초록 ▼

A balance ring (18) which is shrunk fit within each disk (12) of a rotor is selectively ground for detail balance. A plurality of openings (20) through the outer edge of the balance ring receive weights during the assembly balance of the rotor. A snap ring (44) retains the weights within the opening

A balance ring (18) which is shrunk fit within each disk (12) of a rotor is selectively ground for detail balance. A plurality of openings (20) through the outer edge of the balance ring receive weights during the assembly balance of the rotor. A snap ring (44) retains the weights within the openings. An eccentric inwardly extending raised area 26 throughout a substantial minority of the circumference provides for initial gross unbalance correction upon installation.

대표청구항 ▼

A method of balancing an integrally bladed gas turbine engine rotor having a plurality of integrally bladed disks comprising: spinning each disk without a balance ring and determining the initial unbalance; shrink fitting within each disk an eccentrically weighted balance ring in a manner to compens

A method of balancing an integrally bladed gas turbine engine rotor having a plurality of integrally bladed disks comprising: spinning each disk without a balance ring and determining the initial unbalance; shrink fitting within each disk an eccentrically weighted balance ring in a manner to compensate for the initial unbalance; spinning each disk together with the balance ring individually to determine the residual unbalance; correcting the residual unbalance by removal of material only from the balance ring; assembling a plurality of bladed disks to form a rotor; spinning the assembled rotor to determine the unbalance and correcting the unbalance by adding weights at selected locations within the balance ring.