gear box designing

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    Overview

    A machine consists of a power source and a power

    transmission system, which provides controlled application of

    the power.

    Transmissionis an assembly of parts including the speed-changing gears and the propeller shaft by which the power is

    transmitted from an engine to a live axle.

    Often transmission refers simply to the gearboxthat usesgears and gear trains to provide speed and torque conversions

    from a rotating power source to another device.

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    Objective

    To build a gearbox for a electric run motor car:

    Minimize travel time required for a run on a straight route

    Minimize the cost of the gearbox

    Minimize the weight of the gearbox

    Maximize the performance and durability

    Maintain aesthetic design

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    Design Steps

    Geometry of gears

    Type of gear, module, no. of teeth, etc.

    Using C++ code and ANSYS

    Design of shafts and bearings

    Using force calculations

    Design of Casing

    As per final gear design and ANSYS

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    CAD

    Dimensions of gears:

    First Pinion = 20* mm and Module = 2

    First Gear = 18 mm and Module = 2

    Second Pinion = 24* mm and Module 2.5 Second Gear = 22 mm and Module 2.5

    Dimensions of Shafts:

    (for relaxed condition of only max torque=60Nm)

    OD25mm shafts

    (for a conservative design: FOS=3 and max torque=60Nm)

    OD 36mm shafts

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    CAD

    Dimensions of bearings:

    Outer Shafttapered roller

    (single row)

    32007 X/Q

    (From SKF)

    ID=35 OD=62

    T=18

    wt=224 gm

    Intermedia

    te Shaft

    tapered roller

    (single row)

    32205 BJ2/Q

    (From SKF)

    ID=25 OD=52

    T=19.25

    wt=187 gm

    Input shafttapered roller

    (single row)

    32007X

    (From SKF)

    ID=35 OD=62

    T=21

    wt=263 gm

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    CAD

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    CAD

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    CAD

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    CAD

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    CAD

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    CAD

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    CAD

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    Code

    For design of gears, ShigleysMechanical Engineering Design

    was referred to

    Design analysis was carried out for both spur gears and helical

    gears

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    Allowable Bending Stress

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    Bending Stress Number

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    Stress Cycle Factor

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    Reliability Factor

    For a reliability of 95%, the following equation was used:

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    Other Factors

    Temperature factor = 1 for temperatures less than 120oC

    Factor of safety is taken to be 1

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    Output

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    Shaft Design

    3 types of shaft

    Connected to motor on which pinion is attached

    Intermediate

    Connected to wheel drive

    Steps:

    Calculated radial, axial and tangential forces from helical gear

    design provided for both interfaces of gear and pinion.

    Used maximum torque of 60Nm that motor can provide forcalculation (though in steady state the torque will be less)

    Accordingly calculated axial and radial forces on shaft

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    Shaft design (continued)

    Plotted moment diagram and torque diagram and found critical

    point on shaft

    Material used was SAE 4340, got maxhere. Used factor of 0.75 as

    the location was gear location.

    Used FOS of 3 to get new maxas max/FOS Now used this value to get lower bound on OD of shaft

    Repeated the procedure for all the 3 shafts

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    Design of Bearings

    To account for axial forces, used Tapper Roller Bearing

    Because, they can take large axial forces (i.e., they are

    good thrust bearings) as well as being able to sustain

    large radial forces.

    Commonly used for moderate speed, heavy duty

    applications where durability is required.

    We can also use Deep Groove Ball Bearings(calculations

    for this are provided, if we want to use ball bearings), But

    Its life is limited and does not fulfill our requirement .

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    Taper Bearing Design Steps

    Given: Fa, Fr, Shaft diameter(OD) (for all three shafts)

    L= millions of revolutions (50,000 Km)

    L10>L (~170 millions of revolution) (for D=22 in for tyre)

    Also Our bearing should be of light weight

    Used a catalog available online (reference is given) Choose bearing(initially of minimum weight available)

    Calculate L10 for that bearing (SAE 50-oil is used for calculation)

    Check for L10>L.

    If L10

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    Ball Bearing calculations

    For the Shaft Connected to motor on which pinion is attached

    SKF bearing no. 6307

    Fa=4112N, Fr=4825.25N, Shaft Speed= 5500rpm

    C0=17600N, C=26000N, Limiting Speed (SL)=8000rpmFa/C0= 0.2336

    From Page 4.4, DDB: closest to 0.2336 Fa/C0 -> 0.25

    As Fa/Fr >e -> X=0.56, Y=1.2

    P=XFr+YFa= 7636.54N

    L10= (C/P)^3 = 40 million revolutions < L (~ 170 mr) , hence not ok

    Also its weight is higher(0.46kg) than taper roller bearing (0.22kg) for

    the shaft connected to the motor.

    Hence working with Taper Roller Bearing is much better.

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    References

    http://www.skf.com/skf/productcatalogue/jsp/calculation/calc

    ulationIndex.jsp

    http://www.irusa.com.br/catalogos/timken/usa_chap_1.pdf

    http://www.skf.com/skf/productcatalogue/jsp/calculation/calculationIndex.jsphttp://www.skf.com/skf/productcatalogue/jsp/calculation/calculationIndex.jsphttp://www.irusa.com.br/catalogos/timken/usa_chap_1.pdfhttp://www.irusa.com.br/catalogos/timken/usa_chap_1.pdfhttp://www.skf.com/skf/productcatalogue/jsp/calculation/calculationIndex.jsphttp://www.skf.com/skf/productcatalogue/jsp/calculation/calculationIndex.jsp
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    ANSYS

    Purpose:

    ANSYS was used to

    confirm the output of C++ code decrease the weight of gears

    design casing

    decrease weight of casing

    confirm shaft calculations

    Ansys Analysis

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    Optimization of weight of

    Gears Initially used conventional arms for both gears as taught in the

    course

    But these arms were heavy

    So, thought of using other profiles than arms

    Used circular patterns to remove the material Did static structural analysis in Ansys

    Iterative process of removing material and simulating it

    Maximum material was removed keeping FOS > 3

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    Gear 1 (FOS)

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    Gear 1 (Total Deformation)

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    Gear 1 (Von-Mises Equivalent Stress)

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    Gear 2 (FOS)

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    Gear 1 (Total Deformation)

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    Gear 1 (Von-Mises Equivalent Stress)

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    Casing

    Initially used MS casing

    but too heavy (from solidworks CAD model)

    used Al for casing

    Initially made casing with 15 mm thickness (starting guess)

    Did Ansys analysis for it and found out it is overdesigned

    Then designed the casing with 10 mm thickness

    This design was also overdesigned at some places

    Then designed a casing with thickness 5 mm at some places and

    10 mm at other, using Ansys analysis to minimize the weight

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    FOS

    (min value = 3.9)

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    Total Deformation

    (max value = 12 microns)

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    References

    Motor Specification:

    http://agnimotors.com/95_Series_Performance_Graphs.pdf