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F23R 3/00
|
Continuous combustion chambers using liquid or gaseous fuel |
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F23R 3/02
|
Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration |
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F23R 3/04
|
Air inlet arrangements |
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F23R 3/06
|
Arrangement of apertures along the flame tube |
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F23R 3/08
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Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections |
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F23R 3/10
|
Air inlet arrangements for primary air |
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F23R 3/12
|
Air inlet arrangements for primary air inducing a vortex |
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F23R 3/14
|
Air inlet arrangements for primary air inducing a vortex by using swirl vanes |
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F23R 3/16
|
Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow |
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F23R 3/18
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Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants |
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F23R 3/20
|
Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means |
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F23R 3/22
|
Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants movable, e.g. to an inoperative positionFlame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants adjustable, e.g. self-adjusting |
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F23R 3/24
|
Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants of the fluid-screen type |
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F23R 3/26
|
Controlling the air flow |
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F23R 3/28
|
Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply |
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F23R 3/30
|
Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices |
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F23R 3/32
|
Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices being tubular |
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F23R 3/34
|
Feeding into different combustion zones |
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F23R 3/36
|
Supply of different fuels |
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F23R 3/38
|
Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising rotary fuel injection means |
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F23R 3/40
|
Continuous combustion chambers using liquid or gaseous fuel characterised by the use of catalytic means |
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F23R 3/42
|
Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers |
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F23R 3/44
|
Combustion chambers comprising a tubular flame tube within a tubular casing |
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F23R 3/46
|
Combustion chambers comprising an annular arrangement of flame tubes within a common annular casing or within individual casings |
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F23R 3/48
|
Flame tube interconnectors, e.g. cross-over tubes |
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F23R 3/50
|
Combustion chambers comprising an annular flame tube within an annular casing |
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F23R 3/52
|
Toroidal combustion chambers |
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F23R 3/54
|
Reverse-flow combustion chambers |
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F23R 3/56
|
Combustion chambers having rotary flame tubes |
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F23R 3/58
|
Cyclone or vortex type combustion chambers |
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F23R 3/60
|
Support structuresAttaching or mounting means |
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F23R 5/00
|
Continuous combustion chambers using solid or pulverulent fuel |
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F23R 7/00
|
Intermittent or explosive combustion chambers |
