METHOD OF PRODUCING AXIAL BLADE MACHINES (VERSIONS) Russian patent published in 2009 - IPC B23P15/02 

Abstract RU 2354524 C2

FIELD: machine building.

SUBSTANCE: invention relates to power engineering. In compliance with the first version the proposed method of producing axial blade machines, primarily, flue-gas pumps and industrial fans comprises forming the initial workpiece from T-rolling that features smooth radius of transition of the wall-to-shelf, which corresponds to the requirements of durability of stem-to-blade transition radius. Aforesaid T-section is cut into parts with their length corresponding to that of the blade airfoil portion which is cut from the wall of every rolling. The blade airfoil portion is mechanically produced from the shelf. At least one cut is made on the stem and at least one incision for blade air foil portion forming. The workpiece thus produced, is heated and formed. In compliance with the second version, the H-section formed rolling is used to be cut into parts with their length corresponding to that of the blade airfoil portion. Two blades airfoil portions are cut the wall of every part of rolling. The stems of two blades are mechanically produced from the shelves of every part of rolling. The workpiece is cut symmetrically in length. If required, additional parts are welded to the blade airfoil portion to ensure required length. At least one cut and one incision are made on the stem for forming the blade airfoil portion. The workpiece thus produced is heated and formed.

EFFECT: metal material ratio increased to 30 to 50%, reduced labor input and longer life.

10 cl, 5 ex, 12 dwg

Similar patents RU2354524C2

Title Year Author Number
METHOD OF MAKING ROTOR OF BLADE MACHINE 1991
  • Gololobov O.A.
  • Jakhanov E.A.
RU2047464C1
METHOD TO MANUFACTURE LIGHT ARCHED GIRDER 2011
  • Zhandarov Mikhail Aleksandrovich
RU2484214C1
METHOD OF TURBOMACHINE MANUFACTURE AND GRINDING MACHINE FOR ITS EMBODIMENT 1996
  • Gololobov O.A.
  • Mavljutov R.R.
  • Parashchenko V.M.
  • Giljazov M.F.
  • Kabanov V.M.
RU2162782C2
TURBOJET ENGINE LOW-PRESSURE COMPRESSOR SECOND STAGE ROTOR IMPELLER (VERSIONS) 2015
  • Artjukhov Aleksandr Viktorovich
  • Marchukov Evgenij Juvenalevich
  • Konovalova Tamara Petrovna
  • Uzbekov Andrej Valerevich
  • Shishkova Olga Vladimirovna
  • Selivanov Nikolaj Pavlovich
RU2603383C1
TURBOJET ENGINE LOW-PRESSURE COMPRESSOR FIRST STAGE ROTOR IMPELLER (VERSIONS) 2015
  • Artjukhov Aleksandr Viktorovich
  • Erichev Dmitrij Jurevich
  • Marchukov Evgenij Juvenalevich
  • Manapov Irik Usmanovich
  • Poljakov Konstantin Sergeevich
  • Uzbekov Andrej Valerevich
  • Kuznetsov Igor Sergeevich
RU2603382C1
TURBOJET ENGINE LOW-PRESSURE COMPRESSOR THIRD STAGE ROTOR IMPELLER (VERSIONS) 2015
  • Erichev Dmitrij Jurevich
  • Kondrashov Igor Aleksandrovich
  • Marchukov Evgenij Juvenalevich
  • Simonov Sergej Anatolevich
  • Poljakov Konstantin Sergeevich
  • Skarjakina Regina Jurevna
  • Selivanov Nikolaj Pavlovich
RU2603384C1
METHOD OF MANUFACTURE OF BLADES OF GAS-TURBINE ENGINES 1990
  • Antonov E.A.
  • Vjatkin A.S.
  • Matveev A.S.
  • Sukhopara E.E.
  • Mamaev V.B.
RU2013179C1
CURVED THIN-WALLED METAL PROFILE 2021
  • Bryl Feliks Vasilevich
  • Popravko Sergej Gavriilovich
  • Rudenko Rostislav Vladimirovich
  • Bryl Igor Vasilevich
RU2773742C1
TURBOJET LOW-PRESSURE COMPRESSOR ROTOR FOURTH-STAGE IMPELLER 2015
RU2612282C1
GAS TURBINE ENGINE LOW-PRESSURE COMPRESSOR ROTOR IMPELLER (VERSIONS) 2015
  • Marchukov Evgenij Yuvenalevich
  • Kuprik Viktor Viktorovich
  • Konovalova Tamara Petrovna
  • Polyakov Konstantin Sergeevich
  • Simonov Sergej Anatolevich
  • Skaryakina Regina Yurevna
  • Uzbekov Andrej Valerevich
  • Selivanov Nikolaj Pavlovich
RU2611497C1

RU 2 354 524 C2

Authors

Aksenov Anatolij Veniaminovich

Saleev Farid Ismailovich

Ryzhkova Natal'Ja Aleksandrovna

Dates

2009-05-10Published

2007-03-19Filed