DYNAMICS MODELING OF A TORQUE CONVERTER WITH TWO LINKAGE AND INERTIAL MASS

Similar documents
Development of a Meat Slicing Machine Using Locally Sourced Materials

SYNTHESIS OF AIRCRAFT MOTION CONTROL LAWS USING AGGREGATIVE CONTROLLER ANALYTICAL DESIGN PROCEDURE DURING AUTOMATIC IN- FLIGHT REFUELING

NR, NR4. NR n 2900 rpm. NR4 n 1450 rpm. In-line Pumps. Construction. Applications. Operating conditions

All-rounder drill WD-2D WD-4D. WD Carbide Drill. Worldwide Drill. Dc 4 PRODUCT INFORMATION. Wave type. Straight type

NR, NR4 60 Hz. NR n=3450rpm NR 50/250. NR4 n=1750rpm. In-line Pumps

Cluster A.2: Linear Functions, Equations, and Inequalities

Physics FUN Day Sponsored by Knott's Berry Farm, Edwards Airforce Base, and Physics Teachers. Schedule of Events Thursday, February 24, 2005

Mathematics of Flight. Headwinds and Tailwinds

LIEBHERR Mobile Crane LTM

I. Glacier Equilibrium Response to a Change in Climate

CASM electric cylinders The modular electric cylinder system

CASM electric cylinders

Gain-Scheduled Control of Blade Loads in a Wind Turbine-Generator System by Individual Blade Pitch Manipulation

10260 Series Actuators Model Selection Guide

Power System Stabilizer(PSS) Design Using ANFIS Algorithm and Comparing the Results with conventional and fuzzy PSS

10 A at 100 to 240 VAC. G3NE-220T-US (20 A at 75 to 264 VAC) 5 A at 100 to 240 VAC

Safety Analysis of the Winch Launch

Electric Smoke Damper Actuators

Artisan Technology Group is your source for quality new and certified-used/pre-owned equipment


Group constant generation for PARCS using Helios and Serpent and comparison to Serpent 3D model

Note: Exhibitor representatives are registered for the full conference and may attend the sessions of their choice. Profile of Attendees 24%

COMPLETED! PRIME NEW BUSINESS PARK DEVELOPMENT OF NEW B1/B2/B8 UNITS FROM 25,000 TO 100,000 SQFT TO LET/FOR SALE NN14 1EG.

Title ID Number Sequence and Duration. Age Level Essential Question Learning Objectives

Assessment Model. Tony Fisher Senior Research Consultant Canadian Sport Tourism Alliance, 116 Lisgar St., Suite 600 K2P 0C2 Ottawa ON

BASE AND COVER 28 TAPE TYPING UNIT AND 28 TAPE TELETYPEWRITER LUBRICATION P BASE AND SECTION P AT&TCo Standard

Double C-Face Spring-Set Brakes

NOTICE TO AERODROME LICENSE HOLDERS NOTAL 01/2019

COLLISIONS ON AIRTRACK

SUMMER SCHOOL. CU professionals. #SeeUatCU. Discover Georgia and Make Friends While Studying at Caucasus University!

HOW TO IMPROVE HIGH-FREQUENCY BUS SERVICE RELIABILITY THROUGH SCHEDULING

Modeling of aircraft jet noise in airports

Physics Is Fun. At Waldameer Park! Erie, PA

SIMULATION MODELING AND ANALYSIS OF A NEW INTERNATIONAL TERMINAL

Transit Vehicle Scheduling: Problem Description

Journal of Aeronautics & Aerospace

The organisation of the Airbus. A330/340 flight control system. Ian Sommerville 2001 Airbus flight control system Slide 1

You Must Be At Least This Tall To Ride This Paper. Control 27

blac inc. : 04 : 15 HIGH PERFORMANCE HEAVY DUTY ACTUATOR DRS

Time Benefits of Free-Flight for a Commercial Aircraft

Blocking Sea Intrusion in Brackish Karstic Springs

Reliability Analysis of Public Transit Systems Using Stochastic Simulation

Air Traffic Complexity: An Input-Output Approach. Amy R Pritchett, Keumjin Lee and Eric JM Feron School of Aerospace Engineering Georgia Tech

Today: using MATLAB to model LTI systems

Mechanics of Frisbee Throwing

Model Number Structure

460 exp 460EXP - 115

Jameco SKU Number:

Kinematics Review Checklist

PROCESS RELIABILITY RATHER THAN NERVE TINGLING BY GÜHRING GM 300 CHECK AND MEASURING INSTRUMENTS FOR OPTIMAL TOOL CLAMPING

9/20/2012 DEA EFFICIENCY MEASURE BASIC CCR MODEL. Max θ. subject to. 1,...,n. v,...,v. for DMU. where CLASS 4: CONSTANT RETURNS-TO-SCALE MODEL

2012 Performance Framework AFI

Missions, Operations & Ground Infrastructure

OPTIMUM ANCHORING FOR LONG SPAN CABLE-STAYED BRIDGES

Kinematics Review Checklist

Title. Author(s)ISHII, K.; KIKUCHI, M.; SHIRAI, K. Issue Date Doc URL. Type. Note. File Information HIGASHI-HONGANJI HAKODATE BETSUIN

TESTS ON AIR DISTRIBUTION PERFORMANCE IN BIG STORES

MODEL FOLLOWING TOTAL IN FLIGHT SIMULATOR AS AN EDUCATIONAL TOOL

International Seminar on Trade in Services & Tourism Statistics for Selected Asia Pacific Countries

PHY 133 Lab 6 - Conservation of Momentum

Introduction 2. Other Applicable Documents 2. Scope of Delivery 3. Attaching the Snap-on Ferrite Suppressor 4

Applied Soft Computing

SIDERMAT combination Visible breaking and tripping fuse switches from 630 to 1800 A

MX Series MX40-7XXX Series MX40-6XXX Series. Selection Guide. Applications. DuraDrive Series Actuator (Includes Accessories)

A 3D simulation case study of airport air traffic handling

An Overview of he Productive Structure of the Amazon Region: Using the Eyes of an Interregional Input-Output System

LAB 5-2 ENERGY CONSERVATION

GROUP ON INTERNATIONAL AVIATION AND CLIMATE CHANGE (GIACC)

A-CR-CCP-805/PF-001 Attachment A to EO C Instructional Guide

INSTALLATION MANUAL AND OPERATING INSTRUCTIONS. MD25-( ) Series Airspeed Indicator

Applying Integer Linear Programming to the Fleet Assignment Problem

ONTARIO S WATER CONFERENCE & TRADE SHOW. May 1 4, 2016 WINDSOR, ONTARIO HOSTED BY:

Research assistance was received from Mr. J. Bishop and Mrs- Elizabeth Jones who worked on an annotated After Mrs Jones '

SWL Series VALVE REGULATED LEAD-ACID BATTERIES SWL

Bridgwater. Office Investment For Sale 18,725 sq ft (1,740 sq m) FULLY INCOME PRODUCING HOUSE

MATH & SCIENCE DAYS STUDENT MANUAL

Test Report: HB

Test Report. 240W Single Output Switching Power Supply DESIGN VERIFY TEST

60W Single Output Switching Power Supply

LATVIAN AIP DATA SET

Max 500+ Series. Quick Start Guide FREE RECIPES. System Settings Venting Methods Initial Test Run Smart Programs.


Performance Indicator Horizontal Flight Efficiency

STUDY OF ALAQI SECONDARY CHANNEL IN LAKE NASSER

AKTINA* a new productive urban furniture. a solar & sustainable mobility project by CITY INDEX LAB & ENERGIZE

Mechanism Design for Personalized Recommender Systems

Materials Selection Assignment

Design Exploration of Low-Speed Wind Tunnel for Improved Flow Characteristics with STAR-CCM+ and Optimate+

AVIONICS MOUNTS Low Profile, All-Axis Vibration Isolators

Abstract. Introduction

Logan Airport in the Boston Regional Economy: A REMI Analysis

Test Report: EDR-75-12

Estimates of the Economic Importance of Tourism

AiMT. Flight Trajectory Modelling to Increase General Aviation Safety. Advances in Military Technology Vol. 6, No. 1, June 2011

Anthropometry and Range of Motion

Threshold sensitivity of quartz torsion magnetometers on a base of vicalloy and samarium-cobalt

"Free at Last" Cage-based Living Geometry

Canadian Tourism Satellite Account Demystified

R3579. Plastic Female Rod End. Material Housing: Igumid G plastic - Black. Spherical bearing: Iglidor w300.

Summi triumphum. & bc. w w w Ó w w & b 2. Qui. w w w Ó. w w. w w. Ó œ. Let us recount with praise the triumph of the highest King, 1.

Transcription:

UNIVRSIY OF PISI FACULY OF MCHANICS AND CHNOLOGY SCINIFIC ULLIN AUOMOIV series ear XIX no. DYNAMICS MODLING OF A ORQU CONVRR WIH WO LINKAG AND INRIAL MASS Ion ION-GUA * Universit of Pitesti Roania Artice histor: Receive:.7.; Accepte: 9.9.. Abstract: his artice escribes construction of an oe of torque converter with two inkage an two egrees of freeo. his echanis is a echanica appication of the theor on the transission of echanica power b vibrations. he echanica power is transitte fro engine to the output shaft through a caranic transission two osciating evers with inertia ass en a uniirectiona echanis. his torque converter is anaze b AMSi. Dnaics oeing of an autootive appication wi eonstrate its high perforances characteristics. In the oeing of this power transission sste the stiffness of the shafts an various contro ogics are incue. Kewors: torque converter; naics oeing; AMSi. INRODUCION he echanis propose to be anaze in this artice is presente in Figure. It is copose of a universa joint shaft US an asseb of two bars an connecte in couper point A an inertia ass ounte at the en of bar an uniirectiona echanis UM. On the basis of the notations can be writen reations x A () A () x xa () A () where are the position anges of bars an reative to the axis ox. ase on the above resut x (5) (6) he kinetic energ of this echanica sste [] [] is x (7) * Corresponing author. ai: ion.ion@upit.ro Figure. Scheatic representation of the torque converter

76 where are oents of inertia of the input an output shaft an ; ; x x ; (8) Differentiate with respect to tie reation (7) is obtaine (9) he Lagrange equations [] [] [5] for this echanis can be write as for () where are the input an output echanica torque on the input an output shafts respective () () () Fina we obtain the reations () With notations (5) (6) (7) the reations can aso be written in the for (8) With notations ; ; ; it is obtaine the foowing reations g f (9) with initia conitions t ; () SIMULAION SCHM Siuation schee of echanica transission is presente in figure. It is copose fro input shaft inkage echanis uniirectiona echanis an output shaft [8] [9] []. Siuation was ae b two istinct was: - b actuating with prie over with constant spee ; - b actuating with prie over with constant torque.

he ain characteristics of operation b actuating with prie over with constant spee are presente in Figures Figure 5 an Figure 8a. he ain characteristics of operation b actuating with prie over with constant torque are presente in Figure 6 Figure 7 an Figure 8b. ie variation of oa is presente in Figure. Siuations was ae with the foowing initia ata: 5rev / in ; N ; ; 7 ; ; ; 5 ; kg ; kg ; D 5kg ; Figure. Siuation schee of torque converter Figure. ie variation of oa (output torque ) Figure. orques variation an epening on the output spee 77

Figure 5. Output power P an efficienc variation epening on the output spee Figure 6. Output orque an input spee ω epening on the output spee Figure 7. Output power P an efficienc variation epening on the output spee Figure 8. Output spee variation to square variation of output torque a) for prie over with const. ; b) for prie over with const. 78

CONCLUSIONS Fro the anasis of the above charts it is notice ajor ifferences between operation with the oaing in ascening sequence an the operation in escening sequence of oas. hese ifferences increase with increase of oents of inertia an. he axiu power is transitte to the eian spee of the output shaft. RFRNCS [] aon. G. ao. Kineatic an Dnaic Siuation of Mutibo Sstes: he rea-ie chaenge Spring-Verag New-York 99. [] Hartenberg R. S. Denavit. Kineatic Snthesis of Linkages McGraw-Hi ook Copan Lonon 96. [] ran A. G. Sanor G. N. Mechanis e Prentice-Ha Upper Sae River N 98. [] Kane. R. Anatica eeents of echanics Vo. Acaeic Press New York 959. [5] Wison H.. urcotte L. H. Hapern D. Avance atheatics an echanics appications ug MALA Chapan & Ha/CRC. [6] Strang. G. Introuction to Appie Matheatics Cabrige Press 986. [7] Gi P.. W. Murra M. Wright Practica optiization Acaeic Press Inc. Lonon 98. [8] Gueret. Vaéo: Moeing of Copex Sstes with Appications in Autootive ransissions uropean AMSi Users' Conference Paris Ma 6th. [9] Lebrun M. Richars C. W. Iagine: How to Create Goo Moes Without Writing a Singe Line of Coe Fifth Scaninavian Internationa Conference on Fui Power SICFP'97 Linköping Sween Ma 8-9 997. [] Doebein O. Sste Dnaics Moeing an Response Frierich Vieweg & Sohn Verag Wiesbaen 6. 79