FIELD: aircraft engineering.
SUBSTANCE: attachment frame comprises joint between the first and second elements, that is, engine housing and attachment frame. Aforesaid joint comprises eccentric element (13, 43, 1013) fitted in the groove of first element revolving relative to fist axle (131A, 431A, 1131A). Note that aforesaid eccentric element incorporates journal (133, 433) attached to second element, and axle (133A, 433A, 1133A) arranged off center with respect to the first revolving axle. Eccentric element can revolve around aforesaid axle (133A, 433A, 1133A) arranged off center with respect to the first revolving axle.
EFFECT: compact assembly.
19 cl, 12 dwg
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