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OSU Heat Release Auau Kaiwhakamātau

Whakaahuatanga Poto:

Ko te hei whakamatau auau tuku wera OSU whakaaetia e FAA o te Federal Aviation Whakahaere o te United States i tuatahi hangaia e Smith o Ohio State University i 1972, a muri mai ka he mea whakamātautau ngingiha FAA whakaritea mō te whakamatautau i te wera auau tuku o ngā rauemi Aeronautical.


  • Min.Order Rahi: 1 kōwae
  • Utu: whiriwhiringa
  • Pōkai: kahupapa Case
  • Tauira: SL833
  • Paerewa: AITM 2,0006, BSS 7322, FAR WĀHANGA 25 TĀPIRITANGA F Part IV
  • Taipitopito hua

    hua Tags

    OSU Heat Release Rate Tester Stainless Steel Combustion Test Chamber Equipped

    Mōhiohio Hua  o OSU hHeat Tuku Auau Kaiwhakamātau

    The OSU heat release rate tester approved by FAA of the Federal Aviation Administration of the United States was originally designed by Smith of Ohio State University in 1972, and later became a FAA designated combustion test instrument for testing the heat release rate of Aeronautical materials. The test standards are FAR Part 25 Appendix F Part IV, Airbus AITM 2.00. 06, Boeing BSS 7322.

    āhuatanga mahinga o OSU Heat Tuku Auau Kaiwhakamātau

    1. Stainless steel combustion test chamber with high temperature glass observation window;
    2. The heat radiation source is 4 Glowbars heating rods, which can provide 35KW/M2 heat radiation flux.
    3. Two independent PID temperature controllers are used for heating temperature control.
    4. Equipped with fully automatic pneumatic sample propulsion device and shielding door device;
    5. Equipped with upper burner and movable lower burner;
    6. Rotor flowmeter can be used to adjust the gas flow rate of upper and lower burners.
    7. Equipped with movable T-type calibration burner device and flow controller;
    8. Mass flow controller is applied to thermopile temperature calibration automatically.
    9. Water-cooled heat flow meter is equipped with cooling mode to measure the heat radiation flux of the fire surface.
    10. The air temperature control device can provide constant temperature and flow air for the test chamber.
    11. The orifice flowmeter is used to measure the flow pressure entering the test bin.
    12. Equipped with data acquisition system and heat release standard test software.

    Hua  tawhā of OSU Heat Release Rate Tester

     rahi  760mm (W) x 1850mm x (H) x 850mm (D)
     Taumaha  218KG
     whakaritenga hiko  220 V, 35 Amps
     ambient pāmahana  10 ℃ ki 35 ℃
     Houalotú Gas  Temperature tamau a Constant Gas nāianei
     hau ngingiha  mewaro
     Paerewa   AITM 2,0006, BSS 7322, FAR WĀHANGA 25 TĀPIRITANGA F Part IV
     tono  Aviation Materials

     


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