• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 1997.11a
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• pp.19-19
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• 1997

휴대용 미사일의 1단과 2단 추진기관은 체결부품에 의하여 연결되어 발사관 내에서 운반되어지며, 발사 시 1단 추진기관이 분리되게 된다. 이때에 분리력은 1단 추진기관의 압력에 의하여 제공되고 체결부품인 4-팁 와셔는 어느 압력 이상을 받으면 추진기관의 1단과 2단을 분리한다. 정적시험을 하여 구한 결과를 해석치 와 비교했으며 실제상황에 유사한 동적 시험을 하여 필요한 안전계수를 구하였다.

• Journal of the Korean Society of Propulsion Engineers
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• v.4 no.3
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• pp.19-28
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• 2000

In general the data such as thrust, pressure, temperature and combustion time are measured in developing the propulsion system of solid rocket motor through static firing test. But in the case of personal surface to air missile there are required a severe safety specifications in order to eliminate gunner hazard from the exhaust plume of motors. The safety requirements lead to the design of separation device and safety igniter device. The dynamic firing test for the designed two devices should be conducted under the flight environmental conditions to verify the requirements compliance. In this study the technique for dynamic firing test of propulsion system of personal surface to air missile is proposed and the method to design the dynamic test bench is also studied.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 1996.10a
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• pp.351-356
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• 1996

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• The Bulletin of The Korean Astronomical Society
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• v.37 no.2
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• pp.230.1-230.1
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• 2012

본 논문에서는 대구경 광학탑재체의 조립, 정렬 및 시험에 사용되는 고정밀, 고안정 짐발장치의 개발에 대해서 소개하고자 한다. 광학탑재체의 광학시험을 위해 사용되는 짐발장치는 광축높이를 유지하기 위해서 높이조절이 가능해야하고, 조립과정과 광학시험과정 그리고 시험 후 광학탑재체를 짐발 장치로부터 분리하기 위해 수평상태와 수직상태로의 회전이 가능해야 한다. 광학측정 시험과정 중에 결상위치의 미세한 조절을 위해 광학탑재체를 수평상태에서 상하좌우 정밀한 회전이 가능해야한다. 우주궤도환경 하에서 성능측정을 위해 열진공체임버 안에서의 광학시험이 필요하므로 짐발장치를 구성하는 재질은 모두 진공사용이 적합한 것이어야 한다. 광학측정 중에 측정설비주변에서부터 인가된 외란은 광학시험과 같은 민감한 시험에서는 철저하게 제거되어야 하는데, 이와 관련하여 짐발장치의 광학측정시험형상에서의 고유진동수와 같은 동적 특성도 설계과정에 반영하여 안정적인 측정 장치가 되도록 고려되어야 한다.

• Journal of Ocean Engineering and Technology
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• v.17 no.2
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• pp.27-33
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• 2003

본 논문에서는 측정된 가속도신호만을 사용하여 변위응답을 추정하는 시간영역과 주파수영역에서의 동적 응답변환 알고리즘을 제시하였다. 본 알고리즘에서 사용되는 변환변위응답은 속도와 변위성분의 초기조건에 대한 정보 없이 측정된 가속도신호의 적분에 의하여 계산되며 실제 변위응답과 상관관계를 갖는다. 이에 측정된 구조물의 동적응답이 무재하부분과 자유진동부분을 포함하고 있을 때 변환응답을 보정하여 초기치 문제를 해결할 수 방법을 제시함으로써 가속도신호만을 사용하여 실제 변위응답을 추정할 수 있도록 하였다. 제시된 응답변환 알고리즘의 타당성을 평가하기위해 실교량에 대한 현장시험자료를 적용하여 변위응답을 추정하고 실측된 동적 변위와 비교하였다. 또한, 주파수영역에서의 응답변환에서 적분구간을 상이하게 사용함으로써 동적성분과 정적성분으로 분리된 추정응답을 평가할 수 있었으며 이에 따른 충격계수의 계산은 신뢰성 있는 평가방법임을 확인하였다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2008.11a
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• pp.293-296
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• 2008

Most of the guided weapons have been kept and transferred at the launching tube and fired in case of necessity in these day. Launching tube is a kind of case to protect the guided weapons from external environments and conducted as a guide when they are fired. When we attached the guided weapons to launching tube we usually has used explosive bolt. Explosive bolts have been used explosives when they had to be separated. But when they are separated there are some bad effects; a flame, fragments and pyro-shock. Because of these bad effects there are many restriction to use bolt as joining devices to precision guided weapons. To solve these problems, it has been invented ball type bolt. The present work was represented quantitively the margin of separation safty and separation mechanism in ball type bolt to analyse the dynamic separation test. Unlike explosive bolt, ball type bolt is separated without a flame, fragments and pyro-shock. And it also has a good mechanical properties as much as those of explosive bolt.

• Journal of the Korean Society of Propulsion Engineers
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• v.13 no.3
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• pp.41-49
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• 2009

The present paper describes a mathematical modeling and simulation of the separation of a solid rocket booster from an air breathing engine vehicle. The vehicle and booster are considered as a multi-connected body and the booster is assumed to move only along the axial direction of the vehicle. The dynamic motion of the vehicle and the booster were modeled by using Kane's method. The aerodynamic forces on the whole system along various positions of booster were calculated by using DATCOM software and the internal pressure force acting on the effective surface during separation was simply calculated with gas dynamics and Taylor MacColl equation. Numerical simulation was done by using Mathworks-Matlab. From the result, the variation of Mach number and angle of attack are not large during the separation, so the variation of pitch angle and the characteristics of inlet flow for varying the Mach number and angle of attack during the separation test can be identified as neglectable values.

• Journal of the Korean Society of Propulsion Engineers
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• v.15 no.2
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• pp.62-67
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• 2011

Launching tube is a kind of case to protect the guided weapons from external environments and conducted as a guide when they are fired. The guided weapons have been firmly kept at the launching tube and transferred, and would be separated at the required time when they are fired To meet the aim, it has been used explosive bolts which are reliable and efficient mechanical fastening devices having the special feature of a built-in release. The disadvantage of explosive bolt lies in that it is based on the high explosive effect of a pyrotechnic charge. When the explosive bolt is ignited, there are some bad effects; a flame, fragments and pyro-shock. Because of these bad effects there are many restriction to use bolt as joining devices to precision guided weapons. To solve these problems, the aim of the present work is to invent the ball-type separation bolt which is a pyrotechnically releasable mechanical linking device for two mechanical elements that does not suffer from such drawbacks. A standard pressure cartridge can moreover be easily integrated inside the device according to the present work and this with no modification to its structure. The present work was represented quantitatively the margin of separation safety and analysed separation mechanism in ball type separating bolt to perform the dynamic separation test.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 1994.04a
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• pp.116-121
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• 1994

지금까지 대형 구조물에 널리 사용되고 있는 Base Isolator는 특히, 지진하중에 대하여 상부 구조물의 지반분리(base isolation)을 이용한 지진제어를 목적으로 하기 때문에 Seismic Isolator라 한다. 일반적으로 면진베어링에는 LRB(Laminated Rubber Bearing) 방식과 R-FBI(resilient-friction base isolator) 방식으로 크게 나눌 수 있다. LRB 방식은 가장 널리 사용되는 면진베어링으로써 방진고무를 주된 재료로 하고 수직강성을 보강하기 위하여 steel plate를 조합하여 제작하며, 초기강성 및 에너지 소산능력을 증가시키기 위하여 단면중앙에 납(lead plug)를 삽입하기도 한다. R-FBI 방식은 방진고무 적층판 내부에 미끄럼판을 가지고 있으므로 LRB 방식에 비하여 더 큰 수평변위를 발생시킬 수 있다. 이번에 설계 제작한 면진베어링은 LNG 저장탱크의 Seismic Isolation을 목적으로 적용대상의 사양에 맞추어 설계 제작하고 성능평가 시험을 수행하여 LNG 저장탱크, 원자로, 대형 건축물등 지진으로부터 보호되어야 하는 대형구조물의 방진재로 적용할 수 있는가를 평가하고자 한다. 본 논문에서는 제작된 면진베어링의 설계를 검증하고 방진고무(HDR)재료의 물리적 특성시험, 축소모델에 의한 정적, 동적시험을 통하여 시험방법을 소개하고 이러한 시험결과를 기초로 하여 면진베어리의 성능을 평가하였으며, 면진베어링의 온도변화, 외부 수직하중의 변화등에 따른 특성변화와 LNG 저장탱크와 면진베어링의 체결방법에 따른 시험으로 체결방법을 검증하였으며, 대상물의 사양에 적합한가를 고찰하였다.

• Elastomers and Composites
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• v.43 no.3
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• pp.191-198
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• 2008

It is said that polymer modified asphalt using polyethylene as modifier would show phase separation due to density difference and incompatibility between asphalt and polyethylene. In this study, to prevent coalescence of polyethylene in asphalt, we employed peroxides as phase separation inhibitor. On microscope, peroxides (dicumyl peroxide, lauroyl peroxide) with waste vinyl (comprising low density polyethylene) did not show phase separation, however, rheometer test showed phase separation at molecular level, i.e., polyethylene and asphalt are immiscible ultimately. Mechanical properties (tensile strength, Marshall stability, dynamic stability) showed waste vinyl-modified asphalts are highly resistant to plastic deformation and these properties are even better than those of Superphalt.