FIELD: engines and pumps.
SUBSTANCE: non-twistable annular stator assembly of aircraft engine includes rigid annular support element, and at least one device for attachment of engine to aircraft. Engine attachment device includes housing made from composite material and rigidly fixed on annular support element, and rigid element enveloping the composite housing with tight fit to it and containing the connecting element to be attached to the aircraft.
EFFECT: invention allows decreasing the weight of annular stator assembly, thus maintaining its rigidity.
18 cl, 13 dwg
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