Marston, P.G.

Myatt, R.L.

DSpace@MIT

DOE/PC-90350-5DC CICC Retrofit MagnetPreliminary Design,Software Development and Analysis ReportQuarterly Progress ReportContract No. DE-FG22-90PC90350April 1992R. Leonard Myatt and P.G. MarstonSubmitted May 28, 1992Massachusetts Institute of TechnologyPlasma Fusion Center175 Albany StreetCambridge, MA 02159PFCIRR-92-81.0 IntroductionThe January 1992 quarterly progress report' discusses a two-dimensional finite elementanalysis (FEA) of the proposed retrofit MHD coil. The superconducting Cable-in-ConduitConductor (CICC) winding pack has a smooth, semi-elliptical cross section and is supported bya similarly shaped strap which resists the electromagnetic forces tending to separate the coils oneach side of the channel. The coils are designed to produce a peak on-axis field of 4.5 tesla witha nominal current density of 13.05x10' A/r 2 . A sketch of the magnet system and structure isshown in Fig. 1.0-1.The objective of this analysis is to quantify the highly 3-D characteristics of the proposedsuperconducting magnet system, and develop an appropriate support concept. A fully paramatized3-D finite element model of the coil and structure is developed as a means of obtaining the fieldand stress solutions. The flexibility of FEA and a model built using design parameters allowsvariations in the coil end turn bend radius, strap thickness, support details and positions to bestudied. The preliminary results show the calculated stresses as a result of this iterative designprocess.2.0 Summary and ConclusionsThe detailed finite element analysis presented here verifies the credibility of the proposedconstant tension support concept for the DC CICC retrofit MHD magnet. Stresses in the structuralmembers are on the order of 100 to 200 MPa, which are reasonable for the materials beingconsidered. Regions of higher stress can be accommodated by subtle modifications andrefinements to the structure, and more detailed analysis. However, at this stage of design andanalysis, the fundamental structural requirements are met by the proposed design.3.0 Analysis DescriptionThe analysis described here is designed to evaluate the complex 3-D behavior of thedipole coil and support structure. The electromagnetic and structural evaluations are based on a3-D nonlinear finite element analysis of the proposed MHD coil and support concept. The finiteelement model ignores the slight taper in the magnet system which allows the use of threesymmetry planes thereby greatly reducing the model size and computational time.3.1 The Finite Element ModelThe winding pack cross section with a nominal build of 0.72 meter width and 0.88 meterhalf height represents a coil which operates right at the design current density of about 13 MA-turns/m2 . The analysis assumes zero friction between the coil and the strap. Although not entirelytrue, this assumption is necessary due to the size and complexity of the 3-D nonlinear model. Theref. 1 report discusses the effects of friction on the stresses in the coil, and indicates that relativemotion between the strap and the coil is an essential part of the design concept.1The model is generated within the ANSYS PREP7 preprocessor. Fundamental dimensionsare defined by parameters which greatly simplify the inevitable changes to the model which occurduring the design and analysis process. Changes such as mesh density, coil build, end turnsupport plate thicknesses and crossover radii can all be accommodated by simply redefiningnumbers in the parameter list. Figures 3.1-1 to 3.1-3 show the finite element model in somedetail.3.2 Material PropertiesThe nature of the analysis and its objectives establish the level of detail that must beincluded in the model. On this basis, the actual winding pack (i.e., insulation, conductor, conduit)is approximated by smeared orthotropic material properties.Modulus of Elasticity:E, = E, = 28 GPa (Transverse)EY = 58 GPa (Longitudinal)Shear Modulus:G = 7 GPa (Trans-Long)G = 20 GPa (Long-Trans)G = 9 GPa (Trans-Trans)Poisson's Ratio:VX, = 0.30 (Trans Strain from Long Stress)vyZ = 0.16 (Long Strain from Trans Stress)V. = 0.24 (Trans Strain from Trans Stress)These properties are calculated such that the global structural characteristics of the saddle coilare represented. The material properties associated with the strap, end turn support plates, andgussets are simply isotropic constants.3.3 Boundary Conditions and Solution ProcessDisplacement boundary conditions for the structural analysis provide for full machinebehavior by specifying zero displacements across the three symmetry planes. The model is loadedelectromagnetically by a uniform current density of 13.05x10 6 A/nm2 , which produces a nominal4.5 tesla at the machine axis. The first pass of the analysis solves the electrical problem. One endof the coil is set to zero potential, while a known current is applied at the other. The currentdensity is essentially uniform across the build of the coil, as it must be in a superconductingapplication. The second pass of the analysis solves the magnetics problem. J x B body forces arealso calculated and saved automatically as input to the next pass of the analysis which is thestructural solution. The analysis is complete when the nonlinear gap elements have converged asthe coil strains and slips within the confines of the supporting structure.23.4 Structural DetailsDuring the coil manufacturing process, the conductor is bent to form the end turns of themagnet. Plastic deformation occurs, which is often called keystoning as it describes the shape ofthe deformed cross section (see Fig 3.4-1). The amount of distortion is inversely proportional tothe bend radius. For large radii, the effect is small and the distortion is minimal. An end turnwith a large bend radius is inefficient as it consumes valuable space and material, and locallydegrades the quality of the magnetic field. An end turn with a small bend radius is compact andefficient, but results in an array of oddly shaped conductors which, as a result, load and strainwith non-uniformities. Therefore, establishing a minimum bend radius requires striking acompromise. The permanent strain (5) can be quantified by the following simple equation:S = t2 / 8rwhere t is the thickness of the conduit, and r is the bend radius. The maximum deformation ischosen to be 0.5 mm, which establishes a minimum bend radius of about 30 cm.Although the conductor winding pack represents a significant structural cross section, theelectromagnetic forces in the end turn region are high and tend to collapse the opposing coils.These forces are resisted by reinforced support plates which are located under the end turnwinding packs. The construction of these plates is limited locally by the distance between the coiland the channel. Outboard of the channel the plates are well reinforced by gussets which spanthe distance between the two end turns. This support concept is shown in the CAD drawing ofFig 3.4-2.4.0 ResultsThe results of the analysis are best summarized by the graphical output from the computerfinite element model. The following is a series of plots depicting the stresses in the variouscomponents of the system.Figure 4.0-1 shows the tresca stress intensity in the support shell, which extends thelength of the straight section and into the first bend region of the end turn. The nominal stressin the 2" thick shell is about 150 MPa, and peaks to 270 MPa in a very small localized regionat the tight bend. This high stress can be relieved by altering the structure in that particularregion.Figure 4.0-2 shows the tresca stress intensity in the shell extension. Ignoring the regionwhere the shell tapers to a knife edge, all the stresses are also 150 MPa and below.Figure 4.0-3 shows the stresses in the end turn support plate which carries the windingpack up and over the channel. The vast majority of stresses within the structure are below 200MPa. As with the shell extension, there is a local region of high stress due to the sharp taperwhere the two coils diverge to form the end turn.Figure 4.0-4 shows the tresca stress intensity in the gusset plates which bridge the spanbetween the upper and lower support plates at each end of the magnet system. The stressesshown here are all below 100 MPa, and pose no threat to the structural integrity of the design.3However, in the actual design, these plates are joined and closed off by a cover plate, addingrigidity and stability to an otherwise open section.Figure 4.0-5 shows the tresca stress intensity in the aluminum sheath, the structuralelement of the conductor winding pack. At the magnet midplane the stresses match those of the2-D analysis of reference 1. Stresses peak at about 110 MPa in the transition region between theend turn and straight section. Stresses at the end turn mid-span, directly above the channelcenterline, peak at about 80 MPa, an indication that the end turns are well supported by thegusseted plate design presented here.5.0 References1. R.Leonard Myatt and P.G. Marston, "DC CICC Retrofit Magnet Preliminary Design, SoftwareDevelopment and Analysis Report," DOE/PC-90350-4, Submitted February 10, 1992, MOTPlasma Fusion Center, Cambridge, MA4/-4-4B-3-U8':1-9-ThFig 1.0-1 Nominal Magnet Geometry5BUaBtsBacw-4..9-00 Va(/000a-siIFully Defined ElectromagneticallyStructurally 1/8th Symmetry UsedFig 3.1-1 ANSYS 3-D Finite Element Model6End Turn Support PlateViewed From AboveConstant Tension ShellViewed From BelowFig 3.1-2 Support Structure Isometrics7sometric ViewGussetsEnd ViewFig 3.1-3 End Turn Support8Shell Extens ionIGo 9 0 ccpe W * 04OhCOh W Oh OEE00II 00V0h..00 0000Fig 3.4-2 CAD Drawing of Proposed Structure10* CCCU0C;+E hi .. C*(45.4CUEU S* hiC hi ISI U ~6MUC4hihiI04hihi1U.UC4hiI-SC4hiCSC,16SC4hit.C* 0CO 04 4 ,S SS0hi4m A N % 0 " m0-co0CCC00C0.0.C0a)Io1*70)11*' hS 9 1-"aC4hihi0UUhi- - hiS a U54hiU.1*hiUCh6Nhi I H0 0 00 V 0 0 0 0ul + + 0 IN ~~~ +0 +-I~Ni 0 0 00 .14 0 0 0 1- - CO n 6 in 10 V, in 0) 0nn 01 m 0 00Ca0 co ai 14 0 2- 0 U 0v010 1- t10004xLI00QCoCola)iiL12n 10 10 00 0 00 0 00.0~~~ 0 N 0*N N N Nto. soc; c; S S40MFig 4.0-3 Stress Contours in End Turn Support Plate [Pa]13-JI LIt- 0 t- 0 w 0 0 0 0 0 0ea00 0 0 0O 0000 00 0ve cc t 4 W 14 14 14 W + 4 wo) wi- i a " hi hi 0i V) Wi gohi h0) - 0) I 4 04 D 0 0 t 0 0 4 Ito to NO - ~ 1 D (wN SW 64 toH M~ N A A h iFig 4.0-4 Stress Contours in End Turn Gusset Plates [Pa]1440m 9I n 6 4 0 0C~~~~~ + . 4 * 4 . 4~ 0a - UeFig 4.0-5 Stress Contours in Conductor Conduit [Pa]154isisI,S.40040-40hi040hit0aaisN40UN40if.ais000I1-04.hi40400BaC+hia00BCdaIsa S..

DC CICC retrofit magnet preliminary design, software development and analysis report: quarterly progress report, April, 1992

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DC CICC retrofit magnet preliminary design, software development and analysis report: quarterly progress report, April, 1992

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