Vortex transition duct

Rotary kinetic fluid motors or pumps – Working fluid passage or distributing means associated with... – Casing having tangential inlet or outlet

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

415219B, F01D 108, F01D 2524

Patent

active

045127166

ABSTRACT:
A turbine housing construction particularly adapted for use with turbochargers for internal combustion engines. A vortex transition duct is inserted between the source of exhaust gas for driving the turbine and the exhaust gas inlet of the turbine volute. In prior turbocharger constructions, the distribution of the velocity of the exhaust gas fed to and as seen by the turbine volute inlet is uniform. Yet, it is desirable that the radial velocity distribution of exhaust gases entering the turbine volute be of a free vortex distribution. The vortex transition duct of this invention transforms the uniform radial velocity distribution of the exhaust gases, prior to their entry into the turbine volute inlet, into a free vortex distribution.

REFERENCES:
patent: 4177005 (1979-12-01), Bozung et al.
patent: 4381171 (1983-04-01), Chapple

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

Vortex transition duct does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

     

Profile ID: LFUS-PAI-O-35052

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