• Journal of the Korean Society of Propulsion Engineers
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• v.25 no.6
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• pp.74-86
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• 2021

The composite lattice structure is a structure that supports the required load with the minimum weight and thickness. Composite lattice structure is manufactured by the filament winding process using impregnating high-strength carbon fiber with an epoxy resin. Filament winding process can laminate and manufacture only structurally necessary parts, composite lattice structure can be applied to aircraft fuselages, satellite and launch vehicles, and guided weapons to maximize weight reduction. In this paper, the development and evaluation of the composite lattice structure corresponding to the entire process from design, analysis, fabrication, and evaluation of large-scale cylindrical and conical composites lattice structure were performed. To be applicable to actual projectiles and guided weapons, we developed a cylindrical lattice structure with a diameter of 2,600 mm and a length of 2,000 mm, and a conical lattice structure with an upper diameter of 1,300 mm, a lower diameter of 2,500 mm, and a length of 900 mm. The performance of the developed composite lattice structure was evaluated through a load test.

• Proceedings of the KAIS Fall Conference
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• 2007.11a
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• pp.297-299
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• 2007

본 논문은 유한한 유전체 격자구조에 입사되는 TE필드가 유전체 내부에 발생시키는 모드의 필드 분포와 방출하는 필드를 분석하였다. 입사되는 필드는 유전체 격자구조에 일정한 패턴의 모드를 형성한다. 유한한 길이의 격자구조의 영향을 받아 유전체 내부에 유한개의 모드가 만들어지며 모드들은 각기 독립적인 방사패턴을 갖는다. 이러한 방사패턴을 분석함으로써 실제로 제작되는 유전체 격자구조의 분석에 도움이 될 것으로 사료된다.

• Composites Research
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• v.30 no.6
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• pp.338-342
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• 2017

In this paper, evaluation method of structural integrity of cylindrical composite lattice structures was conducted. A finite element analysis was used to evaluate the structural integrity of composite lattice structures. In order to verify the optimal finite element in the evaluation of the structural integrity, finite element models for cylindrical composite lattice structure were generated using beam, shell and solid elements. The results of the finite element analyses with the shell and solid element models showed a good agreement. However, considerable differences were found between the beam element model and the shell and solid models. This occurred because the beam element does not take into account the degradation of the mechanical properties of the non-intersection parts of cylindrical composite lattice structures. It was found that the finite element analysis of evaluation of structural integrity for cylindrical composite lattice structures have to use solid element.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.835-837
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• 2017

In this paper, manufacturing processes of cylindrical composite lattice structures using filament winding method was described. Cylindrical composite lattice structures were manufactured in accordance with four major steps. Silicon mold of lattice shape was installed on mandrel and then continuous fiber was wound on silicon mold. After winding process, in order to ensure the same thickness for all regions, compression process was done for its intersection parts. Finally, the composite lattice structure was demoulded after curing in oven. It was found that the manufactured cylindrical composites lattice structure had 2.4% of dimensional error compared to the design requirements.

• Composites Research
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• v.31 no.4
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• pp.156-160
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• 2018

In this paper, evaluation method of structural integrity for cone-type composite lattice structures with hexagonal cell was conducted. A finite element analysis was used to evaluate the structural integrity of cone-type composite lattice structure. The finite element model for evaluation of structural integrity was generated using solid element. In order to consider the difference in mechanical properties between intersection and non-intersection part, the mechanical properties were applied considering the fiber volume fraction of each part. Compression test of cone-type composite lattice structure were conducted for verification of evaluation method of structural integrity. The analysis result showed 2% errors in displacement and good agreement with test result.

• Proceedings of the KAIS Fall Conference
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• 2007.05a
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• pp.123-125
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• 2007

본 논문에서는 유한한 유전체 격자구조에 수직으로 입사되는 전자기파가 갖는 유효 굴절율을 구하고자 한다. 유전체 격자구조를 다층구조로 모델링하여 모드에 따른 전파상수를 계산하면 주어진 주파수에 따른 유효 굴절율을 계산할 수 있다. 다층구조에서 유효 굴절율을 계산을 응용하면 유전체 모양이나 구조에 따른 유효굴절율을 계산할 수 있으며 주파수 선택특성이나 도파관등에 진행모드 계산에 도움이 될 것으로 사료된다.

• Journal of the Korea institute for structural maintenance and inspection
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• v.24 no.5
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• pp.143-149
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• 2020

The purpose of this study is to manufacture a variable density - hybrid lattice structure control by filling the pore of the metal addictive manufactured lattice structure with lightweight reactive acrylic compounds(RAC). To apply the variable density - hybrid lattice structure to the construction industry, the enhancing adhesion - reactive acrylic compounds(EA-RAC) which increased the adhesion strength was manufactured by adding ordinary portland cement to the RAC. Finally, the EA-RAC was filled into the lattice structure to test the specific density, water absorption, and adhesion strength of the variable density - hybrid lattice structure. The results were obtained with density controllable, water absorption less than 1.0%, and 1-day bonding strength of 1.78 MPa to 1.98 MPa.

• Proceedings of the Korean Nuclear Society Conference
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• 1995.05b
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• pp.703-708
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• 1995

지진 및 냉각재상실사고와 같은 외력에 대한 집합체 구조적 건전성 분석을 위한 해석시 필요한 지지격자의 동적 특성치들을 얻기 위해 17$\times$17 JDFA 중간지지격자에 대한 충격시험을 수행하였으며, 지지격자에 대한 허용충격하중값(Crush Strength)을 구하고 Impact Duration Method를 이용하여 집합체 구조해석에 필요한 지지격자의 동적 강성도 (Dynamic Stiffness)를 구하였다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.832-834
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• 2017

In this paper, the finite element models for composite lattice structures were verified through natural frequency test. Finite element models of composite lattice structure were generated using beam, shell and solid element. Natural frequencies were measured using impact test method under free-boundary condition. The natural frequencies of finite element analysis for shell and solid element showed a good agreement with experimental results. But beam element did not show a good agreement with experimental results, because beam element could not consider the degradation of mechanical properties of non-intersection parts for composite lattice structure.

• Proceedings of the KAIS Fall Conference
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• 2008.11a
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• pp.264-266
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• 2008

본 논문은 유한한 유전체 격자구조의 정확한 주파수 선택 특성을 해석하고자 새로운 방법을 제시하였다. 기존의 오차, 근사화를 갖고 있는 해석방법과는 달리 유한한 구조에서 근사화가 전혀 없는 방법을 제시하였다. 유한한 격자구조의 유전체는 내부에 존재하는 필드 분포가 한정되어 있으며 구조 파라메터등에 따라 유한한 모드만이 생길 수 있어 입사되는 필드에 따른 생성 모드가 한정되어 있다. 본 논문은 이러한 방법을 이용하여 유전체 격자구조의 주파수 선택특성에 활용에 이용될 수 있을 것으로 사료된다.