• Title/Summary/Keyword: Head cooling

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Design and Fabrication of a Conductively Cooled Cryostat by Cryocooler (냉동기 부착형 전도냉각식 Cryostat의 설계 및 제작)

  • Bae, Joon-Han;Sim, Ki-Deck
    • The Transactions of The Korean Institute of Electrical Engineers
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    • v.56 no.11
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    • pp.1921-1924
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    • 2007
  • In order to measure the superconducting transition temperature, the critical current and the alternating current(AC) loss on short samples of high temperature superconductor, a cryocooler cooled cryostat has been designed and built. Two closed-cycle coolers provide cooling with an ultimate sample temperature below 16K. Temperature regulation is provided by 50W of electrical heater that opposes the cooling power from the cold heads. Temperature control feedback is by means of a cernox temperature sensor co-located with the heaters on the second stage of the cold head. Additional temperature sensors are located on the sample mount(B1), on the CVI cold head(B2) and on the Dakin cold head(B3). AC losses on the sample high temperature superconductor were measured at 30K so that the developed device performance was evaluated. In this paper, the design, fabrication and test results on the cryocooler cooled cryostat are presented.

Design of Hall Sensor based Electronic Engine Cooling System (홀 센서 기반 전자식 엔진냉각제어 시스템 설계)

  • Koh, Young-Ho;Kim, Hyun-Hee;Lee, Kyung-Chang
    • Journal of the Korean Society of Industry Convergence
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    • v.20 no.4
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    • pp.325-332
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    • 2017
  • The engine cooling system is a device that maintains the temperature in the engine room at an appropriate level by driving a cooling fan when the temperature in the engine room generated during the vehicle operation occurs over a certain temperature. In recent years, the vehicle cooling system has changed to an electronic system. Therefore, in this paper, we design and develop a hall sensor based electronic engine cooling system. In this paper, a hall sensor module and an actuator module for engine cooling control system are designed. In order to verify the performance of the designed module, the magnetic field control was verified through the simulation of the diameter and the head of the coil.

Cooling Design and Flight Test for Airplane Reciprocating Engine (항공기 왕복엔진 냉각설계 및 인증시험)

  • Lee, Kangyi;Park, Jonghyuk;Park, Sunghwan
    • Journal of Aerospace System Engineering
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    • v.6 no.2
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    • pp.35-41
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    • 2012
  • A reciprocating engine installed on a normal category airplane shall be effectively cooled by air flown through the engine compartment. A airplane powerplant designer has to design cooling air inlets, baffles, seals, and outlets to maintain cylinder head temperatures and oil temperature under the limits, and show compliance with appropriate airworthiness standard. In this study, cooling designs of the installed engine and compliance requirements applicable to the cooling designs were reviewed, and engine cooling flight test results were evaluated for design changes. Engine cooling certification test will be conducted in a next step.

Reliability Evaluations for Shear Strength of Resistance Welded Ball Stud according to Different Cooling Methods

  • Park, In-Duck;Nam, Ki-Woo
    • Journal of Power System Engineering
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    • v.22 no.6
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    • pp.44-50
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    • 2018
  • As a type of bolt with a spherical head, the ball stud is widely used as a part of a ball joint in steering or suspension systems in automobiles. Balls and studs are subjected to heat treatment suitable for each material; in particular, the shear strength of the ball stud must meet the specifications of the production company. This study evaluated the shear strength of joints according to the cooling method of ball studs subject to resistance welding. The shear stress of water cooling was higher than that of air cooling (as-received material). Note, however, th at oil cooling showed lower stress than that of as-received. When judged by standard deviation, mean, and coefficient of variation according to the arithmetic statistics and shape parameter as well as scale parameter, oil cooling is suitable.

Specific Impulse Variation of a Liquid Rocket Engine by Film Cooling (막냉각에 의한 액체로켓엔진의 비추력 변화)

  • Cho, Won-Kook;Park, Soon-Young;Seol, Woo-Seok
    • Aerospace Engineering and Technology
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    • v.8 no.2
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    • pp.133-139
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    • 2009
  • An analysis has been performed on the specific impulse for a liquid rocket engine of gas generator cycle. The present analysis method has been validated through the comparison of the optimal specific impulse for the 300t thrust conceptual engine against the published data. The engine specific impulse can be increased by applying film coolant decreasing the fuel pump head for regenerative cooling despite the decrease of specific impulse of the combustion chamber when the film coolant participates combustion more than the critical amount. The improved condition shows that higher combustion chamber pressure is achieved with less fuel pump head rise by additional film cooling.

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Permissible Safety Limits in Local Cooling Focused on the Parts of Human Body (신체 부위별 냉각허용한계온도에 관한 연구)

  • Hwang, Kyoung-Sook;Choi, Jeong-Wha;Kim, Kyung-Ran
    • Journal of the Korean Society of Clothing and Textiles
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    • v.31 no.1 s.160
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    • pp.119-130
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    • 2007
  • The objects of this study were to investigate responses and peculiarity during local cooling by parts of the human body and to show permissible safety limits without injurious to his health because of excessive cooling when he works hot environments. It were measured rectal temperature, skin temperature, heart rate, total body weight loss, local sweat in back and thigh, clothing microclimate and subjective sensation on 8 subjects and cooling parts were head, neck, chest, abdomen, back, waist, hip, upper arm, forearm, hand, thigh, calf and foot. According to above-mentioned the first experiment, we chose permissible safety limits by parts of the human body for one hour. In the second experiment, it was showed permissible safety limits by parts which examined their safety about health through 4 hours cooling test on 3 subjects. The results are as follows: 1. As a result of the first experiment, we chose permissible safety limits by parts, as follows, head $25^{\circ}C$, neck $20^{\circ}C$, chest $27^{\circ}C$, abdomen $25^{\circ}C$, back $20^{\circ}C$, waist $20^{\circ}C$, upper arm $20^{\circ}C$, forearm $20^{\circ}C$, hand $23^{\circ}C$, thigh $20^{\circ}C$, calf $20^{\circ}C$ and foot $23^{\circ}C$ in $37^{\circ}C$, 50%R.H. environment for 1 hour. 2. As a result of the second experiment, cooling on these safety limits temperatures except chest didn't have a bad effect on health. So it was proved that right permissible safety limits of chest was $28^{\circ}C$. From these results, it has been suggested that skin temperature didn't fall below permissible safety limits when human body was to be cool by parts.

Numerical and Theoretical Study on the Fluid Flow in the Cooling System of a Marine Diesel Engine (선박용 디젤엔진의 냉각수 유동에 대한 수치해석적 및 이론적 연구)

  • Suh, Yong-Kweon;Heo, Seong-Gyu;Chung, Sung-Sik
    • Journal of Advanced Marine Engineering and Technology
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    • v.32 no.1
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    • pp.119-130
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    • 2008
  • Diesel engine is one of the most expensive and important components in a ship. Many researchers are interested in increasing the performance of diesel engines. Design of an optimum cooling system should also contribute to the enhancement of the performance as well as the efficiency of engines. In this study, we investigated the flow pattern within the cooling system of a marine diesel engine by using numerical simulation prior to the study of the heat-transfer problem. The engine cooling system is composed of five cooling units each unit containing a water-jacket and a cylinder head. Based on the calculated data, we also conducted theoretical analysis that can predict the flow-rate delivery in each of the five units.

Study on Cooling Charcteristics of Forced Evaporation by using Steam Ejector (스팀 에젝터에 의한 강제 증발 방식의 냉각 특성에 관한 연구)

  • Son, H.J.;Lee, Y.H.;Kim, Y.G.;Jeong, H.M
    • Journal of Power System Engineering
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    • v.10 no.2
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    • pp.41-46
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    • 2006
  • This study shows a water cooling system by using a steam ejector and jet condenser to drop the temperature of the water by about $5^{\circ}C\;from\;25^{\circ}C$ or higher. In this research, to replace the present water cooling system, we focused on a water cooling system by latent heat of evaporation, thus this system needs a vacuum pressure to evaporate the water in enclosed tank. The water cooling effects are depended on the vacuum pressure in the enclosed tank, and the cooling water is generated by latent head of evaporation. As the experimental results, the absolute vacuum pressure obtained was about $5{\sim}8$ mmHg using a steam driven ejector with jet condenser.

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Fatigue Life Analysis and Cooling Conditions Evaluation of a Piston for Large LPLi Bus Engines (LPG 액정분사식 대형 버스용 엔진 피스톤의 피로수명 해석과 냉각조건 평가)

  • 최경호;이부윤
    • Journal of Advanced Marine Engineering and Technology
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    • v.28 no.5
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    • pp.762-772
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    • 2004
  • Fatigue life of a Piston for large liquid Petroleum liquid injection(LPLi) bus engines is analyzed considering effects of cooling condition parameters : temperature of cooling water, and heat transfer coefficients at oil gallery and bottom surface of piston head. Temperature of the piston is analyzed with varying cooling conditions Stresses of the piston from two load cases of pressure loading. and pressure and thermal loading are analyzed Fatigue life under repeated peak pressure and thermal cycle is analyzed by the strain-life theory. For the two load cases, required loading cycles for engine life are defined, and loading cycles to failure and partial damages are calculated. Based on the resulting accumulated fatigue usage factors, endurance of the piston is evaluated and effects of varying cooling condition Parameters are discussed.

Evaluation of the operating reliability on the concurrent heating-cooling system air conditioner for different refrigerant flow rates with high-head and long-line conditions (동시냉난방 시스템 에어컨의 냉매량 변화에 따른 고낙차 장배관 운전 신뢰성 평가)

  • Lee, Seung-Chan;Kim, Tae-An;Tae, Sang-Jin;Jung, Gyoo-Ha;Moon, Je-Myung;Kim, Youn-Jea
    • Proceedings of the SAREK Conference
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    • 2008.11a
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    • pp.304-309
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    • 2008
  • The heating and cooling performances of system multi-air conditioner for various refrigerant flow rates with high-head and long-line conditions are experimentally investigated. The maximum head and tube length were 110 m and 1000 m, and the two different adjustments of refrigerant flow rates were +20 % and -20 %, respectively. The experimental system was composed of 4 outdoor units with module systems, and 13 indoor units which were joined with the mode change unit by single-tube circuit. Field tests without indoor and outdoor temperature control were performed in a general office building with two different refrigerant flow rates. Especially, the oil level in the compressor was normally maintained at the safety zone. Experimental results were prepared on the p-h diagram.

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