Aircraft Gas Turbine Engine Inner Augmentor Nozzle Section

The Aircraft Gas Turbine Engine Inner Augmentor Nozzle Section is a component that is part of the supply class Gas Turbines And Jet Engines, Aircraft, Prime Moving; And Components in the supply group Engines, Turbines, And Components.

The inner augmentor nozzle section is a critical part of a gas turbine engine. It is located within the engine's augmentor or afterburner section. The augmentor is a component that is used to increase the thrust of the engine by injecting additional fuel into the exhaust stream and igniting it.

The inner augmentor nozzle section is responsible for directing and shaping the flow of the hot exhaust gases as they exit the engine. It is designed to optimize the mixing of the fuel and air, ensuring efficient combustion and maximum thrust generation.

The inner augmentor nozzle section is typically made of high-temperature resistant materials, such as nickel-based alloys, to withstand the extreme heat and pressure conditions within the engine. It is also designed to be durable and resistant to wear and corrosion.

Overall, the inner augmentor nozzle section plays a crucial role in the performance and efficiency of an aircraft gas turbine engine, contributing to the engine's thrust output and overall power.