• 제목/요약/키워드: Engine trouble

검색결과 40건 처리시간 0.026초

가솔린 엔진 배출가스 제어장치에 대한 고장사례 고찰 (Study of Failure Examples for Emission Gas Control System in Gasoline Engine)

  • 이일권;이정호;이영숙;염광욱;한재오;임하영
    • 한국가스학회지
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    • 제20권6호
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    • pp.37-42
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    • 2016
  • 이 논문의 목적은 승용자동차의 배출가스 제어장치에 대한 고장사례 연구이다. 첫 번째 사례의 원인은 퍼지 컨트럴 솔레노이드밸브(PCSV)가 일정한 동작조건에서 열리지 말아야 하나, 오작동 되어 열림으로써 서지탱크로 증발가스가 유입되어 이것이 연료량이 농후한 것으로 측정되었다. 이 결과 엔진의 ECU(Electronic control uint)에서 연료의 분사량을 줄임으로써 공회전시 엔진의 부조화 현상이 발생된 것으로 확인되었다. 두 번째 사례에서는, EGR 밸브를 작동하는 호스가 다른 곳으로 조립되어 진공압력이 공급되지 않았다. 이로 인해 EGR 밸브가 작동되지 않고 다른 곳에서 진공이 누설됨으로써 엔진이 부조화 현상이 발생된 것으로 확인되었다. 세 번째 사례는 두개의 센서 가운데 뒤쪽(Rear side) 산소센서가 다른 자동차의 산소센서로 오장착됨으로 인해 산소량을 감지하지 못해 감속시 급격하게 속도가 줄어든 것으로 확인되었다. 따라서, 배출가스 제어 장치에 관련된 시스템은 최적의 상태로 작동되어 배출가스를 저감하는 역할을 할 수 있도록 철저한 관리가 요구된다.

Automatic Flight Path Control of Small Unmanned Aircraft with Delta-wing ICCAS 2004

  • Nagata, Masanobu;Kumon, Makoto;Kouzawa, Ryuichi;Mizumoto, Ikuro;Iwai, Zenta
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2004년도 ICCAS
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    • pp.1386-1391
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    • 2004
  • It is known that an aircraft with delta-wings which are attached to the body at a large angle like a kite or a hang glider has a measure of maneuverability and stability. Aircrafts of this kind can fly stably. Even if engine trouble occurs, it will not fall and might be able to land. In this paper, one of the conventional control methods, PID control, is applied to the aircraft with LQ local control block. This is based on an idea that the aircraft flies so stably that the automatic control system might be realized by a simple controller. The proposed PID controller consists of several sub-controllers which are constructed to each system neglecting the interference. In addition, the LQ control is involved as a local loop of the aileron and rudder control in order to increase stability of the attitude when circling. The effectiveness of the proposed method is shown through 3D computer simulations and experiments of the flight path control.

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수중 용접봉으로 용접한 누수배관 용접부위의 부식 특성 평가 (Evaluation of Corrosion Characteristics on Welding Zone of Leakage SeawaterPipe Welded by Underwater Welding Electrode)

  • 문경만;이성열;김윤해;이명훈;김진경
    • Journal of Advanced Marine Engineering and Technology
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    • 제32권8호
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    • pp.1240-1247
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    • 2008
  • Leakage trouble on the sea water pipeline in engine room is often resulted from a localized corrosion due to severe corrosive environment caused by both high speed and high pressure of sea water flowing through the inner pipe. In addition, when the ship is in stand-by or emergency condition, underwater welding to control the leakage of sea water from a hole of its pipe is very important in an industrial safety point of view. In this study possibility of underwater welding to control leakage of sea water and corrosion property of its welding zone were investigated with the electrochemical methods by parameters of welding methods and welding electrodes when underwater welding is achieved with a such case that sea water is being leaked out with a height at 50mm from a hole of $2.5mm{\emptyset}$ of test pipe. Corrosion resistance of weld metal zone is better than the base metal and its hardness is higher than that of the base metal. However corrosion potential of weld metal zone showed a negative value than that of the base metal, therefore weld metal zone is preferentially corroded rather than the base metal by performance of galvanic cell due to difference of corrosion potential between weld metal zone and base metal. Eventually it is suggested that leakage of sea water is successfully controlled by underwater welding,

자동차 자가진단과 디지털 홈 네트워크 가전제어를 위한 임베디드 리눅스 시스템 (Embedded Linux System for Car Self-Care-Control and Digital Home Network Appliance Control System)

  • 김국세;방선광;허진;안성수;이준
    • 한국정보통신학회:학술대회논문집
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    • 한국해양정보통신학회 2007년도 춘계종합학술대회
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    • pp.690-694
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    • 2007
  • 본 논문은 Wibro 시대를 맞아 차량내에서 인터넷이 가능하고 다양해지는 자동차 시스템에 적응하고 사용자가 자동차를 스스로 진단하고 이상이 생겼을 때 스스로 판단하여 자동차 정비소에 갔을 때 정확한 판단을 하여 신속하게 처리 할 수 있게 해 주며 자동차에 대해서 잘 모르는 운전자에게 정확한 정보를 제공한다. 주행 중에 자가 진단을 위해 임베디드 리눅스 시스템을 구축하고 자동차 와 진단 시스템의 통신을 위해 CAN과 RS232 통신을 통해 임베디드 리눅스 시스템과 통신을 한다. 또한 Wibro 시대를 맞아 디지털 흠 네트워크 가전들을 내장된 무선 네트워크와 ZigBee 시스템을 통해 언제 어디서나 웹을 통해 접근, 컨트롤 하는 임베디드 리눅스 시스템을 구축한다. 본 임베디드 리눅스 시스템은 초 경량화와 가격대비 성능 및 사용자 UI에 맞춰 시스템 구성하여 안정되고 호환성 높은 시스템을 구축한다. 그리고 미디어 플레이와 웹서버를 포팅하여 사용자 어플리케이션을 제공한다.

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연료전지 수소재순환 이젝터 시스템에 관한 수치해석적 연구 (Numerical Study on a Hydrogen Recirculation Ejector for Fuel Cell Vehicle)

  • 남궁혁준;문종훈;장석영;홍창욱;이경훈
    • 한국신재생에너지학회:학술대회논문집
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    • 한국신재생에너지학회 2007년도 추계학술대회 논문집
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    • pp.156-160
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    • 2007
  • Ejector system is a device to transport a low-pressure secondary flow by using a high-pressure primary flow. Ejector system is, in general, composed of a primary nozzle, a mixing section, a casing part for suction of secondary flow and a diffuser. It can induce the secondary flow or affect the secondary chamber pressure by both shear stress and pressure drop which are generated in the primary jet boundary. Ejector system is simple in construction and has no moving parts, so it can not only compress and transport a massive capacity of fluid without trouble, but also has little need for maintenance. Ejectors are widely used in a range of applications such as a turbine-based combined-cycle propulsion system and a high altitude test facility for rocket engine, pressure recovery system, desalination plant and ejector ramjet etc. The primary interest of this study is to set up an applicable model and operating conditions for an ejector in the condition of sonic and subsonic, which can be extended to the hydrogen fuel cell vehicle. Experimental and theoretical investigation on the sonic and subsonic ejectors with a converging-diverging diffuser was carried out. Optimization technique and numerical simulation was adopted for an optimal geometry design and satisfying the required performance at design point of ejector for hydrogen recirculation. Also, some sonic and subsonic ejectors with the function of changing nozzle position were manufactured precisely and tested for the comparison with the calculation results.

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연료전지 수소재순환 이젝터 성능 해석 (Performance Analysis on a Hydrogen Recirculation Ejector for Fuel Cell Vehicle)

  • 남궁혁준;문종훈;장석영;홍창욱;이경훈
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년도 춘계학술대회논문집
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    • pp.256-259
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    • 2008
  • Ejector system is a device to transport a low-pressure secondary flow by using a high-pressure primary flow. Ejector system is, in general, composed of a primary nozzle, a mixing section, a casing part for suction of secondary flow and a diffuser. It can induce the secondary flow or affect the secondary chamber pressure by both shear stress and pressure drop which are generated in the primary jet boundary. Ejector system is simple in construction and has no moving parts, so it can not only compress and transport a massive capacity of fluid without trouble, but also has little need for maintenance. Ejectors are widely used in a range of applications such as a turbine-based combined-cycle propulsion system and a high altitude test facility for rocket engine, pressure recovery system, desalination plant and ejector ramjet etc. The primary interest of this study is to set up an applicable model and operating conditions for an ejector in the condition of sonic and subsonic, which can be extended to the hydrogen fuel cell vehicle. Experimental and theoretical investigation on the sonic and subsonic ejectors with a converging-diverging diffuser was carried out. Optimization technique and numerical simulation was adopted for an optimal geometry design and satisfying the required performance at design point of ejector for hydrogen recirculation. Also, some ejectors with a various of nozzle throat and mixing chamber diameter were manufactured precisely and tested for the comparison with the calculation results.

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신제품개발용 전문가시스템에 있어서의 지식처리 기법으로서 흑판형 추론 모델의 적용 방법에 관한 연구 (A Study on the Design Expert System for Research and Development Using Blackboard Inference Model)

  • 장승호
    • 한국시뮬레이션학회논문지
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    • 제22권1호
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    • pp.87-95
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    • 2013
  • 신제품의 연구/개발에 있어서는 시제품의 실험결과를 토대로 개량설계를 여러 번 반복하는 경우가 많으며, 이로 인하여 시제품을 만드는 횟수가 많아지게 되는 경향이 있다. 신제품의 연구/개발에 있어서 이와 같은 불필요한 시제품을 만드는 횟수를 저감시키기 위한 목적으로 주로 컴퓨터 시뮬레이션에 기반을 둔 CAD 시스템이 많이 연구 되고 있으며, 일부는 이미 실용화되어 있다. 그러나 이와 같은 종래의 CAD시스템은 시제품의 실험결과를 합리적으로 개량설계에 반영하기 위한 기능을 CAD 시스템 내부에 갖추고 있지 않다. 본 연구에서는 다수의 지식원들의 상호 협조 작업을 통하여 문제해결 능력을 향상시킬 수 있는 특징을 갖는 흑판형 추론모델을 이용하여, 신제품의 개발설계를 적절히 지원하기 위한 전문가 시스템(DESYR ver. 1)의 구축방법을 제시하였으며, 이를 통하여 시제품의 실험결과를 보다 효과적으로 개량설계에 반영할 수 있도록 하였다. 또한, 신형 자기축수의 개발을 통하여 제시한 방법론의 타당성을 검증하였다.

ZigBee와 CAN 통신을 이용한 자동차 배기가스 검출 및 자기진단 시스템 (Car Exhaust Gas Detection and Self-Diagnosis System using ZigBee and CAN Communications)

  • 천종훈;김국세;박종안
    • 한국ITS학회 논문지
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    • 제7권6호
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    • pp.48-56
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    • 2008
  • 본 논문은 대기오염의 주범인 자동차 배기 가스량을 체크하고 차량내의 고장 유 무 진단 시스템 개발이다. 시스템 엔진 정보 추출을 위해 차량 CAN 통신을 이용하고 정보 전송을 위해 ZigBee를 통해 데이터 전송을 한다. 차량 CAN을 위해 차량에서 자체 제공되는 OBD-II 프로토콜을 사용하여 차량의 각종 센서 정보 및 O2 센서 값을 통해 차량 상태 정보 및 배기 가스양을 계산한다. 주행 중인 자동차 엔진 및 내부 고장에 잘 알지 못하는 일반 사용자를 위해 운행 중 실시간 차량의 자가진단 시스템 구축을 목적으로 하고 고장진단 프로토콜 전송을 위한 무선통신 인터페이스로 저 전력 저비용 ZigBee 통신 인터페이스를 구축한다. 자동차 그리고 진단 시스템의 통신을 위해 ZigBee 시스템을 통하여 효율적 저비용 통신 인터페이스를 구성하여 차량내의 엔진 및 각종 센서 정보 네트워크를 지원한다. 차량에서 전송되어 온 각종 센서정보는 ZigBee 기반을 통해 ZigBee 메인 컨트를 시스템에 전송된다. 차량에 이상이 생겼을 때 트러블 코드를 저장하고 자동차가 정비소에 갔을 때 정확한 판단을 하여 신속하게 처리 할 수 있게 해 주며 자동차에 대해서 잘 알지 못하는 운전자에게 정확한 정보를 제공한다. 또한 멀티미디어 시스템 기능을 추가하고 주행 중 무선 인터넷이 가능하도록 시스템을 확장한다. 마지막으로 주행 중 차량 자가진단을 위해 저 전력 임베디드 리눅스 시스템을 구축하고 실 실험을 통하여 구현하고 검증한다.

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차량진단 및 모니터링을 위한 통신과 서버시스템 운용에 관한 연구 (Research on Communication and The Operating of Server System for Vehicle Diagnosis and Monitoring)

  • 유희수;원용관;박권철
    • 대한전자공학회논문지TC
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    • 제48권6호
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    • pp.41-50
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    • 2011
  • 본 논문은 차량의 엔진 및 내부 고장을 잘 알지 못하는 차량운전자들을 위해 휴대기기를 이용한 차량의 운행, 고장, 이상 정보를 모니터링하고 인터넷 환경에서 자료를 조회할 수 있는 서버시스템 운용에 관한 것이다. 운행 중 실시간으로 차량의 상태를 알려주기 위하여 기존의 네비게이션 및 GPS 위주의 텔레메틱스 기술에서 벗어나 차량 내부 망(In-Vehicle Network)에 연결된 엔진, 트랜스미션, 브레이크, 에어백 등의 제어장치인 ECU(Electronics Control Unit) 및 각종 센서들로부터의 데이터 획득을 위해 차량내의 OBD-II(On-Board Diagnostics) 커넥터에 직접연구 개발한 차량 정보 수집 장치를 연결한다. 또한, 무선 통신통신이 가능한 휴대기기(휴대폰, PDA, PMP, UMPC 등)에 차량 진단 프로그램을 탑재하여 차량 주행 중에 발생되는 운행, 고장, 이상 정보를 실시간으로 수집 및 분석한다. 이상 징후 발생 시 알림 메시지를 발생하여 차량의 이상에 대해 신속히 대처 할 수 있다. 이와 동시에, 휴대기기를 통해 수집된 차량 정보 데이터는 무선통신망을 통해 차량 관리 전문회사의 서버로 전송되고, 체계적인 차량 관리에 활용될 수 있도록 하기 위해 구축된 서비스 시스템에서 조회 및 활용되어지게 된다. 따라서 차량에 대한 지식이나 상식이 부족한 모든 운전자에게 차량 관리에 대한 편리함을 제공하여 안전운전 및 경제운전에 관련된 운전이력관리 등의 서비스를 제공할 수 있다. 이러한 편리성을 제공하고자 본 연구에서는 차량에 탑재되는 차량 정보 수집 장치와 운전자가 사용 중인 개인의 무선통신 휴대기기와 인터넷망으로 연계되는 차량 진단 및 모니터링이 가능한 시스템을 구성하였고, 자료의 조회 관리 기술을 연구하였다.

항공기(航空機) 사고조사제도(事故調査制度)에 관한 연구(硏究) (A Study on the System of Aircraft Investigation)

  • 김두환
    • 항공우주정책ㆍ법학회지
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    • 제9권
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    • pp.85-143
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    • 1997
  • The main purpose of the investigation of an accident caused by aircraft is to be prevented the sudden and casual accidents caused by wilful misconduct and fault from pilots, air traffic controllers, hijack, trouble of engine and machinery of aircraft, turbulence during the bad weather, collision between birds and aircraft, near miss flight by aircrafts etc. It is not the purpose of this activity to apportion blame or liability for offender of aircraft accidents. Accidents to aircraft, especially those involving the general public and their property, are a matter of great concern to the aviation community. The system of international regulation exists to improve safety and minimize, as far as possible, the risk of accidents but when they do occur there is a web of systems and procedures to investigate and respond to them. I would like to trace the general line of regulation from an international source in the Chicago Convention of 1944. Article 26 of the Convention lays down the basic principle for the investigation of the aircraft accident. Where there has been an accident to an aircraft of a contracting state which occurs in the territory of another contracting state and which involves death or serious injury or indicates serious technical defect in the aircraft or air navigation facilities, the state in which the accident occurs must institute an inquiry into the circumstances of the accident. That inquiry will be in accordance, in so far as its law permits, with the procedure which may be recommended from time to time by the International Civil Aviation Organization ICAO). There are very general provisions but they state two essential principles: first, in certain circumstances there must be an investigation, and second, who is to be responsible for undertaking that investigation. The latter is an important point to establish otherwise there could be at least two states claiming jurisdiction on the inquiry. The Chicago Convention also provides that the state where the aircraft is registered is to be given the opportunity to appoint observers to be present at the inquiry and the state holding the inquiry must communicate the report and findings in the matter to that other state. It is worth noting that the Chicago Convention (Article 25) also makes provision for assisting aircraft in distress. Each contracting state undertakes to provide such measures of assistance to aircraft in distress in its territory as it may find practicable and to permit (subject to control by its own authorities) the owner of the aircraft or authorities of the state in which the aircraft is registered, to provide such measures of assistance as may be necessitated by circumstances. Significantly, the undertaking can only be given by contracting state but the duty to provide assistance is not limited to aircraft registered in another contracting state, but presumably any aircraft in distress in the territory of the contracting state. Finally, the Convention envisages further regulations (normally to be produced under the auspices of ICAO). In this case the Convention provides that each contracting state, when undertaking a search for missing aircraft, will collaborate in co-ordinated measures which may be recommended from time to time pursuant to the Convention. Since 1944 further international regulations relating to safety and investigation of accidents have been made, both pursuant to Chicago Convention and, in particular, through the vehicle of the ICAO which has, for example, set up an accident and reporting system. By requiring the reporting of certain accidents and incidents it is building up an information service for the benefit of member states. However, Chicago Convention provides that each contracting state undertakes collaborate in securing the highest practicable degree of uniformity in regulations, standards, procedures and organization in relation to aircraft, personnel, airways and auxiliary services in all matters in which such uniformity will facilitate and improve air navigation. To this end, ICAO is to adopt and amend from time to time, as may be necessary, international standards and recommended practices and procedures dealing with, among other things, aircraft in distress and investigation of accidents. Standards and Recommended Practices for Aircraft Accident Injuries were first adopted by the ICAO Council on 11 April 1951 pursuant to Article 37 of the Chicago Convention on International Civil Aviation and were designated as Annex 13 to the Convention. The Standards Recommended Practices were based on Recommendations of the Accident Investigation Division at its first Session in February 1946 which were further developed at the Second Session of the Division in February 1947. The 2nd Edition (1966), 3rd Edition, (1973), 4th Edition (1976), 5th Edition (1979), 6th Edition (1981), 7th Edition (1988), 8th Edition (1992) of the Annex 13 (Aircraft Accident and Incident Investigation) of the Chicago Convention was amended eight times by the ICAO Council since 1966. Annex 13 sets out in detail the international standards and recommended practices to be adopted by contracting states in dealing with a serious accident to an aircraft of a contracting state occurring in the territory of another contracting state, known as the state of occurrence. It provides, principally, that the state in which the aircraft is registered is to be given the opportunity to appoint an accredited representative to be present at the inquiry conducted by the state in which the serious aircraft accident occurs. Article 26 of the Chicago Convention does not indicate what the accredited representative is to do but Annex 13 amplifies his rights and duties. In particular, the accredited representative participates in the inquiry by visiting the scene of the accident, examining the wreckage, questioning witnesses, having full access to all relevant evidence, receiving copies of all pertinent documents and making submissions in respect of the various elements of the inquiry. The main shortcomings of the present system for aircraft accident investigation are that some contracting sates are not applying Annex 13 within its express terms, although they are contracting states. Further, and much more important in practice, there are many countries which apply the letter of Annex 13 in such a way as to sterilise its spirit. This appears to be due to a number of causes often found in combination. Firstly, the requirements of the local law and of the local procedures are interpreted and applied so as preclude a more efficient investigation under Annex 13 in favour of a legalistic and sterile interpretation of its terms. Sometimes this results from a distrust of the motives of persons and bodies wishing to participate or from commercial or related to matters of liability and bodies. These may be political, commercial or related to matters of liability and insurance. Secondly, there is said to be a conscious desire to conduct the investigation in some contracting states in such a way as to absolve from any possibility of blame the authorities or nationals, whether manufacturers, operators or air traffic controllers, of the country in which the inquiry is held. The EEC has also had an input into accidents and investigations. In particular, a directive was issued in December 1980 encouraging the uniformity of standards within the EEC by means of joint co-operation of accident investigation. The sharing of and assisting with technical facilities and information was considered an important means of achieving these goals. It has since been proposed that a European accident investigation committee should be set up by the EEC (Council Directive 80/1266 of 1 December 1980). After I would like to introduce the summary of the legislation examples and system for aircraft accidents investigation of the United States, the United Kingdom, Canada, Germany, The Netherlands, Sweden, Swiss, New Zealand and Japan, and I am going to mention the present system, regulations and aviation act for the aircraft accident investigation in Korea. Furthermore I would like to point out the shortcomings of the present system and regulations and aviation act for the aircraft accident investigation and then I will suggest my personal opinion on the new and dramatic innovation on the system for aircraft accident investigation in Korea. I propose that it is necessary and desirable for us to make a new legislation or to revise the existing aviation act in order to establish the standing and independent Committee of Aircraft Accident Investigation under the Korean Government.

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