JET AIRCRAFT ENGINE SHIPPING STAND
    1.
    发明公开
    JET AIRCRAFT ENGINE SHIPPING STAND 失效
    转运用于飞机喷气发动机

    公开(公告)号:EP0863838A1

    公开(公告)日:1998-09-16

    申请号:EP96942086.0

    申请日:1996-11-27

    IPC分类号: B64F5

    CPC分类号: B64F5/50

    摘要: The shipping stand includes a cradle assembly (224) mounted upon a frame assembly (211) to which a jet aircraft is securable. The frame assembly includes a plurality of wheels (218) for locomotive capability. A plurality of shock absorbers are operatively engaged between the cradle assembly and frame assembly to provide adequate shock protection to a loaded jet aircraft engine when the shipping stand is configured in a truck transport mode. A plurality of lifting mechanisms selectively raise the cradle assembly to a predetermined height creating gaps between upper transport flanges (254) and lower transport flanges. The gaps correspond to the height of spacers (261) positionable between the flanges in the truck transport mode. To place the shipping stand in an air transport mode, the lifting mechanisms are activated, the spacers are removed from between the flanges and the cradle assembly is lowered to eliminate the gaps between the flanges. Each spacer includes indicia which indicate in which mode the shipping stand is configured and further includes an air mode slot and a truck mode slot which cooperates with corresponding mode pins ensuring that the appropriate indicia are viewable when the shipping stand is configured in either the truck transport mode or the air transport mode.

    JET AIRCRAFT ENGINE TRANSPORT APPARATUS
    2.
    发明公开
    JET AIRCRAFT ENGINE TRANSPORT APPARATUS 失效
    JETTRIEBWERKSTRANSPORTVORRICHTUNG

    公开(公告)号:EP0868372A1

    公开(公告)日:1998-10-07

    申请号:EP96943528.0

    申请日:1996-11-27

    IPC分类号: B64F5 F01D25 F02C7

    摘要: A jet aircraft engine transport apparatus is disclosed which utilizes three major subcomponents. The first subcomponent is a shipping stand (210) which enables a jet aircraft engine to be configured for transport in either a truck transport mode or air transport mode. The second subcomponent is a fan dolly (10) which releasably secures the fan section (F) of the jet aircraft engine for transport. The fan dolly serves the dual purpose of enabling removal of the fan section from the jet aircraft engine and providing a means of transport so that the fan section may be transported on the fan dolly or loaded onto a fan shipping frame (310), the third major subcomponent of the transport apparatus of this invention. The fan shipping frame enables transport of the fan section in either an upright or horizontal position, and further provides for a fan storage container (370) for securing the fan blades of the fan section.

    摘要翻译: 公开了一种使用三个主要子部件的喷气飞机发动机输送装置。 第一个副部件是一个运输支架,使喷气式飞机发动机可以配置成以卡车运输方式或空运方式运输。 第二副部件是风扇台车,其可释放地固定喷气飞机发动机的风扇部分用于运输。 风扇小车用于从喷气飞机发动机移除风扇部分并提供运输工具的双重目的,使得风扇部分可以在风扇上运输或装载到风扇运输框架上,第三主要子部件 本发明的输送装置。 风扇运输框架能够使风扇部分在直立或水平位置传送,并进一步提供用于固定风扇部分的风扇叶片的风扇存储容器。

    SHIPPING FRAME FOR FAN SECTION OF AIRCRAFT ENGINE
    3.
    发明公开
    SHIPPING FRAME FOR FAN SECTION OF AIRCRAFT ENGINE 失效
    运输车辆FÜREIN MANTELGEBLASE EINES FLUGZEUGOTORS

    公开(公告)号:EP0863839A1

    公开(公告)日:1998-09-16

    申请号:EP96942820.0

    申请日:1996-11-27

    IPC分类号: B64F5 B65D85

    摘要: A fan shipping frame (310) includes a frame assembly for supporting a loaded fan section of a jet aircraft engine. A plurality of caster (360) assemblies attached to the shipping frame provide locomotive capability and adjustable height positioning so that a loaded fan section may be transferred onto the appropriate transport aircraft or vehicle. Rail members (322) mounted on the frame assembly are alignable with rail members of a fan dolly so that the fan section may be directly transferred from the fan dolly onto the shipping frame. A template bracket (332) integral with the shipping frame enables the fan section to be mounted thereon. A platform assembly rotatably mounted to the shipping frame may be deployed to enable the fan section to be tilted from a vertical transport position to a horizontal transport position wherein, the shipping frame may be transported in either position. A storage container mounted on the shipping frame stores the removed fan blades of the fan section in either position.

    摘要翻译: 风扇运输框架包括用于支撑喷气飞机发动机的加载的风扇部分的框架组件。 连接到运输框架的多个脚轮组件提供机车能力和可调节的高度定位,使得负载的风扇部分可以被转移到适当的运输飞机或车辆上。 安装在框架组件上的轨道构件可与风扇台架的轨道构件对准,使得风扇部分可以从风扇台车直接传送到运输框架上。 与运输框架一体的模板支架可使风扇部分安装在其上。 可旋转地安装到运输框架上的平台组件可以被布置成使得风扇部分能够从垂直运输位置倾斜到水平运输位置,其中运输框架可以在任一位置运输。 安装在运送框架上的存储容器将风扇部分的已移除的风扇叶片存储在任一位置。

    JET AIRCRAFT ENGINE SHIPPING STAND
    4.
    发明授权
    JET AIRCRAFT ENGINE SHIPPING STAND 失效
    TRANSPORTVORRICHTUNGFÜREIN FLUGZEUG-STRAHLTRIEBWERK

    公开(公告)号:EP0863838B1

    公开(公告)日:2001-10-24

    申请号:EP96942086.8

    申请日:1996-11-27

    IPC分类号: B64F5/00 B65D85/68

    CPC分类号: B64F5/50

    摘要: The shipping stand includes a cradle assembly (224) mounted upon a frame assembly (211) to which a jet aircraft is securable. The frame assembly includes a plurality of wheels (218) for locomotive capability. A plurality of shock absorbers are operatively engaged between the cradle assembly and frame assembly to provide adequate shock protection to a loaded jet aircraft engine when the shipping stand is configured in a truck transport mode. A plurality of lifting mechanisms selectively raise the cradle assembly to a predetermined height creating gaps between upper transport flanges (254) and lower transport flanges. The gaps correspond to the height of spacers (261) positionable between the flanges in the truck transport mode. To place the shipping stand in an air transport mode, the lifting mechanisms are activated, the spacers are removed from between the flanges and the cradle assembly is lowered to eliminate the gaps between the flanges. Each spacer includes indicia which indicate in which mode the shipping stand is configured and further includes an air mode slot and a truck mode slot which cooperates with corresponding mode pins ensuring that the appropriate indicia are viewable when the shipping stand is configured in either the truck transport mode or the air transport mode.

    摘要翻译: 运输支架包括安装在框架组件上的支架组件,喷气式飞机可安装在该组件上。 框架组件包括用于机车能力的多个轮子。 多个减震器可操作地接合在支架组件和框架组件之间,以便当货运架构成卡车运输模式时,为负载的喷气式飞机发动机提供适当的冲击保护。 多个提升机构选择性地将托架组件升高到预定高度,从而在上传送凸缘和下传送凸缘之间形成间隙。 间隙对应于在卡车运输模式中可在凸缘之间定位的间隔件的高度。 为了将运输支架放置在空运模式中,升降机构被启动,间隔件从凸缘之间移除,托架组件下降以消除凸缘之间的间隙。 每个间隔件包括指示运输台被配置的哪个模式的标记,并且进一步包括空气模式槽和卡车模式槽,其与相应的模式销相配合,确保当运输架配置在卡车运输模式中时可以看到适当的标记 或空运方式。

    JET AIRCRAFT ENGINE TRANSPORT APPARATUS
    5.
    发明授权
    JET AIRCRAFT ENGINE TRANSPORT APPARATUS 失效
    喷气式飞机发动机运输设备

    公开(公告)号:EP0868372B1

    公开(公告)日:2002-03-06

    申请号:EP96943528.8

    申请日:1996-11-27

    IPC分类号: B65D85/68 B64F5/00

    摘要: A jet aircraft engine transport apparatus is disclosed which utilizes three major subcomponents. The first subcomponent is a shipping stand (210) which enables a jet aircraft engine to be configured for transport in either a truck transport mode or air transport mode. The second subcomponent is a fan dolly (10) which releasably secures the fan section (F) of the jet aircraft engine for transport. The fan dolly serves the dual purpose of enabling removal of the fan section from the jet aircraft engine and providing a means of transport so that the fan section may be transported on the fan dolly or loaded onto a fan shipping frame (310), the third major subcomponent of the transport apparatus of this invention. The fan shipping frame enables transport of the fan section in either an upright or horizontal position, and further provides for a fan storage container (370) for securing the fan blades of the fan section.

    摘要翻译: 公开了一种利用三个主要子部件的喷气飞机发动机运输装置。 第一子组件是运输支架(210),其使得喷气飞机发动机能够被配置用于以卡车运输模式或空中运输模式运输。 第二个子部件是一个扇形推车(10),它可拆卸地固定喷气飞机发动机的风扇部分(F)以便运输。 风扇小推车具有这样的双重目的,即能够将风扇部分从喷气飞机发动机上移除并且提供运输工具,使得风扇部分可以在风扇小车上运输或者装载到风扇运输框架(310)上,第三 本发明运输设备的主要子部件。 风扇运输框架能够以直立或水平位置运输风扇部分,并且还提供用于固定风扇部分的风扇叶片的风扇存储容器(370)。

    SHIPPING FRAME FOR FAN SECTION OF AIRCRAFT ENGINE
    6.
    发明授权
    SHIPPING FRAME FOR FAN SECTION OF AIRCRAFT ENGINE 失效
    球童一MANTELGEBLASE飞机发动机

    公开(公告)号:EP0863839B1

    公开(公告)日:2002-02-20

    申请号:EP96942820.0

    申请日:1996-11-27

    IPC分类号: B64F5/00 B65D85/68

    摘要: A fan shipping frame (310) includes a frame assembly for supporting a loaded fan section of a jet aircraft engine. A plurality of caster (360) assemblies attached to the shipping frame provide locomotive capability and adjustable height positioning so that a loaded fan section may be transferred onto the appropriate transport aircraft or vehicle. Rail members (322) mounted on the frame assembly are alignable with rail members of a fan dolly so that the fan section may be directly transferred from the fan dolly onto the shipping frame. A template bracket (332) integral with the shipping frame enables the fan section to be mounted thereon. A platform assembly rotatably mounted to the shipping frame may be deployed to enable the fan section to be tilted from a vertical transport position to a horizontal transport position wherein, the shipping frame may be transported in either position. A storage container mounted on the shipping frame stores the removed fan blades of the fan section in either position.