초록 ▼

The airflow from the compressor of a gas turbine engine into the combustion chamber or chambers principally comprises combustion air which enters the upstream end of the combustion chamber and dilution air which enters the combustion chamber at some point downstream of the combustion chamber inlet,

The airflow from the compressor of a gas turbine engine into the combustion chamber or chambers principally comprises combustion air which enters the upstream end of the combustion chamber and dilution air which enters the combustion chamber at some point downstream of the combustion chamber inlet, the combustion air being made up of primary and secondary air entering the combustion chamber primary and secondary zones. In order to cope with the control of emissions from the combustion chambers, it is desirable to control the combustion air fuel ratio over the engine operating range by controlling air mass flow to the combustion and dilution zones of the combustion chamber. The invention proposes that this control can be achieved by providing a variable rate diffuser upstream of the primary, secondary and dilution air inlets, the variable rate diffuser comprising vortex generator having an associated variable air bleed. The air bleed functions to control the strength of the generated vortex which in turn controls the rate of diffusion of the air supply to the combustion chamber.

대표청구항 ▼

A gas turbine engine combustion apparatus having fluidic means for varying the air flow to the combustion apparatus to control the air:fuel ratio over an operating range of the gas turbine engine, said apparatus comprising; a variable rate vortex controlled diffuser including a primary duct for rece

A gas turbine engine combustion apparatus having fluidic means for varying the air flow to the combustion apparatus to control the air:fuel ratio over an operating range of the gas turbine engine, said apparatus comprising; a variable rate vortex controlled diffuser including a primary duct for receiving a supply of air and having an exit end for discharging the same, a secondary duct surrounding the exit end of said primary duct, a fence in said secondary duct positioned downstream of the exit end of said primary duct for generating a vortex to diffuse a portion of the air discharged from said primary duct, a bleed duct communicating with said secondary duct upstream of said fence and of said exit end of said primary duct for controlling the vortex, and a capture tube positioned within said secondary duct and spaced downstream of said fence for receiving a portion of the air directly from said primary duct; a combustion chamber defined by a casing and having an outlet at its downstream end, a first air inlet means at its upstream end for receiving as primary air a portion of the air from said capture tube, a second air inlet means positioned downstream from said first air inlet means for receiving secondary air, and a third air inlet means positioned downstream from said second air inlet means for receiving dilution air, said first air inlet means including an opening at the upstream end of said combustion chamber for receiving directly air discharged from said capture tube; a second casing attached to said capture tube and extending downstream therefrom around a part of said combustion chamber casing, said second casing defining with said combustion chamber casing a first annular housing for directly receiving a portion of the air discharged from said capture tube, and delivering it as secondary air unmixed with fuel to said combustion chamber through said second air inlet means which comprise downstream openings in said combustion chamber casing providing communication between said combustion chamber and said first annular housing to direct the secondary air transversely of and into said chamber to insure proper mixing and promote further uniform combustion; a third casing attached to said secondary duct of said variable rate vortex controlled diffuser, said third casing extending from said secondary duct downstream around said second casing and a portion of said combustion chamber casing and attached thereto, said third casing defining with said second casing and said combustion chamber casing a second annular housing for receiving diffused air and delivering it into said combustion chamber, said third air inlet means including openings in said combustion chamber casing providing communication between said combustion chamber and one of said first and second annular housings to direct the dilution air transversely of and into said combustion chamber for penetrating and cooling the hot combustion gases therein and for creating a substantially uniform temperature profile for such gases at said combustion chamber outlet; and a unified fuel injection apparatus having a circumferential array of fuel injectors in which at each circumferential position, a single fuel injector is located at the upstream end of said first air inlet means.