1. Background to turbojet engines

The design and construction of a turbojet engine involves the use of materials (figure 1 ):

This is due to a wide operating temperature range, from -50 ˚C to 1,250 ˚C, and to the constant need to minimize mass;
working under severe mechanical and environmental conditions;
with long-lasting properties.

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Background to turbojet engines

Bibliography

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(2) - SMITH (L.S.), GITTOS (M.F.) - A Review of Weld Metal Porosity and Hydrid Cracking...

Aerospace series – Welded and brazed assemblies for aerospace construction – Weldability and solderability of materials – Part 10: General information. - NF L06-380-10 - 2-03
Aerospace series – Welded and brazed assemblies for aerospace construction – Weldability and solderability of materials – Part 20: homogeneous assemblies of aluminum and aluminum alloys. - NF L06-380-20 - 2-03
Aerospace series – Welded...