Page 586 - Automotive Engineering Powertrain Chassis System and Vehicle Body
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Design and material utilization   C HAPTER 18.1


                                     All figures relate to the body structure
                                     and exclude fenders and closures

















                                                           Mass (kg)            307
                                                           Torsional stiffness (Nm/deg)  17 360
                                                           First torsion (Hz)    36
                                                           First bending (Hz)    52
                                                           Number of parts      317
           Fig. 18.1-3 Land Rover Freelander with monocoque body and plastic front wings. (Reprinted with permission from SAE paper 1999-
           01-3181 Copyright 1999 Society of Automotive Engineers Inc.)


           Until this day the hot rolled grades of steel are used (typ-  The Lotus Elise featured the punt, which has also been
           ically HR 4) but it is easy to see why efforts are being  termed a spaceframe concept and as this is more of
           made to downscale these relatively massive ladder frames  a transitionary structure this will be described in greater
           with consideration being given to using newer material in  detail later on together with similar aluminium internally
                                               2
           thinner gauges, e.g. HSS up to 300 N/mm (TRIP steels  structured bodies.
                         2
           up to 590 N/mm are now being used for 80 chassis parts  It has been debated as to what exactly constitutes
           on the Mitsubishi Paquera). Design modifications must  a chassis-less design as various forms can incorporate
           be made to accommodate the thinner gauges and con-  some features of the original underframe, e.g. subframes
           sideration has already been given to alternative material  and longitudinal/sidemember sections. Engineers such as
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           forms such as hydroformed sections (described later), as  Garrett claim that the ideal form of chassis-less con-
           referenced by the ULSAB process, which could be used  struction emerged in the 1940s with the launching of the
           to bolster stiffness and crashworthiness. Although better  Austin A30 as shown in Fig. 18.1-5.
           suited to more conventional car body design, the in-  They would argue that using their aircraft design
           corporation of tailored blanks again offers an alternative  principles they were able to incorporate all the essential
           approach giving the engineer strengthening exactly where  load bearing requirements into a relatively lightweight
           required and a further opportunity for parts consolida-  body without even building in partial box sections that
           tion/reduced weight. This enduring type of rugged and  were featured in ‘integral’ or ‘unitary’ designs, with
           versatile design has persisted as it answers the diverse  elements of the chassis incorporated in the underbody.
           needs of military purchasers but it is not surprising that as  However, even with such box sections and subframes the
           fleet average economy targets are considered more criti-  easily spot welded and finished bodies provided a signi-
           cally the monocoque is now becoming more stringent for  ficant advance in bodyweight reduction while meeting
           the more volume-oriented 4   4 vehicles – as featured by  most engineering and manufacturing criteria.
           the Land Rover Freelander (Fig. 18.1-3). Durability is  The unitary design (monocoque is referred to in the
           satisfied by the use of hot-dip or iron–zinc alloy coating as  industry but some say this should be reserved for com-
           steel substrates replace the use of expensive aluminium  petition type bodies of tube configuration) is by far the
           for outer panels and the model features another material  most popular type of body and using the powerful FEM
           innovation in the selection of polymer front wings.  analytical programs that exist today (see below) the
             Before leaving body-on-chassis design it should be  design can be optimized at the design stage to maximize
           mentioned that other types of chassis include the steel  the use of properties and thereby reduce the number of
           backbone type used by Lotus and the designs featuring  prototypes, rework and development time. The more
           triangular sectional arrays as shown in Fig. 18.1-4. These  numerical data that can be gathered at this stage related
           were steel square or tubular sections, and later Lotus  to materials behaviour the more efficient modelling will
           adopted another chassis configuration termed the ‘punt’,  be, and this applies to other simulation processes besides
           also shown.                                        those predicting dynamic and static behaviour such as


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