HB 7081-2012
Aerodynamic performance test method of axial turbine for aircraft gas turbine engine (English Version)

Standard No.

HB 7081-2012

Language

Chinese, Available in English version

Release Date

2013

Published By

Professional Standard - Aviation

Latest

HB 7081-2012

Replace

HB 7081-1994

Scope

This standard specifies the general requirements, test procedures, data processing and result evaluation for aviation gas turbine engine axial flow turbine and guide aerodynamic performance testing. This standard is applicable to aerodynamic performance testing of axial flow single-stage and multi-stage turbines with or without air conditioning, single-rotor, dual-rotor turbines and guides using air or gas as the test working fluid.

HB 7081-2012 Referenced Document

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

HB 7081-2012 history

• 2013 HB 7081-2012 Aerodynamic performance test method of axial turbine for aircraft gas turbine engine
• 1994 HB 7081-1994 Axial flow turbine aerodynamic performance test