公开(公告)号：US20050001763A1

公开(公告)日：2005-01-06

申请号：US10610544

申请日：2003-07-02

Applicant: Shaowei Han ,  Kevin Chin

Inventor： Shaowei Han ,  Kevin Chin

IPC: G01S19/04 ,  G01S5/14 ,  G01S19/07 ,  G01S19/11 ,  G01S19/48

CPC classification number: G01S19/44

Abstract: A method of, apparatus for, and computer-readable medium for rapid, real time kinematics determination requiring lowered information transmission for position updates than traditional RTK systems. Position signals are received from a base station and roving system and a compressed position signal is received from the base station. A position estimate using an integrated method is determined using the received position signals from the base station and the roving system and the compressed position signal from the base station. Ambiguity resolution of the position estimate is enhanced by applying a quality control procedure using derived validation criteria. A second position estimate is derived based on the enhanced ambiguity resolution. Because of the use of the compressed position signal smaller transmissions may be performed at a more rapid rate providing a higher position update rate.

Abstract translation: 一种用于快速，实时运动学确定的方法，装置和计算机可读介质，其需要比传统RTK系统更低位置更新的信息传输。 从基站和粗纱系统接收位置信号，并从基站接收压缩位置信号。 使用来自基站和粗纱系统的接收到的位置信号和来自基站的压缩位置信号来确定使用集成方法的位置估计。 通过使用衍生的验证标准应用质量控制程序来增强位置估计的模糊度解析。 基于增强的模糊度分辨率导出第二位置估计。 由于使用压缩位置信号，可以以更快的速率执行更小的传输，从而提供更高的位置更新速率。

公开(公告)号：US06283707B1

公开(公告)日：2001-09-04

申请号：US09520619

申请日：2000-03-07

Applicant: Kevin Chin

Inventor： Kevin Chin

IPC: B63H114

CPC classification number: F01D5/16 ,  F01D5/26 ,  Y10S416/50

Abstract: An aerofoil blade damper comprising an elongate member which is inserted within a core passage of the blade and extends within the blade with the damper retained therein at one end which is closest to the blade root with the remainder of the damper free to move relative to and within the passage; such movement generating friction which dissipates any vibration. The damper comprises a plate insert including at least two discrete substantially oppositely directed contact regions which are arranged, in use, to frictionally engage the passage. The discrete contact regions may be provided by protrusions in the form of contact pads or arms extending from the plate or be provided by the corrugations of the plate. A contact load on the contact regions is provided by the resilience of the damper, an interference fit of the damper and/or centrifugal loading of the damper and contact regions during operation.

Abstract translation: 一种翼型叶片阻尼器，其包括细长构件，所述细长构件插入在所述叶片的芯通道内并且在所述叶片内延伸并且所述阻尼器保持在所述叶片中的最靠近叶片根部的一端处，其中阻尼器的其余部分相对于 在通道内 这种运动产生消除任何振动的摩擦。 阻尼器包括板插入件，其包括至少两个离散的基本上相对定向的接触区域，其在使用中被布置成与通道摩擦接合。 分立的接触区域可以由接触垫或臂的形式的突起提供，所述接触垫或臂从板延伸或由板的波纹提供。 通过阻尼器的弹性，阻尼器的过盈配合和/或操作期间阻尼器和接触区域的离心负载来提供接触区域上的接触负载。