• Title/Summary/Keyword: Thrust Force

Search Result 681, Processing Time 0.025 seconds

The Effect of Running Speed and Slope on the Lower Extremity Biomechanics (달리기 속도와 경사가 하지관절의 생체역학에 미치는 영향)

  • Kim, Jongbin
    • Journal of Convergence for Information Technology
    • /
    • v.10 no.4
    • /
    • pp.160-167
    • /
    • 2020
  • This study analyzes the effects of changes in running velocity and slope on the biomechanical factors of the lower limb joints. For this purpose, 15 adult males in their 20s ran according to changes in running speed (2.7, 3.3 m/s) and slope ( -9°, -6°, 0°, 6°, 9°) on the treadmill, and their running characteristics (stride length, stride frequency). The range of motion of the lower limb joint and the vertical ground reaction force were greater in UR (p <.05), and the moment of the lower limb joint, braking force, thrust and load factor was large in DR (p <.05). In joint power, the ankle joint was greater in DR, and hip joint was greater in the UR (p <.05). These results show that the injuries of the ankle joint will be greater than other cases when running DR at a speed of 3.3 m/s.

Dynamic Properties of Tiny Piezoelectric linear Motor by Applied Voltage (인가 전압에 따른 초소형 압전 리니어 모터의 동특성)

  • Yoo, Kyoung-Ho;Ko, Hyun-Phill;Kang, Chong-Yun;Kim, Hyun-Jai;Ko, Tae-Kuk;Yoon, Seok-Jin
    • Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
    • /
    • 2005.07a
    • /
    • pp.62-63
    • /
    • 2005
  • Recently, a tiny piezoelectric linear motor using a vibration made of the transducer has been invented. The motor consists of a shaft, mobile element, and piezoelectric transducer using a piezoelectric radial mode bimorph disk. The fringe of the bimorph disk is fixed firmly which means this area has no degree of freedom. Therefore, the radial mode of the tranducer transfers to the flexurd mode. The mobile elements move along the shaft by the impact force generated by the flexurd mode of the piezoelectric transducer. The piezoelectric ceramic disks have thickness of 0.1 mm and diameter of 3.5 mm. The elastic disk is introduced between two disks of the ceramic, which has thickness of 0.1 mm and diameter of 3.8 mm. The fringe of the elastic disk is fixed by a brass cylinder which height is 1.2 mm. The Pyrex shaft is used which has diameter of 1 mm and height of 10 mm. The motors are operated at their resonant frequencies. The dynamic properties of the motor have been intensively measured and analyzed according to the applied voltage wave forms at the resonant frequencies. As the sawtooth and rectangular voltage waves are applied, the velocity, the thrust force, and the velocity dependence of the mobile position are measured. The dynamic characteristics are also analyzed within a period of each wave using laser vibrometer. The velocity of the mobile is moderately constant along the shaft. The better dynamic characteristics are obtained in the case of applying the rectangular wave.

  • PDF

Numerical Investigation of Ground Effect of Dual Ducted Fan Aircraft During Hovering Flight (제자리 비행하는 이중 덕트 팬 비행체의 지면 효과에 대한 수치적 연구)

  • Lee, Yujin;Oh, Sejong;Park, Donghun
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.50 no.10
    • /
    • pp.677-690
    • /
    • 2022
  • By using an actuator disk method based flow solver, aerodynamic analysis is carried out for a dual ducted fan aircraft, which is one of the VTOL compound aircrafts, and its associated ground effect is analyzed. The characteristics and accuracy of the solver for ground effect analysis is evaluated through a comparison with the results obtained from the sliding mesh technique. The aerodynamic performance and flow field characteristics with respect to the distance from the ground are analyzed. As the ground distance decreases, the fan thrust increases, but the deterioration of total normal force and hovering flight efficiency is identified owing to the decrease in the vertical force of the duct, fuselage, and wing. By examining the flow field in the bottom of the fuselage, the ground vortices and fountain flow generated by the interaction of the fan wake and ground are identified, and their influence on the aerodynamic performance is analyzed. The strength and characteristics of outwash with respect to the ground distance and azimuth direction are analyzed through comparison/examination of velocity profile. Influence of the ground effect with respect to collective pitch angle is also identified.

Research of Performance for the Propulsion System of Maglev Vehicle (도시형 자기부상열차 추진특성에 관한 성능연구)

  • Kim, Bong-Seup;Koh, Joon-Kyun;Park, Do-Young;Kang, Byung-Gwan
    • Proceedings of the KSR Conference
    • /
    • 2011.10a
    • /
    • pp.2342-2347
    • /
    • 2011
  • This paper introduces the performance test of the prototype vehicle, which will be in operation for Urban Maglev Program. While common trains with steel wheels use rotary induction motors for propulsion, maglev trains gain thrust force from linear induction motors maintaining the constant airgap with levitation electromagnets. Therefore, not only the behavior of the linear induction motor should be well understood, but also the way of propulsion that minimizes its effect on the levitation system should be took into account. Performance test procedures of maglev trains are proposed and carried out, and the characteristics of acceleration and deceleration are verified to agree with the design criteria. Tests are mainly performed on the linear section of the test line, and the driving characteristics on the section with a 6‰ incline are examined additionally. As a result, the performance of the prototype vehicle in the reverse operation can satisfy the requirement about the acceleration and deceleration, 4.0$m/s^2$. And, the design modifications of the commercial vehicle and the performance specifications required on the demonstration line are investigated.

  • PDF

A Study on the Ship Resistance and Moment Prediction for Running Attitude of 30 Feet Catamaran Sailing Yacht (30ft급 쌍동형 세일링 요트의 항주자세에 따른 실선저항 및 모멘트 추정에 대한 연구)

  • Park, Chung-Hwan;Jang, Ho-Yun;Jeong, Jin-Wook;Lee, Byung-Sung;Chun, Ho-Hwan
    • Journal of the Society of Naval Architects of Korea
    • /
    • v.47 no.3
    • /
    • pp.321-327
    • /
    • 2010
  • During sailing by wind-driven thrust on the sail, a catamaran sailing yacht generates leeway and heeling. For estimating resistance and moment prediction of a real ship by changing of running attitude, a model test of the ship has to be carried out. This study aims at establishing experimental techniques for a catamaran sailing yacht by changed attitude during running direction. Through the model test, drag and side force of the real ship are predicted. Also through experiment, rolling and yawing moments were considered.

Design of Large Multi-Electromagnetic Shaking System (대형 멀티 전자기 가진 시스템 설계)

  • Im, Jong-Min;Moon, Sang-Moo;Eun, Hee-Kwang;Choi, Seok-Weon;Choi, Joon-Min
    • Aerospace Engineering and Technology
    • /
    • v.7 no.2
    • /
    • pp.76-81
    • /
    • 2008
  • The vibration test system of satellite environment test dept. has been used successfully for the vibration tests of a majority of korean space programs. To meet the recent needs of large size test facility available for the vibrational tests of the huge launch vehicles and satellites, KARI have developed the large size multi-electromagnetic shaking system with $3{\times}3m$ head expander system. The new system will consist of three electromagnetic shakers which has 160 kN thrust force individually, and be able to sustain up to 8 tons test load and 300 kNm overturing moment. This paper describes the design components in the development process of multi-excitation shaker system.

  • PDF

A Study of Characteristic correlation go after the variable of shear process design for Carbon Tool Steel (I) (탄소공구강의 전단설계 변수에 따른 특성 상관관계 연구 (I))

  • Ryu, Gi-Ryoung;Ro, Hyun-Cho;Song, Jae-Son;Park, Chun-dal
    • Design & Manufacturing
    • /
    • v.6 no.2
    • /
    • pp.84-89
    • /
    • 2012
  • In recent years, technology of press plastic working having made remarkable progress. We can say this because it facilitates mass production and have superior performances in machining speed and equivalency of quality than other processing methods. In characteristics of press plastic working, mold manufacturing according to characteristics of each product should be preceded before processing and it has a great influence on machining speed and quality of products and etc according to manufacturing method. Therefore, mold design technology is a critical technology in press plastic working. There are lots of variables in press plastic working according to worked material, mold materials, conditions of heat treatment, clearance and so on. Abrasion of mold depends on these kind of conditions and sheared surface which is crucial for quality of product also depends on them. In this study, we conduct research on abrasion loss of mold according to 8, 10 and 12% of clearance for thickness of 1.0mm of worked material out of mold design variables of the products whose worked materials are high carbon steel and carbon tool steel by a practical experiment.

  • PDF

A Study of Characteristic correlation go after the variable of shear process design for Carbon Tool Steel (II) (탄소공구강의 전단설계 변수에 따른 특성 상관관계 연구 (II))

  • Ryu, Gi-Ryoung;Ro, Hyun-Cho;Song, Jae-Son;Park, Chun-dal;Youn, Il-chae
    • Design & Manufacturing
    • /
    • v.6 no.2
    • /
    • pp.90-95
    • /
    • 2012
  • The sheet metal forming proceccing is very important and indispensable in the automotive industry because the accuracy of prsee worked parts is directly related to the automotive quality. But when making mold it is difficult and expensive to modify mold. mold design technology is a critical technology in press plastic working. When design the mold there are lots of variables in press plastic working according to worked material, mold materials, conditions of heat treatment, clearance and so on. Abrasion of mold depends on these kind of conditions and sheared surface which is crucial for quality of product also depends on them. In this study, we conduct research on abrasion loss of mold according to 8, 10 and 12% of clearance for thickness of 1.0mm of worked material out of mold design variables of the products whose worked materials are high carbon steel and carbon tool steel by a practical experiment and perform a comparative evaluation of difference of abrasion loss mold with the alloy tool steel (STD11) and Tungsten Carbide (WC).

  • PDF

Study on Structural Integrity of Bearingless Main Rotor Hub System of Helicopter (헬리콥터 무베이링 메인 로터 허브 시스템의 구조 건전성에 관한 연구)

  • Lee, Mu-Hyoung;Park, Ill-Kyoung;Kim, Sung-Joon;Hwang, In-Hee;Kim, Tae-Joo
    • Journal of the Korean Society for Aviation and Aeronautics
    • /
    • v.20 no.4
    • /
    • pp.50-56
    • /
    • 2012
  • Rotor system is a very important part which produce lift, thrust and control force in helicopter. Component of rotor system must have structural integrity for applied load. The estimation of structural integrity is regarded greatly as important in aerospace field. In this study, the process of structural analysis performed for bearingless main rotor system of helicopter. The composite flexbeam and torque tube of bearingless main rotor are very thick, so 3D layered soild elements of MSC.PATRAN were used to get the finite element analysis results. To estimate structural integrity, non-linear static analysis considering geometric non-linearity is performed. In addition, detailed finete element analysis and non-linear static analysis are performed to consider the stress concentration for fitting effect and contact surface. The estimation process of structural integrity for bearingless main rotor system of helicopter may help the design.

CFRP Drilling Experiments: Investigation on Defect Behaviors and Material Interface Detection for Minimizing Delamination (탄소섬유복합재 가공의 결함특성 및 결함 저감을 위한 경계검출)

  • Kim, Gyuho;Ha, Tae In;Lee, Chan-Young;Ahn, Jae Hoon;Kim, Joo-Yeong;Min, Byung-Kwon;Kim, Tae-Gon;Lee, Seok-Woo
    • Journal of the Korean Society for Precision Engineering
    • /
    • v.33 no.6
    • /
    • pp.453-458
    • /
    • 2016
  • CFRP (Carbon Fiber Reinforced Plastic) and CFRP-metal stacks have recently been widely used in the aerospace and automobile industries. When CFRP is machined by a brittle fracture mechanism, defect generation behaviors are different from those associated with metal cutting. The machining quality is strongly dependent on the properties of CFRP materials. Therefore, process control for CFRP machining is necessary to minimize the defects of differently manufactured CFRPs. In this study, defects in drilling of CFRP substrates with a variety of fiber directions and resin types are compared with respect to thrust force. An experimental study on material interface detection is carried out to investigate its benefits in process control.