• 한국항공운항학회지
• /
• 제25권4호
• /
• pp.130-140
• /
• 2017

Lightning protective design of an aircraft fuel system is closely related to the safety of the flight. Recently, composite material in building an aircraft becomes more important because it can reduce the weight of the aircraft. The composite materials decrease the protection against the effect of lightning. Lightning protective design of metal material aircraft has been researched for a long time and the design technique has been announced widely. However, research on the lightning protective design using composite material aircraft is very limited. In this study, lightning protective design for fuel tank structural component, access cover, fuel filler cap and drain valve in carbon fiber composite material aircraft have been presented. To show the compliance with FAA airworthiness standard regarding the presented protection designs, three steps, including lightning strike analysis, lightning environment analysis and certification test, were conducted in accordance with FAA AC 20-53.

• 한국자동차공학회논문집
• /
• 제25권1호
• /
• pp.1-10
• /
• 2017

In reverse engineering, one of the main tasks is reconstructing the mechanical properties of used materials. For an isotropic material, it could be defined by a single tensile test using a coupon extracted from the structure. In contrast, CFRP composites require many tests and complex procedures to define all the material properties because CFRP is an orthotropic material and a stacked laminate. In this paper, the procedure to reconstruct composite material properties is studied by using the classical lamination theory and the test data of three different laminates from a composite structure. A sample reconstruction of composite material properties using a composite car body is introduced to verify the method.

• 한국재난정보학회 논문집
• /
• 제12권4호
• /
• pp.432-439
• /
• 2016

방호 방폭 보강용 복합재료의 특성상 모델을 구성하고 사용하기 위해서는 재료 각각의 물성치가 필요하며, 이러한 물성 데이터를 도출하기 위해서는 수많은 실험을 통해 도출된 결과를 여러 계산식을 통하여 도출된 값으로 입력해야 하며, 일반적인 재료가 아닌 특수 목적용 소재의 경우는 이를 수행하는데 많은 어려움이 있다. 본 연구에서는 Ansys Workbench 환경에서 제공하는 복합재 적용 물성을 적용하여 ACP와 AUTODYN에서 방호 방폭 보강용 복합섬유 패널의 모델링 및 구조 해석을 수행하였다.

• 한국강구조학회 논문집
• /
• 제16권5호통권72호
• /
• pp.621-628
• /
• 2004

본 연구에서는 보강판의 좌굴방지를 위해 기존에 주로 사용되는 보강재를 복합재료를 사용하여 대체하는 새로운 개념을 소개한다. 강재 보강재를 복합재료로 대체함으로써 용접의 불편함과 피로 등에 의한 손상 및 부식을 원천적으로 제거할 수 있다. 강판에 접착되는 복합재료는 강판이 좌굴할 때까지 완전히 접착된 것으로 가정하였다. 이렇게 구성되는 판은 길이와 폭 방향으로 변단면의 형태를 가지며 비등방성의 재료특성을 나타낸다. 이러한 비등방성 변단면 판의 좌굴해석을 위해 범용 유한요소 프로그램인 LUSAS를 사용하였으며 여러 가지 매개변수 변화 해석을 통해 비등방성 변단면 판의 좌굴거동 특성을 살펴보았다.

• 한국분말재료학회지
• /
• 제14권5호
• /
• pp.292-297
• /
• 2007

The present study was focused on the synthesis of a $TiB_2$ dispersed copper matrix composite material by the combination of the mechanical milling and plasma activated sintering processes. The $Cu/TiB_2$ mixed powder was prepared by the combination of the mechanical milling and reduction processes using the copper oxide and titanium diboride powder as the raw material. The synthesized $Cu/TiB_2$ mixed powder was sintered by the plasma activated sintering process. The hardness and electric conductivity of the sintered bodies were measured using micro vickers hardness and four probe method, respectively. The relative density of $Cu/TiB_2$ composite material sintered at $800^{\circ}C$ showed about 98% of theoretical density. The $Cu-1vol%TiB_2$ composite material has a hardness of about 130Hv and an electric conductivity of about 85% IACS. The hardness and electric conductivity of $Cu-3vol%TiB_2$ composite material were about 140 Hv and about 45% IACS, respectively.

• Structural Engineering and Mechanics
• /
• 제85권5호
• /
• pp.573-592
• /
• 2023

This paper presents a careful theoretical investigation into interfacial stresses in composite aluminum-slab reinforced concrete beam bonded by a prestressed hybrid carbon-glass composite material. The model is based on equilibrium and deformations compatibility requirements in and all parts of the strengthened beam, i.e., the aluminum beam, the slab reinforced concrete, the hybrid carbon-glass composite plate and the adhesive layer. The theoretical predictions are compared with other existing solutions. Numerical results from the present analysis are presented both to demonstrate the advantages of the present solution over existing ones and to illustrate the main characteristics of interfacial stress distributions. It is shown that the stresses at the interface are influenced by the material and geometry parameters of the composite beam. This research is helpful for the understanding on mechanical behaviour of the interface and design of the hybrid structures.

• 대한조선학회논문집
• /
• 제46권2호
• /
• pp.203-217
• /
• 2009

The researches on the development of composite material propeller with outstanding damping effects have been actively attempted for the reduction of radiation noise of underwater vehicle propeller. Composite material suitable for the flexible propeller has the following advantages, such as high specific strength and specific stiffness, low thermal expansion coefficient, high resistance against environmental deterioration, low possibility of corrosion due to cavitation, nonoccurrence of rapid fracture due to fatigue, easy molding of complicated shape, easy repair maintenance and low production costs, etc. For the confirmation of optimal fiber array structures of composite material for the production of the flexible propeller blades, in this study, mechanical characteristics of its specimens according to materials were obtained and structural characteristics of propeller blade were also examined according to materials and stacking fiber arrays.

• 한국의류학회지
• /
• 제33권5호
• /
• pp.701-710
• /
• 2009

This study was conducted to develop excellent insole with good thermal insulation using new materials. We investigated that aerogel/fiber composite can be used as padding materials of shoes by comparing surface shape, moisture regain, water vapor permeability, thermal insulation and compression rate of insole materials tried with nonwoven fabric padding materials and insole sold in market. The results are as follows. Surface shapes were shown that the most appropriate material for sealing aerogel/fiber composite was high density fabric as per size of particle of aerogel. Moisture regain of aerogel/fabric composite was better than nonwoven fabric padding samples. However, when compared to insole sold in market, its moisture regain was worse than those of insole merchandises. Water vapor permeability was higher in material padded with nonwoven fabric than materials padded with aerogel/fiber composite in all three kinds of sealing fabrics. Thermal conductivity of aerogel/fabric composite was lower than nonwoven fabric material regardless of sealing fabrics. Thermal insulation of aerogel/fiber composite was higher than padding material of nonwoven fabric regardless of sealing fabrics. Compression rate of nonwoven (SP1) was higher than that of aerogel/fiber composite (SP2). Compressive elastic recovery rate of SP1 was also higher than that of SP2, which its compression rate and compressive elastic recovery rate were both poor. As the above result, ultra porous aerogel/fiber composite were proved to be material of good thermal insulation with lower thermal conductivity and also compression rate was proved to be low. Therefore, we can say that aerogel/fiber composite have high possibility to be used as insole materials for cold winter shoes requiring good thermal insulation protection.

• 한국철도학회:학술대회논문집
• /
• 한국철도학회 1999년도 추계학술대회 논문집
• /
• pp.437-446
• /
• 1999

The structural behavior of the composite material light rail vehicle body are investigated. Composite material is very useful for light rail vehicle structure due to its high specific strength and lightweight characteristics. The main carbody is made of aluminum alloy. The side wall and roof with composite panels can reduce total vehicle weight about 2000kg. In addition, with the lower density of the foam, enhances lightness in the panel and to save the operation expenses. The finite element analysis code, ANSYS is used to evaluate the stability of the body structure under the various load conditions.

• 전산구조공학
• /
• 제10권2호
• /
• pp.225-232
• /
• 1997

서로 다른 기지의 성질을 갖는 재료들을 혼합하여 만든 합성재료의 새로운 물성치는 일반적으로 실험으로 규명하고 있다. 혼합하는 재료들의 체적비에 따라 실험으로 측정한 합성재료의 탄성계수와 포와송비는 그 합성재료로 만들어지는 구조물의 역학적 거동을 예측하는 해석적 모델의 기본자료로 사용된다. 합성재료 탄성물성치의 수치적 예측은 합성재료에 대한 유한요소 모델로 해석한 정적변위와 균질.등방성으로 가정한 모델을 해석한 정적변위와의 차이를 최소화하는 구속적 비선형 최적화기법을 사용하여 수행하였다. 유한요소 모델은 체적비에 따라 혼합물질을 분배하기 용이하도록 제안하였으며 구속조건 및 하중조건은 일축인장에 의한 거동을 예측하도록 설정하였다. 본 논문에서는 고체입자를 섞어 만든 합성재료의 탄성물성치를 예제를 통하여 수치적으로 예측하고 그 결과를 실험결과 및 이론식들과 비교.검토하였다.