FIELD: mechanical engineering.
SUBSTANCE: invention relates to the field of turbo and aircraft engine technology, namely to devices for connecting the external and internal bodies of a turbomachine. The device for connecting the inner and outer bodies 1 and 2 of the turbomachine contains rods 3, the ends of which are pivotally connected to the corresponding brackets 5 of the body 2 and the brackets 4 of the body 1, as well as an intermediate ring element 9. The brackets 4 and 5 are fixed to the corresponding bodies 1 and 2 by means of a power attachment. On the inner surface of the body 2, made with the flanges of the horizontal connector 6, an annular groove is formed in which an element 9 is mounted, fixed with the possibility of a connector on the brackets 5. In this case, the means of power fastening from the side of the body 2 pass through the element 9 and form a gap with the latter.
EFFECT: invention is aimed at improving the convenience of assembly, speeding up and simplifying the assembly process while ensuring the required relationship between the inner and outer bodies in operation.
3 cl, 3 dwg
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Authors
Dates
2021-10-12—Published
2020-12-29—Filed