The combustion chamber of a gas turbine engine is the place where the fuel-air mixture undergoes combustion - it burns.
4/16/09-
( D ) Gases are cooled to a desired temperature.
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Allow me to add to this:
yup it's
Gases are cooled to a desired temperature.
<page 88 in you Penn Foster Heat book>
combustion it is where the fuel and air mixture burns and the expanding gasses drive the turbine
A mixture of fuel oil and compressed air is ignited
mixture of fuel oil and compressed air is ignited.
SI engine means Spark Ignition Engine where combustion products(air,fuel)are ignited in combustion chamber by means of spark from spark plug which is located on cylinder head..CI engine means Compression Ignition Engine,here combustion is take place by means of compression..
When an engine runs as it should the fuel/air mix in the combustion chamber ignites at the spark plug and the flame front spreads from there. In an engine that's knocking there are hotspots in the combustion chamber causing the fuel/air mixture to ignite prematurely a bit all over the place.
DI means Direct Injection. Diesel engine depending on combustion categorised in Direct injection or InDirect injection Engine. Direct Injection engine combustion takes place directly above the piston. But indirect injection combustion initially takes place pre-combustion chamber and after transfered to above piston.DI engine more fuel efficient, easily start in cold condition, But Noise more.
Gas turbines are a type of Internal Combustion engine, however; Assuming that you want to know the difference between a recpirocating piston engine and a gas turbine engine, the simple answer is that ICE's (Internal combustion engines) create work by moving a crank that is connected to a piston. An explosion in the piston chamber pushes a piston (or series of pistons) attached to a crankshaft, which turns the shaft. The gas turbine works by turning a shaft connected to a turbine. The turbine is powered by a compressed feul-air mixture. A stream of gas is compressed with air and forced through a chamber containing the turbine. The turbine turns the shaft as a result of complex mechanics that control the movement and flow of the compressed fuel-air mixture. The basic mechanical difference: A reciprocating piston engine uses a linear "back and forth" motion to turn a shaft, and the gas turbine engines relies on a constant circular motion to turn a shaft.
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.
The importance of engine is gigantic! As we all know engine is the heart of power plant. Inside the engine they are taking place 3 conversions: At first, the fuel injected into the combustion chamber and combustion takes place. The chemical energy of fuel is converted into thermal energy! Thermal energy is received and converted by the piston to Mechanical energy which is led to installation's shaft! All these processes are taking place inside the engine, and must complete with accuracy! So, it is absolutely understood that engine is of vital importance for the whole installation!
Type your answer here... what is another term for combution chamber in a furnace or fire place.
External Combustion engine is an engine in which combustion of fuel takes place outside the cylinder. e.g.Coal fired steam engines in trains
The importance of engine is gigantic! As we all know engine is the heart of power plant. Inside the engine they are taking place 3 conversions: At first, the fuel injected into the combustion chamber and combustion takes place. The chemical energy of fuel is converted into thermal energy! Thermal energy is received and converted by the piston to Mechanical energy which is led to installation's shaft! All these processes are taking place inside the engine, and must complete with accuracy! So, it is absolutely understood that engine is of vital importance for the whole installation!
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.
An aeroplane's engine sucks air. Combustion takes place due to jet fuel. The force of the combustion propels the aircraft.