• Journal of Korean Society of Environmental Engineers
• /
• v.35 no.12
• /
• pp.960-966
• /
• 2013

In this study, operation data from an actual plant in M city were analyzed to evaluate effects of water supply into sewage sludge on the co-incineration of municipal solid waste (MSW) and sewage sludge. Design capacity of the stoker incinerator is 50 m3/day. Maximum portion of sewage sludge in the total waste input was 20%. According to this research, moisture content increase up to 85% of sewage sludge could be possible by water supply on MSW input to the incinerator. Therefore, stable operation of incinerator could be achieved. As water was added into sewage sludge up to 85%, input quantity of sewage sludge to frequency (Hz) was similar to theoretical input. Also, it is concluded that stable management of incinerator without leachate combustion and damages of refractory bricks and castable could be achieved by the reduction of low heating value.

• Proceedings of the Korean Vacuum Society Conference
• /
• 2000.02a
• /
• pp.39-39
• /
• 2000

당사는 1996년 SPUTTERING SYSTEM 제작을 시작으로 하여 진공관련장치 및 부품을 제작, 납품하는 기업입니다. 그 동안 산업체 및 대학, 연구소 등에 제작 납품된 품목은 양산용SPUTTER 연구실험용SPUTTER, ION PLATING, RIE SYSTEM, E-BEAM 증착기 산업용 AL-EVAPORATOR, 산업용 AIP SYSTEM, 고온열처리로, 진공건조장치 진공 배기SYSTEM, 기타 진공관련장치가 있으며 진공부품으로는 OIL ROTARY PUMP, DIFFUSION PUMP, VALVE 및 배관부품 등이 있습니다. 그밖에 취급하는 품목으로는 진공게이지류 및 터보펌프를 판매하고 있습니다. 일부 장치는 기술력을 인정받아 일본, 동남아시아, 중국 등에 수출되었습니다. 당사는 항상 고객이 필요로 하는 진공응용장치를 다년간 축적된 제조기술과 연구력을 바탕으로 만족스러운 제품을 공급하고 있기에 이를 소개하고자 합니다.

• 월간 기계설비
• /
• no.5 s.202
• /
• pp.64-69
• /
• 2007

소형저장탱크의 보급으로 벌크로리 공급시스템이 확대되고 체계적인 수요관리가 가능해짐에 따라 LP가스산업의 발전에 많은 기여를 할 것으로 기대된다. 또한 500kg미만 소형저장탱크의 고압배관시공에 고압호스가 가능해짐에 따라 2006년 11월 소형저장탱크용 고압호스 성능인증기준이 제정되게 되었다. 새로 제정된 소형저장탱크용 고압호스의 성능인증 기준을 기술하여 고압호스제조업체, 소형저장탱크 시공업체 등의 관련업체에 참고자료가 되기를 바란다.

• Transactions of the Korean Society of Mechanical Engineers B
• /
• v.34 no.2
• /
• pp.213-218
• /
• 2010

A cooling system utilizing liquid helium to chill the cryopanel (800 mm $\times$ 700 mm dimensions) down to 4.2 K was designed, implemented, and tested to verify the role of the cryopanel as a heat sink for the payload of a spacecraft inside the large thermal vacuum chamber (effective dimensions : 8 m ($\Phi$) $\times$ 10 m (L)) of KARI (Korea Aerospace Research Institute). Two LHe (Liquid Helium) Dewars, one for the main supply and the other for refilling, were used to supply liquid helium or cold helium gas into this cryopanel, and flow control for the target temperature of the cryopanel within requirements was done through fine adjustment of the pressure inside the LHe Dewars. The return helium gas from the cryopanel was reused as a thermal barrier to minimize the heat influx on the core liquid helium supply pipe. The test verified a cooling time of around three hours from the ambient temperature to 40 K (combined standard uncertainty of 194 mK), the capacity for maintaining the cryopanel at intermediate temperatures, and a 1 K uniformity over the entire cryopanel surface at around 40 K with 20 W cooling power.

• Journal of the Korean Institute of Gas
• /
• v.14 no.6
• /
• pp.27-30
• /
• 2010

This paper presents the system design process of district community cooling system using LNG cold energy. The newly developed LNG cooling system includes several heat exchangers, LNG storage tank, thermal mass storage tank, several cold energy storage tanks, gas air-conditioners, compressors, constant pressure regulators, cold energy and hot energy supply pipes. In addition, the gas air-conditioner system is installed to supply not sufficient cold energy due to low level of city gas consumptions during a summer period. This system design is very effective and safe to supply cold energy mass of fresh air by exchanging two thermal masses of an air and 200kcal/kg cold energy of LNG. The district community cooling system with LNG cold energy does not produce CO2 and freon gases in the air.

• Proceedings of the KIEE Conference
• /
• 2011.07a
• /
• pp.732-734
• /
• 2011

본 논문에서는 [SPD와 Sensing 회로를 내장한 영상 전송 및 장애관리시스템 설계 및 구현에 대하여 기술하였다. STP 케이블을 이용하여 영상신호 및 제어신호, 장애정보신호, SPD신호로 총 4종류의 신호를 STP케이블 Pair별로 구성하여 장거리(2km) 전송하도록 하여 전송거리와 배관, 배선의 제약을 해결하였고, 경제성에서도 타 케이블 보다 우위를 점하고 있으며, 각각의 카메라별 전송신호 및 영상, 장애정보와 전원공급 및 SPD 상태, 감시와 녹화를 위한 각각의 장비별 전원공급 및 SPD 상태를 이력관리와 함께 관리할 수 있는 통합 관리프로그램으로 관리자가 수백대의 카메라를 효율적으로 관리할 수 있도록 설계 및 구현하였다.

• 유체기계공업학회:학술대회논문집
• /
• 2006.08a
• /
• pp.279-282
• /
• 2006

Upon a turbopump's running, cavitation may occur at the inlet of the LOx pump by pressure drop and heat transfer along the LOx feeding line. Since the cavitation can cause serious damage to the pump or to stop running, the absence of the cavitation at the inlet of a turbopump should be confirmed before the using the turbopump. In the present study, the calculation of the volume fraction of LOx gas phase at the inlet of the pump are performed with different temperatures of LOx in the tank, pressure drops and heat transfers along the feeding line. This calculation method can be applied to define the limits of thermal and hydraulic characteristics during the design of a LOx feeding system.

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2017.05a
• /
• pp.1112-1114
• /
• 2017

The liquid rocket engine determines the routing of the component placement and layout by adapted the cycle method, the hardware configuration, the gimbal type on the functional implementation, and so on. In this paper, the conceptual routing of major pneumatic lines such as helium (He) supply pneumatic line for driving, many purge pneumatic line and main ignition line based on the main components installed in the liquid rocket engine was performed.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.6 no.4
• /
• pp.37-45
• /
• 2002

The development process of KSR-III propulsion feeding system is subscripted. The purpose of propulsion feeding system is to feed a certain amount of propellant from propellant tank to engine by the end of combustion. Pressure-fed liquid rocket, KSR-III has the unique characteristics of both pressure regulator and cavitation venturi as a passive flow control device. Main parameters of feeding system are confirmed by both water test and CFD(전산유체) technique. Flow control effect with venturi is confirmed by water test. Initial stabilization characteristic of pressure regulator is confirmed by real propellant test. And, to avoid the effect of resonance between rocket and feeding system, this article deal with POGO(포고) analysis to the feeding system.

• Journal of the Korean Institute of Gas
• /
• v.21 no.5
• /
• pp.70-76
• /
• 2017

The standards related to the "Urban Gas Business Act" and the "Safety Control and Business Regulation of Liquefied Petroleum Gas Act" prescribe the separation distance between gas piping joint excluding welded joints and electric equipments(electric switch, watt meter, breaker, connector, etc). The "Korea Electro technical Regulation" also prescribes the distance between gas piping joints and electric equipments in accordance with the gas related standards. In case of the standards related to the "Urban Gas Business Act", the distance criteria stipulated in the standard of supplying facilities are different from those stipulated in the standard of using facilities. In this study, we have conducted pilot test on the possible ignition distance from the piping joint when LP gas is leaked from the point. We have also examined the adequacy of current standards on the separation distance between gas piping joint and electric equipments. As a result of the tests, we have found that ignition is able to occur at a distance of 30 cm as stipulated in the current standards or more when LP gas is leaked from the joint of the pipe. Therefore, we have made a decision that the criteria for separation distance between gas piping joint and electric equipment specified in the current standards related to the "Urban Gas Business Act" and the "Safety Control and Business Regulation of Liquefied Petroleum Gas Act" is appropriate.