Turbo-compressor apparatus

Pumps – Motor driven – Fluid motor

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

384121, F04B 1700

Patent

active

044823037

ABSTRACT:
A turbo-compressor apparatus in which the turbine section and the compressor section are placed back-to-back. A non-rotating shaft axially supported in the apparatus supports an anti-friction bearing which, in turn, rotationally supports a rotor assembly. A separating member preferably comprised of a material of low thermal conductivity is provided between the turbine section and the compressor section. A fully floating, non-rotating sleeve bearing incorporating both thrust and radial surfaces is allowed to float freely on the shaft. Thus, thrust forces from the spinning rotor are initially absorbed at the large radial bearing surfaces located at approximately the center of the bearing and are thereby transferred to the small areas at either end of the sleeve bearing. The thrust forces are finally transferred from the sleeve bearing to the stationary shaft. The mechanically locked sleeve bearing also serves to retain the rotor on the stationary shaft. In the preferred embodiment, the stationary shaft is supported at only one of its ends, the unsupported end extending into a cylindrical opening in the rotor assembly which opening may be a blind hole.

REFERENCES:
patent: 1130616 (1915-03-01), Lorenz
patent: 2319913 (1943-05-01), Bentley
patent: 3059415 (1962-10-01), Birmann
patent: 3071691 (1963-01-01), Haddad et al.
patent: 4260339 (1981-04-01), Lofts
patent: 4339922 (1982-07-01), Navarro

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Turbo-compressor apparatus does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Turbo-compressor apparatus, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Turbo-compressor apparatus will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-2358428

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.