• Title/Summary/Keyword: Penumatic Pipe

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A Study on the Indexing Table by the Penumatic Poeration (공기압 구동 원주 할출 기구의 개발에 관한 연구)

  • 오진안;강인각;한창수
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 1997.04a
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    • pp.734-738
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    • 1997
  • In this study, we developed the indexing table opering by pneumatic actuation. We doubled the torque of index table by using specialy desingned air pipe and two pistons. And by locating two pistons We perform several tests and this results is written below.

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Flow Rate Prediction of Pneumatic Pipe System Using Concept of Conductance (컨덕턴스의 개념을 사용한 공압관 시스템의 유량 예측)

  • Kim, Jin-Hyeon;Deng, Ruoyu;Kim, Heuy-Dong
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.38 no.5
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    • pp.431-436
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    • 2014
  • Conductance is a concept contrary to flow resistance and is extensively used as a flow index on how easily fluid is transported through a pneumatic pipe or fluid device. However, research on flow conductance is very rare to date, and a systematic investigation is needed for the standardization of pneumatic devices. In the present study, a computational fluid dynamics method was applied to solve the compressible Navier-Stokes equations with two-equation turbulence models. The present CFD results were validated with existing experimental data. The conductance values and friction factors at the inlet and outlet of a pneumatic pipe were used to assess the flow rates. The present results showed that the conductance depends on the pressure ratio at the inlet and outlet of a pipe.

Conceptual Design of Penumatic System Routing for Liquid Rocket Engine (액체로켓엔진의 공압류 라우팅 개념 설계)

  • Kim, Okkoo;Park, Soonyoung;Jung, Eunhwan
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.1112-1114
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    • 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.

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