FIELD: machine building.
SUBSTANCE: rotor of gas turbine consists of section on side of compressor and of section on side of turbine containing separate parts compressed one to another and united into one rotor unit by means of tie rod. Each part of the rotor has an orifice for the tie rod. The orifice passes in axial direction of the rotor and the tie rod passes through this orifice at a distance from parts of the rotor. An additional part of the rotor is positioned between the section of the rotor on the turbine side and the section of the rotor in the compressor side. This additional part corresponds to a support wheel connected to the tie rod ensuring power and/or geometric locking. The additional part of the rotor on the side of connection with the tie rod is of a barrel-type profile. Another invention of the group refers to the blade heat machine containing the above said rotor.
EFFECT: increased reliability of rotor of gas turbine due to reduced amplitude of oscillations of tie rod.
11 cl, 5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| TURBINE WITH AT LEAST ONE ROTOR CONSISTING OF ROTOR DISKS AND COUPLING BOLT | 2008 |
|
RU2429350C2 |
| ROTOR FOR BLADED MACHINE WITH AXIAL FLOW | 2008 |
|
RU2479725C2 |
| TURBOMACHINE ROTOR SECTION | 2010 |
|
RU2518749C2 |
| SECTION OF ROTOR FOR TURBOMACHINE; ROTATING BLADE FOR TURBOMACHINE | 2010 |
|
RU2486348C2 |
| MACHINE CONVERTING FLOW KINETIC POWER INTO MECHANICAL POWER AND ROTOR OF THIS MACHINE | 2005 |
|
RU2347912C2 |
| ROTOR EIGHTH STAGE IMPELLER OF HIGH-PRESSURE COMPRESSOR (HPC) OF TURBOJET ENGINE (VERSIONS), HPC ROTOR IMPELLER DISC, HPC ROTOR IMPELLER BLADE, HPC ROTOR IMPELLER BLADE RING | 2016 |
|
RU2630924C1 |
| IMPELLER WHEEL OF SEVENTH STAGE OF HIGH PRESSURE COMPRESSOR (HPC) ROTOR OF TURBOCHARGER ENGINE (VERSIONS), HPC ROTOR IMPELLER WHEEL DISC, HPC ROTOR IMPELLER WHEEL BLADE, HPC ROTOR IMPELLER WHEEL BLADE RING | 2016 |
|
RU2630923C1 |
| NINTH STAGE IMPELLER WHEEL OF HIGH PRESSURE COMPRESSOR (HPC) ROTOR OF TURBOCHARGER ENGINE, HPC ROTOR IMPELLER WHEEL DISC, HPC ROTOR IMPELLER WHEEL BLADE, HPC ROTOR IMPELLER WHEEL BLADE RING | 2016 |
|
RU2630925C1 |
| COOLING OF GAS TURBINE STRUCTURAL ELEMENT, SAY, ROTOR DISC OR TURBINE BLADE | 2010 |
|
RU2547354C2 |
| TURBO-ELECTRO-GENERATOR | 2009 |
|
RU2418957C2 |
