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Joint assembly of the elements of the turntable of the test facility of the accident-resistant fuel system of the helicopter

机译:联合组装直升机的耐用燃料系统的测试设施的转盘元件

摘要

The utility model relates to the field of helicopter engineering, namely to test facilities for testing the fuel system of a helicopter. To increase the reliability of the junction of the inner and outer frames of the turntable while creating conditions for a more even distribution of the load on the parts of the outer frame 12 and the inner frame 13 and to increase the accuracy during assembly, the junction of the elements of the turntable for testing the fuel system of the helicopter contains a bearing unit 7 with a spherical bearing 31 located in the housing of the bearing unit and mounted on the axis of the pin 16 connecting the elements of the turntable - the outer frame 12 and the inner frame 13 installed in it. On the outer frame 12, the housing 28 of the bearing unit is fixed, and it is equipped with a load distribution plate 8, connected to the housing of the bearing unit; pin 16 is made with an outer flange 19 and is provided with its own plate 14 formed by a flat part rigidly connected to the inner frame 13, and a cylindrical part 20 rigidly connected to the outer flange 19 of the pin 16. The inner frame 13 is also provided with a load distribution plate 15, through which the connection of the inner frame 13 with the plate 14 of the pin 1 is made. f-ly, 12 ill.
机译:本实用新型涉及直升机工程领域,即测试燃油系统的测试设施。为了提高转盘的内部和外框架的连接的可靠性,同时产生外框12和内框架13的部件上的负载的更均匀分布的条件,并在组装期间增加准确性,结合条件用于测试直升机的燃料系统的转盘的元件包含轴承单元7,轴承单元7具有位于轴承单元的壳体中的球形轴承31,并安装在销16的轴线上,连接转盘的元件 - 外部框架12和安装在其中的内框架13。在外框架12上,轴承单元的壳体28固定,并且配备有负载分配板8,连接到轴承单元的壳体;销16采用外凸缘19制成,并且设置有其自身的板14,其由刚性连接到内框架13的平坦部分形成,以及刚性地连接到销16的外凸缘19的圆柱形部分20。内框架图13还提供了负载分配板15,通过该负载分配板15通过该负载分配板15,内框架13与销1的板14的连接。 F-LY,12岁。

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