地面振动试验以及重量和平衡测量的系统和方法

种用于提升飞行器(10)的设备可包含被安装在支撑表面(64)上的多个起重机构(74)。每个起重机构(74)可被配置为在飞行器(10)的组件(38)上给予个向上的力(90)其用于提升飞行器(10)脱离支撑表面(64)。该设备(70)包含被配置为安装到起重机构(74)的梁结构(100)。该设备(70)可还包含从梁结构(100)悬吊的起重横梁(140)。测量装置(178)可被安装到起重横梁(140)并且可被配置为啮合与组件(38)相关联的起重支点(54)以确定当飞行器被提升脱离支撑表面(64)时飞行器(10)的重量。 An apparatus for lifting an aircraft (10)...

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Format Patent
LanguageChinese
Published 15.08.2017
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Summary:种用于提升飞行器(10)的设备可包含被安装在支撑表面(64)上的多个起重机构(74)。每个起重机构(74)可被配置为在飞行器(10)的组件(38)上给予个向上的力(90)其用于提升飞行器(10)脱离支撑表面(64)。该设备(70)包含被配置为安装到起重机构(74)的梁结构(100)。该设备(70)可还包含从梁结构(100)悬吊的起重横梁(140)。测量装置(178)可被安装到起重横梁(140)并且可被配置为啮合与组件(38)相关联的起重支点(54)以确定当飞行器被提升脱离支撑表面(64)时飞行器(10)的重量。 An apparatus for lifting an aircraft (10) may include a plurality of lifting mechanisms (74) mounted on a supporting surface (64). Each lifting mechanism (74) may be configured to impart an upward force (90) on a component (38) of the aircraft (10) for lifting the aircraft (10) off the supporting surface (64). The apparatus (10) may include a beam structure (100) configured to be mounted to the lifting mechanisms (74). The apparatus (10) may also include a lifting beam (140) suspended from the beam structure (100). A measurement device (178) may be mounted to the lifting beam (140) and may be configured to engage a jack point (54) associated with the component (38) to determine a weight of the aircraft (10) when the aircraft is lifted off the supporting s
Bibliography:Application Number: CN201310131556