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1. 发明公开

EP2653847A3 System and method for ground vibration testing and weight and balance measurement 有权
标题翻译：系统和方法，用于地面振动试验和重量和平衡测量
公开(公告)号：EP2653847A3
公开(公告)日：2016-03-09
申请号：EP13163431.3
申请日：2013-04-11
申请人： The Boeing Company
发明人： Miller, Mark E. , Davis, George V.
IPC分类号： G01M7/02 , G01G19/07 , G01M1/12 , B64F5/00
CPC分类号： B64F5/0045 , B64F5/60 , G01G19/07 , G01M1/125 , G01M7/02 , G01M7/027
摘要： 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 surface (64).

2. 发明授权

EP2653847B1 System and method for ground vibration testing and weight and balance measurement 有权
标题翻译：用于地面振动测试和重量和平衡测量的系统和方法
公开(公告)号：EP2653847B1
公开(公告)日：2017-09-13
申请号：EP13163431.3
申请日：2013-04-11
申请人： The Boeing Company
发明人： Miller, Mark E. , Davis, George V.
IPC分类号： G01M7/02 , G01G19/07 , G01M1/12 , B64F5/00
CPC分类号： B64F5/0045 , B64F5/60 , G01G19/07 , G01M1/125 , G01M7/02 , G01M7/027

3. 发明公开

EP3255404A1 SYSTEM AND METHOD FOR GROUND VIBRATION TESTING AND WEIGHT AND BALANCE MEASUREMENT 有权
标题翻译：用于地面振动测试以及重量和平衡测量的系统和方法
公开(公告)号：EP3255404A1
公开(公告)日：2017-12-13
申请号：EP17183624.0
申请日：2013-04-11
申请人： The Boeing Company
发明人： MILLER, Mark E. , Davis, George V.
IPC分类号： G01M7/02 , G01G19/07 , G01M1/12 , B64F5/00
CPC分类号： B64F5/0045 , B64F5/60 , G01G19/07 , G01M1/125 , G01M7/02 , G01M7/027
摘要： 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 surface (64).
摘要翻译：用于提升飞机（10）的设备可以包括安装在支撑表面（64）上的多个提升机构（74）。每个升降机构（74）可以被构造成在飞机（10）的部件（38）上施加向上的力（90）以将飞机（10）提升离开支撑表面（64）。装置（10）可以包括构造成安装到提升机构（74）的梁结构（100）。装置（10）还可以包括从梁结构（100）悬挂的提升梁（140）。测量装置（178）可以被安装到起重横梁（140）并且可以被配置为接合与部件（38）相关联的起重点（54）以确定当飞机被提升时飞机（10）的重量离开支撑表面（64）。

4. 发明公开

EP2653847A2 System and method for ground vibration testing and weight and balance measurement 有权
标题翻译：系统与Verfahren zurBodenschwingungsprüfungund Gewichts- und Gleichgewichtsmessung
公开(公告)号：EP2653847A2
公开(公告)日：2013-10-23
申请号：EP13163431.3
申请日：2013-04-11
申请人： The Boeing Company
发明人： Miller, Mark E. , Davis, George V.
IPC分类号： G01M7/02 , G01G19/07
CPC分类号： B64F5/0045 , B64F5/60 , G01G19/07 , G01M1/125 , G01M7/02 , G01M7/027
摘要： 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 surface (64).
摘要翻译：用于提升飞机（10）的装置可以包括安装在支撑表面（64）上的多个提升机构（74）。每个提升机构（74）可以构造成向飞机（10）的部件（38）施加向上的力（90），用于将飞行器（10）从支撑表面（64）提升。设备（10）可以包括被配置为安装到提升机构（74）的梁结构（100）。装置（10）还可以包括从梁结构（100）悬挂的提升梁（140）。测量装置（178）可以安装到提升梁（140），并且可以被构造成接合与部件（38）相关联的千斤顶点（54），以确定当飞机被提升时飞行器（10）的重量离开支撑表面（64）。

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