Centrifugal compressor

Rotary kinetic fluid motors or pumps – With diversely oriented inlet or additional inlet for...

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

415144, 415165, 415186, 4152083, F04D 2944

Patent

active

052363015

ABSTRACT:
An improved centrifugal compressor for use in gas turbine engines includes a secondary air flow inlet in the compressor shroud at a location downstream of the inducer, with passive elements in the secondary air inlet for effectively preventing flow out of the secondary air inlet from the compressor impeller at part speed design operation, while augmenting and enhancing flow of secondary air flow into the compressor impeller at maximum design speed operation of the compressor impeller.

REFERENCES:
patent: 2405282 (1938-02-01), Birmann
patent: 3217655 (1965-11-01), Sercy et al.
patent: 3462071 (1969-08-01), Garve
patent: 3887295 (1975-06-01), Yu
patent: 4248566 (1981-02-01), Chapman et al.
patent: 4479755 (1984-10-01), Skoe
patent: 4743161 (1988-05-01), Fisher et al.
patent: 4781530 (1988-11-01), Lauterbach et al.

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

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

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

Rate now

     

Profile ID: LFUS-PAI-O-2239730

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