1 Subject content and application scope
This standard specifies the technical requirements, calibration, test run procedures, data acquisition and processing methods of the steady-state temperature measuring system for missile used turbojet and turbofan engines during ground test.
This standard is applicable to the steady-state temperature measurement of platinum resistance temperature sensor and thermocouple temperature sensor of missile used turbojet and turbofan engines (hereinafter referred to as engines).
2 Normative references
GB 2614 Specification for industrial thermocouple assemblies
GB 2903 Copper/Copper-Nickel (constantan) thermocouple wires and their reference tables
JJG 617 National metrological verification regulation of the People's Republic of China
QJ 1457 General specification for platinum resistance temperature sensors
JB 1822 Compensating wires for industrial thermocouples
3 Technical requirements
3.1 Composition of measuring system
3.1.1 The block diagram for thermocouple temperature measuring system is shown in Figure 1.
1 Subject content and application scope
2 Normative references
3 Technical requirements
4 Calibration of the temperature measuring system
5 Test run procedures
6 Test run data acquisition and processing
Additional explanation
