QJ 2655.4-1994 in English

VALID

Measurement Method for Parameter of Turbojet Engine and Turbofan Engine for Missile - Fuel Flow

Issued on:1994-04-27
Implemented on:1994-11-01
File Format:PDF
Delivery:Via email within 1~3 business days

Price(USD)： $90.00
$88.00

Standard No:	QJ 2655.4-1994
Document status:	VALID
Title in English:	Measurement Method for Parameter of Turbojet Engine and Turbofan Engine for Missile - Fuel Flow
Title in Chinese:	弹用涡轮喷气和涡轮风扇发动机参数测量方法燃油流量
Language:	English
File Format:	Electronic (PDF)
Delivery:	Via email within 1~3 business days
Issued on:	1994-04-27
Implemented on:	1994-11-01
ICS Classification:	49.050-Aerospace engines and propulsion systems
Chinese Classification:	V72-Spacecraft power system
Professional Classification:	QJ-Aerospace
Related Keywords:	fuel flow measuring system fuel flow measurement steady-state fuel flow measuring system fuel flow turbojet engine
Related Topics:	Test method for aerodynamic performance of axial flow turbine of aviation gas turbine engine Air six parameter measurement method turbine Parameter measurement method Turbine Meters and Flow Measuring wheel technical parameters How Turbine Measures turbo fan The function of turbine flow meter Turbine flow meter k coefficient How to use the measuring wheel Vortex fan parameters Aviation turbojet and turbofan engine vibrations Gas turbine engine overspeed rupture Eddy current braking industry Eddy current brake industry Gas turbine flow meter installation Turbo fan structural design

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 fuel flow measuring system for missile used turbojet and turbofan engines during ground test.

This standard is applicable to the fuel flow measurement of missile used turbojet and turbofan engines (hereinafter referred to as engines) with turbine flow sensor.

2 Normative references

Q 28 Calculation method for static accuracy of pressure sensors
QJ 2655.1 Measuring method for parameters of missile used turbojet and turbofan engines - Intensity of pressure

3 Technical requirements

3.1 Composition of fuel flow measuring system

The block diagram for fuel flow measuring system is shown in Figure 1.

1 Subject content and application scope
2 Normative references
3 Technical requirements
4 Calibration of measuring system
5 Test run procedures
6 Test run data acquisition and processing
Additional explanation

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