This article was automatically translated from the original Turkish version.
The Auxiliary Power Unit (APU) is a gas turbine engine commonly used in aircraft, military and commercial vehicles, locomotives, and some large sea vehicles. The primary function of the APU is to provide electrical and pneumatic power before the main engines are started or when they are shut down.
The importance of the APU in the aviation sector is significant because it performs critical functions such as maintaining cabin systems while on the ground, starting the main engines, and providing emergency power. In commercial aircraft, it is typically located in the tail section and operates on jet fuel.
APUs are not limited to aircraft. They are also used in military vehicles, diesel locomotives, and some large trucks and trailers. For example, in military tanks, the APU is used to start the main engine and generate power with low fuel consumption during prolonged operations.
Auxiliary Power Unit (Credit: http://www.blackrockapu.com)
The Auxiliary Power Unit (APU) performs essential roles in aircraft, military vehicles, locomotives, and some large commercial land vehicles.
Aircraft engines require high-pressure air before they can be started. The APU generates this demand by producing pneumatic air (compressed air) to enable engine start-up.
When the aircraft is on the ground, the main engines are turned off. However, cabin systems such as lighting, climate control, avionics systems and others require electrical power. The APU generates electricity as an alternative to the main generators.
This feature reduces reliance on ground power units (GPU) at airports and saves fuel.
The pressurized cabins and air conditioning systems of aircraft are supported by the APU, especially when on the ground.
If a failure or power interruption occurs in the main engines, the APU activates as a backup power source.
For example, in commercial aircraft such as Airbus A320 and Boeing 737, the APU plays a critical backup role by generating electricity independently from the main engines during flight.
The APU is not only used in aircraft but also in military tanks, armored vehicles, locomotives, and large commercial trucks.
By supporting systems without unnecessarily running the main engines of aircraft and vehicles, the APU reduces fuel consumption and carbon emissions.
Especially newer generation APUs are designed to be more efficient and produce lower emissions.
The Auxiliary Power Unit (APU) is a system that generates electrical, pneumatic, and hydraulic energy using a small gas turbine or internal combustion engine. The operating principle of the APU, used in aircraft and some land and sea vehicles, can be examined in three main stages: Start-up, Operation, and Shutdown.
1- The starter motor engages.
2- Fuel injection begins.
3- The turbine begins operation.
4- The APU reaches steady state.
Once the APU is operational, it provides power for two main systems:
1- Electrical Generation:
2- Pneumatic Power Generation:
While operating, temperature, pressure, and fuel consumption are continuously monitored. If any abnormality is detected, safety systems activate and shut down the APU.
1- The APU load is reduced.
2- Fuel flow is cut off.
3- The cooling process begins.
4- The APU shuts down completely.
The operating principle of the APU varies according to its intended use:
1- Normal Mode:
2- Emergency Status Mode:
3- Fuel Saving Mode:
4- Cold Weather Mode:
The APU operates on the principle of a small gas turbine and consists of the following components:
1- Air Intake System
2- Fuel System
3- Starter System
4- Combustion Chamber
5- Turbine and Generator
6- Exhaust System
7- Control and Protection Systems
The Auxiliary Power Unit (APU) is installed in a specific location on aircraft to ensure safe and efficient operation. Although its position varies depending on aircraft design, it is typically located in the tail section or, in some specialized designs, beneath the fuselage or within the body.

Location of the APU in aircraft (Credit: ucaklar.org)
In most commercial and military aircraft, the APU is located as follows:
1- In the Aircraft’s Tail Section (Tail Cone / Rear Fuselage)
2- Beneath the Fuselage or Within the Wings
3- In Helicopters: Within the Fuselage or Near the Wing Root
The following engineering criteria are considered when determining the APU’s location on an aircraft:
1- Exhaust Gas Direction
2- Aerodynamic Balance
3- Maintenance and Accessibility
4- Fuel and Pneumatic Connections
Click to view the simulation explaining the operating principle of the Auxiliary Power Unit.
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Primary Functions of the APU
1. Starting the Aircraft’s Main Engines
2. Providing Electrical Power While on the Ground
3. Enabling Air Conditioning Operation
4. Providing Emergency Power
5. Supporting Military and Commercial Vehicles
6. Improving Fuel Efficiency and Environmental Benefits
Operating Principle of the APU
A) Start-up (Starting Phase)
B) Operation (Running Phase)
C) Shutdown (Shutdown Phase)
Different Operating Modes of the APU
Components of the APU
Location of the APU in Aircraft
Typical APU Location
Factors Influencing APU Location Selection
APU Location by Aircraft Model
Location and Importance of the APU Exhaust Outlet
Advantages of the APU