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Spare parts supply from own inventory (see list) and external sources

Airframe Repair (in-house technician)

Transmission components repair / refurbishment (in-house technician)

Radio components repair (in-house technician)

Component Repair Management

Spare parts supply from own inventory (see list) and external sources

Component Repair Management

Spare parts supply

Component Repair Management

Spare parts supply

Component Repair Management

NDT

Spare parts supply

Component Repair Management

NDT

Spare parts supply

Component Repair Management

NDT

Spare parts supply

Component Repair Management

NDT

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We will post here information of public interest about our activity, our company and the aviation industry in general.

The turbojet is an airbreathing jet engine, usually used in aircraft. It consists of a gas turbine with a propelling nozzle. The gas turbine has an air inlet, a compressor, a combustion chamber, and a turbine (that drives the compressor). The compressed air from the compressor is heated by the fuel in the combustion chamber and then allowed to expand through the turbine. The turbine exhaust is then expanded in the propelling nozzle where it is accelerated to high speed to provide thrust. Two engineers, Frank Whittle in the United Kingdom and Hans von Ohain in Germany, developed the concept independently into practical engines during the late 1930s.

Air intake

An intake, or tube, is needed in front of the compressor to help direct the incoming air smoothly into the moving compressor blades.

Combustion chamber

In a turbojet the air and fuel mixture burn in the combustor and pass through to the turbine in a continuous flowing process with no pressure build-up. Instead there is a small pressure loss in the combustor.

Nozzle

After the turbine, the gases expand through the exhaust nozzle producing a high velocity jet. In a convergent nozzle, the ducting narrows progressively to a throat.

Compressor

The compressor is driven by the turbine. It rotates at high speed, adding energy to the airflow and at the same time compressing it into a smaller space.

Turbine

Hot gases leaving the combustor expand through the turbine. Typical materials for turbines include inconel and Nimonic.

Afterburner

An afterburner or “reheat jetpipe” is a combustion chamber added to reheat the turbine exhaust gases. The fuel consumption is very high, typically four times that of the main engine.

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