TURBINE COMPRESSOR Russian patent published in 2005 - IPC

FIELD: compressor arrangements.

SUBSTANCE: turbine compressor has pressure-tight tank provided with inner space and individual inlet ports from both sides. The fist socket of the bearing and the second socket of the bearing are mounted from the left and right sides of the inner space of the pressure-tight tank and are provided with through openings in their central parts. The driving motor is mounted between the first and second sockets of the bearing. The driving shaft whose both ends pass through the through openings in the first and second sockets of the bearing is mounted in block with the driving motor. The sealing member which is inserted with the use of the driving shaft is secured to the first socket of the bearing. The radial bearing means is interposed between the driving shaft and first socket of the bearing between the driving shaft and the second socket of the bearing. The first working wheel is secured to one end of the driving shaft. The second working wheel is secured to the other end of the driving shaft. The first diffuser is secured to the sealing member. The second diffuser is secured to the second socket of the bushing. The connecting pipe is used for connection of the inlet ports. The axial bearing means is interposed between the driving shaft and sealing member.

EFFECT: simplified assembling.

14 cl, 5 dwg