HB 20060-2011
Damper design requirements of aero engine (English Version)
- Standard No.
- HB 20060-2011
- Language
- Chinese, Available in English version
- Release Date
- 2011
- Published By
- Professional Standard - Aviation
- Latest
- HB 20060-2011
- Scope
- This standard specifies the design criteria, design process, design content and design methods, and verification test items for aero-engine elastic supports (hereinafter referred to as elastic supports). This standard applies to the design of elastic supports for aviation gas turbine engines. The design of elastic supports for aviation-derived gas turbines and other types of gas turbines can also be used as a reference.
HB 20060-2011 Referenced Document
- GB/T 1182 Geometrical product specifications(GPS)—Geometrical tolerancing—Tolerances of form, orientation, location and run-out*， 2018-09-17 Update
- GB/T 131 Geometrical Product Specifications (GPS). Indication of surface texture in technical Product documentation
- GB/T 4458.4 Mechanical drawings dimensioning
- GB/T 4458.5 Mechanical drawings Indication of tolerances for size and of fits
- GJB 190-1986 Demonstration of reliability,maintainability and supportability requirements for material
- GJB 2103A-1997 Aviation gas turbine power plant terminology and symbols
- GJB 450A-2004 General requirement for materiel reliability program
- HB 5013-1996 Inspection category of heat treatment parts
HB 20060-2011 history
- 2011 HB 20060-2011 Damper design requirements of aero engine
