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電炸裝置分析儀

UNIVERSAL CUSTOMIZED SYSTEM FOR ROCKET MOTORS TESTING 型號:EDA
EDA電炸裝置分析儀是一種通用測量和控制裝置,用於精確定義高能量材料或爆炸裝置樣品的點火,並同時高速測量動態壓力、溫度和發射光。

EDA 可精確調節點火電流值和時間,以產生精確的恒定電流、電壓或功率脈衝。可記錄和評估最大壓力、燃燒時間、點火延遲時間、電流和電壓位準、壓力梯度、壓力上升時間和/或燃燒速率。
  • EDA™ 電炸裝置分析儀是一種通用測量和控制裝置,用於精確定義高能量材料或爆炸裝置樣品的點火,並同時高速測量動態壓力、溫度和發射光。

    EDA 可精確調節點火電流值和時間,以產生精確的恒定電流、電壓或功率脈衝。可記錄和評估最大壓力、燃燒時間、點火延遲時間、電流和電壓位準、壓力梯度、壓力上升時間和/或燃燒速率。
     

    應用

    EDA 是在高壓釜試驗儀(TSV 系列和HPA 1500)中進行火砲和火箭推進劑彈道實驗以及在研究、開發、品質控制、鑑定和監視計劃中測試電起爆裝置(保險插銷、手榴彈、雷管等)的必要分析儀。

    世界各地的爆炸物和汽車產業、研發和品質控制實驗室都信賴 EDA 的精確性和可靠性。


    優勢和特點

    • 結構緊湊,既可實現正確點火,又可進行高速測量。
    • 精確的電流源,確保精準上升時間。
    • 測定點火元件的橋絲電阻。。
    • 調節點火電流、電壓或功率位準以及脈衝持續時間。
    • 提供兩種不同的控制裝置,分別用於不同的應用場合。
    • 用於靜態和動態測量的應變規感測器,或用於壓力、動力、加速度等動態測量的壓電感測器。
    • 可安裝溫度感測器和發射光感測器。
    • ABSW™ 軟體用於校正、測量、控制脈衝電流源和結果評估。


    有兩種基礎版本的 EDA 分析儀可供選擇:

    版本 EDA *) EDA Light
    電流上升時間 ≤ 20 μs ≤ 50 μs
    最大輸出電流和電壓 10 A / 20 V 11 A / 22 V
    點火電流和電壓的測量和記錄 YES NO
    可選輸入端數量 2 4
    電流流量觸發訊號 是,可根據記錄訊號進行調整 是,僅開/關
    典型應用 測試電點火器和雷管,測量點火電壓
    和電流
    透過量測高壓釜中的燃燒壓力來測試
    高能量材料

    *)根據要求而提供。

    評估前不同無煙火藥在高壓釜 (密閉容器 )內的
    燃燒壓力-時間曲線
    評估點火器的延遲時間 - 兩個壓力值以及
    點火電壓和電流

     

    評估Vivacity 與推進劑燃燒質量比的關係  評估壓力梯度與壓力的關係

     

    合規 

    • EN 13763-16
    • EN 13763-17
    • EN 13763-18
    • EN 13763-19
    • EN 13763-20
    • EN 16265
    • ISO 14451-2
    • SAE/USCAR 28
  • The EDA™ Electro-explosive Devices Analyzer is a universal measuring and control unit serving for precisely-defined ignition of samples of energetic materials or explosive devices, combined with the simultaneous high-speed measurement of dynamic pressure, temperature and emitted light.

    The EDA allows for precise adjustment of ignition current value and time for generation of precise constant current, voltage or power impulse. Maximum pressure, burning time, ignition delay time, current and voltage levels, pressure gradient, pressure rise time and/or the burning rate may be recorded and evaluated.
     

    APPLICATIONS

    The EDA is a necessary accessory for ballistic experiments with gun and rocket propellants in closed vessels (TSV Series and HPA 1500), as well as for testing electric initiators (fuse-heads, squibs, detonators etc.) in research, development, quality control, qualification and surveillance programs. The explosive and automotive industry, research, development and quality control laboratories around the world rely on the EDA for its precision and reliability


    ADVANTAGES & FEATURES

    • Compact solution for both proper ignition and high-speed measurement
    • Precise current source with guaranteed rise time
    • Determination of bridge-wire resistance of ignition elements
    • Adjustment of ignition current, voltage or power level and impulse duration
    • Two different control units designed for different applications available
    • Strain-gauge transducers for static and dynamic measurements or piezoelectric transducers for dynamic measurements of pressure, force, acceleration etc. 
    • Temperature and emitted light sensors available for incorporation
    • The ABSW™ software for calibration, measurement, control of the pulse current source and results evaluation


    There are two basic versions of EDA analyzer available: 

    Version EDA *) EDA Light
    Current rise time  ≤ 20 μs ≤ 50 μs
    Max output current
    and voltage 
    10 A / 20 V 11 A / 22 V
    Measurement and recording
    of ignition current and voltage  
    YES NO
    No of optional inputs 2 4
     Current flow trigger signal   YES,
    adjustable from recorded signal
    YES,
    ON/OFF only
    Typical applications  Testing of electric igniters and detonators
    with measurement of ignition voltage and current
    Testing of energetic materials by
    measurement of burning pressure in the closed vessels

    *)  On request only

     

     Burning pressure-time profiles of different smokeless powders
    in a closed vessel before evaluation
    Evaluation of a delay time of an igniter – two pressure
    values, together with the ignition voltage and current

     

     Evaluated dependence of Vivacity on the propellant burnt mass ratio  Evaluated dependence of the pressure gradient
    on pressure

     

    COMPLIANCE 

    • EN 13763-16
    • EN 13763-17
    • EN 13763-18
    • EN 13763-19
    • EN 13763-20
    • EN 16265
    • ISO 14451-2
    • SAE/USCAR 28