公开(公告)号：US20130334363A1

公开(公告)日：2013-12-19

申请号：US13702521

申请日：2011-06-07

Applicant: Michael Lam

Inventor： Lawrence Lam ,  Michael Lam

IPC: B64C13/28 ,  B64C9/14

CPC classification number: B64C13/28 ,  B64C9/02 ,  B64C9/14 ,  B64C9/16

Abstract: An aircraft control system is presented. The system includes a wing including a flap track, and a shuttle connected to the flap track and configured to slide along a length of the flap track. The system includes a flap panel pivotally attached to the shuttle at a flap pivot. The flap panel is configured to rotate about the flap pivot. When the shuttle is deployed along a length of the flap track, the shuttle is configured to prevent rotation of the flap panel about the flap pivot, and when the shuttle is withdrawn into a stowed position, the shuttle is configured to allow the flap panel to rotate about the flap pivot.

Abstract translation: 介绍飞机控制系统。 该系统包括翼片，其包括翼片轨道，以及连接到翼片轨道并构造成沿着翼片轨道的长度滑动的梭子。 该系统包括在翼片枢轴处枢转地附接到梭子的翼片板。 翼片板被配置为围绕翼片枢轴旋转。 当梭子沿着翼片轨道的长度展开时，梭子被构造成防止翼片板围绕翼片枢轴旋转，并且当梭子被收回到收起位置时，梭子构造成允许翼片板 围绕襟翼枢轴旋转。

公开(公告)号：US08539393B2

公开(公告)日：2013-09-17

申请号：US13244070

申请日：2011-09-23

Applicant: James C Word ,  Konstantinos G Adam ,  Michael Lam ,  Sergiy Komirenko

Inventor： James C Word ,  Konstantinos G Adam ,  Michael Lam ,  Sergiy Komirenko

IPC: G06F17/50

CPC classification number: G03F1/22 ,  G03F1/70 ,  G03F7/70433

Abstract: Disclosed are techniques for simulating and correcting the mask shadowing effect using the domain decomposition method (DDM). According to various implementations of the invention, DDM signals for an extreme ultraviolet (EUV) lithography mask are determined for a plurality of azimuthal angles of illumination. Base on the DDM signals, one or more layout designs for making the mask may be analyzed and/or modified.

Abstract translation: 公开了使用域分解方法（DDM）来模拟和校正掩模阴影效应的技术。 根据本发明的各种实现方式，针对多个方位角的照明来确定用于极紫外（EUV）光刻掩模的DDM信号。 基于DDM信号，可以分析和/或修改用于制作掩模的一个或多个布局设计。

公开(公告)号：US6079672A

公开(公告)日：2000-06-27

申请号：US993241

申请日：1997-12-18

Applicant: Lawrence Y. Lam ,  Michael Lam

Inventor： Lawrence Y. Lam ,  Michael Lam

IPC: B64C9/00 ,  B64C9/06

CPC classification number: B64C9/06 ,  B64C9/00 ,  Y02T50/32 ,  Y02T50/44

Abstract: An aircraft aileron system unique in its construction, method of deployment and the functional results obtained, is comprised of two panels located at the rear portion of the wing, in a spanwise direction and aligned with the wing's trailing edge. The panels are independently hinged at their leading edges and rotate to make angular deflections with respect to the wing. The upper, aileron panel is restricted to upward deflection only from its neutral position and in operation is deployed independently as an aileron. The lower, auxiliary flap panel is capable of both upward and downward deflections from its neutral position, and is deployed independently downward as an auxiliary flap. Both panels are deployed together upwardly only as an aileron. Alternatively, the aileron panel may be capable only of upward deployment while the auxiliary flap panel is capable of downward deployment only, to provide a simpler aileron system. For roll control of an aircraft during cruise, the aileron panel on one side only is deflected up while the aileron panel on the other side remains in its neutral position. The aileron system, in conjunction with flap arrangements, offers multiple aircraft control function with advantages over past and present systems for aircraft control.

Abstract translation: 其结构独特的飞行器副翼系统，部署方法和所获得的功能结果由位于机翼后部的翼面方向的两个面板组成，并与机翼的后缘对准。 面板在其前缘独立地铰接并旋转以相对于机翼产生角度偏转。 上副翼面板仅从其中立位置限制向上偏转，并且在操作中作为副翼单独部署。 下部辅助翼片板能够从其中立位置向上和向下偏转，并且作为辅助翼片独立地向下展开。 两个面板仅作为副翼部署在一起。 或者，副翼板仅能够向上展开，而辅助翼板仅能够向下展开，以提供更简单的副翼系统。 对于巡航期间的飞行器的滚动控制，一侧的副翼面板仅在另一侧的副翼面板保持在其中立位置时被偏转。 副翼系统结合皮瓣安排，提供多种飞机控制功能，具有优于过去和现在的飞机控制系统的优点。