Fuel nozzle for gas turbine engine with external and internal re

Power plants – Combustion products used as motive fluid – Combined with regulation of power output feature

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

60740, F02C 722

Patent

active

044662408

ABSTRACT:
This invention relates to the mounting and support of fuel nozzles for gas turbine engines with the capability of removal externally and internally so that external removal capability negates the necessity of turbine and combustor teardown and allows access without engine removal from the aircraft.

REFERENCES:
patent: 2548904 (1951-04-01), Neal et al.
patent: 2944388 (1960-07-01), Bayer
patent: 3159971 (1964-12-01), Moebius et al.
patent: 3879940 (1975-04-01), Stenger 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

Fuel nozzle for gas turbine engine with external and internal re does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Fuel nozzle for gas turbine engine with external and internal re, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Fuel nozzle for gas turbine engine with external and internal re will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-1936207

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