NEXGEN Aviation Fuel Burner
Get a quote：
Whats/App: +86 185 0176 3615
Web: qinsun-lab.com
The NexGen Aviation Fuel Burner is suitable for a variety of aerospace testing applications:
Aircraft Cabin Materials: Evaluate seat cushions, insulation, and cabin panels for flame spread and smoke toxicity in compliance with FAR 25.853. FAR 25.855. and FAR 25.867.
Cargo Compartment Materials: Conduct burn-through resistance testing on cargo liners and panels.
Soft and Hard Tubing Assemblies: Test fuel, hydraulic, and electrical conduit assemblies under controlled flame conditions.
Electrical Components and Engine Assemblies: Assess fire resistance of electric motor housings, connectors, and wiring.
Material R&D and Certification: Support aerospace material certification for FAA and international standards.
Typical test materials include seat foams, insulation panels, composite laminates, electrical housings, tubing, and other interior aircraft components.
Standards
The NexGen Burner supports compliance with multiple international aviation and safety standards:
BSS 7303 – Aerospace composite material combustion and heat release testing.
BSS 7323 – Aerospace material smoke generation and toxicity evaluation.
BSS 7387 – Aerospace material flame spread and combustion behavior testing.
AITM 2.0056 – Cone calorimeter heat release rate measurement.
AITM 2.0010 – Smoke generation measurement for aerospace materials.
AITM 2.0009 – Flame spread performance measurement for aerospace materials.
FAR Part 25 Appendix F Part II – Cabin material combustion, flame spread, and smoke toxicity testing.
FAR Part 25 Appendix F Part III – Cabin material flame spread and smoke performance measurement.
FAR Part 25 Appendix F Part VII – Cabin material heat release and combustion performance testing.
ISO 2685:1998 – Fire resistance testing methods for aerospace materials.
Domestic Standards: MH/T 6086. HB 7263. MH/T 6041. GB/T 25352. HB 7044 – Various fuel combustion and burn-through testing methods.
Parameters
| Parameter Category | Details |
|---|---|
| Dimensions | 20 mm (W) × 1150 mm (L) × 250 mm (D) |
| Weight | 10 kg |
| Flame Temperature | ≥ 2000 ± 50 ℉ |
| Flame Heat Flux | ≥ 10.6 W/cm² |
| Power Supply | 220 V, 5 A |
| Fuel Requirement | Aviation Grade 2 Fuel |
| Gas Requirement | Compressed air ≥ 120 psi |
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