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.

You do not have access to this resource.

Exclusive to subscribers. 97% yet to be discovered!

Already subscribed? Log in!

The Ultimate Scientific and Technical Reference

A Comprehensive Knowledge Base, with over 1,200 authors and 100 scientific advisors

+ More than 10,000 articles and 1,000 how-to sheets, over 800 new or updated articles every year

From design to prototyping, right through to industrialization, the reference for securing the development of your industrial projects

This article is included in

Material processing - Assembly

This offer includes:

Knowledge Base

Updated and enriched with articles validated by our scientific committees

Services

A set of exclusive tools to complement the resources

Practical Path

Operational and didactic, to guarantee the acquisition of transversal skills

Doc & Quiz

Interactive articles with quizzes, for constructive reading

Ongoing reading
Background to turbojet engines

Bibliography

(1) - MORGAN (E.J.) - Atmospher Control Criteria for Welding Titanium - . Conference Proceedings from Advanced in Welding Processes, Harrogate (1978).
(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...