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A combustion chamber is where combustion occurs in a controlled fashion. Because the basic idea of a rocket is burning fuels and directing them in the opposite direction to that of travel, a controlled burning - as happens in the combustion chamber - is exactly what a rocket needs to work.
180o C
The temperature inside the combustion chamber of a jet engine is one of the hottest manufactured by man. It can run about 1400 degrees Celsius or 2552 degrees Fahrenheit.
Temperatures in the combustion chamber can reach 4,500*F or 2,500*C.
the air temp at the end of the compression stroke for the ignition of diesel fuel within the combustion chamber is approx between 450*c - 675*c Brent
The combustion chamber. The temperature of the air/fuel mixture combusting is approximately 1800 degrees f.
Can combustors are self contained cylindrical combustion chambers. Each "can" has its ownfuel injector, igniter, liner, and casing. Made up of individual combustion chambers. This type of combustion chamber is so arranged that air from the compressor enters each individual chamberthrough the adapter. Each individual chamber is composed of two cylindrical tubes, the combustionchamber liner and the outer combustion chamber. Combustion takes place within the liner. Airflowinto the combustion area is controlled by small louvers located in the inner dome, and by roundholes and elongated louvers along the length of the liner.
More modern engines use a fuel injection system where the fuel is computer controlled and injected in the right amounts and right time into the chamber. Older engines may use carburettors, which spray the fuel into the chamber, but are controlled mechanically.
incubation
2500K around 4000*F or 2225*C
Can combustors are self contained cylindrical combustion chambers. Each "can" has its ownfuel injector, igniter, liner, and casing. Made up of individual combustion chambers. This type of combustion chamber is so arranged that air from the compressor enters each individual chamberthrough the adapter. Each individual chamber is composed of two cylindrical tubes, the combustionchamber liner and the outer combustion chamber. Combustion takes place within the liner. Airflowinto the combustion area is controlled by small louvers located in the inner dome, and by roundholes and elongated louvers along the length of the liner.
Diesel Engine combustion chamber types : Swirl port combustion chamber type and Preignition port combustion chamber type.