Aircraft Gas Turbine Engine Combustion Chamber Frame

The Aircraft Gas Turbine Engine Combustion Chamber Frame 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 combustion chamber frame is a structural component of a gas turbine engine that houses the combustion chamber. It provides support and stability to the combustion chamber and helps to maintain the integrity of the engine during operation. The frame is typically made of high-strength materials such as steel or titanium to withstand the high temperatures and pressures generated by the combustion process.

The combustion chamber frame also plays a crucial role in directing the flow of air and fuel into the combustion chamber and ensuring efficient combustion. It is designed to optimize the mixing of air and fuel, promote complete combustion, and minimize emissions.

Overall, the combustion chamber frame is an essential component of an aircraft gas turbine engine, contributing to its performance, reliability, and safety.