Thermal Acoustic Insulation Material Burn-through Resistance Test

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Thermal Acoustic Insulation Material Burn-through Resistance Test is used for measuring the burn-through resistance of thermal and acoustic insulation materials under high-intensity open flame. Its design and manufacture meet the requirements of GB/T25352-2010, FAR25 and the CCA Transportation Aircraft Standard CCAR-25-R4.

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(max file size 512 MB)

Specifications:-

Warranty:-1 year, 1 Year

Customized support:-OEM, ODM

Anemometer:-Vane type

Model Number:-D312

Power:-Electronic

Certification:-CSA, pock, Reach, IECEE, sock, UL, EPA, GS

Nominal fuel flow:-0.378 L/min

Application:-Insulation Material

Material:-SUS 304 Stainless Steel

Range of the heat flow meter 🙁 0~57) KW/m2

Standard:-ASTM C1696

Burner structure:-Gun type burner

Working power:-AC220V, 50HZ

 Main technical parameters
Laboratory The length and width of the test room should not be less than 3.05m.
Burner structure An improved gun type burner. The flame characteristics and appropriately adjusts fuel burner setting determines the pressure, and inlet airflow to achieve a suitable nozzle depth, stator position flame.
Nozzle The nozzle should be able to maintain fuel pressure to produce a nominal fuel flow of 0.378 L/min.
Fuel rail The motor and adjust the operation of the fuel rail so located 8 mm away from the front end of the guide rail are that the fuel nozzle is used to automatically outlet fixing piece. The outlet fixing piece should be installed at the end of the ventilation pipe.
Internal fixed piece The inner in the middle of the ventilation fixed piece is located pipe, 95mm away from the tip of the fuel nozzle. Adjust duct, the entire igniter is located between 10 o’clock the tab so that when viewed in the air and 11 o’clock.
Fan The fan has a diameter of 133mm and a height of 89mm. The power is 120W.
Burner cone The burner the end of the vent tube and has a length extension cone is mounted at of (305 ± 3) mm. The wide (280 ± 3) mm, high (152 ± 3) mm burner cone should have opening.
Fuel It is JP-8, Jet A equivalent fuel. The flow rate should aviation fuel or internationally be (0.378 ± 0.0126) L / min. If, the No. 3 jet fuel or other equivalent fuel may be used when the fuel is not available the fuel nominal flow, temperature and heat flow values meet the requirements of 6.4 and 6.5 of the GB/T 25352-2010 standard.
Fuel pressure regulator The fuel pressure regulator should provide a nominal flow of 0.378 L/min. A nozzle with a nominal flow rate of 0.378 L/min and an 80° injection angle provides a flow rate of 0.378 L/min at a fuel pressure of 0.71 MPa.

 

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What is ASTM test method?

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ASTM is a national methods for petroleum and organizations. ISO is an international organization that has methods for petroleum and representations from all countries including ASTM. ISO the standards of testing materials with global establishes documents and updates consensus from associated national the experts of the organizations.