Combustion chamber for turbo engines

Power plants – Combustion products used as motive fluid – External-combustion engine type

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

431352, 431353, F02C 722

Patent

active

041626117

ABSTRACT:
A fuel injection nozzle for a turbo engine is mounted at the base of a costion chamber, either tubular or annular, by means of an intermediate inwardly flared member having openings through its sides for admitting cooling air. An annular flange structure around the intermediate member supports the same and defines an annular space with the base of the chamber for a layer of cooling air admitted to that space through holes in the base. Several forms are disclosed in each of which the various holes and air inlets are dimensioned and positioned to provide a stoichiometric mixture of air and fuel under substantially all conditions of operation.

REFERENCES:
patent: 3820324 (1974-06-01), Grindley et al.
patent: 3906718 (1975-09-01), Wood
patent: 3916619 (1975-11-01), Masai et al.
patent: 3934409 (1976-01-01), Quillevere 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

Combustion chamber for turbo engines does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Combustion chamber for turbo engines, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Combustion chamber for turbo engines will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-19463

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