BLADE REACTOR FOR PYROLYSIS OF HYDROCARBONS Russian patent published in 2010 - IPC B01J3/08 B01J19/18 F01D5/12 

Abstract RU 2405622 C2

FIELD: technological processes.

SUBSTANCE: invention relates to apparatus for thermal pyrolysis of hydrocarbons in order to obtain lower olefins. The reactor comprises a rotor with working blades which form an axial blade array, a fixed toroidal collar which adjoins the ends of said blades, and a housing which surrounds the collar and the periphery of the rotor in such a way that a passage with an annular meridional section is formed. One or more partitions are mounted in the passage, an inlet orifice being arranged after each partition and an outlet orifice being arranged in front of each partition. Nozzle blades forming a nozzle array are mounted on the inlet side of the rotor array, and diffuser blades forming a diffuser array are mounted on the outlet side of the rotor array. There is a space without blades between the outlet of the diffuser array and the inlet of the nozzle array. The group of nozzle blades arranged directly after each partition can be separated from the remaining nozzle blades by a diaphragm such that a channel is formed connecting the corresponding inlet orifice to said group of blades. The geometrical parametres of the nozzle and diffuser arrays can change in a circular direction in order to provide the same pressure at the inlet of the rotor array and at the outlet of the rotor array.

EFFECT: invention increases output of lower olefins, reduces consumption of raw material, simplifies design and starting up the reactor, prevents radial leakage through gas between the rotor and the housing.

3 cl, 7 dwg, 4 tbl

Similar patents RU2405622C2

Title Year Author Number
METHOD OF PREPARING LOWER OLEFINS, REACTOR FOR PYROLYSIS OF HYDROCARBONS, AND APPARATUS FOR HARDENING PYROLYSIS GASES 1998
  • Bushuev V.A.
RU2124039C1
METHOD OF COOLING THE ROTOR OF A HIGH PRESSURE TURBINE (HPT) OF GAS TURBINE ENGINE (GTE), HPT ROTOR AND HPT ROTOR BLADE COOLED BY THIS METHOD, KNOT OF THE DEVICE OF TWISTING OF AIR OF HPT ROTOR 2018
  • Marchukov Evgenij Yuvenalevich
  • Kuprik Viktor Viktorovich
  • Andreev Viktor Andreevich
  • Komarov Mikhail Yurevich
  • Kononov Nikolaj Aleksandrovich
  • Selivanov Nikolaj Pavlovich
RU2684298C1
HIGH-PRESSURE TURBINE ROTOR OF A GAS TURBINE ENGINE (VERSIONS) 2018
  • Marchukov Evgenij Yuvenalevich
  • Kuprik Viktor Viktorovich
  • Andreev Viktor Andreevich
  • Komarov Mikhail Yurevich
  • Kononov Nikolaj Aleksandrovich
  • Krylov Nikolaj Vladimirovich
  • Selivanov Nikolaj Pavlovich
RU2691868C1
METHOD FOR DECOKING OF TUBULAR FURNACES FOR HYDROCARBON STOCK PYROLYSIS 1999
  • Bushuev V.A.
RU2168533C2
GAS TURBINE ENGINE LOW-PRESSURE TURBINE (LPT) (VERSIONS), ROTOR SHAFT CONNECTION UNIT WITH LPT DISC, LPT ROTOR AIR COOLING PATH AND AIR FEEDING APPARATUS FOR COOLING LPT ROTOR BLADES 2018
  • Marchukov Evgenij Yuvenalevich
  • Kuprik Viktor Viktorovich
  • Andreev Viktor Andreevich
  • Zolotukhin Andrej Aleksandrovich
  • Komarov Mikhail Yurevich
  • Kononov Nikolaj Aleksandrovich
  • Krylov Nikolaj Vladimirovich
  • Selivanov Nikolaj Pavlovich
RU2684355C1
RADIAL DIFFUSER BLADE FOR CENTRIFUGAL COMPRESSORS 2010
  • Radhakrishnan Sen
  • Tapinassi Libero
  • Svensdotter Clary Susanne Ingeborg
RU2581686C2
METHOD AND DEVICE FOR INTRODUCING ALKALI METAL COMPOUNDS INTO HEATED MEDIUM FLOW IN PYROLYSIS PIPE FURNACES 1999
  • Bushuev V.A.
RU2154522C1
MARINE PROPELLER 1995
  • Shishkov Valerij Mikhajlovich
RU2106283C1
JET-REACTIVE TURBINE 2015
  • Korolev Sergej Konstantinovich
  • Ovcharenko Andrej Yurevich
  • Korol Aleksej Andreevich
RU2614946C2
METHOD OF SEALING AIR CHANNELS 2014
  • Pismennyj Vladimir Leonidovich
RU2582725C2

RU 2 405 622 C2

Authors

Bushuev Vladimir Andreevich

Dates

2010-12-10Published

2009-03-23Filed