FIELD: engines and pumps.
SUBSTANCE: method of assembling integral bladed disks of, particularly, turbojet engine compressor disks comprises mounting vibration damper both on the blades and between them, and welding the disks together. Proposed vibration damping device is be mounted on disk blades to dampen blades vibration by welding the disks together. It comprises appliances to close the blades and gaps there between, and locking appliances to hold and clamp the former ones arranged on the blades. Blades closing appliances are made from elastically deformed material.
EFFECT: reduced vibrations, ruling out resonance vibrations in friction welding.
17 cl, 5 dwg
| Title |
Year |
Author |
Number |
| METHOD OF RESTORING ONE-PIECE BLADED DISK AND TEST PIECE (VERSIONS) |
2006 |
- Bueh Bernar
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|
RU2397329C2 |
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2010 |
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|
RU2537997C2 |
| METHOD OF OBTAINING BLANK OF GAS TURBINE ENGINE BLADE FOR LINEAR WELDING BY FRICTION |
2016 |
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- Salimgareeva Gulnaz Khalifovna
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|
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2004 |
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- Fert Zhan P'Er
- Son'Jak Fransis Zhill' Bazil'
- Mirokur Zherar
|
RU2364728C2 |
| CLUTCH DISK |
2000 |
- Rajk Vol'Fgang
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- Ehlizon Khans-Diter
- Kimmig Karl-Ljudvig
|
RU2232314C2 |
| 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 |
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|
RU2662755C2 |
| GAS TURBINE ROTOR DISC, GAS TURBINE ENGINE WITH SAID DISC, AND BLADE ROOT STRAP |
2008 |
|
RU2487249C2 |
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2016 |
- Eskin Izold Davidovich
- Ermakov Aleksandr Ivanovich
- Garshin Egor Alekseevich
|
RU2665789C2 |
| AXLE COMPRESSOR BLISK AND ROTOR OF LOW-PRESSURE COMPRESSOR OF AIRCRAFT GAS TURBINE ENGINE |
2019 |
- Eskin Izold Davidovich
- Ermakov Aleksandr Ivanovich
|
RU2740442C2 |
| 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 |
