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81. 发明申请

WO1997019851A1 JET AIRCRAFT ENGINE SHIPPING STAND 审中-公开
标题翻译：喷气机飞机发动机
公开(公告)号：WO1997019851A1
公开(公告)日：1997-06-05
申请号：PCT/US1996019006
申请日：1996-11-27
申请人： STANLEY AVIATION CORPORATION , LILJA, Gerald, D. , FOWLER, Frank , HATCH, Robert, F.
发明人： STANLEY AVIATION CORPORATION
IPC分类号： B64F05/00
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（211）上的支架组件（224），喷气式飞机可保持在该框架组件上。框架组件包括用于机车能力的多个轮子（218）。多个减震器可操作地接合在支架组件和框架组件之间，以便在装载架被配置为卡车运输模式时，为加载的喷气式飞机发动机提供足够的冲击保护。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（254）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（261）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，并且托架组件被降低以消除凸缘之间的间隙。每个间隔件包括标记，其指示在哪种模式下运输支架被配置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中时可以看到适当的标记模式或航空运输模式。

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