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1. 发明授权

US06856499B2 MEMS variable inductor and capacitor 有权
标题翻译： MEMS可变电感器和电容器
公开(公告)号：US06856499B2
公开(公告)日：2005-02-15
申请号：US10402032
申请日：2003-03-28
申请人： Robert B. Stokes
发明人： Robert B. Stokes
IPC分类号： H05K1/16 , H01F17/00 , H01F21/04 , H01G5/04 , H01G5/14 , H03H7/01 , H01G7/00
CPC分类号： H01G5/14 , H01F17/0006 , H01F21/04 , H01F2007/068 , H01G5/18 , H03H7/0115 , H03H2007/008
摘要： A variable passive component is provided for fabrication on a microelectromechanical system (MEMS) device. A conductive portion is provided on a low-profile sliding dielectric sheet that cooperates with a conductive portion disposed on a substrate to provide a variable passive component. The passive component can be a variable inductor provided by moving a shorted spiral inductor formed on the dielectric sheet over a spiral inductor on the substrate with varying degrees of overlap causing varying inductance values. The passive component can be a variable capacitor that consists of a large conductive pad on a dielectric plate which slides over two adjacent pads on the substrate with varying overlap causing varying capacitance values.
摘要翻译：提供可变无源部件用于在微机电系统（MEMS）装置上制造。导电部分设置在与设置在基板上的导电部分配合以提供可变无源部件的薄型滑动电介质片上。无源部件可以是可变电感器，其通过将形成在电介质片上的短路螺旋电感器移动到衬底上的螺旋电感器上，并以不同程度的重叠使电感值变化而提供。无源部件可以是可变电容器，其由电介质板上的大导电焊盘构成，其在基板上的两个相邻焊盘上滑动，具有变化的重叠，导致变化的电容值。

2. 发明授权

US08191820B1 Flying wing aircraft 有权
标题翻译：飞翼飞机
公开(公告)号：US08191820B1
公开(公告)日：2012-06-05
申请号：US12001218
申请日：2007-12-11
申请人： Bryan Wayne Westra , Roxanne Marie Sato , Douglas Ellwood Shultz , James Franklin Kerswell , Perry Bruce Petersen , Scott Walter Collins
发明人： Bryan Wayne Westra , Roxanne Marie Sato , Douglas Ellwood Shultz , James Franklin Kerswell , Perry Bruce Petersen , Scott Walter Collins
IPC分类号： B64C39/10 , B64C5/04 , B64C5/12 , B64C21/04
CPC分类号： B64C39/10 , B64C5/12 , B64C9/12 , B64C21/04 , B64C21/08 , B64C39/12 , B64D27/20 , Y02T50/166
摘要： The invention is an aircraft that includes a flying wing having a plurality of extendable flaps mounted on the trailing edge of the flying wing. A canard is mounted on the nose of said flying wing. A system is mounted in the flying wing for providing high pressure air over the canard and the flaps. A second system is provided for controlling the flow of air over the canard to provide pitch control of the aircraft.
摘要翻译：本发明是一种飞行器，其包括具有安装在飞翼的后缘上的多个可延伸翼片的飞翼。鸭子安装在飞行翼的鼻子上。系统安装在飞翼中，用于在鸭舌和襟翼上提供高压空气。提供了一种第二系统，用于控制在鸭子上的空气流动，以提供飞行器的俯仰控制。

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