BLADES SYSTEM AND APPROPRIATE GAS TURBINE Russian patent published in 2016 - IPC F01D5/26 

Abstract RU 2580447 C2

FIELD: machine building.

SUBSTANCE: invention relates to the blades system (11) comprising a rotor (12) and several blades (14) distributed along the perimeter (U) of the rotor (12) in form of rim (10), wherein two neighbouring blades (14) of the rim (10) create a pair (a, b, b', b'', d, e, h) of blades, between its blades (14) a dampening element (A, B, B', B'', D, E, H) is located, and wherein due to centrifugal force acting in radial direction (R) during the rotor (12) rotation around the rotor axis each dampening element (A, B, B', B'', D, E, H) contacts with two blades (14) of the appropriate pair (a, b, b', b'', d, e, h) of blades. To ensure frequency dissonance of the oscillating properties of the blades (14) resulting in absence of the necessity in machining of the blade body (22), it is suggested that the blade rim (10) has at least two pairs (a, b, b', b'', d, e, h) of blades having different dampening elements (A, B, B', B'', D, E, H).

EFFECT: improved design.

4 cl, 7 dwg

Similar patents RU2580447C2

Title Year Author Number
SYSTEM OF BLADES 2007
  • Kajzer Andreas
RU2417323C2
LOW-PRESSURE COMPRESSOR OF GAS TURBINE ENGINE OF AVIATION TYPE 2016
  • Marchukov Evgenij Yuvenalevich
  • Erichev Dmitrij Yurevich
  • Ilyasov Sergej Anatolevich
  • Kuprik Viktor Viktorovich
  • Savchenko Aleksandr Gavrilovich
  • Shishkova Olga Vladimirovna
  • Selivanov Nikolaj Pavlovich
RU2614709C1
GEAR MEASURING VIBRATION AMPLITUDES OF SHROUDED BLADES OF TURBINE BY DISCRETE-PHASE METHOD 1996
  • Borishanskij K.N.
  • Grigor'Ev B.E.
  • Grigor'Ev S.Ju.
  • Gudkov N.N.
  • Kondakov A.Ju.
  • Naumov A.V.
  • Gruzdev A.V.
RU2143103C1
DETERMINATION OF IMPELLER MACHINE VANED ROTOR DIAMETER 2011
  • Kljajn Karsten
RU2562928C2
LOW-PRESSURE COMPRESSOR OF GAS TURBINE ENGINE OF AVIATION TYPE 2016
  • Marchukov Evgenij Yuvenalevich
  • Ilyasov Sergej Anatolevich
  • Kuprik Viktor Viktorovich
  • Konovalova Tamara Petrovna
  • Polyakov Konstantin Sergeevich
  • Savchenko Aleksandr Gavrilovich
  • Skaryakina Regina Yurevna
  • Selivanov Nikolaj Pavlovich
RU2614708C1
METHOD OF MAKING ROTOR OF BLADE MACHINE 1991
  • Gololobov O.A.
  • Jakhanov E.A.
RU2047464C1
METHOD AND MONITORING SYSTEM FOR CONTROLLING CONDITION AND EMERGENCY PROTECTION OF BLADE DEVICES OF ROTOR ENGINES 2002
  • Deduchenko F.M.
  • Dyljuk A.G.
  • Konovalov I.L.
  • Lipko A.N.
RU2241216C2
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
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
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

RU 2 580 447 C2

Authors

Kajzer Andreas

Dates

2016-04-10Published

2011-09-20Filed