• Title/Summary/Keyword: 초경량자체

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Lightweight Automobile Design with ULSAB Concept Using Structural Optimization (구조 최적설계 기법을 이용한 초경량차체 개념의 경량 자동차 설계)

  • 신정규;송세일;이권희;박경진
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.14 no.3
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    • pp.277-286
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    • 2001
  • Among the ULSAB methods for the lightweight automobile body, Tailor Welded Blank(TWB) is adopted and the design process is developed for the existing component. Topology optimization conducted to find the distribution of the variable thickness. The number of parts and the welding lines are determined from it. In the detail design, size optimization is carried out to find the optimum thickness of each part and then, the final parting lines are tuned by shape optimization. A commercial optimization software GENESIS is utilized for the optimization processes.

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Design and Implementation of Tiny TCP/IPv6 Protocol for Wireless Sensor Networks (센서 네트워크를 위한 초경량 TCP/IPv6 프로토콜의 설계 및 구현)

  • Kim, Shin-Jae;Kim, Young-Gyun;Lee, Wan-Jik;Heo, Seok-Yeol;Shin, Bum-Joo
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.10 no.8
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    • pp.1955-1961
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    • 2009
  • As a core technology realizing ubiquitous world, recent researches are being concentrated to wireless sensor network. However, most research results were focused to the sensor network technology itself, even though interworking between the sensor network and Internet is also one of primitive requirements for ubiquitous world. In this paper, we design the tiny TCP/IPv6 profile which makes it possible to inter-connect the sensor network device to IPv6 based Internet. To confirm operation of the designed profile, we experimentally implemented and evaluated minimum TCP/IPv6 based on TinyOS. The evaluation result shows that throughput of our tiny TCP/IPv6 is almost same as that of TinyOS component.

Status And Perspectives of Ultra-Lightweight Silica Aerogel Superinsulation Materials (초경량 실리카 에어로젤 초단열재의 현황 및 전망)

  • Dong Jin, Suh
    • Clean Technology
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    • v.28 no.4
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    • pp.301-308
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    • 2022
  • Since nanoporous silica aerogel was first synthesized in 1931, its potential as an ultra-lightweight superinsulation material has been steadily attracting attention. Silica aerogel is the best thermal insulation material to date. However, the potential applications of this lightweight material have so far been hindered by its inherent fragibility and brittleness arising from its ultra-porous nature. Although the monolithic form of silica aerogel has the best ultra-lightweight superinsulation properties, it cannot be used in this form. Instead it is used in the form of powders, particles, and blankets. However, these forms still have shortcomings. Silica aerogel is most widely applied in the form of a fiber-reinforced aerogel blanket, but this form is likely to generate dust when handled. Although silica aerogel particles have been proven to be non-toxic to humans, dust formation remains a major barrier to the widespread application of silica aerogel blankets. This paper will investigate the unique properties of silica aerogel and determine what fields it can be used in or potentially be used in due to its unique properties. In addition, we will review the important advances in silica aerogel synthesis technology and its commercialization so far, and then consider the problems that exist for its widespread commercialization in the future and how to overcome them.

A Study on Development and Site selection of an AIRFIELD (경비행장 개발 및 입지선정에 관한 연구)

  • Park, Sang-Yong
    • The Korean Journal of Air & Space Law and Policy
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    • v.30 no.2
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    • pp.3-36
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    • 2015
  • As of end of 2014, the population engaging in aviation activities for leisure has reached approximately 13 million, where approximately 356 cases involve a general aircraft, 200 cases involve light aircraft, and 636 cases involve an ULM. The industry for leisure has become a very promising industry in line with rapidly rising living standards which are expected to further increase in the future. The demand for such services is expected to increase over time. The purpose of this paper is to review the development and site selection of airfields in anticipation of these developments in the industry. While the government also has experience in the review of airfield location and candidate sites, it is not the government that carries out the actual construction. As such, the feasibility of the site needs to be verified in terms of actual construction. This study identified factors for Site Selection of factors through a review of related documents and existing research reports. A questionnaire was also used to collect the views of experts in the field, which was then analyzed. The Research model was confirmed in the layered form for an AHP analysis. The factors for Site Selection were identified as the technical / operational factors and economic / political elements for a two-stage configuration. The third step consisted of technical and operational elements. The final step is was constructed a total of 11 elements (weather, surface conditions, obstacle limitation surface, airspace conditions, operating procedures, noise problems, environmental issues, availability of facilities, construction and investment costs, contribution to the local economy, accessibility, demand / the proximity of demand). The surveys are conducted for more than 10 General and light aircraft pilots, professionals, and instructor. The analysis results showed a higher level in the technical / operating elements (73.2%) in the first step, while the next step sawa higher level of the operational elements (30.9%) than the other. The factors for Site Selection were any particular elements did not appear high, the weather conditions (17.5%), noise problems (19.8%), the proximity of demand (6%), accessibility (5.7%), environmental issues (11.1%), availability of facilities (8%), airspace conditions (7.9%), obstacle limitation surface (12%), construction and investment costs (4.2%) and to operating procedures (4.9%), contribution to the local economy (3.8%).

Pulse GMA weldability evaluation for 440MPa coated and uncoated steel (440MPa 급 도금, 비도금 강판의 Pulse GMA 용접성 평가)

  • So, Woo-Ju;Kim, Dong-Cheol;Kang, Mun-Jin
    • Proceedings of the KWS Conference
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    • 2010.05a
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    • pp.67-67
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    • 2010
  • 최근 전 세계적으로 유가상승 및 환경에 대한 관심이 증대되면서 자동차 업계에서는 차량 경량화를 통한 연비향상에 대한 연구가 활발히 진행되고 있다. 대표적인 차량 경량화 방법으로 초경량 철강 차체의 개발을 들 수 있는데 이는 고강도강을 차체에 적용함으로써 강성을 증대시킴과 동시에 두께 감소에 의한 경량화를 이루는 방법이다. 하지만 고강도강은 자체의 높은 강성을 지니는 반면 첨가된 합금원소에 의하여 용접성이 떨어지는 제약을 가지고 있다. 펄스 GMA 용접은 One Drop Per Pulse (ODPP) 의 안정된 용적 이행으로 스패터 발생이 거의 없으며 일반 GMA 용접에 비하여 용접성이 우수하여 자동차 차체 조립공정에 적용되고 있다. 본 연구에서는 440MPa 급 도금, 비도금 강판 및 이종 강판의 겹치기 용접 실험을 통해 강종별, 두께별 펄스 아크 용접에 대한 용접성 평가 및 데이터 베이스를 구축하고자 하였다. 용접부 단면마크로, 인장시험, 경도시험을 통해 적정 용접영역을 확보하였으머, 고속카메라 촬영을 통해 보호가스에 따른 용적 이행 현상을 확인하였다.

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Pulse GMA weldability of AHSS for Automobile body (자동차 차체용 AHSS 소재에 대한 펄스 GMA 용접성 평가)

  • So, Woo-Ju;Kim, Dong-Cheol;Kang, Mun-Jin;Rhee, Se-Hun
    • Proceedings of the KWS Conference
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    • 2009.11a
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    • pp.31-31
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    • 2009
  • 최근 전세계적으로 유가상승 및 환경에 대한 관심이 증대되면서 자동차 업계에서는 차량 경량화를 통한 연비향상에 대한 연구가 활발히 진행되고 있다. 대표적인 기술개발 사례로서 초경량 철강 차체의 개발을 들 수 있다. 이는 고장력강을 적용함으로써 강성을 증대시킴과 동시에 두께감소에 의한 경량화를 이루고자 추진되고 있다. 하지만 고장력강은 자체의 높은 강성을 지니고 있는 반면, 일반 강종에 비해서 스프링백이 크고 용접성도 많이 떨어지는 제약을 안고 있다. 아크 용접법 중 하나인 AC pulse MIG 용접은 DCEP (direct current electrode positive) 와 DCEN (direct current electrode positive) 구간이 주기적으로 반복하는 용접법으로 스패터 발생이 거의 없으며 특히 갭 접합성이 우수하여 자동차 차체 조립공정에 적용되고 있다. 본 연구에서는 자동차 차체용 AHSS 소재의 겹치기 용접 실험을 통해 실제 생산라인에서 용접 이음부에 발생되는 갭에 대해 강건한 용접 공정 조건을 제시하였다. 먼저 고속카메라 촬영을 통해 AC pulse MIG 용접에서 EN ratio 변화에 따른 와이어 용융현상을 분석 하였으며 단면마크로, 인장시험, 인장 파단면 분석을 통해 겹치기 용접에서 0~2mm 사이의 갭 발생에 강건한 용접 조선을 제시하였다.

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Research about Multi-spectral Photographing System (PKNU No.2) Development (다중영상촬영을 위한 PKNU 2호 개발에 관한 연구)

  • 최철웅;김호용;전성우
    • Korean Journal of Remote Sensing
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    • v.19 no.4
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    • pp.291-305
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    • 2003
  • The cost of deploying Geological and Environmental information gathering systems, especially when such systems obtain remote sensing and photographic data through the use of commercial satellites and aircraft. Besides the high cost equipment required, adverse weather conditions can further restrict a researcher's ability to collect data anywhere and anytime. To mitigate this problem, we have developed a compact, multi-spectral automatic Aerial photographic system. This system's Multi-spectral camera is capable of the visible (RGB) and infrared (NIR) bands (3032*2008 pixel). It consists of a thermal infrared camera and automatic balance control, and can be managed by a palm-top computer. Other features includes a camera gimbal system, GPS receiver, weather sensor among others. We have evaluated the efficiency of this system in several field tests at the following locations: Kyongsang-bukdo beach, Nakdong river (at each site of mulkeum-namji and koryung-gumi), and Kyungahn River. Its tested ability in aerial photography, weather data, as well as GPS data acquisition demonstrates its flexibility as a tool for environmental data monitoring.

LUAV Software Certification Method using Checklists based on DO-178C (DO-178C 기반 체크리스트를 활용한 무인동력비행장치 소프트웨어 인증 방안)

  • Ji-Hun Kwon;Dong-Min Lee;Kyung-Min Park;Eun-Hee Lee;Sauk-Hoon Im;Yong-Hun Choi;Jong-Whoa Na
    • Journal of Aerospace System Engineering
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    • v.17 no.1
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    • pp.33-41
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    • 2023
  • As seen in the case of the Boeing 737 Max accident, the proportion of aircraft software is rapidly increasing. However, it is vulnerable to safety issues. In case of domestic aircraft software, to operate a Light Unmanned Aerial Vehicle (LUAV) less than an empty weight of 150 kg, safety certification is required for an Ultra-Light Vehicle (ULV). However, software certification procedure is not included. Since the use of LUAVs has increased recently, software verification is required. This paper proposed a checklist of LUAV software that could be applied to LUAV referring DO-178C, an aviation software certification standard. A case study of applying the proposed checklist to the Model-based Development-based Helicopter Flight Control Computer (FCC) project currently used by domestic and foreign advanced companies and institutions was conducted.

Research for Calibration and Correction of Multi-Spectral Aerial Photographing System(PKNU 3) (다중분광 항공촬영 시스템(PKNU 3) 검정 및 보정에 관한 연구)

  • Lee, Eun Kyung;Choi, Chul Uong
    • Journal of the Korean Association of Geographic Information Studies
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    • v.7 no.4
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    • pp.143-154
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    • 2004
  • The researchers, who seek geological and environmental information, depend on the remote sensing and aerial photographic datum from various commercial satellites and aircraft. However, the adverse weather conditions and the expensive equipment can restrict that the researcher can collect their data anywhere and any time. To allow for better flexibility, we have developed a compact, a multi-spectral automatic Aerial photographic system(PKNU 2). This system's Multi-spectral camera can catch the visible(RGB) and infrared(NIR) bands($3032{\times}2008$ pixels) image. Visible and infrared bands images were obtained from each camera respectively and produced Color-infrared composite images to be analyzed in the purpose of the environment monitor but that was not very good data. Moreover, it has a demerit that the stereoscopic overlap area is not satisfied with 60% due to the 12s storage time of each data, while it was possible that PKNU 2 system photographed photos of great capacity. Therefore, we have been developing the advanced PKNU 2(PKNU 3) that consists of color-infrared spectral camera can photograph the visible and near infrared bands data using one sensor at once, thermal infrared camera, two of 40 G computers to store images, and MPEG board to compress and transfer data to the computer at the real time and can attach and detach itself to a helicopter. Verification and calibration of each sensor(REDLAKE MS 4000, Raytheon IRPro) were conducted before we took the aerial photographs for obtaining more valuable data. Corrections for the spectral characteristics and radial lens distortions of sensor were carried out.

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