Improved fuel injector for a gas turbine engine

Power plants – Combustion products used as motive fluid – Combustion products generator

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

60743, F23R 320

Patent

active

052207943

ABSTRACT:
The high cost of fuel injection nozzles for a gas turbine engine may be reduced by utilizing nozzles (60) formed of simple tubes (63) of capillary cross section having an integral flange (62) formed on one end (86) thereof.

REFERENCES:
patent: 2706520 (1955-04-01), Chandler
patent: 3099134 (1963-07-01), Calder et al.
patent: 3142961 (1964-08-01), Carlisle
patent: 3283502 (1965-02-01), Lefebvre
patent: 3353351 (1967-11-01), Bill et al.
patent: 4798190 (1989-01-01), Vaznaian
patent: 4815665 (1989-03-01), Haruch
patent: 4967563 (1990-11-01), Shekleton
patent: 4989404 (1991-02-01), Shekleton
patent: 5027603 (1991-07-01), Shekleton 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

Improved fuel injector for a gas turbine engine does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Improved fuel injector for a gas turbine engine, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Improved fuel injector for a gas turbine engine will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-1435236

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