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中央真空系统
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《国外塑料》 2005年第2期74-74,共1页
位于巴特恩豪森的巴顿菲尔挤出技术有限公司最近生产了一套新的内测量型中央真空系统交付用户。在传统的系统中,每一个真空回路都自配一个大的可建立相同高压的计量泵,可是,每一次测量都需要调节外部进气量达到不同程度的真空。这种... 位于巴特恩豪森的巴顿菲尔挤出技术有限公司最近生产了一套新的内测量型中央真空系统交付用户。在传统的系统中,每一个真空回路都自配一个大的可建立相同高压的计量泵,可是,每一次测量都需要调节外部进气量达到不同程度的真空。这种方法不经济,而且新鲜空气进入时会形成很大的噪音。 展开更多
关键词 中央真空系统 计量泵 分压阀 塑料工业 生产设备
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Design of a New Type of Distribution Valve for Hydraulic Breaker and Analysis of Energy Consumption
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作者 ZHAO Hong-qiang 《Journal of China University of Mining and Technology》 EI 2006年第1期46-49,共4页
Energy consumed by distribution valves causes an energy loss for the output energy of hydraulic breakers, which has a significant influence on its efficiency. A new type of distribution valve used for hydraulic breake... Energy consumed by distribution valves causes an energy loss for the output energy of hydraulic breakers, which has a significant influence on its efficiency. A new type of distribution valve used for hydraulic breakers, de- signed to reduce energy consumption, is analyzed on the basis of the operating principle and energy loss of the current distribution valve. The new distribution valve adopts a cone valve and the optimization technique of unequal open de- gree for the valve port. Theoretical calculations and analyses have proven that the new distribution valve can reduce en- ergy loss by 9.0127J, or energy consumption by 31%, during an impact cycle and the efficiency of the hydraulic breaker can be raised by 4.5%. It has the following characteristics: little leakage, little pressure loss and low energy consump- tion. 展开更多
关键词 hydraulic breaker distribution valve energy loss
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Design and integrated simulation of a pressurized feed system of the dual-thrust hybrid rocket motor 被引量:9
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作者 LI JunHai YU NanJia +1 位作者 ZENG Peng CAI GuoBiao 《Science China(Technological Sciences)》 SCIE EI CAS 2013年第4期989-1000,共12页
A new pressurized feed system of the dual-thrust hybrid rocket motor for flight is presented in this paper.The feed system supplies 90% hydrogen peroxide (90%H 2 O 2) with two different flows of 4.5 and 2 kg s 1.The o... A new pressurized feed system of the dual-thrust hybrid rocket motor for flight is presented in this paper.The feed system supplies 90% hydrogen peroxide (90%H 2 O 2) with two different flows of 4.5 and 2 kg s 1.The oxidizer flow is changed through regulating the mass flow of the high-pressure gas and switching the performance modes of the unique oxidizer flow control valve simultaneously.The models of the gas storage container,pressure regulator valve,control orifice,propellant tank,oxidizer flow control valve and cavitating venturi are generated and used to compute the instantaneous pressure,temperature and mass flow rate.There is a good agreement between the simulated and experimental results.Parameter sensitivity analysis is also conducted.It is found that the throat diameter of the cavitating venturi in feed line 1 is the main factor affecting the mass flow in both boost and sustaining phase.Other parameters have limited effects on the mass flow rate and the transition time of the system. 展开更多
关键词 pressurized feed system mathematical modeling liquid propellant tank variable flow dual-thrust hybrid motor
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