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低燃温
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  low flame temperature
    Effects of Carbon Black on Burning properties of Plateau Double Base Propellant with Low Flame Temperature
    炭黑对低燃温双基平台推进剂燃烧性能的影响
短句来源
    Adjustment on the Combustion Performance of Low Flame Temperature and Low Burning Rate Double Base Propellant
    低燃速低燃温双基推进剂燃烧性能的调节
短句来源
    The Catalytic Combustion of DB Propellant with Low Burning Rate and Low Flame Temperature
    低燃速低燃温双基推进剂的催化燃烧
短句来源
    A Non-lead Catalyzed Nitramine Modified Double Base Propellant with Low Burning Rate and Low Flame Temperature
    一种非铅催化硝胺改性双基低燃速低燃温推进剂
短句来源
    The combustion performance, thermal decomposition, and quenched surface appearance and element distribution of double-base (DB) propellant containing general lead and copper salt catalysts with low burning rate and low flame temperature were investigated.
    研究了含普通铅、铜盐催化剂的低燃速、低燃温双基推进剂的燃烧性能、热分解性能及熄火表面形貌特征和元素分布。
短句来源
更多       
  low flame temperature
    Effects of Carbon Black on Burning properties of Plateau Double Base Propellant with Low Flame Temperature
    炭黑对低燃温双基平台推进剂燃烧性能的影响
短句来源
    Adjustment on the Combustion Performance of Low Flame Temperature and Low Burning Rate Double Base Propellant
    低燃速低燃温双基推进剂燃烧性能的调节
短句来源
    The Catalytic Combustion of DB Propellant with Low Burning Rate and Low Flame Temperature
    低燃速低燃温双基推进剂的催化燃烧
短句来源
    A Non-lead Catalyzed Nitramine Modified Double Base Propellant with Low Burning Rate and Low Flame Temperature
    一种非铅催化硝胺改性双基低燃速低燃温推进剂
短句来源
    The combustion performance, thermal decomposition, and quenched surface appearance and element distribution of double-base (DB) propellant containing general lead and copper salt catalysts with low burning rate and low flame temperature were investigated.
    研究了含普通铅、铜盐催化剂的低燃速、低燃温双基推进剂的燃烧性能、热分解性能及熄火表面形貌特征和元素分布。
短句来源
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  low flame temperature
At low flame temperature, however, nanoparticles are not formed and the particle morphology is similar to the morphology produced by the conventional spray pyrolysis.
      
Generally, conditions of low flame temperature, combined with high air temperature and high relative humidity produce the greatest attenuation.
      
This is mainly due to the low flame temperature caused by the high EGR rate.
      
  low flame temperature
At low flame temperature, however, nanoparticles are not formed and the particle morphology is similar to the morphology produced by the conventional spray pyrolysis.
      
Generally, conditions of low flame temperature, combined with high air temperature and high relative humidity produce the greatest attenuation.
      
This is mainly due to the low flame temperature caused by the high EGR rate.
      
  low combustion temperature
When the reaction is ignited a second time in the combusted region or the preheating region, part of the specimens cannot be completely synthesized due to the low combustion temperature.
      
A relatively low combustion temperature reduces the decomposition of minerals and the volatilization of metals.
      
Explain how FBC Boiler operates the low combustion temperature 4.
      
Lean burning means that the HCCI engine cannot create particulates, and the low combustion temperature limits thermal NOx to 0.1-2 ppm.
      
The low combustion temperature also results in minimal NOx formation.
      
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The influence of carbon black (CB)on burning properties of plateau double base propellant with low flame temperaure has been researched by the experiment. It is shown that with the content of CB raised,the burning rate of the propellant is increased and their plateau (or mesa) zone translate into higher pressure;But with the content of CB raised continuouslly more than a centain content,the burning rate is decreased and the plateau zone disappears.In the paper this phenomenon is explained theoretically and the...

The influence of carbon black (CB)on burning properties of plateau double base propellant with low flame temperaure has been researched by the experiment. It is shown that with the content of CB raised,the burning rate of the propellant is increased and their plateau (or mesa) zone translate into higher pressure;But with the content of CB raised continuouslly more than a centain content,the burning rate is decreased and the plateau zone disappears.In the paper this phenomenon is explained theoretically and the relationship of the content of CB with the burning rate is fit.

研究了炭黑对低燃温双基平台推进剂燃烧性能的影响。指出随着炭黑含量的增加,推进剂燃速也增加,平台或麦撒燃烧区向高压移动;但当炭黑达到某一含量后,炭黑含量再增加,燃速反而下降,平台燃烧区消失。对此现象作了理论解释,并用二次多项式拟合出炭黑含量与燃速的关系。

This paper discusses the reduced smoke propellant of HTBP applied to air-to-air missile rocket motors.This propellant include medium combustion rate,low microwave attenuation of exhaust, optimum mechanical property at-40~70℃. Temperature impact and temperature cycles tests,aerodynamical heationg have been verified,The results show that this propellant is stable and reliable for air-to-air missiles.

研究了应用于空空导弹发动机中的一种少烟、低燃温下羟推进剂。推进剂具有中等燃速、微波衰减量低、在+70—-40℃内具有优良的力学性能,经受了测试冲击、温度循环、气动加热及各种环境考验。试验证明:该推进剂性能稳定、可靠。

To meet the special requiremets of the gas generator and pyrotechnie starter, a propellantformula,composed of GAP as binder and sphcrical phase-stabilized AN as oxidizer, is rescarched andprepared. The formula for gas generator is fuel-riched with clean exhaust, lower comhustiontemperature,lower residue and less smoke. Its burning rate is 2. 3-5. 8mm/s and burning rate pressureexponent 0. 55,combustion temperature lower than 1 200℃, combustion residue 2. 894. Its mechanicalproperties are also met the use requirements....

To meet the special requiremets of the gas generator and pyrotechnie starter, a propellantformula,composed of GAP as binder and sphcrical phase-stabilized AN as oxidizer, is rescarched andprepared. The formula for gas generator is fuel-riched with clean exhaust, lower comhustiontemperature,lower residue and less smoke. Its burning rate is 2. 3-5. 8mm/s and burning rate pressureexponent 0. 55,combustion temperature lower than 1 200℃, combustion residue 2. 894. Its mechanicalproperties are also met the use requirements.

为了满足火药起动器、燃气发生器的特殊要求.研制了一种排气洁净,无烟、无腐蚀、低燃温、低残渣的富能燃气发生剂配方。这种燃气发生剂以聚叠氦缩水甘油醚(GAP)为粘合剂.球形、相稳定的改性硝酸按(PSAN)为氧化剂。该燃气发生剂热稳定性好.在大气中燃烧无可见烟雾.燃速为2.3~5.8mm/s.燃速压强指数为0.55.燃温小于1200℃,燃烧残渣含量为2.8%。力学性能满足使用要求。

 
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