AXIAL THREE-STAGED COMPRESSOR Russian patent published in 1999 - IPC

Abstract RU 2136974 C1

FIELD: compressor construction, in particular, multiple-staged compressors. SUBSTANCE: compressor has blades composed of parts 4,5,6 directed at different angles to axis of rotation of rotor. Guiding part 4 of blade is directed at an angle of 0-10 deg, compression part 5 at an angle of 15-60 deg and releasing part 6 at an angle of 50-85 deg to rotor axis. Cylindrical surface of rotor is divided into equal sections. Length of guiding part 4 of blades 3 is gradually increasing within each section to define air intake cavity. Compression part 5 of each blade has thickness gradually increasing toward releasing part 6. Releasing part 6 of each blade has constant thickness and its side surfaces define in conjunction with surfaces of adjacent blades slit channels. EFFECT: increased efficiency by creating increased pressure. 3 dwg

Similar patents RU2136974C1

Title Year Author Number
ROTARY ENGINE 1995
  • Popkov Ivan Ivanovich
RU2094634C1
MULTICOMPRESSOR LIQUID-PROPELLANT ROCKET ENGINE 1995
  • Popkov Ivan Ivanovich
RU2120051C1
FUEL SYSTEM OF FOUR-STROKE INTERNAL COMBUSTION ENGINE 1995
  • Popkov Ivan Ivanovich
RU2105187C1
THREE-STAGE MULTIPLE-CIRCUIT COMPRESSOR 1995
  • Popkov Ivan Ivanovich
RU2097604C1
FLYING VEHICLE 1996
  • Popkov I.I.
RU2134215C1
AXIAL-FLOW BLOWER 1995
  • Popkov Ivan Ivanovich
RU2109173C1
ROTARY JET ENGINE 1994
  • Popkov Ivan Ivanovich
RU2118687C1
TURBOJET ENGINE 1994
  • Popkov Ivan Ivanovich
RU2122132C1
TWO-STROKE MULTICYLINDER ROTARY-PISTON ENGINE 1995
  • Popkov Ivan Ivanovich
RU2101526C1
SUBMERSIBLE VEHICLE HULL 1997
  • Popkov I.I.
RU2133208C1

RU 2 136 974 C1

Authors

Popkov I.I.

Dates

1999-09-10Published

1994-10-25Filed