Dilution air dispensing apparatus
AssigneeThe United States of America as represented by the Secretary of the Air Force
InventorRobert C. King
Life of this patent
Estimating the term…
Abstract
A dilution air dispensing apparatus for a double dome combustor with dilution air dispensing holes that are staggered on the opposite walls of the centerbody. The wakes on the downstream side of the jets provide avenues of access for the deflected combustion gases to continue their travel across the combustor and into the regions downstream of the opposite domes. The gases then mix with the remaining undeflected gases from the domes and with the spent dilution air before reaching a combustor exit plane.
Claims3
A dilution air dispensing apparatus for a double dome combustor comprising in combination:
- a first dome combustor having an inlet opening and an exhaust opening, a first fuel nozzle operatively arranged in said inlet opening to dispense fuel to said first dome combustor,
- a second dome combustor having an inlet opening and an exhaust opening, a second fuel nozzle operatively arranged in said inlet opening to dispense fuel to said second dome combustor, said first and second dome combustor being joined towards their inlet ends to form a dilution air dispensing cavity therebetween, said dilution air dispensing cavity being formed by the inner adjacent walls of said first and second dome combustors, said dilution air dispensing cavity having a rearward portion which is located approximately one-third of the dome length from the inlets to said first and second dome combustors, first and second rows of dilution holes are formed in the adjacent inner walls of said dilution air dispensing cavity, said first and second rows of dilution holes being located in said rearward portion of said dilution air dispensing cavity and being staggered with respect to each other, said dilution holes admitting dilution air respectively to said first and second dome combustors, said dilution air respectively altering the paths of combustion gas flow in said first and second dome combustors toward the opposite combustor dome exhaust opening.
Dependencies are inferred from the claim text.