Aviation Propulsion Fuel Test System
Get a quote：
Whats/App: +86 181 0160 0864
Web: gellowen.co.uk
The Aviation Propulsion Fuel Test System is a precision testing platform designed for evaluating fuel combustion and performance in aircraft propulsion components. You can use it to conduct automated fuel burn tests on aerospace power units, measuring fuel flow, pressure, temperature, and combustion characteristics under controlled conditions. The system incorporates the FAA-approved NexGen Aviation Fuel Burner, compatible with previous generation burners such as Park DPL 3400. Lennox Model OB-32. and Carlin Model 200 CRD, while providing enhanced control and modularity for future upgrades.
Application
The Aviation Propulsion Fuel Test System is suitable for a wide range of aerospace testing applications:
Aircraft Propulsion Components: Automated fuel combustion testing for turbines, pumps, and engine assemblies.
Fuel System Evaluation: Measure fuel system performance, burn characteristics, and low-temperature operability.
Component Fire Safety: Conduct controlled burn tests on aircraft fuel lines, fuel pumps, and connected systems.
R&D and Certification Testing: Support FAA, ISO, and SAE compliance testing of fuel systems and propulsion components.
Integration Testing: Test aircraft modules and subassemblies under simulated operational and thermal load conditions.
Typical test products include aircraft turbine fuel pumps, valves, fuel lines, engine components, and other fuel system assemblies.
Standards
The system supports compliance with international and domestic standards for aviation fuel system testing:
FIRE TEST HANDBOOK: Chapter 12 – Material and component fire testing methods.
ISO 8217 – Aviation turbine fuel specifications.
ISO 11170 – Aircraft fuel pump performance testing.
ASTM D1655 – Aviation turbine fuel standards.
ASTM D3241 – Fuel combustion performance and low-temperature testing.
SAE AS22771 – Aviation engine fuel system component testing.
SAE AS1241 – Fuel pump performance and durability tests.
FAR Part 33 – Aircraft engine airworthiness, including fuel system design and testing.
FAR Part 23 / Part 25 Appendix F – Fire resistance and performance requirements for fuel systems in transport and general aviation.
DEF STAN 91-091 – UK Defense fuel system performance testing.
EUROCAE ED-79 / ED-79A – Aircraft engine fuel system certification and testing.
BSS Series (e.g., BSS 7220) – Fuel system material flammability and compatibility evaluation.
Parameters
| Parameter Category | Details |
|---|---|
| Dimensions | 1500 mm (W) × 1800 mm (H) × 900 mm (D) |
| Weight | 150 kg |
| Fuel Requirement | Aviation kerosene |
| Compressed Air Requirement | ≥ 120 PSI |
| Power Supply | 220 V, 10 A |
| Operating Temperature | 10°C – 35°C |
| Sample Mounting | Horizontal and vertical installation supported |
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