• Proceedings of the Acoustical Society of Korea Conference
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• spring
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• pp.279-282
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• 2000

진동가속도를 감지하는 힘평형 서보 가속도계의 성능특성을 결정하는 질량지지 장치를 4개의 팔로 구성된 형태로 설계하고 응답특성을 조사하였다. 스프링의 길이, 폭, 두께에 따른 질량지지 장치의 응답특성을 유한요소법을 이용하여 계산하고, 이를 바탕으로 힘평형 서보 가속도계의 감도, 사용주파수 범위 및 동적 범위를 예측하였다. 그리고 레이저 간섭계를 이용하여 힘평형 서보 가속도계의 각각의 진동 주파수 및 가속도의 크기에 따른 간섭무의 수의 변화와 이때의 응답전압간을 이용하여 가속도계의 응답특성을 측정하였으며, 수치해석을 통해 얻은 결과와 비교 분석하였다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2008.05a
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• pp.14-17
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• 2008

A poppet type shutoff valve under the pneumatic control has been adapted for the MOV (Main Oxidizer shutoff Valve) for KSLV (Korea Space Launch Vehicle). The MOV controls the supply of liquid oxygen into the combustion chamber just by opening and shutting operations. The poppet part of the poppet valves is usually connected with the piston, but on the other hand that of the MOV is separated and just contacted with the piston in order to secure the flexibility of the valve design. For the prevention of the collision with valve body by an undesirable movement of the piston part, it is necessary to evaluate the force during the valve closing. The analysis of the force balance of the MOV at the moment of the valve closing have been performed and some important design parameters for the force balance control have been introduced.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.37 no.8
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• pp.812-818
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• 2009

A MOV(Main Oxidizer shutoff Valve) controls the flow rate of liquid oxygen into the rocket combustor by opening and shutting operations piloted by a pneumatic force. In order to improve the effective design for sealing parts of poppet and piston assemblies, the poppet assembly has been designed to be just contacted with the piston assembly. However, to avoid a gap at the poppet/piston contact surface and to evaluate the MOV operating performance, an analyze on the force balance during the closing motion have been performed. For the accuracy of the analysis, the friction forces and the hydraulic forces have been respectively obtained by experiments and CFD analysis. Through the analysis, some important design parameters such as the spring constant, poppet friction and orifice size in the force balance have been introduced and the required operation performance of the MOV has been proved feasible.

• The Journal of the Acoustical Society of Korea
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• v.20 no.5
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• pp.14-20
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• 2001

The mass-spring system with four arms for the force-balance servo accelerometer was designed and fabricated. The response characteristics of a mass-spring system was calculated with the change of arms thickness and seismic mass by the finite element method (FEM). Furthermore, the response characteristics of accelerometer was measured using the change of interference pattern and response voltage value by Michelson interferometer. The response characteristics with changing length and thickness of arm was changed drastically, and changing seismic mass was minor effect for the response characteristics of mass-spring system. The measured resonant frequencies have good agreement with that of numerical analysis within 5％ range.

• Aerospace Engineering and Technology
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• v.12 no.2
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• pp.108-117
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• 2013

The oxidizer shutoff valve of a gas generator controls the mass flow rate of the propellant of a rocket engine using pilot pressure and spring the force of the valve. The developing oxidizer shutoff valve can be shut off if the pilot pressure is removed from the actuator. Therefore, force balancing is necessary to analyze the characteristics of the forces with respect to the opening and closing of the valve in order to evaluate its performance. In light of this, the valve has been designed to adjust the control pressure required to open the poppet and to determine the working fluid pressure at which the valve starts to close. Under cryogenic flow test as a tests level of C.R.T(Control Random Test), the chattering phenomena occurred due to much leakage of a metal seat section. The pressure for chattering of the oxidizer valve is predicted at about 11 bar using force balancing analysis.

• Aerospace Engineering and Technology
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• v.11 no.1
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• pp.84-90
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• 2012

Fuel shutoff valve of a combustion chamber controls propellant mass flowrate of a rocket engine, by using pilot pressure and spring force. The developing fuel shutoff valve can be self sustained even though pilot pressure is removed in an actuator. Therefore, it is necessary to analyze the characteristics of the forces with respect to the opening and closing of the valve in order to evaluate its performance. In light of this, the valve has been designed to adjust the control pressure for the opening of the poppet and to determine the working fluid pressure at which the valve starts to close. This paper also has been predicted flow coefficient of the valve by Fluent(ver. 12.0) CFD analysis. Various results from the prediction and the analysis have been compared with experiments.

• Journal of Biosystems Engineering
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• v.11 no.2
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• pp.4-13
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• 1986

뿌리작물(作物)을 수확(收穫)하기 위(爲)하여 진동(振動)을 이용(利用)한 4절(節)링크로 구성(構成)되는 시작기(試作機)를 설계(設計), 제작(製作) 및 실험을 수행(遂行)하였다. 수확기(收穫機)의 작동중(作動中) 발생(發生)하는 불균형력(不均衡力)을 상쇄(相殺)시키기 위(爲)한 힘의 평형장치(平衡裝置)를 설계(設計)하기 위(爲)하여 각(各) 요소(要素)의 가속도(加速度) 및 동력학적(動力學的)인 힘을 분석(分析)하였고, 진동기구(振動機構)에 의(依)하여 발생(發生)되는 이론적(理論的)인 토크와 측정(測定)된 토크를 비교분석(比較分析)하였다. 설계(設計)된 힘의 평형장치(平衡裝置)는 불균형력(不均衡力)의 대부분(大部分)을 상쇄(相殺)시켜주고, 이론적(理論的)인 토크는 실측(實測)토크의 변화경향(變化傾向)과 잘 일치(一致)하였다.

• Journal of the Korean Society of Propulsion Engineers
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• v.21 no.4
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• pp.28-35
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• 2017

A main oxidizer shutoff valve controls the supply of the oxidizer flow into the combustion chamber of a liquid rocket engine. This shutoff valve also carries out the pre-chilling of oxidizer supply lines by permitting recycling flow for stable transient start of the engine. In the present paper, the flow tests for the recycling line of the valve were conducted in order to evaluate the cooling performance of the main oxidizer shutoff valve. In addition, cryogenic life-cycle tests were performed with an assumption of the increase of spring constant with increasing valve operating times due to ductile-brittle transition effects.

• Proceedings of the KIEE Conference
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• 2002.11c
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• pp.118-121
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• 2002

본 논문에서는 힘을 측정하여 도립진자를 제어하는 방법을 제안하였다 기존의 각도를 측정하여 도립진자를 0도로 보내는 Set Point Control보다 힘을 제어하여 도립진자를 수직한 영역(Boundary Control)으로 보내는 제어를 하면 제어입력이 감소하고, 외란과 자중이 평형이 되는 위치에서 제어입력은 0이 됨을 보였다.

• 월간산업보건
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• s.89
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• pp.39-41
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• 1995

스트레스의 정의 스트레스란 엄밀히 말해서 하나의 힘(force)이며 이 힘이 한 체계(System)에 가해졌을때는 그 양태(form)를 변경시킨다. 사건(events)이나 상황의 형태로서의 심리적 및 사회적인 힘(force)이나 압력(pressure)이 한 개인의 평형을 왜곡시킬 결과를 초래할때 그것들을 스트레스라고 할 수 있다. 심리적긴장도 또한 스트레스라고 할 수 있는데 이 경우에 긴장을 야기시키는 인자를 "스트레써(stressor)"라고 할 수 있다. 스트레스는 반드시 나쁜 것이라고는 말할 수 없다. 왜냐하면 적은 양의 스트레스는 우리들에게 동기유발을 주기때문이다(환언하면 무스트레스도 스트레스다). 예를 들어 한 위기상황은 우세를 되찾기 위한 전향적 사고를 불러일으킴으로써 사태를 극복케하여 성공에 이르도록 하는 사례가 종종 있다.