Gas turbine outlet arrangement

Power plants – Reaction motor – Interrelated reaction motors

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

60262, F02K 302

Patent

active

046961593

ABSTRACT:
An outlet section for a turbofan gas turbine engine (10) includes an internal flow separator (24), and a small convoluted mixer (28) for initiating mixing between the coaxial fan air stream (22) and hot core engine exhaust gas (26). Mixing is enhanced by an increasing-decreasing diameter nozzle plug (38), having a maximum diameter (40) proximate the annular outlet opening (16). The downstream edge (42) of the outer engine fairing (14) is turned radially inward for enhancing forward thrust in cooperation with the decreasing diameter surface (18) of the plug (38).

REFERENCES:
patent: 3377804 (1968-04-01), Wright et al.
patent: 3514955 (1970-06-01), Paulson et al.
patent: 3696617 (1972-10-01), Ellis
patent: 3750402 (1973-08-01), Vdoviak et al.
patent: 4117671 (1979-01-01), Neal et al.
patent: 4135363 (1979-01-01), Packman
patent: 4222235 (1980-09-01), Adamson et al.
patent: 4226297 (1980-10-01), Cicon
patent: 4298089 (1981-11-01), Birch et al.
patent: 4543784 (1985-10-01), Kirker
patent: 4592201 (1986-06-01), Dusa 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

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

Rate now

     

Profile ID: LFUS-PAI-O-1583609

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