GJB 6357-2008 (English Version) PDF

Standard No.: GJB 6357-2008
Language: Chinese, Available in English version
Release Date: 2008
Published By: Military Standard of the People's Republic of China-General Armament Department
Latest: GJB 6357-2008

Scope: This specification specifies the general requirements for the design, performance, test and acceptance of helicopter turboshaft engine reducers (hereinafter referred to as reducers). This specification is applicable to the development, production and acceptance of turboshaft engine reducers for helicopters; it is also applicable to reducers for turboprop engines, propfan engines, turbofan engines, parallel reducers for power systems composed of two engines, and gas turbine starters reducer. When improving and modifying the reducer that has been mass-produced, the modified part can also be designed and verified by referring to this specification.

GJB 6357-2008 Referenced Document

GJB 1181-1991 General outline for packaging, loading, unloading, storage and transportation of military equipment
GJB 145-1986 General rules for sealing and packaging
GJB 242-1987 General specification for aerospace turboprop and turboshaft engines
GJB 243-1987 Aviation gas turbine power plant flight test specifications
GJB 269A-2000 General specifications for aerospace rolling bearings
GJB 3872-1999 General requirements for comprehensive equipment support
GJB 450-1988 General outline of reliability for equipment development and production
GJB 594-1988 Metal plating layer and chemical coating layer selection principles and thickness series
GJB 833-1990 Aero engine packaging mark
GJB 834-1990 Aviation engine packaging qualification test
GJB 835-1990 General specifications for aero-engine packaging boxes

2008 GJB 6357-2008 General specification for helicopter turboshaft engine reduction gearbox