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The ideal temperature for the back of a turbine jet engine, also known as the exhaust gas temperature (EGT), can vary depending on the specific engine and its operating conditions. However, in general, the EGT should be around 1,600-2,000 degrees Fahrenheit.
The temperature of the back of a turbine jet engine is typically measured using thermocouples, which are small temperature sensors that are placed at various points in the engine. These sensors can withstand high temperatures and provide accurate readings of the EGT.
The temperature of the back of a turbine jet engine is important because it affects the efficiency and performance of the engine. If the temperature is too high, it can cause damage to the engine and decrease its lifespan. On the other hand, if the temperature is too low, it can lead to inefficient combustion and reduced power output.
There are several factors that can affect the temperature of the back of a turbine jet engine, including the air temperature, altitude, engine load, and fuel mixture. Additionally, the design and condition of the engine itself can also impact the EGT.
The temperature of the back of a turbine jet engine is primarily controlled through the fuel-to-air ratio. By adjusting the amount of fuel being injected into the engine, the temperature can be regulated to ensure that it stays within the optimal range. Advanced engines also have computer systems that monitor and adjust the fuel mixture in real-time to maintain a consistent EGT.