Gas turbine engine diffuser

Power plants – Combustion products used as motive fluid – External-combustion engine type

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

415210, 415218, F02C 720

Patent

active

039786641

ABSTRACT:
Apparatus for diffusing the working medium gases which flow from the compression section of a gas turbine engine is disclosed. A controlled diffuser comprising an inner and an outer flow path shroud initially increases the static pressure and decreases the velocity of the medium gases flowing therebetween. The diffusion process is completed downstream of the flow path shrouds in a dump region of rapidly increasing flow area. The inner and outer shrouds of the controlled diffuser are concentrically supported at both the upstream and downstream ends. The inner and outer shrouds support the compressor exit vanes within the path of working medium gases flowing from the compressor and damp vane vibration during operation of the engine.

REFERENCES:
patent: 2577918 (1951-12-01), Rowe
patent: 2614385 (1952-10-01), Feilden
patent: 2699040 (1955-01-01), Gaubatz
patent: 2711072 (1955-06-01), Wetzler
patent: 2720080 (1955-10-01), Oulianoff
patent: 2852914 (1958-09-01), Robin et al.
patent: 3364678 (1968-01-01), Alford

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

Gas turbine engine diffuser does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

     

Profile ID: LFUS-PAI-O-2166160

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