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MEI/Marlin Engineering ME1500-3 & ME1700-3 NexGen Aviation Fuel Burner System for FAA-Compliant Aircraft Seat Fire Testing

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Brand MEI/Marlin Engineering
Origin USA
Manufacturer Type Authorized Distributor
Origin Category Imported
Model ME1500-3 + ME1700-3
Pricing Available Upon Request

Overview

The MEI/Marlin Engineering ME1500-3 and ME1700-3 NexGen Aviation Fuel Burner System is a fully FAA-recognized, next-generation combustion test apparatus engineered for regulatory compliance with U.S. Federal Aviation Regulations (FAR) and international aviation fire safety standards. Designed as the certified successor to discontinued legacy burners—including the Park DPL 3400, Lennox OB-32, and Carlin 200 CRD—the NexGen system preserves proven combustion physics while integrating precision instrumentation for real-time monitoring of fuel flow, air pressure, temperature, and thermal flux. It operates on controlled kerosene-based aviation fuel (Jet A or equivalent), generating a stable, repeatable flame characterized by a minimum peak temperature of 2000 ± 50 °F (1093 ± 28 °C) and a minimum incident heat flux of 10.6 W/cm²—both validated per ASTM E119 and FAA AC 25.853-1 calibration protocols. The system is purpose-built for vertical and horizontal flammability assessments of aircraft interior components, with primary application in seat cushion, seat back, and trim material qualification under FAR Part 25 subparts F and G.

Key Features

  • Corrosion- and high-temperature-resistant Inconel 600 alloy conical burner nozzle assembly, rated for continuous operation at >1100 °C
  • Integrated modular subsystems: precision fuel rail with solenoid shutoff valve, calibrated fuel pressure gauge (0–100 psi), thermocouple-monitored fuel temperature sensor (±0.5 °C accuracy), and regulated air supply manifold with adjustable damper (airflow range: 0–2.0 m³/min)
  • Dual-stage thermal conditioning: dual 0.14 m³ ice-bath reservoirs for independent control of fuel and combustion air temperature (maintained at 21 ± 2 °C per FAR 25.853 Appendix F)
  • Structural framework fabricated from powder-coated structural steel with integrated digital caliper scale (resolution: 0.1 mm) for repeatable burner-to-specimen distance verification
  • Movable specimen support carriage with motorized positioning and removable drip pan (stainless steel, 304 grade) for collection and gravimetric analysis of flaming drips
  • FAA-mandated thermal mapping configuration: seven grounded, ceramic-insulated, 30 AWG K-type (NiCr-NiAl) thermocouples (1.6 mm diameter, 0.254 mm OD sheath) mounted on a calibrated angle-iron comb fixture for standardized heat flux profile validation
  • Water-cooled radiometric heat flux sensor (calibrated to ±2% traceable to NIST SRM 2250) mounted on rigid cantilever bracket with thermal isolation bushings

Sample Compatibility & Compliance

The ME1500-3/ME1700-3 system supports full-spectrum aviation interior fire testing across multiple component classes: aircraft seat cushions and backs (FAR 25.853), thermal/acoustic insulation panels (FAR 25.855), cargo compartment liners (FAR 25.855), flexible/hard ducting assemblies (FAR 25.863), and electrical harnesses and connectors (FAR 25.867). It is fully compatible with test methodologies specified in FAA Advisory Circulars AC 25.853-1, AC 25.855-1, and AC 25.863-1, as well as harmonized national standards including MH/T 6086–2018, HB 7263–2015, MH/T 6041–2006, GB/T 25352–2010, and HB 7044–1994. All hardware and procedural workflows are designed to meet GLP-compliant documentation requirements and support 21 CFR Part 11–ready electronic audit trails when integrated with validated LIMS or test management software.

Software & Data Management

While the core burner operates as a stand-alone analog-controlled test rig, optional digital integration modules enable synchronization with third-party data acquisition systems (e.g., National Instruments DAQmx, Keysight PathWave) via IEEE 488.2 (GPIB) or RS-485 Modbus RTU interfaces. Real-time signals—including fuel pressure (4–20 mA), air temperature (Pt100 RTD), and thermocouple voltages (cold-junction compensated)—are logged at ≥10 Hz sampling rate. Calibration records, thermocouple placement maps, and flame geometry verification reports are stored in ISO/IEC 17025–compliant format. Firmware updates and configuration files adhere to DO-178C Level C software assurance guidelines for airborne systems.

Applications

This system serves as the primary fire-test platform for Tier 1 aerospace suppliers, FAA Designated Engineering Representatives (DERs), and independent certification laboratories performing qualification testing for EASA ETSO-C127, FAA TSO-C127, and SAE AS4694 compliance. Typical use cases include: pre-certification screening of flame-retardant polyurethane foams and aramid fabrics; comparative evaluation of intumescent coatings on composite seat shells; validation of fire barrier layer performance in multi-layer sandwich constructions; and root-cause analysis of ignition propagation mechanisms in hybrid seat structures containing metal, polymer, and textile substrates.

FAQ

Is this system approved by the FAA for official certification testing?

Yes—the ME1500-3/ME1700-3 NexGen Burner System is listed in FAA AC 25.853-1 Appendix B as an approved alternative to legacy burners and is routinely accepted by DERs and FAA ACOs for formal compliance submissions.

Can the system be configured for non-seat applications such as cargo liner or duct testing?

Yes—modular mounting interfaces, interchangeable specimen holders, and programmable airflow/fuel profiles allow reconfiguration for FAR 25.855, 25.863, and 25.867 test geometries without hardware modification.

What calibration documentation is provided with shipment?

Each unit ships with NIST-traceable calibration certificates for all sensors (fuel pressure transducer, RTDs, thermocouples, heat flux sensor), a full geometric verification report, and a flame temperature/heat flux profile map generated per ASTM E119 Annex A4.

Does the system support automated test sequencing and reporting?

While not bundled as standard, the system’s analog I/O and Modbus interface enable seamless integration with LabVIEW, MATLAB, or custom Python-based test orchestration platforms that generate ASTM E84-compliant summary reports and raw-data archives compliant with FAA Order 8110.4B.

Are spare parts and technical support available outside the U.S.?

MEI/Marlin Engineering maintains global distributor partnerships with certified service centers in Europe, APAC, and Canada; all critical consumables—including burner nozzles, thermocouple combs, and fuel filters—are stocked and shipped within 72 hours under ISO 9001:2015 quality controls.

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