HB 20059-2011
Centrifugal compressor design requirement of aero engine (English Version)

Standard No.

HB 20059-2011

Language

Chinese, Available in English version

Release Date

2011

Published By

Professional Standard - Aviation

Latest

HB 20059-2011

Scope

This standard specifies the design basis, design criteria, design process, design content and design methods, and verification test items for aeroengine centrifugal compressors. This standard applies to the design of aeroengine centrifugal compressors. The centrifugal compressor design of aviation gas turbine auxiliary power units and aviation-derived gas turbines can also be used as a reference.

HB 20059-2011 Referenced Document

• GJB 2103A-1997 Aviation gas turbine power plant terminology and symbols

HB 20059-2011 history

• 2011 HB 20059-2011 Centrifugal compressor design requirement of aero engine