公开(公告)号：US09016665B2

公开(公告)日：2015-04-28

申请号：US13611830

申请日：2012-09-12

Applicant: Chuang-Chia Lin ,  Alan Leingang ,  Dave Lopes ,  Dennis Robertson ,  Christopher M Sanden ,  Odd Harald Steep Eriksen ,  Brian Snyder

Inventor： Chuang-Chia Lin ,  Alan Leingang ,  Dave Lopes ,  Dennis Robertson ,  Christopher M Sanden ,  Odd Harald Steep Eriksen ,  Brian Snyder

IPC: B64D9/00 ,  B66D1/54 ,  G06F11/30 ,  H05K13/00 ,  B66C1/40 ,  G01L1/14 ,  G01L5/10 ,  B66D1/58

CPC classification number: B64D9/00 ,  B66C1/40 ,  B66D1/54 ,  B66D1/58 ,  G01L1/142 ,  G01L5/103 ,  G06F11/30 ,  H05K13/00 ,  Y10T29/49117

Abstract: Health and usage monitoring systems for aircraft hoist systems are described herein. In some embodiments, a health and usage monitoring system comprises a capacitive load cell and a processing unit for communication with the capacitive load cell, the capacitive load cell comprising a load receiving surface and a capacitive assembly coupled to the load receiving surface, the capacitive assembly comprising parallel electrically conductive plates separated by a reversibly deformable spacer construction wherein the parallel plates comprise aligned apertures providing a passageway through the capacitive assembly for the hoist system cable.

Abstract translation: 本文描述了用于飞机起重机系统的健康和使用监测系统。 在一些实施例中，健康和使用监测系统包括电容式测力传感器和用于与电容式测力传感器通信的处理单元，电容性测力传感器包括负载接收表面和耦合到负载接收表面的电容性组件，电容组件 包括由可逆变形的间隔件结构分开的平行导电板，其中平行板包括对准的孔，提供通过用于提升系统电缆的电容组件的通道。

公开(公告)号：US20140070153A1

公开(公告)日：2014-03-13

申请号：US13611830

申请日：2012-09-12

Applicant: Chuang-Chia Lin ,  Alan Leingang ,  Dave Lopes ,  Dennis Robertson ,  Christopher M. Sanden ,  Odd Harald Steep Eriksen ,  Brian Snyder

Inventor： Chuang-Chia Lin ,  Alan Leingang ,  Dave Lopes ,  Dennis Robertson ,  Christopher M. Sanden ,  Odd Harald Steep Eriksen ,  Brian Snyder

IPC: B64D9/00 ,  G06F11/30 ,  H05K13/00 ,  B66D1/54

CPC classification number: B64D9/00 ,  B66C1/40 ,  B66D1/54 ,  B66D1/58 ,  G01L1/142 ,  G01L5/103 ,  G06F11/30 ,  H05K13/00 ,  Y10T29/49117

Abstract: Health and usage monitoring systems for aircraft hoist systems are described herein. In some embodiments, a health and usage monitoring system comprises a capacitive load cell and a processing unit for communication with the capacitive load cell, the capacitive load cell comprising a load receiving surface and a capacitive assembly coupled to the load receiving surface, the capacitive assembly comprising parallel electrically conductive plates separated by a reversibly deformable spacer construction wherein the parallel plates comprise aligned apertures providing a passageway through the capacitive assembly for the hoist system cable.

Abstract translation: 本文描述了用于飞机起重机系统的健康和使用监测系统。 在一些实施例中，健康和使用监测系统包括电容式测力传感器和用于与电容式测力传感器通信的处理单元，电容性测力传感器包括负载接收表面和耦合到负载接收表面的电容性组件，电容组件 包括由可逆变形的间隔件结构分开的平行导电板，其中平行板包括对准的孔，提供通过用于提升系统电缆的电容组件的通道。