• Title/Summary/Keyword: 역설계.

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Reverse Engineering (역설계)

  • Nobles, Herbert D.
    • Journal of the KSME
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    • v.33 no.4
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    • pp.311-314
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    • 1993
  • 역설계란 제품에서부터 역으로 그것의 수학적인 형상을 얻는 기법이다. 생산현장과 설계분야에서 역설계의 응용사례는 많다. 예를 들면 자동차 외형설계자는 자유곡면(free form)을 만들고, 이것 에서 역으로 스템핑 다이(stamping die)를 가공한다. 물론 외형 설계자는 자유곡면을 생성하기 위해 스틸이나 커크사이트(kirtsite)보다는 원하는 형상을 만들기 쉬운 진흙을 사용한다. 생산부 서에서는 가공물의 설계도가 분실되거나 훼손되어 완성된 제품에서 도면이 복사되어야 할 경우가 생기게 된다. 역설계는 복제가 요구되는 어떤 형상도 적용이 가능하다. 응용대상은 특히 완구, 인조팔, 스템핑다이, 폼 블록(from block), 욕조기, 가구, 일상용품 등이며 적용대상은 광범위하다. 역설계는 설계자가 습득해야 할 필요기술이고, 현재의 CAD/CAM 적용영역을 새로운 세계로 확대시킬 것이다.

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3D Image Scan Data-based Sweeping Shape Reconstruction Algorithm (3D 이미지 스캔 데이터 기반 SWEEPING 형상 역설계 알고리즘)

  • Kang, Tae-Wook
    • Annual Conference of KIPS
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    • 2015.04a
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    • pp.896-897
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    • 2015
  • 본 연구는 3D 이미지 스캔 데이터 기반으로, SWEEPING 형상을 효과적으로 역설계하는 기술에 관한 것이다. 사용자가 미리 정의한 형상 단면 모델 데이터베이스를 이용해, 3차원 SWEEPING 형상을 자동으로 역설계하는 알고리즘을 제안한다. 이를 위해, 3D 이미지 스캔 데이터인 포인트 클라우드에서 자동으로 추출한 단면 포인트들을 처리해, 파라메터 정보를 추출하고, 미리 정의된 형상 단면들과 상호간 유사도를 비교한 후, 가장 유사한 형상 단면을 획득한다. 이러한 기술은 SWEEPING 형상 모델의 역설계 과정을 자동화하는 데 도움을 줄 것이다.

System Architecture for Effective Point Cloud-based Reverse Engineering of Architectural MEP Pipe Object (효과적인 포인트 클라우드 기반 건축 MEP 파이프 객체 역설계 처리를 위한 시스템 아키텍처)

  • Kang, Tae-Wook
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.15 no.9
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    • pp.5870-5876
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    • 2014
  • The aim of this study was to suggest the System Architecture for Effective Architectural MEP Pipe Reverse Design(PRD) based on the Point Cloud and derive the consideration. To do this, the requirement and use-cases related to the MEP pipe reverse design work were defined and the architecture for the reverse design automation was proposed. To identify a consideration for finding the architecture issues, a prototype was developed using the architecture and evaluated.

A Study on Optimal Laser Scanning method for Reverse Engineering at Interior Remodeling Project (리모델링 프로젝트의 역설계 적용을 위한 최적 3차원 레이저 스캐닝 정보 획득 방안에 관한 연구 - 실내 리모델링을 대상으로 -)

  • Lee, Sangseol;Kwon, Soonwook
    • Korean Journal of Construction Engineering and Management
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    • v.15 no.3
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    • pp.3-11
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    • 2014
  • Recently, remodeling construction project has been prevalently conducted in major city areas in Korea. However, remodeling construction project has a difficulty in conducting a construction because of non-existing drawing or lack of drawing information. To solve these problems, modeling techniques by using reverse engineering have been widely studied in other industries such as aerospace and automobile industry. But reverse engineering techniques have not been used in remodeling construction projects because those technology haven't supplied less accuracy during required time for surveying. So, this study suggests optimal method of acquiring accurate 3D laser scanner information for reverse engineering at interior remodeling project.

Reverse-Engineering and Analysis of Performance for Medium-Altitude Long Endurance Unmanned Aerial Vehicle (중고도-장기체공 무인비행을 위한 비행체 성능 분석 및 역설계)

  • Shim, Ho-Joon;Chang, Kyoungsik;Chung, In Jae;Kim, Sun-Tae;Joh, Chang-Yeol
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.44 no.6
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    • pp.520-529
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    • 2016
  • The main purpose of this study was to analyze the performance of a medium-altitude long endurance unmanned aerial vehicle through reverse-engineering method. The external configuration data of the RQ-1 Predator was reverse-engineered from related photos and specification data available on public domains, which also were used to generate the CATIA modeling and weigh distribution data of the UAV. The aerodynamic characteristics of RQ-1 Predator were mainly predicted the vortex lattice method and an empirical method, which the propeller performance was analyzed by the empirical method proposed by Howe. The rate of climb, service ceiling, range, and the loiter endurance of the UAV was analyzed, which showed good agreement with the reference data.

Geometry-to-BIM Mapping Rule Definition for Building Plane BIM object (건축물 평면 형상에 대한 형상-to-BIM 맵핑 규칙 정의)

  • Kang, Tae-Wook
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.20 no.10
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    • pp.236-242
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    • 2019
  • Recently, scanning projects have been carried out in various construction and construction fields for maintenance purposes. The point cloud generated by the scan results is composed of a number of points representing the object to be scanned. The process of extracting the necessary information, including dimensions, from such scan data is called paradox. The reverse engineering process of modeling a point cloud as BIM involves considerable manual work. Owing to the time-consuming reverse engineering nature of the work, the costs increase exponentially when rework requests are made, such as design changes. Reverse engineering automation technology can help improve these problems. On the other hand, the reverse design product is variable depending on the use, and the kind and detail level of the product may be different. This paper proposes the G2BM (Geometry-to-BIM mapping) rule definition method that automatically maps a BIM object from a primitive geometry to a BIM object. G2BM proposes a process definition and a customization method for reverse engineering BIM objects that consider the use case variability.

Reverse Design for Composite Rotor Blade of BO-105 Helicopter (BO-105 헬리콥터 복합재 로터 블레이드 역설계)

  • Lee, Chang-Bae;Jang, KiJoo;Im, Byeong-Uk;Shin, SangJoon
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.49 no.7
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    • pp.539-547
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    • 2021
  • Helicopter rotor blade is required to be designed by considering the interacting effects among aerodynamics, flexibility, and controllability. The reverse design allows the structural components to have common characteristics by using the configuration numerics and experimental results. This paper aims to design the composite rotor blade which will feature common characteristics with that of BO-105. The present engineering design procedure is done by dividing the rotor blade into a few sections and composite laminates across the cross section. For each section, variational asymptotic beam sectional analysis (VABS) program is used to evaluate its flapwise, lagwise, and torsion stiffnesses to have discrepancy smaller than certain tolerance. Finally, CAMRAD II is used to predict the stress acting on the rotor blade during the specific flight condition and to check whether the present deign is structurally valid.

The Inverse Design Technique of Propeller Blade Sections Using the Modified Garabedian-McFadden Method (Modified Garabedian-McFadden 방법을 이용한 프로펠러 날개 단면의 역설계 기법)

  • C.M. Jung;J.K. Cho;W.G. Park
    • Journal of the Society of Naval Architects of Korea
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    • v.36 no.4
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    • pp.28-36
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    • 1999
  • An efficient inverse design method based on the MGM(Modified Garabedian-McFadden) method has been developed. The 2-D Navier-Stokes equations are solved for obtaining the surface pressure distributions and coupled with the MGM method to perform the inverse design. The MGM method is a residual-correction technique, in which the residuals are the difference between the desired and the computed pressure distribution. The developed code was applied to several airfoil shapes and the propeller. It has been found that they are well converged to their targeting shapes.

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Reverse Engineering Procedure of Metal Brake Pad for Part 25 Aircraft (수송류 항공기용 금속계 제동패드의 역설계 절차)

  • Min-ji Kim;Kyung-il Kim;Kyung-taek Kim
    • Journal of Advanced Navigation Technology
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    • v.27 no.5
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    • pp.621-628
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    • 2023
  • This study derived a reverse engineering procedure for verifying the design identity of original parts and developed parts for PMA(Parts Manufacturer Approval) and STC(Supplemental Type Certificate) of metal brake pads for transport aircraft, which are critical parts among aircraft parts and equipment. In Korea, the regulations for reverse engineering procedures are regulated by the Parts Manufacturer Approval Guidelines, and in the United States, AC No. 21. 303-4. In the reverse engineering for the brake pad, the detailed procedures for each component were determined by selecting verification test items to confirm identity based on sample quantity, dimensional tolerance, mechanical property measurement, material, weight and volume characteristics for each component. In addition, as a result of analyzing the regulation of Korea and United States, in the case of Korea, it is necessary to establish technical standards for braking systems for transport aircraft and regulations related to flight tests.