• Title/Summary/Keyword: Deflection Angle

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Evaluation of Cutter Orientations in 5-Axis High Speed Milling of Turbine Blade (터빈블레이드의 5축 고속가공에서 가공경로와 공구기울임 방향의 선정)

  • 임태순;이유하;이득우;김정석
    • Proceedings of the Korean Society of Machine Tool Engineers Conference
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    • 2002.04a
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    • pp.155-160
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    • 2002
  • Recently, the development of aerospace and automobile industries has brought new technological challenges, rebated to the growing complexity of products and the new geometry of the models. High speed milling with a 5-Axis milling machine has been widely used fur 3D sculptured surface parts. When turbine blades are machined by a 5-axis milling, their thin and cantilever shape causes vibrations, deflections and twists. Therefore, the surface roughness and the waviness of the workpiece are not good. In this paper, the effects of cutter orientation and the lead/tilt angle used to machine turbine blades with a 5-axis high speed ball end-milling were investigated to improve geometric accuracy and surface integrity. The experiments were performed using a lead/tilt angle of 15$^{\circ}$ to the workpiece with four cutter directions such as horizontal outward, horizontal inward, vertical outward, and vortical inward directions. Workpiece deflection, surface roughness and the machined surface were all measured with various cutter orientations such as cutting directions, and lead/tilt angle. The results show that the best cutting strategy for machining turbine blades with a 5-axis milling is horizontal inward direction with a tilt angle.

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Dynamic Characteristics of Cantilever Pipe Conveying Fluid with Moving Mass Considering Nozzle Angle (노즐 경사각을 고려한 이동질량을 가진 유체이송 외팔 파이프의 동특성 해석)

  • 윤한익;손인수;김현수;조정래
    • Journal of Ocean Engineering and Technology
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    • v.16 no.6
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    • pp.18-24
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    • 2002
  • The vibrational system in this study consists of a cantilever pipe conveying fluid, the moving mass upon it, and an attached tip mass. The equation of motion is derived by using the Lagrange equation. The influences of the velocity and the velocities of fluid flow in the pipe have been studied on the dynamic behavior of a cantilever pipe using a numerical method. While the moving mass moves upon the cantilever pipe, the velocity of fluid flow and the nozzle angle increase; as a result, the tip displacement of the cantilever pipe, conveying fluid, is decreased. After the moving mass passes over the cantilever pipe, the tip displacement of the pipe is influenced by the potential energy of the cantilever pipe and the deflection of the pipe; the effect is the result of the moving mass and gravity. As the velocity of fluid flow and nozzle angle increases, the natural frequency of he system is decreased at the second mode and third mode, but it is increased at the first mode. As the moving mass increases, the natural frequency of the system is decreased at all modes.

Isolated Pore Generation Mechanism and Mechanical Properties in MAS System with 3Y-TZP (MAS계에서 3Y-TZP 첨가에 따른 독립 기공 생성기구와 기계적 성질)

  • 최성철;박현철
    • Journal of the Korean Ceramic Society
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    • v.30 no.11
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    • pp.881-890
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    • 1993
  • MAS system has narrow sintering temp. range due to the liquid phae sintering and thereby densify rapidly. And especially, its poor mechanical properties limitedthe industrial application. In this study, the improvement of mechanical properties and densification is suggested by the consideration of the toughening mechanisms and isolated pore generation mechanism which is derived by the liquid phase sintering theory in 3Y-TZP added composites. After Pressureless sintering up to 140$0^{\circ}C$ for 5hr, the dihedral angle and contact angle are analyzed by the observation of microstructure. As a result of microstructure analysis, the sintering stage of the specimen sintered for 5hr is analyzed as solid-skeleton stage. And the isolated pore generation mechanisms are considered as (1) The swelling of the liquid phase is predominent due to the facts that dihedral angle is larger than 60$^{\circ}$, contact angle is large and that liquid volume fraction is smaller than 10%. (2) The porous characteristics of the MAS system is also suggested as: the SiO2-rich liquid film is firstly formed at the srface and therefore this reduces the contiguity of the pore, which induces the isolated pore. The strength and fracture toughness increased with the addition of 3Y-TZP and the main fracture toughness improvement mechanisms are analyzed as the crack deflection.

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Performance of Sealing Integrity and Banding strain of HV Polymeric bushing with Thermal Mechanical Test (열-기계적 시험에 따른 초고압 폴리머 부싱의 굽힘변형 및 기밀성능에 관한 연구)

  • Cho, Han-Goo;Yoo, Dae-Hoon;Kang, Hyung-Kyung;Lee, Chul-Ho
    • Proceedings of the KIEE Conference
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    • 2009.07a
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    • pp.1441_1441
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    • 2009
  • This paper describes performance of sealing integrity and bending strain of HV polymeric bushing with thermal mechanical test. Generally the properties of FRP tube can be influenced by the winding angle, wall thickness and winding tension. As a results, multi winding bushing shows that it has max deflection in the range of 16.5~16.9 mm.

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사각펀치의 압입공정에서 예비성형체의 형상이 펀치변형에 미치는 영향

  • 박상수;이정민;김병민
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2004.05a
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    • pp.84-84
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    • 2004
  • 다단 냉간단조 공정에서는 결함이 없는 재료의 유동, 금형내부의 완전한 충만과 금형의 수명향상 등을 위하여 예비성형체의 설계가 중요시되고 있다. 특히 최근 제품의 정밀도에 관심이 집중되어 냉간 상태에서 완제품으로 성형하여 후속 기계가공을 없앰으로써 재료의 절약, 에너지 절감, 가공공정수 단축 등 냉간단조를 고부가가치 가공의 유력한 수단으로 응용하려는 추세이다. 이러한 경우 예비성형체의 형상은 제품의 정밀도와 금형의 수명에 지대한 영향을 미친다.(중략)

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Structural Behaviors for Pressurized Fabric Leaning Arches

  • Kim, Jae Yeol
    • Architectural research
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    • v.3 no.1
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    • pp.45-52
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    • 2001
  • In this paper, a pressurized single vertical arch and a pressurized leaning arch composed of flexible fabric material are considered. These arches have also been considered as a possible support structure for the tent-like structures. Two different boundary conditions are considered in leaning arches with fixed bases and pinned bases. The behaviors of the leaning arches are investigated for two tilt angles as 15, 30. For each angle, two loading conditions are considered as uniformly distributed load and wind loads. The F.E.M. is used through the all analysis procedures. For the results, load-deflection relationships, buckling modes, differences between two boundary conditions and deformed configurations are discussed.

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Study on the Dynamic Characteristics of Rolling Stocks Passing on the High Speed Turnout System (고속용 분기기를 통과하는 철도차량의 동특성 예측연구)

  • 정우진;신정렬;양신추;김남포
    • Proceedings of the KSR Conference
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    • 2000.05a
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    • pp.226-233
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    • 2000
  • This study has been performed to develop the practical method to estimate the change of dynamic characteristics of rolling stocks passing on the high speed turnout system. Each part of turnout system are modeled in consideration of alignment, enter angle and amount of deflection and they are used to achieve dynamic analysis with a train model. Analysis results are compared with test results to confirm its validation

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THE COLLISION EFFECTS OF THE PARTICLES IN THE ACCRETION DISK

  • Yoo, K.H.
    • Publications of The Korean Astronomical Society
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    • v.11 no.1
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    • pp.125-137
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    • 1996
  • The collision of two particles in the accretion disk may lead to be a mechanism of heat generation. By using hydrodynamic equations, the mean free path, the collision frequency and the deflection angle due to the collision of the particles are derived as a function of the mass accretion rate. The mean free path seems to be a smaller fraction compared to the dimension parameter of the system. The radiative flux in the disk is obtained under the influence of the collision of the particles.

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Numerical Analysis and Design of the 2-D Variable Convergent-Divergent Thrust Vectoring Nozzle (2-D 가변 추력편향 노즐 설계 및 유동해석)

  • Kim, Yoon-Hee;Kang, Hyung-Seok;Choi, Seong-Man;Chang, Hyun-Soo
    • Journal of the Korean Society of Propulsion Engineers
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    • v.15 no.5
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    • pp.27-34
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    • 2011
  • A numerical analysis was peformed for the supersonic aircraft with variable pitch thrust vector nozzle. Based on the requirement of the mixed turbofan engine of the supersonic aircraft, two dimensional thrust vector nozzle with variable pitch angle was designed. To investigate the effect of the thrust vectoring nozzle, the numerical analysis was conducted by using Fluent under the several pitch deflection angle.