Aero engine

Our products can be found in all corners of the sector, from commercial aircraft and business jets, to military aircraft and helicopters.

AEROSPACE

We ensure the precision and quality required for the aero engine components. Our precision forgings are widely used in aero and helicopter engines. Moreover, in order to guarantee the reliability throughout the service life, we apply all the high strict quality control procedures required by Internation Entities and Customers. We are part of the main Aero Engine Programs: CFM Leap 1ABC; P&W GTF series; Rolls Royce Trent XWB, Trent 1000-TEN, Trent 7000, BR and PEARL series; GE GE9X, Honeywell HTF7000 series.

APPLICATIONS

Fan case module

The fan case module is a very delicate part of an aircraft engine. The pieces that compose it must be very light and resistant to keep the efficiency of the aircraft and to be able to contain potential fragments of blades mainly due to FOD. Before entering in service these components have to pass numerous tests.

Front fan case
Mount ring
Inner ring
V-groove

High & low pressure compressor

Located downstream of the fan stages, they represent the way to increase efficiency on a jet propulsion system. Compressors have to decrease the air flow and increase contemporarily the pressure at the exit of each stage. Rotor and stator blades may be able to resist to failure, their cases are designed like the fan case module.

Outer/Inner Guide Vane Ring
Compressor case

Combustion chamber

The combustion chamber is the place where the combustion of the comburent mixed with fuel occurs. High temperature resistance is the “must be” for this component. Superalloys are generally used for the manufacturing of the combustion chambers. The design of combustion chambers shall take into consideration perfect fuel-air ratio that permits an efficient combustion (reduction of fuel consumption).

Combustor case
Combustor lining
Diffuser case

Turbine

The turbine is the machine which drives fan and compressor. Its role is to transform the energy of the combusted gas. The main limitation factor of the turbine design is the elevated operative temperature in combination with high rotation speed of their blades. A good compromise can be found in Nickel-based material (alloys and superalloys).

HP Turbine Shroud
LP Turbine Case
Turbine Shaft
HP Turbine Case
IP Turbine Case

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Aero engine

AEROSPACE

APPLICATIONS

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