Method and apparatus for enhancing gas turbo machinery flow

Rotary kinetic fluid motors or pumps – With passage in blade – vane – shaft or rotary distributor...

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

415142, 415914, F01D 904, F01D 906

Patent

active

058138285

ABSTRACT:
In a conduit constituting the outlet from turbo machinery such as a turbine or compressor, stall gas having high static pressure and low velocity is collected. This stall gas is then routed through struts--preferably teardrop shaped--to more central low static pressure and high velocity gas flow areas. At these areas, the gas is discharged, preferably through multiple manifold openings. Mixing of the collected high static pressure, low velocity stall gas with the low static pressure, high velocity main stream gas occurs. Turbine noise, vibration, and back pressure are decreased with resulting improvements of efficiency. Variations are illustrated including adaptation of gas flow transfer utilizing turning vanes, fairings, rectangular duct turns, and struts for placement in turbine turbo machine outlets having high turbulence or variable swirl.

REFERENCES:
patent: 3405865 (1968-10-01), Lagelbauer
patent: 3572960 (1971-03-01), McBride
patent: 4712980 (1987-12-01), Gely et al.
patent: 5161947 (1992-11-01), Eckfeldt et al.
patent: 5340276 (1994-08-01), Norris 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

Method and apparatus for enhancing gas turbo machinery flow does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Method and apparatus for enhancing gas turbo machinery flow, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Method and apparatus for enhancing gas turbo machinery flow will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-680827

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