FIELD: machine building.
SUBSTANCE: system (1) of blades consists of rotor and of multitude of blades arranged along circumference of rotor by a rim. At least two damping elements (5, 7) are positioned one behind another between two directly adjacent blades in a circumferential direction of the rotor. Adjacent damping elements (5, 7) contact one another due to effect of radial centrifugal force at rotation of rotor around rotation axis. One of both damping elements (5, 7) contacts one of both blades, while another of both damping elements (7, 5) contacts another of both blades. Two of three contacts between damping elements and blades are made along surface, while one of three contacts is made along a line. Kinetic stable system is created due to combination of damping elements with surface contact of platform of a blade and linear contact (Hertz contact) on another platform of pair of blades.
EFFECT: preventing distortion and local breakaway of all surfaces of contact and effective damping various oscillating states.
10 cl, 2 dwg
| Title |
Year |
Author |
Number |
| TURBOMACHINE COMPRESSOR IMPELLER |
2013 |
- Erichev Dmitrij Jur'Evich
- Konovalova Tamara Petrovna
- Uzbekov Andrej Valer'Evich
|
RU2529279C1 |
| BLADES SYSTEM AND APPROPRIATE GAS TURBINE |
2011 |
|
RU2580447C2 |
| 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 |
2016 |
- Eskin Izold Davidovich
- Ermakov Aleksandr Ivanovich
- Garshin Egor Alekseevich
|
RU2665789C2 |
| METHOD OF DAMPING, RESPECTIVELY, SUPPRESSION OF MECHANICAL OSCILLATIONS, OCCURRING DURING OPERATION, IN VANE OF TURBINE MACHINE, AND ALSO VANE OF TURBINE MACHINE FOR IMPLEMENTATION OF METHOD |
2011 |
- Shvedovich Jaroslav Leshek
- Kappis Vol'Fgang
- Panning Lars
- Shvartsendal' Sebast'Jan Mark
- Nojbauehr Markus
- Khol' Andreas
- Vallashek Jorg
|
RU2531103C2 |
| PLACE OF MOUNTING OF WORKING BLADES OF BOOSTER ROTORS AND COMPRESSOR OF AVIATION ENGINES OF FIFTH GENERATION; BOOSTER ROTOR AND ROTOR OF HIGH PRESSURE COMPRESSOR OF FIRST GENERATION AVIATION ENGINE, WITH WORKING BLADES, FIXED WITH HELP OF SWALLOWTAIL TYPE LOCKS IN RING GROOVES OF THESE DEVICES; METHOD OF ASSEMBLING PLACE OF MOUNTING WORKING BLADES OF BOOSTER ROTORS AND COMPRESSOR |
2016 |
- Eskin Izold Davidovich
- Ermakov Aleksandr Ivanovich
- Garshin Egor Alekseevich
|
RU2662755C2 |
| ROTOR AND TURBOMACHINE COMPRISING SAID ROTOR |
2014 |
- Regis Viguie
- Damien Verhelst
- Andre Preumont
- Bilal Mokrani
- Renaud Bastaits
|
RU2602713C2 |
| PLACE OF MOUNTING OF WORKING BLADES AND LOW AND HIGH PRESSURE COMPRESSOR OF AVIATION ENGINES OF FIFTH GENERATION, ROTOR OF LOW PRESSURE COMPRESSOR AND ROTOR OF HIGH PRESSURE COMPRESSOR OF FIFTH GENERATION AVIATION ENGINE, WITH WORKING BLADES, FIXED WITH HELP OF DOVETAIL TYPE LOCKS IN RING GROOVES OF THESE DEVICES, METHOD OF ASSEMBLING PLACE OF MOUNTING WORKING BLADES OF ROTORS AND COMPRESSOR |
2017 |
- Eskin Izold Davidovich
- Garshin Egor Alekseevich
- Ermakov Aleksandr Ivanovich
|
RU2686353C2 |
| AIRCRAFT TURBOJET ENGINE FAN ROTOR WITH LONG WIDE-CHORD HOLLOW BLADES WITH DAMPERS |
2019 |
- Eskin Izold Davidovich
- Falaleev Sergej Viktorinovich
|
RU2727314C1 |
| AXLE COMPRESSOR BLISK AND ROTOR OF LOW-PRESSURE COMPRESSOR OF AIRCRAFT GAS TURBINE ENGINE |
2019 |
- Eskin Izold Davidovich
- Ermakov Aleksandr Ivanovich
|
RU2740442C2 |
| METHOD OF ASSEMBLING INTEGRAL BLADED DISKS AND DEVICE TO DAMPEN BLADES OF ABOVE DISKS |
2005 |
- Fert Zhan-P'Er
- Vasso Mark
- Bruar Did'E
|
RU2371587C2 |
