CNC Maching Combustion Chamber

The combustion chamber in the turbine accessories is a crucial component.

The main function of the combustion chamber is to fully mix the fuel and air and burn them to produce high-temperature and high-pressure gas to drive the turbine to rotate and generate power.

directional casting combustor
The structure of the combustion chamber needs to be able to withstand extremely high temperatures and pressures, and is generally made of high-temperature resistant materials, such as Inconel, Nimonic, single crystal materials, etc. During operation, the combustion chamber must ensure the stability and continuity of combustion, while minimizing energy loss and pollutant emissions. Accurate design and manufacturing are critical to achieving the best performance of the combustion chamber, which directly affects the efficiency, power output and reliability of the entire turbine system. Different types of turbine engines also have different requirements for combustion chambers to adapt to different application scenarios and working conditions.

Combustion chamber composition:

The inner wall of the combustion chamber is usually made of high-temperature alloys or other high-temperature resistant materials to withstand the action of high-temperature combustion gases.

The nozzle system is used to inject fuel and air and ensure that they are evenly mixed.

The combustion chamber requires an ignition system to ignite the mixed gas and start the combustion process.

The combustion chamber is usually designed with cooling structures, such as cooling channels, cooling nozzles, etc., to cool the inner wall of the combustion chamber to prevent overheating.

The operating temperature of the turbine combustion chamber is usually very high, generally reaching 1000℃ or even higher.

The specific operating temperature varies depending on the application scenario, turbine model and design requirements. For example, in aircraft engines, advanced turbine combustion chambers may have to withstand temperatures exceeding 1500℃; while in turbines for some industrial applications, the temperature may be relatively low, but it is usually above 1000℃.

In order to cope with such high temperatures, the combustion chamber is usually made of special high-temperature resistant materials, and there will be corresponding cooling designs to maximize its service life and ensure performance.

The operating environment of the turbine combustion chamber has the following characteristics

High temperature and pressure

facing extremely high temperature and pressure, which is the basic condition for its normal working state.

High-speed airflow

There is fast-flowing air and combustion gas inside.

Chemical erosion

some corrosive chemicals may be produced during the combustion of fuel.

Vibration and shock

due to the operation of the turbine, it will be subject to a certain degree of vibration and mechanical shock.

Small space

usually installed in a relatively compact space.

High load

continuously bear large power and energy loads.

The main application areas of turbine accessory combustion chambers are:

Aerospace: In aircraft engines, it provides powerful power for aircraft and ensures flight performance.

Gas turbine: It is used for large gas turbine equipment such as power generation and industrial drive to meet energy needs.

Ship power: It provides propulsion power for ships and ensures the navigation ability of ships.

Energy industry: It may also be used in some distributed energy systems or special energy projects.

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