Fuel nozzle guide for a gas turbine engine combustor

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

60 3932, F23R 360

Patent

active

054638640

ABSTRACT:
An improved fuel nozzle guide (100) for a gas turbine engine combustion chamber (65) includes an eccentric detent (150) which allows only a predetermined amount of limited pivotable movement of a retainer (125) and bushing (105) employed in the guide.

REFERENCES:
patent: 3273343 (1966-09-01), Cretella
patent: 3451215 (1969-06-01), Barr
patent: 3589127 (1971-06-01), Kenworthy et al.
patent: 4322945 (1982-04-01), Peterson et al.
patent: 4365470 (1982-12-01), Matthews et al.
patent: 4525996 (1985-07-01), Wright et al.
patent: 4686823 (1987-08-01), Coburn et al.
patent: 4870818 (1989-10-01), Suliga
patent: 4934145 (1990-06-01), Zeisser
patent: 4999996 (1991-03-01), Duchene et al.
patent: 5222358 (1993-06-01), Chaput 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 guide for a gas turbine engine combustor 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 guide for a gas turbine engine combustor, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Fuel nozzle guide for a gas turbine engine combustor will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-190952

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