• Title/Summary/Keyword: gear parameter

Search Result 90, Processing Time 0.021 seconds

Analysis of vibration characterization of a multi-stage planetary gear transmission system containing faults

  • Hao Dong;Yue Bi;Bing-Xing Ren;Zhen-Bin Liu;Yue, Li
    • Structural Engineering and Mechanics
    • /
    • v.88 no.4
    • /
    • pp.389-403
    • /
    • 2023
  • In order to explore the influence of tooth root cracks on the dynamic characteristics of multi-stage planetary gear transmission systems, a concentrated parameter method was used to construct a nonlinear dynamic model of the system with 30-DOF in bending and torsion, taking into account factors such as crack depth, length, angle, error, time-varying meshing stiffness (TVMS), and damping. In the model, the energy method was used to establish a TVMS model with cracks, and the influence of cracks on the TVMS of the system was studied. By using the Runge- Kutta method to calculate the differential equations of system dynamics, a series of system vibration diagrams containing cracks were obtained, and the influence of different crack parameters on the vibration of the system was analyzed. And vibration testing experiments were conducted on the system with planetary gear cracks. The results show that when the gear contains cracks, the TVMS of the system will decrease, and as the cracks intensify, the TVMS will decrease. When cracks appear on the II-stage planetary gear, the system will experience impact effects with intervals of rotation cycles of the II-stage planetary gear. There will be obvious sidebands near the meshing frequency doubling, and the vibration trajectory of the gear will also become disordered. These situations will become more and more obvious as the degree of cracks intensifies. Through experiments, the theoretical results are in good agreement with experimental results, verifying the correctness of the theoretical model. This provides a theoretical basis for fault diagnosis and reliability research of the system.

A Study of Aircraft Ground Motion (항공기 지상운동 특성에 관한 연구)

  • Song, Won Jong
    • Journal of Aerospace System Engineering
    • /
    • v.11 no.6
    • /
    • pp.17-25
    • /
    • 2017
  • Vertical reaction force between ground and tire is an important parameter determining the ground behavior characteristics of aircraft. This parameter can be used to calculate the lateral force and friction. However, it is hard to obtain this parameter in real-time when the aircraft is taxiing. Therefore, pre-analysis of ground behavior and vertical reaction force should be conducted using ground simulation results to prevent rollover or hazardous scenarios. In this paper, a Landing Gear and Full-Aircraft model was constructed using VI-Aircraft S/W. The roll behavior of aircraft was analyzed using steering simulation results compared with taxi-test data.

A Study on Development of Railway Reducer for Low Noise/Vibration (소음/진동을 고려한 철도 감속기 개발에 대한 연구)

  • 이형우;박노길
    • Journal of the Korean Society for Precision Engineering
    • /
    • v.21 no.2
    • /
    • pp.130-137
    • /
    • 2004
  • A dynamic model of railway reducer is developed by the lumped parameter method. The model accounts for shafts, bearings flexibilities, gyroscopic effects and the force couplings among the transverse and torsion motions due to gearing. Vibration/noise analysis as well as strength of gear teeth, and bearing life are considered. Excitation forces of railway reduction are considered as the mass unbalance of the rotors, misalignment and a function of gear transmission error which comes from the modified tooth surface. A campbell diagram, in which the excitation sources caused by the mass unbalance of the rotors, misalignment and the transmitted errors of the gearing are considered, shows that, at the operating speed, there are not the critical speed. The program which can be used to analyze and predict vibration/noise characteristics by mass unbalance, misalignment and gear transmission error of railway reduction is developed with this system model.

A Study on the Radiated Noise of a Shaft-Plate System By an Axial Force (축방향력에 의한 축 플레이트계의 방사소음에 관한 연구)

  • ;Grosh, Karl
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
    • /
    • 1998.04a
    • /
    • pp.524-529
    • /
    • 1998
  • Analogous problem for a gear dynamics where helical gears excite logitudinal forces in the shaft is studied. These shaft forces excite the supporting gear housing through bearing, causing structural vibration. In this study, shaft is modeled as a rod, and bearing is modeled by a massless spring. A simple model for gear housing is a clamped circular plate. To model this force transmission, the transfer functions from the shaft to a clamped circular plate are analytically derived by using the spectral method and four-pole parameter. Finally, radiated noise is computed, using the acoustic relations due to plate surface vibration.

Design of Fuzzy Compensator for Compensate Backlash in Gear (기어의 백래쉬 보상을 위한 퍼지 보상기 설계)

  • KIM Nam boon;HUH Uk youl;KIM Jin geol;KIM Byung yoon
    • The Transactions of the Korean Institute of Electrical Engineers D
    • /
    • v.53 no.12
    • /
    • pp.799-803
    • /
    • 2004
  • In rotating systems, backlash impose limitations on the quality of control. System with gear is an example where this is a well-known limitation. In order to increase the controller performance, we design a fuzzy system to compensate the backlash effect. We prove that under certain conditions the fuzzy compensator guarantees that the backlash output converges to the desired trajectory. Simulation results show that the fuzzy compensator is robust to the backlash parameter.

ACN Estimation for Medium-class Aircraft (중형수송기 Aircraft Classification Number 예측)

  • Chung, Jin-Deog;Bae, Joong-Won;Lee, Hae-Chang
    • Journal of Aerospace System Engineering
    • /
    • v.4 no.3
    • /
    • pp.34-38
    • /
    • 2010
  • ACN(Aircraft Classification Number) is allocated by marketing group during early stage of aircraft design phase and is a critical parameter to decide whether the designed aircraft can be landed or not in a certain airport. The loading on the main landing gear wheels, selection of main landing gear tire and estimation of ACNs for flexible and rigid pavements were done for the proposed medium-class aircraft. The estimated ACN values are compared with the similar class aircraft. And PCN(Pavement Classification Number) values of airport in Korea are surmmarized. Results showed that the currently proposed medium-class aircraft can land any airport in Korea.

  • PDF

Analysis of Vibration Parameters for the Fault Diagnosis of Reduction Unit for High-speed Train (고속철도차량 감속기 결함진단을 위한 진동 파라미터 분석)

  • Kim, Jae Chul;Ji, Hae Young;Lee, Kang Ho;Moon, Kyung Ho;Seo, Jung-Won
    • Journal of the Korean Society for Precision Engineering
    • /
    • v.30 no.7
    • /
    • pp.679-686
    • /
    • 2013
  • The reduction unit is one of the most important components in railway cars, due to the transmission of torque from the motor to the wheels. Faulty reduction gears in high-speed trains result from excessive wear on the gear or damage to the gear. These types of gear defects have a significant effect on high-speed rail operation and safety; thus, a diagnosis system for the reduction unit is needed. Vibration diagnosis technology is one of the most effective diagnostics. In this paper, the vibration parameters of a reduction unit were evaluated during a driving-gear test and a full-vehicle test, using kurtosis and the crest factor. These tests were performed under normal operating conditions; a specimen tester was used to diagnose problems in defective gears.

Effect Analysis of Carrier Pinhole Position Error on the Load Sharing of Planetary Gear (캐리어의 핀홀 위치 오차가 유성기어의 하중 분할에 미치는 영향 분석)

  • Kim, Jeong-Gil;Park, Young-Jun;Lee, Geun-Ho;Kim, Jae-Hoon
    • Journal of the Korean Society of Manufacturing Process Engineers
    • /
    • v.15 no.4
    • /
    • pp.67-72
    • /
    • 2016
  • Planetary gear sets are widely used in power transmission components, which have high efficiency and good durability. Their most important design parameter is the load-sharing characteristics among several planetary gears. In this study, the load sharing of planetary gears was analyzed according to the carrier pinhole position error of planetary gear sets. The loads acting on planetary gears varied with the pinhole position error of the carrier, and the load sharing of planetary gears improved as the input load increased. In addition, the load of the planetary gear with a carrier pinhole position error was relatively higher than that of other planetary gears without carrier pinhole position errors. This trend appeared more clearly in the non-floating-type carrier than the floating-type carrier.

Experimental Investigation to Establish Correlation Between Specific Film Thickness and Vibration Signals in Spur Gear System (스퍼 기어의 진동 신호와 비 유막 두께(Specific Film Thickness)의 상관관계에 관한 실험적 연구)

  • Kim, Jong Sik;Amarnath, M.;Lee, Sang Kwon
    • Transactions of the Korean Society of Mechanical Engineers A
    • /
    • v.38 no.9
    • /
    • pp.1005-1012
    • /
    • 2014
  • Gears are critical elements in automobiles, and their use as power transmitting machine elements in engineering applications is quite extensive. In the areas of contact between gear teeth, the condition of a gear is likely to deteriorate due to contact fatigue, wear, material defects, lubrication failure, etc. Thus, it is necessary to monitor its condition to ensure smooth power transmission. Gear teeth deterioration causes failures such as abrasive wear, scuffing, pitting, and spalling. These failures lead to a higher level of vibration signals in the gear system. This paper presents the results of an experiment on the surface fatigue wear of a spur gear system. The correlation between the estimated specific film thickness, statistical parameter of the vibration signals, and Stribeck curve was considered in this study.