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    • 2. 发明公开
    • SYSTEM AND METHOD FOR GROUND VIBRATION TESTING AND WEIGHT AND BALANCE MEASUREMENT
    • 用于地面振动测试以及重量和平衡测量的系统和方法
    • EP3255404A1
    • 2017-12-13
    • EP17183624.0
    • 2013-04-11
    • The Boeing Company
    • MILLER, Mark E.Davis, George V.
    • G01M7/02G01G19/07G01M1/12B64F5/00
    • B64F5/0045B64F5/60G01G19/07G01M1/125G01M7/02G01M7/027
    • 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).
    • 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)。
    • 3. 发明公开
    • System and method for ground vibration testing and weight and balance measurement
    • 系统与Verfahren zurBodenschwingungsprüfungund Gewichts- und Gleichgewichtsmessung
    • EP2653847A2
    • 2013-10-23
    • EP13163431.3
    • 2013-04-11
    • The Boeing Company
    • Miller, Mark E.Davis, George V.
    • G01M7/02G01G19/07
    • B64F5/0045B64F5/60G01G19/07G01M1/125G01M7/02G01M7/027
    • 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).
    • 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)。