FIELD: engines and pumps.
SUBSTANCE: proposed attachment assembly is mounted in gas turbine engine between inner first and second bearings, wherein run first and second rotors, respectively, and engine outer frame. Proposed assembly comprises first annular plate part and first bearing attachment gadget nearby its one edge and second annular plate part nearby its one edge. First and second plate parts are jointed together to make single unit to be fitted into gas turbine engine.
EFFECT: simple mounting and sufficient rigidity.
3 dwg
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