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Created with Pixso. Aircraft Material Faa 25.853 Seat Piping Components Flame Combustion Tester

Aircraft Material Faa 25.853 Seat Piping Components Flame Combustion Tester

Marchio: GOLD
Numero di modello: GD-MHT6086
MOQ: 1 insieme
Prezzo: USD9000-9500/set
Tempo di consegna: 30 giorni
Condizioni di pagamento: L/C,T/T,Western Union,MoneyGram
Informazione dettagliata
Luogo di origine:
Cina
Certificazione:
ISO
Prodotto:
Tester per la combustione di fiamme di materiali aerospaziali
Standard:
Faa 25.853,MH/T 6086
Angoli del bruciatore:
0°, 45°, 90°
Powe massimo:
2000VA
Temperatura della fiamma regolabile:
Da 0 a 1100 ℃
Alimentazione elettrica:
CA 220 50/60Hz
misuratore di portata di calore:
campo di misura 0-17 W/cm2, precisione ±3%
Termocoppie di tipo K:
7 pezzi
Imballaggi particolari:
Imballaggio standard esportatore
Capacità di alimentazione:
5 set/al mese
Descrizione di prodotto
Aircraft Material Faa 25.853 Seat Piping Components Flame Combustion Tester
Product Overview

The Aircraft Material FAA 25.853 Seat Piping Components Flame Combustion Tester is a sophisticated testing system designed for evaluating the flame resistance of various materials used in aerospace applications. As aviation technology advances, the importance of comprehensive flame retardant performance testing has become increasingly critical.

This multi-functional combined testing bench performs relevant combustion tests on airborne equipment, accessories, and structural components within designated aircraft fire zones using large combustible gas burners and small-scale gas combustion. Test samples include cables, electrical connectors, hoses, and pneumatic components.

The latest second-generation burner has been completely redesigned according to the most recent FAA requirements, addressing issues with previous models including production discontinuation and temperature/heat instability. This advanced burner fully meets FAA requirements for combustion testing of different aircraft materials.

Aircraft Material Faa 25.853 Seat Piping Components Flame Combustion Tester 0
Compliance Standards
  • RTCA/DO-160G Section 26 - Fire Flammability Category A,B
  • Airbus AITM, Boeing BSS, and FAR Part 25
  • MH/T 6086 Burn-through test of aircraft cargo hold liner
Technical Specifications
Parameter Specification
Burner angles 0°, 45°, 90°
Air pressure regulator adjustment range 0-0.8 MPa
Power supply AC 220V 50/60Hz
Maximum power 2000 VA
Flame temperature adjustment 0 to 1100℃
Laboratory space requirements Longer than 6 meters, wider than 3 meters, and taller than 3 meters
Heat flow meter Measuring range 0-17W/cm², accuracy ±3%
Type K thermocouples 7 pieces
Aircraft Material Faa 25.853 Seat Piping Components Flame Combustion Tester 1 Aircraft Material Faa 25.853 Seat Piping Components Flame Combustion Tester 2
Key Features
Burner System
  • Constructed of stainless steel with main components including air pressure regulator, turbulence generator, combustion pipes, oil supply pipes, igniter, silencer, and conical nozzle
  • Equipped with imported American silencer to prevent harsh noise from high-speed airflow
  • Combustion pipes and oil supply pipes made of stainless steel, resistant to high temperatures and corrosion
  • Spark plug installed at nozzle with automatic ignition device for safety and ease of operation
  • Conical nozzle made of stainless steel, resistant to high temperatures, corrosion, and deformation
  • Equipped with laser level for precise observation and calibration of positions
  • Includes imported high-precision angle level for easy observation of burner rotation angle
Burner Support System
  • Precision-machined components, aesthetically pleasing and corrosion-resistant
  • Mounted on mobile platform with automatic movement to ignition, temperature calibration, heat flow calibration, and testing positions
  • Automatic angle adjustment for testing operations at 0°, 45°, and 90° angles
Mobile Platform
  • Welded from I-beams for stability and sturdiness
  • Equipped with electric guide rails and positioning switches for smooth movement and accurate positioning
  • Cable chain mechanism to protect control cables
  • All power and data cables packaged in cable chains for cleanliness and safety
Air Supply System
  • Stable air supply with touch screen control, clean and oil-free
  • High-flow solenoid valve for automatic air supply and shutdown
  • Flexible hose connection for easy movement with burner
  • Continuous supply of dry air with stable pressure and flow rate above 0.6 MPa during testing
  • Imported high-precision pressure regulating valve for 0-0.8 MPa regulation
Fuel Supply System
  • Consists of pressure stabilizing tank, fuel tank, oil filter, inlet flow meter, and solenoid valve
  • Stable fuel supply pressure and flow for complete fuel atomization
  • Fuel tank capacity for test time over 30 minutes (customizable)
  • High-purity nitrogen device with high-precision depressurization valve
  • Stainless steel high-pressure resistant gas tank and fuel storage tank
  • Liquid level alarm system for real-time fuel monitoring
  • Fuel filter, pressure sensor, and oil temperature sensor for parameter collection
  • Imported fuel nozzle for excellent atomization and stable flame
Aircraft Material Faa 25.853 Seat Piping Components Flame Combustion Tester 3
Laboratory Environment Requirements
  • Recommended laboratory space: minimum 6 meters long, 3 meters wide, and 3 meters high
  • Laboratory must be equipped with smoke extraction facilities
  • No airflow in laboratory - doors and windows should be closed during experiments to prevent burner thermal field disruption
  • Combustion chamber must be equipped with fire extinguishing facilities
  • Large air compressor and compressed air storage tank required
  • Nitrogen cylinders required