CM3332 Bus Body Design

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    CDM2Name of Work Design of bus Body

    ClientTamilnadu State Express Transport

    corporation

    Reference No. CTC/0101210801

    Design Algorithm Input/Computations/Decisions

    100 Description, location and overall

    geometry of producta. urpose o e ve c e

    Bus/Truck(t)/Cargo truck/ Refrigerated

    truck ( R ) others B

    b. Kind of body StrutureStiffned panel/Sandwich/grid Stiffened/grid

    c. Shape of body configuration

    Retagular ono box shape/two box Rectangular one box shape

    d. Shape of front and rear

    Flat/Curved streamlined Flat

    102 Dimensions

    a. Overall length L in mm 10,100

    b. Overall Width B in mm 2430c. Height of side walls H above the

    chassis in mm 2350

    102 Internal arrangements

    a. Whether separate driver's cabin

    provided yes/No No

    b. The lenth ldof drivers cabin in mm NA

    c. Whether the passenger/ Cargo cabin is

    integral with drivers cabin or separtely on

    a trailer NA

    d. Location, Width Wdand height hdof

    driver entry door in mm 700e. Location, Width Wdand height hdof

    helper entry door opposite drivers door

    in mm 700

    f. If driver cabin is separate, length Lc of

    cargo cabin in mm NA

    Design Input

    Design of all composite busbody

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    g. Whether the top is covered or open 30

    h. If top is open height hf of the side walls NAi.. If top is open whether the side walls

    can be rigity fixed or hinged for loadingand un loading NAj. Whether the bus is ordinary

    (OB),Luxury bus(LB), or Air-conditioned

    bus(AB)

    k. No of passengers seats to be fixed 45+2

    l. No. Of additional passengers allowed to

    travel as standees 60

    m. Cargo weight Wcto be permitted

    inside in kg 1000kg

    n. No . Of seats per row 4

    o. Distance between successive row,lsof

    seats in mm 1000p. Self weight of seats in kg 20kg

    q. Method of fixing of seats

    Fixed on the floor board by bolting Fixed on floor board

    r Whether luggage carrier racks/ boxes to

    be provided yess. Whether interior padding is to be

    provided on the side walls

    Yes if 1025 is LB or AB NA

    t. Location width Weand height heof

    passanger entry door in mm 700

    u. Location width Wpc

    and height hpc

    ofpassanger entry door in mm

    This can be same as helper entry door in

    1012 if the driver cabin is integral with

    passanger cabin 700

    v. If the bus is AB, Temperature T in C

    inside during operation NA

    x.

    w. If the bus is AB, location and weight of

    air conditioner in kg NA

    x. Type of cargo

    Vegetables/Meat/ Fish /Others NA

    y. Whether the cargo can exert weight onwalls during acceleration / deceleration /

    storage / or while negotiating curves

    No. of the cargo is firmly fixed on floor

    with gap between wall and cargo NA

    z. Location width W rand heighy hrof the

    cargo door NA

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    bb Whether metallic lining is required

    inside to take local impacts NA

    cc. Temperature oc cabin in C NA

    dd. Whether insulated container only with

    no AC or with refrigerator attached NA

    ee. if with refrigerator location and weight

    of refrigerator NA130. Support conditions

    a.Whether to be supported in chassis

    (SC) or to be an integral monocoqe

    shell(SM) SCb.If 1061 is SC

    No . And dimensions of longitudinal

    beams in chassis over body to be

    supported

    Two channels

    229mm x 76mm x 6.35mm

    c.Spacing Wcof chassis beam in mm 840

    d. Environmental temperature in C 45

    e. Design temperature Dt in C

    ( if not given takes as 90 C for vehicles

    exposed to sunlight on outside pannel 90

    f. Minimum environmental temperature in

    C 15 Cg. Minimum design temperature DTM in C

    D TM can be minimum of

    1073,1054,1037 15 C

    110. Major product elements of

    busbody and dimensions

    120. Functional requirements

    m. Expected life given in running km 3x 10^5 KM

    130. Operational Static and Dynamc

    loads

    a. Total design pay load in kg Wp

    Wp is passanger and cargo / luggage

    weight 9000kg

    b. Snow load Ps on roof in N/mm2

    if not applicable take Ps as zero NA

    c. Self weight of body in kgAssumed 50% of pay load for deign

    purpose 5000kg

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    d. No. of fitting with concentrated load

    effect their location and weigh tin kg give

    sl. No. location as distance in mm from

    front and weight in kg under 3 column on

    right hand side 6150N131. Aerodynamic loads

    a. Pressure acting on front end on roof

    and front wall rear walls pa in N/mm2 rear end

    b. wind pressure Pwin N/mm2, when

    vehicle, is stationery in N/mm2 Not to be consideredc. Impact factor a

    a. Vertical accelerator mZSfor symmenric

    load

    b. Vertical accelerator mZUfor

    unsymmenric load

    c. Longitudinal l accelerator or load factor

    mSC

    d. Load factor for corning mYe.Load factor for kerbing mK

    f. Load factor for turn over mR

    2.5

    1.3

    0.7

    1.01.0

    1.5

    d. Fatigue design load and the no. of

    cycles during lie period 10^6

    e. Normal operational speed Vm in km ph 60

    f. Peak operational speed Vp in km ph 100

    g. Frequency vibration due to traffic or

    other wise in HZ 50

    h. Corrosion or chemical attack nil

    i. whether moisture effect can give

    degradation Nil effectj. whether moisture effect can give

    degradation Impact in sea coast and

    places where deicing is done Negligible

    k. whether thrmal stresses can arise due

    to thermal expansion or thermal gradient NO

    l. Whether degradation due to fire, friction

    UV radation other radiations, biological

    attacks or lightning to be considered NO

    200. Selection of geometry in addition

    to wht is alredy taken in input data

    210. Manufacturing method

    2. Design selections

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    a. If to be designed as per any standard,

    specify standard no Nob. Type body construction

    Steel frame and panel (SP) / steel and

    sandwich (SS)/Steel and grid (SG)/ all

    sandwich with no steel (AS) / all grid with

    no steel (AG)

    SP for wall,Sg for floor and SS for

    roof

    c. If 2002 is not FP go tod. Spacing of cross steel arches lse in mm

    ( Normally these can be considering with

    the seat spacing so that a windows can

    be provided in between frame for

    passangers sitting in each row to see

    outside) 1000mm

    e. No of frame nfin long direction

    nf= (L or Lc)/ Ise+1 10100/1000+ 1=11

    f. No.of lingitudinal members of steel

    frame excluding bottom panel 9g. Location of lingitudinal beam

    If must be such that windows can be

    placed without obstruction 9h. Spacing of cross members on the floor

    panel lsfin mm

    Keep it same as that of the wall cross

    members 1000

    i. No.of lingitudinal members on the floor

    panel and that spacing wsf in mm 13

    j. Method of joining of steel members

    Welding / Bolting Welding

    k. Type of panel between steel frame onthe floor

    Sandwich / Grid / stiffened panel / single

    skin gridl. Tytpe of panel on roof

    Sandwich / Grid / stiffenedpanel/ single

    skin Sandwich

    m. Type of panel on side wall

    Sandwich / Grid / stiffened / single skin Single skin

    n. Type of panel / or the front end for

    impact resistence stiffenedo. Panel structure of single skin

    Flat / corrugated Flat

    p. Panel material E-glass CSM-Polyester

    q. Grid material E-glass UDC-Polyester

    r. Sandwich material

    E-glass CSM-Polyester and

    polyurethane

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    s. Grade polyester resin

    Isophthalic is to be used automobile

    grade for ompact resistence Isophthalict. Heat distortion temperature HDT of

    resin in C

    HDT < 100 100

    u. Gel coat resin and thickness

    Normally 0.5 mm thickness 0.5

    v. Whether gel coat to be pigmented

    Yes if not painting is planned no

    w. UV stabiliser material its grade and

    percentage Tinovin 0.1%

    x. Pigment grade colour and percentage NA

    y. Whether filler can be added to lay up at

    if so name of material and percentage

    Yes 10% maximum Calcium carbonatez. Area density Wcsm of CSM in gsm 450

    aa. Text of rovings for grid constrution 2400

    ab. Area of density of WRM to be used 610Selection of design criteria

    a. Whether to be designed by strength of

    material approach only/strength of

    materials for preliminary selection and

    FEM for optimisation

    strength of materials for each

    element as Fem for final assembly

    designb. Whether design for functional

    requirements to be under taken

    Not provided in this modle No

    c. Any design for safety under non-

    mechanical /environment effects to be

    considered No

    d. factor of safetyv 6DESIGN FOR SAFETY

    a. Weight of passanger Wpin N

    Wp = np 90 x 9.81

    9000 x 9.81

    =88290

    b. Chassis weight Wc in N 37200

    Weight of front axle with wheel and axle

    in N 10,000

    Rear axle with wheel and acceleration in

    N 14,050Weight of milds / is stracture in its body

    and floor in N 13000

    Weight of the ghaged windows in N 4500

    Weight of the 50 suels in N 7500

    Weight of mi fillling in N 6150

    Design of roof Phril

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    a. Type of stracture Sandwich with form wire

    b. Span lsin mm 1000

    c. Width of panel Wsin mm 2430d. Assumed stractural behaviour

    Plate if Ws < 2ls

    beam if Ws > 2ls beam

    Design palm load on moffing in N

    25 x 90 x 9.81

    = 22072.5

    Design pressure Pdin N/ mm2

    22072.5/10100 x 2430

    =0.0008993Assumed skin thickness no of sand with t

    in mm

    Assumed 2 mm min / mm 2 in CSM 450 mat

    Assumed core thickness C in mm 25

    Moment of inertia

    I = 2 t/2 + 2 (25F x t / 2 )2 t 2 x 2^3 / 12 + 2 (25+1)2 x 2

    Deflection ymax in mmymax = 1/38h x Plx ls ^4 / EI

    1 x 0.0008993 x 1000^4 / 384 x

    6300 x 2705= 0.1374

    if deflection is acceptable

    yes if ymax < span / 200 Yes

    Bending moment M in N-mm / mm

    M = Pd . L s^2/ 8

    0.0008993 x 1000^2 / 8

    = 112.4125

    Allowable bending moment Mal

    12.5 x 2 x 27

    = 675

    If design acceptable

    Yes if M < Mal yes

    Design of bottom panel

    Type of stracture Grid floor

    span lb in mm 1000Width wb in mm 2430

    Assumed stractural bed view Equalent or plate

    Spacing a of grid beam placed in the

    axial direction in mm 100

    thickness tl of grid beam placed

    longitudnally 10

    Spacing b of grid beam placed

    longitudnally in mm 100

    Thickness tt of grid beamplaced 10

    Depth of beam dh in load in loaded

    direction in mm 50Depth dt of beam in direction 25

    Dx = El t l dl ^3 / 12 a

    30000 x 10 x 25 ^3 / 12 x 100

    = 3906250 x 8

    Dy = El t l dl ^3 / 12 a 3906250 x 8

    2H = 2a (Jl / a + Jt /b 7812500 x 8

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    Distributed load

    (88290+ 7500 + 6150) / 10100 x

    2430 =

    0.0041535

    Deflection Ymax in mm

    ymax = 16 p d/ 3.14^2 D

    16 x 0.0041535 x 10^6 / 3.14^2 x

    5.34133 x 8

    = 15.075 mm

    Bending moment Mx in N-mm

    m l = 16 p d a / 3.14 ^4 x w^4 [D]

    16 x 0.00415.35 x 100 / 3.14^4 x

    1000^4 x 8 x 5.3413 x 10^-6

    = 1.5998 x 10 ^-9

    Bending moment Mx in N-mm

    m l = 16 p d a / 3.14 ^4 x w^4 [D]

    16 x 0.00415.35 x 100 / 3.14^4 x

    24830^4 x 8 x 5.3413 x 10^-6 =

    4.5883 x 10 ^-11

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