HB/Z 20001-2011
NC milling process of titanium alloy monolithic components for aircraft (English Version)

Standard No.

HB/Z 20001-2011

Language

Chinese, Available in English version

Release Date

2011

Published By

Professional Standard - Aviation

Latest

HB/Z 20001-2011

Scope

This guiding technical document stipulates the equipment, tooling, workshop environment, process flow, process control, quality control, personnel, safety and other requirements for CNC milling of aircraft titanium alloy integral structural parts. This guiding technical document is applicable to CNC milling of titanium alloy overall structural parts of aircraft fuselages and titanium alloy engine casings and blades of aviation companies.

HB/Z 20001-2011 Referenced Document

• HB 7814-2006 General requirements of NC programming

HB/Z 20001-2011 history

• 2011 HB/Z 20001-2011 NC milling process of titanium alloy monolithic components for aircraft