• 제목/요약/키워드: Pneumatic Type

검색결과 193건 처리시간 0.024초

공압베인모터 설계 및 성능특성에 관한 실험적 고찰 (An Experimental Study on the Design and Performance Characteristics of Vane type Pneumatic Motors)

  • 김동수;김유일;김미성
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 1997년도 추계학술대회 논문집
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    • pp.472-475
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    • 1997
  • It is well known that pneumatic motors convert fluid power into mechanical power with a low efficiency. The Value of the efficiency depends on several factors, of which the most important are ; type of motor, speed, supply pressure, sie and geometry of the motor. This paper presents an analytical and experimental study of the performance of he vane type pneumatic motors. This investigation deals with all the pneumatic motors. This investigation deals with all the pneumatic motors. This investigation deals with all the major aspects of the air flow through a vane type pneumatic motor and pints out which are the main causes of the low efficiency of the motor, and therefore indicates which changes in a motor design an lead to optimum performance.

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하이브리드형의 공압 서비스 로봇의 개발 (Development of the Pneumatic Service Robot with a Hybrid Type)

  • 최철우;최현석;한창수
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 추계학술대회논문집A
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    • pp.686-691
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    • 2001
  • In this paper, the pneumatic service robot with a hybrid type is developed. A pneumatic has the advantage of good compliance, high payload-to-weight and payload-to-volume ratios, high speed and force capabilities. Using pneumatic actuators which have low stiffness, the service robot can guarantee safety. By suggesting a new serial-parallel hybrid type for the service robot which separates into positioning motion and orienting motion, we can achieve large workspace and high strength-to-moving-weight ratio at the same time. A sliding mode controller can be designed for tracking the desired output using the Lyapunov stability theory and structural properties of pneumatic servo systems. Through many experiments of circular trajectory, the pneumatic service robot is evaluated and verified.

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저마찰 고속형 공기압 실린더의 설계에 관한 연구 (A Study on the Design of a Low-Friction, High-Speed Pneumatic Cylinder)

  • 김도태;김동수;주민진
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2008년도 추계학술대회A
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    • pp.1230-1235
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    • 2008
  • Of all of pneumatic components utilized in the make up of pneumatic circuits on either automatic assembly machine or industrial equipment, the pneumatic cylinder is more oriented toward being a structural as well as a pneumatic member. The structural design must be based to a large degree on the end of application of the cylinder on the equipment it is operating. In this paper, design studies of a double-acting pneumatic cushion type cylinder with low-friction and high-speed driving have been developed. Of interest here is to investigate the structural analysis of cylinder tube, piston rod, end cover, and to analyze the buckling of piston rod. Also, a relief valve type cushion mechanism is considered. This cushion mechanism is found to be adequate under a high-speed driving of pneumatic cylinders.

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관절 경직 환자의 물리 치료를 위한 공압 구동형 하이브리드 로봇 개발 (Development of the Hybrid Type Robot Using a Pneumatic Actuator For Physical Therapy Of Ankylosis)

  • 최현석;최철우;한창수;한정수
    • 대한의용생체공학회:의공학회지
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    • 제24권2호
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    • pp.127-132
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    • 2003
  • 본 논문에서는 관절 경직 환자의 재활 치료를 위한 공압 실린더를 이용한 하이브리드형 로봇을 연구 개발하였다. 공압 실린더는 우수한 컴플라이언스를 가지고 있고 부피나 중량에 비해 높은 구동력을 가지고 있다 낮은 강성을 지닌 공압 구동기는 안정이 보장되어야 하는 물리 치료용 로봇의 구현에 적용하기 적당하다. 본 연구에서 제안한 로봇 시스템은 직렬형과 병렬형을 결합한 하이브리드 형으로 위치 결정부와 자세 결정부로 구분되며 하이브리드 구조를 통해 넓은 작업영역과 구동력을 얻을 수 있었다. 슬라이딩 모드 제어기를 이용하여 로봇 시스템의 공압 서보시스템의 추종성과 안정성을 얻을 수 있었으며 실험을 통하여서 개발된 시스템에 대한 검증을 하였다.

크랭크 레버형 평행개폐 공기압 척의 수명 분석 (Life Analysis of Parallel Opening Type Pneumatic Chuck)

  • 강보식;송창섭;장지성;지상원
    • 한국정밀공학회지
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    • 제26권9호
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    • pp.96-102
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    • 2009
  • In this study, performs analysis of the life of parallel opening type pneumatic chucks that are usually applied in the factory automation line. Pneumatic chucks have complicated failure cause because they are organized as a complex of various elements. Therefore, we analyzed the main failure mode of pneumatic chuck, and then performed life test and performance test according to the international standards. On the basis of these processes, shape parameter of pneumatic chuk is proposed that is the main factor for the calculation of zero failure test time for the reliability of pneumatic chuck and their data analysis of life distribution.

OWC형 파력발전 공기챔버의 공기감쇠력 실험연구 (An Experimental Study of Pneumatic Damping at the Air Chamber for OWC type Wave Energy Device)

  • 최학선;류재문;홍석원;김진하
    • 한국해양공학회:학술대회논문집
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    • 한국해양공학회 2004년도 학술대회지
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    • pp.138-144
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    • 2004
  • Pneumatic damping through a orifice type duct for OWC type wave energy device is studied experimentally. Forced oscillation tests are made to measure chamber pressure and velocity of air flaw through orifice. Pneumatic damping coefficient are deducted from the experimental research, and discussion are made far the influence of frequency, heave amplitude, and orifice size. Finally two formula are proposed for the estimation of non-dimensional pneumatic damping coefficient by regression analysis. The proposed formula proves to be a reliable method far practical application.

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공압 쿠션 실린더의 충격압 흡수를 위한 스프링형 니들밸브의 동특성에 관한 연구 (Simulation Study on Dynamic Analysis of Spring Type Needle Valve to Absorb Surge Pressure in Pneumatic Cushion Cylinder)

  • 이재구;;이준;이재천;신현명
    • 유공압시스템학회논문집
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    • 제2권1호
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    • pp.15-22
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    • 2005
  • The purpose of this study is to find the effective dynamic characteristics of an improved pneumatic cushion cylinder with a spring type needle valve. The dynamic model represented the peak pressure control method when the pneumatic cushion cylinder is moving forward or backward in the horizontal direction. It was found from the simulation results that the peak pressure in the cushion chamber is affected by the spring, which helps to understand the performance of the pneumatic cushion cylinder and to improve or design a better cushion needle valve component. From the simulation results, the stability of pneumatic cushion cylinder with a spring type needle valve was superior and its cushion capability was also better than that without the spring.

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OWC형 파력발전 공기챔버의 공기감쇠력 실험 연구 (An Experimental Study of Pneumatic Damping at the Air Chamber for an OWC-type Wave Energy Device)

  • 최학선;홍석원;김진하;류재문
    • 한국해양공학회지
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    • 제18권4호
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    • pp.8-14
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    • 2004
  • Pneumatic damping through an orifice-type duct for an OWC-type wave energy device is studied experimentally. Forced oscillation tests are used to measure chamber pressure and velocity of air-flow through an orifice. Pneumatic damping coefficients are deducted from the experimental research, and the influence of frequency, heave amplitude, and orifice size are discussed. Finally, two formulas are proposed for the estimation of non-dimensional pneumatic damping coefficient by regression analysis. The proposed formula proves to be a reliable method for practical application.

Honeycomb 스포크 구조를 갖는 비 공기압 타이어의 진동 특성 (Vibration Characteristics of Non-pneumatic Tire with Honeycomb Spokes)

  • 조홍준;이치훈;김광원;김두만
    • 한국자동차공학회논문집
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    • 제21권4호
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    • pp.174-180
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    • 2013
  • The vibration characteristic of tire is heavily related to the noise and comfort on driving. Therefore, in this paper, we investigate modal charateristic of non-pneumatic tires with Honeycomb spokes. The modal analysis of non-pneumatic tire is investigated for geometric of non-pneumatic tire(NPT) which is designed according to the cell angle of honeycomb cell. Investigation of natural frequencies and mode shapes of non-pneumatic tire are compared regular type NPT with auxetic type NPT. The analysis is based on the finite element method and used ABAQUS program which is able to analyze of non-linear. The material of NPT is used for the Ogden energy model which is model of hyperelastic material. As a result, natural frequencies and mode shapes of non-pneumatic tires with honeycomb spokes are affected by the angle of honeycomb cell.

항공기 착륙장치 동하중 해석 (Dynamic Load Analysis of Aircraft Landing Gear)

  • 신정우;김태욱;황인희
    • 한국항공운항학회지
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    • 제16권1호
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    • pp.1-6
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    • 2008
  • Role of landing gear is to absorb energy which is generated by aircraft ground maneuvering and landing. Generally, in order to absorb the impact energy, oleo-pneumatic type shock absorber is used in aircraft landing gear. Oleo-pneumatic type shock absorber has a good energy absorption efficiency and is light in weight because structure of oleo-pneumatic type shock strut is relatively simple. In this study, dynamic load analysis for swinging arm type landing gear was performed to predict landing loads. Modeling of landing gear was conducted with MSC.ADAMS, and dynamic landing loads were analyzed based on ADS-29. Optimum landing loads were generated through adjustment of damping orifice and the analysis results were presented with various aircraft attitude.

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