ROTOR OF AIRCRAFT GAS-TURBINE ENGINE COMPRESSOR WITH TWIN OF BLISKS AND TWIN OF BLISK WITH CLASSIC IMPELLER AND WITH TWIN OF CLASSIC IMPELLER WITH IMPELLER WITH FOURTH-TO-SIXTH STAGE WITH DEVICES FOR DAMPING VIBRATIONS OF WORKERS OF THESE CLIPS AND IMPELLERS, FAN ROTOR AND BOOSTER ROTOR WITH DEVICE FOR DAMPING OF VIBRATIONS OF WORKING WIDE CHORD BLADES OF FAN, TWIN ASSEMBLY METHOD WITH DAMPER DEVICE

FIELD: motors and pumps.SUBSTANCE: group of inventions refers to the rotors of compressors and fans of fifth-generation aviation gas turbines with compressor impellers manufactured using the "blisk" technology, and fan impellers with wide-chord or wide-chord hollow blades with dampers for damping the vibrations of the blades of these wheels. Term "twin" here is applied to the connection of two impellers of a rotor of a turbomachine, in the structural element of one of which the proposed damping device is located, which suppresses oscillations of the working blades of the other wheel. Twin can consist of two blisks, glare and a single impeller with several steps, blisk and a "classic" impeller with locking fasteners of blades to the disk and two "classic" wheels. Note that each rotor impeller with damping vibrations of working blades with the proposed damper, except for the wheels of the first and last stage, can be part of two sparks. Rotor of the HPC is proposed, consisting of a twin of two blisks - first and second stage impellers, twin from the blisk of the second stage and the "classic" third-stage wheel and the blisk from the "classic" third-stage wheel and the single wheel from the fourth to the sixth step and from the disc with the teeth of the labyrinth seal. And the blisk of the first stage is made in one piece with the ring with the teeth of the labyrinth seal. Blisk of the second stage - with a ring with the teeth of a labyrinth seal and a flange for fixing to the blisk of the first stage and with the rotor shaft of the HPC, and the "classic" wheel and single wheel - with rings with teeth of the labyrinth seal and a flange for fastening to the blisk of the second stage or the wheel of the third stage. Blades are mounted on the "classic" third-stage wheel with the help of the groove "swallowtail" and fixed from the axial displacement by a thrust ring attached to the front end of the rim of the third stage disc and the flange of the second twin wheel. Blades with the fourth to the sixth stage of the HPC rotor are installed on a single impeller HPC rotor in three profiled ring grooves. Platforms of these blades fit tightly to each other, ensuring reliable fixation of the blades in a tangential direction. At the blades of the first wheel of each twin of the rotor of the HPC, those at the blades of both blisks and the "classic" impeller of the third stage, the feather is made without a quadrangular fragment in the form of a trapezoid or a rectangle w