The main combustion chamber and the secondary combustion chamber are sequentially formed.
The invention concerns an axially stepped annular combustion chamber, in particular for an aircraft gas turbine, the combustion chamber essentially comprising an independent main combustion chamber (5') and an independent pilot combustion chamber (5).
The main combustion chamber (5) is formed surrounding the secondary combustion chamber (8).
An internal combustion engine has a main combustion chamber (20) in communication with a preliminary combustion chamber (30) and has an isolating valve (32) for isolating the preliminary from the main chamber.
The housing forms a main combustion chamber (300).
The invention relates to a mixture-charged gas engine (1) with at least one cylinder (3).
Mixed gas jetted from wick is burned in primary combustion chamber (55).
Described herein is a combustion pre-chamber apparatus for a main combustion chamber of an internal combustion engine that includes a body that defines an internal combustion cavity.
The flow of fuel from the fuel injector and the flow of air from the burner are ignited in the main combustion chamber by the ignition of the air/ fuel mixture in the initial combustion chamber.
The main combustion chamber (5) is enclosed by an outer furnace body (4).
A gas turbine engine combustor (26) includinga primary combustion chamber (28), a mixer element (34), a mixing chamber (46) and a secondary combustion chamber (48).
An outlet of the charge distributor (3) is aligned to the main combustion chamber (5).
The approach includes utilizing a conventional dry low NOx combustor for the main combustor and thermal reactors for the reheat apparatuses.
Further, a tapered reduced diameter portion functioning as a fan-shaped nozzle is added so that a combustion gas can efficiently move from the main combustion chamber to a sub-combustion chamber.
The main combustion chamber (130) is formed between the piston (112) and the cylinder head (126).
The heat outlet is in communication with upper portions of the main combustion chamber and of the secondary combustion chamber so as to discharge heat generated during the combustion of the fuel upward.
An internal combustion engine includes a cylinder head (10) defining at least a portion of a main combustion chamber (14).
Venturi tube type inner circulators (42) are set on four corners of the base (40). mechanical fluidizing machine (4) is set on the bottom of the main combustion chamber (1).
The combustion furnace (4) is divided by a second partition (5) into a main combustion chamber (6) and a heat recovery chamber (7).
The hollow transfer screw is arranged across the main combustion chamber and the secondary combustion chamber, and rotates via driving means so as to sequentially transfer the fuel.
Requêtes fréquentes français :1-200, -1k, -2k, -3k, -4k, -5k, -7k, -10k, -20k, -40k, -100k, -200k, -500k, -1000k,
Requêtes fréquentes anglais :1-200, -1k, -2k, -3k, -4k, -5k, -7k, -10k, -20k, -40k, -100k, -200k, -500k, -1000k,
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