کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
731204 1461528 2015 8 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Experimental investigation of heat conduction performance and development of automatic temperature measurement device on modular artillery charge system
ترجمه فارسی عنوان
بررسی تجربی عملکرد هدایت حرارتی و توسعه دستگاه اندازه گیری دما اتوماتیک بر سیستم بارگیری مدولار توپخانه
کلمات کلیدی
دستگاه اندازه گیری دما اتوماتیک، سیستم اتوبوس مدولار، عملکرد هدایت حرارتی، نظریه مشابهی
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی کنترل و سیستم های مهندسی
چکیده انگلیسی


• We construct a measurement system with real-time data collection function.
• We examine experimentally thermal performances of modular artillery charge system.
• We develop a non-contact automatic online temperature measurement device.
• A non-contact measurement method is proposed to obtain modular charge temperatures.

The heat conduction performance experiment is conducted on the modular artillery charge system (MACS). Utilizing the experimental measurement system, the change history of the modular charge temperature is obtained. On the basis of the heat conduction performance experiment of modular propellant charge, an unsteady-state heat conduction model describing the temperature change of the MACS is built and the finite-difference implicit schemes are theoretically deduced using the volume equilibrium method for numerical simulation. The validation of the numerical model is checked through compared with the experimental results. An automatic online temperature measurement device on the MACS is developed, based on the non-contact measurement method which is proposed in this paper. As a part of the device, an initial charge temperature sensor (ICTS) is also developed according to the similarity principle. The temperature measurement device where the numerical codes are embedded is assembled in the turret to calculation successively the temperature change of the modular charge with the environment temperature of ammunition rack. Meanwhile, for trajectory calculation and firing data correction, the temperature information obtained from the device may be simultaneously transferred to the gunner task terminal computer through a Controller Area Network (CAN) bus interface.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Measurement - Volume 59, January 2015, Pages 88–95
نویسندگان
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