable fairing and an engine inlet for a high cruise speed aircraft are introduced. The fairing has a generally semi-cylindrical shape with tapering at either end. The fairing is movably attached to the wing and the circumference of the inlet to allow for rotational movement. The front portion of the fairing is partially outside of the inlet and forms a piece of the airplane wing and the back portion resides inside the inlet. The fairing can be rotated along its longitudinal axis to one of two states, allowing air to flow into the main engine inlet either from above or below the wing. A second embodiment of the invention adds to the fairing structure an actual inlet portion, which can also be rotated to either above or below the wing and accommodate boundary layer diversion features and movable ramps needed for high supersonic speeds.
摘要翻译：介绍了一种用于高速巡航飞机的可旋转整流罩和发动机入口。整流罩具有通常为半圆柱形的形状，其两端呈锥形。整流罩可移动地附接到机翼和入口的圆周以允许旋转运动。整流罩的前部分部分在入口外部，形成飞机机翼，后部位于入口内。整流罩可以沿其纵向轴线旋转到两种状态之一，允许空气从机翼上方或下方流入主发动机入口。本发明的第二实施例增加了整流罩结构的实际入口部分，其也可以旋转到机翼的上方或下方，并且适应高超声速度所需的边界层转向特征和可移动坡道。

3. 发明申请

US20070165369A1 DISPLAY DEVICE 失效
标题翻译：显示设备
公开(公告)号：US20070165369A1
公开(公告)日：2007-07-19
申请号：US11563148
申请日：2006-11-25
申请人： LIN-YUN HONG , HSUAN-CHEN CHEN , CHIEN-LI TSAI , CHUN-CHI LIANG , KE-CHENG LIN , PENG ZHAO
发明人： LIN-YUN HONG , HSUAN-CHEN CHEN , CHIEN-LI TSAI , CHUN-CHI LIANG , KE-CHENG LIN , PENG ZHAO
IPC分类号： G06F1/16 , G03G21/18
CPC分类号： G06F1/1616 , G06F1/1637
摘要： A display device includes a frame defining an opening, a shell, and a display panel installed between the frame and the shell. The display panel is viewable via the opening of the frame. A latch is formed on the frame. A fixing portion is formed on the shell and slidably engaged with the latch of the frame for slidably fixing the shell to the frame. A plurality of fasteners extends through the frame to engage with the shell to thereby fasten the frame and the shell together.
摘要翻译：显示装置包括限定开口，框架和安装在框架和壳体之间的显示面板的框架。显示面板可通过框架的开口来观看。在框架上形成闩锁。固定部分形成在壳体上并与框架的闩锁可滑动地接合，以将壳体可滑动地固定到框架上。多个紧固件延伸穿过框架以与壳体接合，从而将框架和壳体紧固在一起。

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