• 제목/요약/키워드: Motor Support Structure

검색결과 33건 처리시간 0.023초

동체 내삽형 추진기관 연결장치 연구 (Research on the Rocket Motor Support Structure Inserted inside the Missile Fuselage)

  • 박경민
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2010년도 제35회 추계학술대회논문집
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    • pp.265-270
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    • 2010
  • 본 연구에서는 유도무기 동체 내에 고체 추진기관을 삽입하여 장착할 경우 적용할 수 있는 연결장치와 조립체 개념을 제안하였다. 유도탄 동체 내에 추진기관을 삽입하여 장착하는 경우는 동체가 비행중 받는 하중에 더하여 추진기관의 연소에 의해 야기되는 여러 가지 효과 즉, 추력에 의한 축하중, 진동, 연소 중 발생하는 추진기관의 축방향 변형 등을 견디는 구조여야 한다. 본 연구에서 제안된 추진기관 연결장치를 통해 간결하면서도 설계 요구조건을 모두 만족하는 추진기관 장착 시스템을 구성할 수 있었다.

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KSLV-1 킥모터지지부 콘 구조물 구조 해석 (Structural analysis of Kick Motor support cone structure)

  • 안재모;김광수;장영순;이영무
    • 항공우주기술
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    • 제5권2호
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    • pp.159-165
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    • 2006
  • 본 연구에서는 KSLV-1 2단 킥모터를 지지하는 구조물인 킥모터지지부의 콘 구조물에 대한 구조 해석을 수행하였다. 킥모터지지부는 큰 구조물외에 트러스 구조물로 구성되어있으며, 킥모터로부터 발생하는 하중은 콘 구조물이 지지하게 된다. 킥모터로부터 발생하는 하중은 1단 추력 시 관성으로 인해 발생하는 인장 하중과 2단 킥모터 추력 시 발생하는 압축 하중이며 비행 자세에 따른 전단 하중과 굽힘 하중이 있다. 본 연구에서는 콘구조물에 부가될 수 있는 여러 가지 하중 조건에 대하여 해석을 수행하였으며, 압력 배출에 유무에 따른 구조 해석도 수행하였다. 등가 하중 기준으로 킥모터 추력으로 발생되는 등가 압축 하중보다 관성으로 인해 발생하는 등가 인장 하중이 더욱 크고 구조 해석 결과 역시 안전 여유 계수가 작게 나왔다.

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Design and development of in-wheel motor-based walking assistance system

  • Park, Hyeong-Sam;An, Duk-Keun;Kim, Dong-Cheol;Lee, Sang-Hyun
    • International Journal of Advanced Culture Technology
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    • 제10권3호
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    • pp.371-376
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    • 2022
  • The purpose of this study is to develop a walking assistance system with mobility support and life support functions so that the elderly with reduced physical ability and patients who are uncomfortable when moving can move comfortably indoors and outdoors, and help social life. An obstacle recognition sensor module that can be applied indoors and outdoors is installed on a lightweight walking aid. The purpose of this study is to develop a walking assistance system with mobility support and life support functions so that the elderly with reduced physical ability and patients who are uncomfortable when moving can move comfortably indoors and outdoors, and help social life. An obstacle recognition sensor module that can be applied indoors and outdoors is installed on a lightweight walking aid. It is a system structure of an integrated actuator and brake system that can avoid obstacles in consideration of the safety of the elderly and is easy to install on the device. In this paper, the design of a lightweight walking aid was designed to increase the convenience of the socially disadvantaged and the elderly with reduced exercise ability. In addition, in order to overcome the disadvantage of being inconvenient to use indoors due to the noise and vibration of the motor during operation, an In-Wheel type motor is applied to develop and apply a low noise, low vibration and high efficiency drive system.

다점 지지 고출력 고정도 초음파 모터 (A High power and Precision Ultrasonic Linear Motor with Multi-support Mechanism)

  • 이선규;윤철호;이현민;차현록;김완수;강장성
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2006년도 춘계학술대회 논문집
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    • pp.151-152
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    • 2006
  • Nowadays, great attention has been shown to the question of ultrasonic linear motor for accomplishing the high positioning accuracy and high driving force in the semiconductor and optical industry. Ultrasonic linear motors have many advantages such as simple structure, quick response, ability to maintain position without energy consumption, and electromagnetic effect. And BLT has attracted attention to accomplish large vibration amplitude and large mechanical force. Authors designed and developed the new type of ultra sonic linear motor with multi support mechanism, achieved 75N of output force and 0.45m/s of velocity.

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소형 위성 발사체 2단부 모드 시험 (Modal Test of the 2nd Stage of Small Launch Vehicle)

  • 서상현;정호경;윤세현;박순홍;장영순
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2006년도 춘계학술대회논문집
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    • pp.258-261
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    • 2006
  • The structure of small launch vehicle can be divided into engine section and payload section. This paper introduces modal test of the payload section of small launch vehicle which is composed to satellite, PLA (Payload Adapter), VEB (Vehicle Equipment Bay), KMS (Kick Motor Support) and KM (Kick Motor). From this test, dynamic properties of the 2nd stage structure of small launch vehicle can be obtained. In this test, to simulate free-free boundary condition, test object was hung by 4 bungee cords and excited by using impact hammer Modal test data are analyzed by using TDAS(Test Data Analysis Software). As the result, modal parameters and mode shapes below 100Hz of the 2nd stage of small launch vehicle were identified.

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A New Fuzzy Logic based Modeling and Simulation of a Switched Reluctance Motor

  • Wadnerkar, Vikas S.;Bhaskar, Mithun M.;Das, Tulasi Ram;RajKumar, A.D.
    • Journal of Electrical Engineering and Technology
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    • 제5권2호
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    • pp.276-281
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    • 2010
  • The switched reluctance motor (SRM) is an older member of the electric machines family. Its simple structure, ruggedness and inexpensive manufacturing potential make it extremely attractive for industrial applications. However, these merits are overshadowed by its inherent high torque ripple, acoustic noise and difficulty to control. In this paper, a control strategy of the angle position control for the SRM drive based on fuzzy logic is illustrated. The input control parameter, the output control parameter and fuzzy control with FAM table formulation strategy are described and simulated with control patterns, and the decision form of the fuzzy control is illustrated and simulated, and the scope of implementing in a Fuzzy based ASIC chip is enlightened with literature support.

초고속열차용 축소모델 선형동기전동기의 개념 및 기본설계 연구 (A Study on a Concept and Basic Design of a Small-Scaled LSM for Ultra-High Speed Railway Transit)

  • 박찬배;이형우;이병송;박현준
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 2009년도 춘계학술대회 논문집
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    • pp.905-911
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    • 2009
  • The viscosity drive method by the wheel which is widely used in the conventional railway systems needs a large friction force between the wheel and the guide-rail, which brings on a thrust force for a quick acceleration and a high-speed travelling. In addition, the viscosity drive method needs an increase of the vehicle weight for a large friction force. However, a maglev train is possible to be driven by the electro-magnet instead of the wheel, which produces a levitation and thrust force without any contact. In general, low-speed maglev train uses a linear induction motor(LIM) for propulsion that is operated under 300[km/h] due to the power-collecting and end-effect problems of LIM. In case of high-speed maglev train, a linear synchronous motor(LSM) is more suitable than LIM because of a high-efficiency and high-output properties. LSM has a driving principle as same as a conventional rotary synchronous motor(RSM), and the torque of RSM becomes the thrust force of LSM. A conventional LSM has relatively large air-gap compared with a conventional RSM. So, it must be achieved a design that is considered normal force by finite-asymmetric structure, end-effect on the entry and exit part, and support structure of a moving part. Therefore, in this research, authors accomplish a conceptualizing and basic design of a small-scaled LSM, and characteristics analysis using FEM.

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수직펌프의 진동 연구 (A Study on Vibration of Vertical Pump)

  • 김연환;김희수;이준신;배용채;이현
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 1997년도 추계학술대회논문집; 한국과학기술회관; 6 Nov. 1997
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    • pp.58-63
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    • 1997
  • The natural frequencies of the support system for a vertical pump, which are a key factor affecting the dynamic stability of the pump support system, are not easily predictable with analytical approaches only, due to the difficulties estimating the effective stiffness of the connections between the concrete base, the motor structure, the discharge elbow and the suction column of the pump system. This paper presents the results of a finite element analysis and an experimental study performed to identify and modify the characteristics of the pumping structure. The difficulties of modelling the effective stiffness were overcome by utilizing experimental results in the analysis. Based on analytical and experimental results, appropriate structural modifications are taken to reduce excessive vibration of the pump system to a satisfactory level.

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스위벨 밸브 튜브 커플러 개발을 위한 해석 연구 (An Analytical Study on the Improvement of the Performance of Swivel Valve Tube Couplers)

  • 이준호;성재경
    • 한국기계가공학회지
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    • 제10권3호
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    • pp.1-6
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    • 2011
  • This study focused on the localization of swivel type tube couplers, which all depend on imports. In this study, a computer application analysis was performed using a finite element method as a preliminary study. In the major developments related to the objective of this study, the air brake system produced by car makers represents a different in the installation point of an air tank according to the type of cars or in the length and direction of its hoses and that leads to cause lots of problems. For solving such problems, the design of the major elements in a swivel type tube coupler was analyzed using a finite element method, and its validity was also verified. In the process that verifies the validity of this study, it was necessary to investigate how much external force affects the desorption of the tube support, which is the most important element in swivel type tube couplers. For achieving the investigation, a pressure test was implemented for the tube support according to the Federal Motor Vehicle Safety Standards(FMVSS). In the results of the pressure test, all samples satisfied the FMVSS. In addition, several tests were implemented by installing the sample of the developed swivel type tube coupler to an actual vehicle. In particular, rotation tests with various angles were applied by welding the swivel type coupler to an air tank through an argon welding process. In the results of the installing test for an actual vehicle, it was verified that the designed structure was determined as a structure that is able to endure the eccentric torque and deformation pressure applied to several directions that are the major problems in such fixed type tube couplers. Therefore, in the comparison of the performance of the developed product with the product of PARKER, it was possible to verify that the localized swivel type tube coupler developed in this study shows more excellent than that of the existing products by PARKER.

KSLV-I 2단부 구조체 모드 시험 (Modal Test of the 2nd stage structure of KSLV-I)

  • 서상현;정호경;윤세현;박순홍;장영순
    • 항공우주기술
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    • 제6권1호
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    • pp.114-119
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    • 2007
  • 본 연구는 KSLV-I 페이로드 페어링을 제외한 2단 구조부에 대한 모드시험 결과를 기술하고 있다. 2단부는 크게 위성 분리부, 탑재부, 킥모터 지지부, 킥모터로 구성되어 있다. 번지코드를 이용하여 자유경계단 조건을 모사하였고 가진은 대형 가진 망치를 사용하였다. 이러한 모드시험 결과를 통하여 모드변수를 추출할 수 있고, 2단부 구조체의 동특성을 파악할 수 있다. 시험 결과는 TDAS를 사용하여 분석하였고, 100Hz 이하의 모드변수 및 모드형상을 추출하였다.

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