• Title/Summary/Keyword: defense structures

Search Result 280, Processing Time 0.027 seconds

Flexural properties, interlaminar shear strength and morphology of phenolic matrix composites reinforced with xGnP-coated carbon fibers

  • Park, Jong Kyoo;Lee, Jae Yeol;Drzal, Lawrence T.;Cho, Donghwan
    • Carbon letters
    • /
    • v.17 no.1
    • /
    • pp.33-38
    • /
    • 2016
  • In the present study, exfoliated graphite nanoplatelets (xGnP) with different particle sizes were coated onto polyacrylonitrile-based carbon fibers by a direct coating method. The flexural properties, interlaminar shear strength, and the morphology of the xGnP-coated carbon fiber/phenolic matrix composites were investigated in terms of their longitudinal flexural strength and modulus, interlaminar shear strength, and by optical and scanning electron microscopic observations. The results were compared with a phenolic matrix composite counterpart prepared without xGnP. The flexural properties and interlaminar shear strength of the xGnP-coated carbon fiber/phenolic matrix composites were found to be higher than those of the uncoated composite. The flexural and interlaminar shear strengths were affected by the particle size of the xGnP, while the particle size had no significant effect on the flexural modulus. It seems that the interfacial contacts between the xGnP-coated carbon fibers and the phenolic matrix play a role in enhancing the flexural strength as well as the interlaminar shear strength of the composites.

The Holding Characteristics of the Glass Filter Separators of Molten Salt Electrolyte for Thermal Batteries (열전지용 용융염 전해질의 유리필터분리판의 담지특성)

  • Cho, Kwang-Youn;Riu, Doh-Hyung;Huh, Seung-Hun;Shin, Dong-Geun;Kim, Hyoun-Ee;Cheong, Hae-Won;Cho, Sung-Baek
    • Journal of the Korean Ceramic Society
    • /
    • v.45 no.8
    • /
    • pp.464-471
    • /
    • 2008
  • The electrolyte separator for thermal battery should be easily handled and loaded a large amount of the molten salt. Ceramic fibers, especially fibrous commercial glass filters were used as an electrolyte separator and the lithium based molten salts were infiltrated into the ceramic filters. The pore structures of the ceramic filter and the melting properties of the lithium salts affected to the electrolyte loading and leakage. During the infiltration, ions of $Li^+$ and $F^-$ in the molten salts were reacted with the glass fiber and caused to be weaken the fiber strength.

Pyroshock Measurement and Characteristic Analysis of Explosive Bolt and Pyrotechnic Initiator (폭발볼트와 착화기의 파이로충격 계측 및 특성 분석)

  • Lee, Juho;Hwang, Dae-Hyun;Jang, Jae-Kyeong;Lee, YeungJo;Kim, Dong-Jin;Lee, Jung-Ryul;Han, Jae-Hung
    • Transactions of the Korean Society for Noise and Vibration Engineering
    • /
    • v.27 no.2
    • /
    • pp.213-220
    • /
    • 2017
  • Pyroshock produced by the pyrotechnic devices can induce failures in nearby electronic devices. To handle and mitigate pyroshock inducing problems, appropriate measurement of pyroshock is essential. In this study, pyroshock measurement technique is established using laser Dopper vibrometers (LDVs) and shock accelerometers. Pyroshock produced by the explosive bolts and the pyrotechnic initiators under various environments is measured. The characteristics of pyroshock including the effects of supporting structures, propagation form on thin plate, sensor (contact and non-contact) types are discussed.

Data Structure for the Design Program of Solid Rocket Motors (고체 추진기관 구조체 설계 프로그램 개발을 위한 설계 부품 자료 구조)

  • Lee, Kang-Soo;Kim, Won-Hoon;Lee, Bang-Eop
    • Korean Journal of Computational Design and Engineering
    • /
    • v.17 no.5
    • /
    • pp.364-374
    • /
    • 2012
  • In this paper, we proposed a data structure to represent structural components of solid rocket motors (SRM) in an automated design program. To propose the data structure, we searched the necessary functions for the automated design program should have. In order to design the structural components of solid rocket motors sufficiently with a design program, it should have the functions to represent the shapes of the components, the drawing and analysis models, the design variables, various product structures, interferences, characteristic properties, design equations, and tightening sets. By modifying the data structure of an element object that is a general purpose data structure to represent a general component of a product, a new data structure was proposed to satisfy all the necessary functions with optimum. Finally, a design program for the structural components of solid rocket motors was developed successfully with the proposed data structure.

A Study of the Affected Layer and Stress Corrosion Crack of Ultra-high-strength Steel (300M) for Aircraft Parts (항공기용 초고장력강(300M) 부품의 가공변질층과 응력부식균열에 관한 연구)

  • Ahn, Jinwoo;Kim, Taehwan
    • Journal of the Korean Society of Manufacturing Process Engineers
    • /
    • v.19 no.4
    • /
    • pp.1-8
    • /
    • 2020
  • Mechanical components that support structures in aerospace and power generation industries require high-strength materials. Particularly, in the aerospace industry, aluminum alloys, titanium alloys, and composite materials are increasingly used due to their high maneuverability and durability to withstand low temperature extreme environments; however, ultra-high-strength steel is still used in key components under heavy loads such as landing gears. In this paper, the fault cause analysis and troubleshooting of aircraft parts made of ultra-high-strength steel (300M) broken during normal operation are described. To identify the cause of the defect, a temporary inspection of the same aircraft was performed, and material testing, non-destructive inspection, microstructure examination, and fracture area inspection of the damaged parts were performed. Fracture analysis results showed that a crack in the shape of a branch developed from the tool mark in the direction of the intergranular strain. Based on the results, the cause of fracture was confirmed to be stress corrosion.

Contribution Analysis to Identify the Source of Ship Hull Vibration (선체 진동 특성 규명을 위한 기여도 분석)

  • Lee, Jun Woo;Ahn, Se Jin;Oh, Jun Seok;Kim, Tae Hyeong;Jeong, Weui Bong
    • Transactions of the Korean Society for Noise and Vibration Engineering
    • /
    • v.26 no.5
    • /
    • pp.528-535
    • /
    • 2016
  • The vibration of a ship gives a significant effect on the noise radiated into the water. This paper focused on the vibration of ship hull due to the sub-generator located on the deck in the anchored condition. The contributions of the transfer paths between sub-generator and ship hull were analyzed using the TPA and the OTPA method. While the sub-generator was operation and the main engine was turned off, the vibrations were measured simultaneously at the 38 locations of the ship and the one hydrophone was arranged to measure the underwater radiated noise at the overside ship. The results of the transfer path by applying TPA and OTPA were compared and discussed. As a result of these methods, the top of stovepipe and valve are contributive. Reinforcing these structures is the most effective to reduce the vibration of ship hull.

Gradient field based method for segmenting 3D point cloud (Gradient Field 기반 3D 포인트 클라우드 지면분할 기법)

  • Vu, Hoang;Chu, Phuong;Cho, Seoungjae;Zhang, Weiqiang;Wen, Mingyun;Sim, Sungdae;Kwak, Kiho;Cho, Kyungeun
    • Proceedings of the Korea Information Processing Society Conference
    • /
    • 2016.10a
    • /
    • pp.733-734
    • /
    • 2016
  • This study proposes a novel approach for ground segmentation of 3D point cloud. We combine two techniques: gradient threshold segmentation, and mean height evaluation. Acquired 3D point cloud is represented as a graph data structures by exploiting the structure of 2D reference image. The ground parts nearing the position of the sensor are segmented based on gradient threshold technique. For sparse regions, we separate the ground and nonground by using a technique called mean height evaluation. The main contribution of this study is a new ground segmentation algorithm which works well with 3D point clouds from various environments. The processing time is acceptable and it allows the algorithm running in real time.

WORM-HUNTER: A Worm Guard System using Software-defined Networking

  • Hu, Yixun;Zheng, Kangfeng;Wang, Xu;Yang, Yixian
    • KSII Transactions on Internet and Information Systems (TIIS)
    • /
    • v.11 no.1
    • /
    • pp.484-510
    • /
    • 2017
  • Network security is rapidly developing, but so are attack methods. Network worms are one of the most widely used attack methods and have are able to propagate quickly. As an active defense approach to network worms, the honeynet technique has long been limited by the closed architecture of traditional network devices. In this paper, we propose a closed loop defense system of worms based on a Software-Defined Networking (SDN) technology, called Worm-Hunter. The flexibility of SDN in network building is introduced to structure the network infrastructures of Worm-Hunter. By using well-designed flow tables, Worm-Hunter is able to easily deploy different honeynet systems with different network structures and dynamically. When anomalous traffic is detected by the analyzer in Worm-Hunter, it can be redirected into the honeynet and then safely analyzed. Throughout the process, attackers will not be aware that they are caught, and all of the attack behavior is recorded in the system for further analysis. Finally, we verify the system via experiments. The experiments show that Worm-Hunter is able to build multiple honeynet systems on one physical platform. Meanwhile, all of the honeynet systems with the same topology operate without interference.

Drift displacement data based estimation of cumulative plastic deformation ratios for buildings

  • Nishitani, Akira;Matsui, Chisa;Hara, Yushiro;Xiang, Ping;Nitta, Yoshihiro;Hatada, Tomohiko;Katamura, Ryota;Matsuya, Iwao;Tanii, Takashi
    • Smart Structures and Systems
    • /
    • v.15 no.3
    • /
    • pp.881-896
    • /
    • 2015
  • The authors' research group has developed a noncontact type of sensors which directly measure the inter-story drift displacements of a building during a seismic event. Soon after that event, such seismically-induced drift displacement data would provide structural engineers with useful information to judge how the stories have been damaged. This paper presents a scheme of estimating the story cumulative plastic deformation ratios based on such measured drift displacement information toward the building safety monitoring. The presented scheme requires the data of story drift displacements and the ground motion acceleration. The involved calculations are rather simple without any detailed information on structural elements required: the story hysteresis loops are first estimated and then the cumulative plastic deformation ratio of each story is evaluated from the estimated hysteresis. The effectiveness of the scheme is demonstrated by utilizing the data of full-scale building model experiment performed at E-defense and conducting numerical simulations.

Optimization of Sandwich Structures of a Small Aircraft Wing using Automated Aero- Structure Interaction Systems (자동화된 공력-구조 연계 시스템을 이용한 소형항공기 날개 샌드위치구조 최적설계)

  • Park, Chan Woo;Chu, Jae Myeong;Shul, Chang Won;Jun, Seung Moon
    • Journal of the Korean Society for Precision Engineering
    • /
    • v.30 no.10
    • /
    • pp.1061-1068
    • /
    • 2013
  • In this research, the design optimization of a composite sandwich has been performed for using as an airplane wing skin. Automated analysis framework for aero-structure interaction is used for calculating load data on the wing. For automated analysis framework, FLUENT is used for computational fluid dynamics (CFD) analysis. CFD mesh is generated automatically by using parametric modeling of CATIA and GAMBIT. A computational structure mechanics (CSM) mesh is generated automatically by the parametric method of the CATIA and visual basic script of NASTRAN-FX. The structure is analyzed by ABAQUS. Composite sandwich optimization is performed by NASTRAN SOL200. Design variables are thicknesses of the sandwich core and composite skin panel plies. The objective is to minimize the weight of the wing and constraints are applied for wing tip displacement, global failure index and local failure indexes.