FAA FAR Heat Release Rate Tester

NegotiableUpdate on 01/10

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Overview

Introduction to FAA FAR OSU Heat Release Rate Tester: The OSU heat release rate tester recognized by the Federal Aviation Administration (FAA) of the United States was initially designed by Smith from Ohio State University in 1972 and later became the FAA designated combustion testing instrument. Used to measure whether the materials inside the aircraft cabin can withstand an unexpected 35 kW/m2 radiation heat intensity, in compliance with FAR25.853 standard. The laboratory, control unit, and data acquisition and analysis software used in the development process of this instrument are all in accordance with Federal Aviation Administration

Product Details

FAA FAR OSUHeat release rate tester

Rate of heat release(OSU)

FAA FAR OSU Thermal Release Rate TesterModel: ME1200-1

FAA FAR OSU Thermal Release Rate TesterInstrument Introduction: Federal Aviation Administration of the United StatesFAAApprovedOSUThe initial design of the heat release rate tester was developed by Ohio State UniversitySmithexist1972Completed annually, later becameFAASpecify the combustion testing instrument.

FAA FAR OSU Thermal Release Rate TesterPurpose:OSUHeat release rate tester, used to measure whether the materials inside the aircraft cabin can withstand an unexpected 35 kW/m²Radiant heat intensity, in compliance with FAR25.853 standard. The laboratory, control unit, and data acquisition and analysis software used in the development of this instrument are all in accordance with Chapter 5 of the Federal Aviation Administration Fire Testing Manual. It mainly consists of three parts: test box, control unit, and data receiving and processing software.

FAA FAR OSU Thermal Release Rate TesterCompliant with standards:FAR Part 25 Appendix F Part IV、Airbus AITM 2.0006、Boeing BSS 7322.

FAA FAR OSU Thermal Release Rate TesterTechnical parameters:

1.Stainless steel combustion testing chamber, including high-temperature resistant glass observation window;

2.The thermal radiation source is4branchGlowbarsHeating rod, available35KW/M²Thermal radiation flux;

3.use2An independentPIDTemperature controller, used for heating temperature control;

4.Equipped with fully automatic pneumatic sample propulsion device and platform screen door device;

5.Equipped with an upper burner and a movable lower burner;

6.Rotary flowmeter can be used to adjust the gas flow rate of upper and lower burners;

7.Equipped with movableTType calibration burner device and flow controller;

8.Automatic application of mass flow controller for temperature calibration of thermoelectric stack;

9.A water-cooled heat flux meter is used to measure the heat radiation flux on the fire surface, equipped with a cooling method;

10.The airflow temperature control device can provide constant temperature and constant current airflow to the testing chamber;

11.Measure the flow rate and pressure entering the testing chamber using an orifice flowmeter;

12.Equipped with data acquisition system and heat release standard testing software;