Cold compressor rotors
Metallurgical assembly in jet engine construction
Article REF: BM7778 V1
Cold compressor rotors
Metallurgical assembly in jet engine construction

Author : Jean-Pierre FERTE

Publication date: January 10, 2006 | Lire en français

Logo Techniques de l'Ingenieur You do not have access to this resource.
Request your free trial access! Free trial

Already subscribed?

3. Cold compressor rotors

The "cold" compressors of turbojet engines, which include the low-pressure compressor and the upstream part of the high-pressure compressor, are made up of a set of successive discs, mechanically or metallurgically interconnected and fitted with blades, whose function is to compress the air to be burned in the combustion chamber.

3.1 Choice of materials

The external constraints are as follows:

  • virtually finished machined parts, which means using processes that generate low welding shrinkage;

  • parts with certified service life, working in low-cycle fatigue and requiring proven non-propagation of potential defects.

You do not have access to this resource.
Logo Techniques de l'Ingenieur

Exclusive to subscribers. 97% yet to be discovered!

You do not have access to this resource. Click here to request your free trial access!

Already subscribed?


Article included in this offer

"Aerospace systems"

( 77 articles )

Complete knowledge base

Updated and enriched with articles validated by our scientific committees

Services

A set of exclusive tools to complement the resources

View offer details
Contact us