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1.发明授权公开(公告)号：US06474596B1
公开(公告)日：2002-11-05
申请号：US09678259
申请日：2000-10-03
IPC分类号： B64D2700
CPC分类号： B64D27/26 , B64D2027/266
摘要： A suspension system for an aircraft powerplant attached to an aircraft frame and having a housing. The suspension system includes a spindle mounted in a spindle support rigidly joined to the aircraft frame, a bearing cage affixed to the housing and having a bearing positioned therein, a pair of suspension arms connected to the spindle support, and a pair of lateral linkrods configured to link the housing and the suspension arms. The side surfaces of the bearing cage and the suspension arms define a clearance therebetween concentric to the Y-axis. The bearing cage is configurable along the spindle such that the bearing cage is limited to displacement relative to the longitude of the spindle while maintaining contact with the spindle.
摘要翻译： 一种用于飞机动力装置的悬挂系统，其连接到飞机框架并具有壳体。 悬挂系统包括安装在刚性地连接到飞行器机架的主轴支架中的主轴，固定到壳体并且具有定位在其中的轴承的轴承座，连接到主轴支撑件的一对悬架臂和配置成的一对横向连杆 以连接外壳和悬挂臂。 轴承保持架和悬挂臂的侧表面与Y轴同心地形成一个间隙。 轴承保持架可以沿主轴配置，使得轴承保持架被限制为相对于主轴经度的位移，同时保持与主轴的接触。
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公开(公告)号：US6129509A
公开(公告)日：2000-10-10
申请号：US342730
申请日：1999-06-29
CPC分类号： F02C7/052 , B64D33/02 , F02C7/20 , B64D2033/0246 , B64D2033/0293 , Y02T50/671
摘要： The particle trap (15) that extends behind an elbow in the air flow stream (6) in a turbo-prop engine is delimited at the back by an end plate (12) to which intake housing suspension rods (10) supporting the front of the rotating shaft (2), are fastened. It is divided by suspension arms (11) which may be drilled (21) to restore the continuity of the annular chamber forming the trap. Therefore the intake housing suspension device extends through the trap. This type of trap makes use of the inertia of solid bodies carried by the air drawn in, and which could damage the engine blades, and to collect them.
摘要翻译： 在涡轮驱动发动机中在空气流（6）中延伸到弯头后面的颗粒捕集器（15）在后面由端板（12）界定，入口壳体悬架杆（10）支撑在 旋转轴（2）被紧固。 它被悬挂臂（11）分开，可以钻（21）以恢复形成陷阱的环形室的连续性。 因此，进气室悬挂装置延伸穿过疏水阀。 这种陷阱利用被吸入的空气携带的固体的惯性，并且可能损坏发动机叶片并收集它们。
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