Gas turbine engine gaseous fuel injector

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

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

60748, F02C 100

Patent

active

047139382

ABSTRACT:
A gaseous fuel injector for an industrial gas turbine plant is arranged to operate on fuel produced from a coal gasifier for normal running or natural gas for starting purposes. The injector is self purging to prevent the ingestion of natural gas or combustion products into the passage of the fuel injector for the lower calorific value fuel. The fuel injector has fuel ducts and gas flow passages in a duct assembly attached to the head of each flame tube of a gas generator. For starting, natural gas flows through the duct and the central passage, while air flows through the outer passage preventing ingestion of natural gas and combustion products into the outer fuel duct. When running on fuel from a coal gasifier both ducts run full of fuel, as do the passages. The air for the coal gasifier may be provided by the gas generator.

REFERENCES:
patent: 3691765 (1972-09-01), Carlisle
patent: 3713588 (1973-01-01), Sharpe
patent: 4342198 (1982-08-01), Willis
patent: 4425755 (1984-01-01), Hughes

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

Rate now

     

Profile ID: LFUS-PAI-O-812507

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