This standard specifies the general requirements, test procedures, data processing and result evaluation for aviation gas turbine engine rotor axial force tests. This standard is applicable to the axial force test of rotors of aviation gas turbine engines, compressor components, turbine components, etc. using force ring testing systems.
HB 20042-2011 Referenced Document
GB/T 2298 Mechanical vibration,shock and condition monitoring.Vocabulary
GJB 241 General specification for aerospace turbojet and turbofan engines
GJB 242 General specification for aerospace turboprop and turboshaft engines
HB 20042-2011 history
2011HB 20042-2011 Test methods of rotor thrust for aircraft engine