solid185

中文 翻译 阿房宫赋翻译下载德汉翻译pdf阿房宫赋翻译下载阿房宫赋翻译下载翻译理论.doc 实体185 3维8节点结构实体 SOLID185要素描述 SOLID185应用于3-D实体结构的建模. 它被定义为每个节点有三个自由度的八节点模型:即在节的x, y, 和z方向.这种单元具有可塑性,超弹性 ,应力加劲 , 蠕变, 大的偏斜, 和大的过度疲劳能力. 它也具有模拟几乎不能压缩的弹塑性材料和完全不能压缩的超弹性材料形变的混合公式。 为了获得更多的关于SOLID185单元的详细资料，您可以查看ANSYS, Inc. Theory Reference SOLID185单元的输入数据 图185.1展示了SOLID185单元的几何图形和节点位置 。SOLID185单元具有八节点、正交各相异性的材料属性。默认单元的坐标系是向着各个方向的。 你可以用ESYS定义单元的坐标系, ESYS形成了正交各向异性材料方向的基础。 Node and Element Loads.描述了单元载荷. 压力可以作为 表 关于同志近三年现实表现材料材料类招标技术评分表图表与交易pdf视力表打印pdf用图表说话 pdf 面载和输入，作用在单元的表面上，如图 185.1。正压力作用于单元内， 温度可能作为节点的单元体载荷输入. 节点I的温度T(I) 默认为TUNIF. 如果全部的其他的温度未指明的, 则默认为T(I)。 对于任何的其他的输入温度格式, 未指明的温度默认为TUNIF。 由于积分通量，相似的默认产生，除非零代替TUNIF。 KEYOPT(6) = 1为了使用混合公式设置了这个单元。 关于混合公式的详细资料, 请看ANSYS原理参考中的应用混合u-P公式。 你可以用ISTRESS或ISFILE命令给单元施加一个初压力。 为了更多的信息, 看ANSYS Basic Analysis Guide中初压力加载。 交替地, 你可以设置KEYOPT(10) = 1，从使用者子程序USTRESS来读得最初的压力。 为了使用者子程序的详细资料, 看ANSYS使用者可 设计 领导形象设计圆作业设计ao工艺污水处理厂设计附属工程施工组织设计清扫机器人结构设计 的特性指导。 正如坐标系中描述的那样, 你能使用ESYS来规定材料属性和过度疲劳/压力输出。 使用RSYS选择符合材料的坐标系和全局的坐标系的输出。 对于超弹性物质材料, 应力和过度疲劳的输出总是与全局笛卡尔的坐标系有关，而不是符合材料和单元坐标系。 这个单元自动地包括了压力载荷刚度的影响. 如果压力载荷刚度影响需要不对秤的矩阵, 使用NROPT,UNSYM. "SOLID185输入摘要" 包含单元输入的摘要. 对于单元输入的普通描写, 看Element Input。 SOLID185输入摘要 节点 I, J, K, L, M, N, O, P 自由的度 UX, UY, UZ 实常数 无, 如果KEYOPT(2) = 0, HGSTF -沙漏坚硬缩放比例因素，如果KEYOPT(2) = 1 (默认是1.0; 任何的正数都有效。 如果开始为0.0, 其值自动地设置为 1.0.) 材料属性 不包括, EY, EZ, PRXY, PRYZ, PRXZ (或NUXY, NUYZ, NUXZ), ALPX, ALPY, ALPZ (或CTEX, CTEY, CTEZ或THSX, THSY, THSZ), 密度, GXY, GYZ, GXZ, 湿气 表面载荷 压力 面1 (J-I-L-K) 面2 (I-J-N-M), 面3 (J-K-O-N), 面4 (K-L-P-O), 面5 (L-I-M-P), 面6 (M-N-O-P) 体载荷 温度 T(I), T(J), T(K), T(L), T(M), T(N), T(O), T(P) 特殊特性 可塑性 超弹性 粘弹性 粘塑性 蠕变 应力钢化 大的偏斜 大的过度疲劳 最初的压力输入 单元技术的自动机械选择 单元生死 支持与TB命令有关的下面的数据表：: ANEL, BISO, MISO, NLISO, BKIN, MKIN, KINH, CHABOCHE, HILL, RATE, CREEP, HYPER, PRONY, SHIFT, CAST, SMA, ELASTIC, SDAMP, PLASTIC, and USER. 看 ANSYS, Inc. Theory Reference 获得更多的材料模型的详细资料。 KEYOPT(2) 单元技术: 0 --  全部综合有： 方法 快递客服问题件处理详细方法山木方法pdf计算方法pdf华与华方法下载八字理论方法下载 1 --  统一的简化的有沙漏控制整合 2 --  加强的过度疲劳公式 3 --  简化提高的过度疲劳公式 KEYOPT(6) 单元公式 0 --  使用纯的位移公式(默认) 1 --  使用混合公式 KEYOPT(10) 自定义初的压力: 0 --  没有使用者子程序提供初的压力(默认). 1 --  从使用者子程序USTRESS 读最初的压力数据 注意：看the Guide to ANSYS User Programmable Features 获得使用者书写子程序的相关信息。 SOLID185单元技术 · SOLID185使用这个方法（也是以可选择的简化的积分方法而著名）是统一的=简化的综合方法, 或提高过度疲劳公式的方法, 具体如下: · 方法(选择的简化的积分) 在几乎不能压缩的例子，这种方法有助于防止体积的网孔禁闭。 在具有平均体应变的单元的高斯综合点，这个选项取代了体应变 。 但是在主要是弯曲的问 题 快递公司问题件快递公司问题件货款处理关于圆的周长面积重点题型关于解方程组的题及答案关于南海问题 中，这方法不能防止任何剪切禁闭， 在这样得情况下, 使用提高的单元疲劳公式。 在不清除、变形主要是弯曲问题的情况下, 提高疲劳共识是首选的. 为获得更多的相关信息, 请看the ANSYS, Inc. Theory Reference. 统一简化的积分 同样在几乎不能压缩的例子，这种方法有助于防止体积的网孔禁闭。 因为这种方法有唯一的积分点, 这选项比以前的方法更有效 (可选择的简化积分方法) 。然而, 人工的精力控制沙漏结果可能相应地影响求解的精确性。 当时用这个选项的时候, 通过对比总精力(SENE标签在ETABLE) 和沙漏控制的人造的精力(AENE标签在ETABLE)来检查求解。 如果人造的精力与总数精力之比小于5%,求解是一般可接受的。 如果他们的比超过5%, 应该精炼网孔（重新划分网孔），在求解阶段，你也可以发出通OUTPR,VENG 命令来监控总数精力和人造的精力。 为获得更多的相关信息，请看ANSYS, Inc. Theory Reference. 加强的过度疲劳公式 在几乎不能压缩的例子中，他能防止主要是剪禁闭弯曲问题和体积禁闭的问题。这个公式能介绍13内部的DOFs (ANSYS使用者不可接触到的)。如果混合u-P公式和加强的过度疲劳公式被调用, 仅仅是克服剪-锁的9 DOF 运行。 因为额外的内部的DOFs和静态冷凝, 这选项的有效性的比其他的方法(可选择的简化的积分的方法) 选项或统一的简化的积分选项低 。 为获得更多的相关信息，请看ANSYS, Inc. Theory Reference. 简化的加强过度疲劳公式 在主要是弯曲的问题中，他能防止剪禁闭。 这是加强的疲劳公式的特殊例子，通常介绍9内部的DOFs （ANSYS使用者难以接近的）。 因为在那里是没有内在的DOFs解决体积的锁, 当材料是几乎不能压缩的时候， 不应该使用这公式 除非在同时使用混合u-P的时候。当使用混合u-P公式的时候, 简化的过度疲劳公式与加强的过度疲劳公式结果相同。 因为额外的内在的DOFs和静态冷凝, 这选项的有效性的比其他的方法(可选择的简化的积分的方法) 选项或统一的简化的积分选项低 ，但是由于用较少内在的DOFs所以更有效。 为获得更多的相关信息，请看ANSYS, Inc. Theory Reference. SOLID185输出数据 与单元有关的求解输出有两种形式： · 节的位移包括的在总的节的解答 · 其余的单元输出清看Table 185.1: "SOLID185 Element Output Definitions"（单元185 元素输出定义） 图185.2 SOLID185压力输出（图略） 压力方向的表明是为了全局方向。 单元输出定义表使用了下列各项符号: 冒号(:) 表示该项能通过成分明的方法[ETABLE, ESOL]提取。O列表使该项可由Jobname.OUT提取。在R表示该项刻有结果文件提取。 在O或R列中, Y表示该项总是可以获取的；数字和脚注表示该项优势是可以获取的 。 “-”表示该项是不获取的。 SOLID185 单元输出定义表 名称 定义 O R EL 单元号 - Y 节点 节点- I, J, K, L, M, N, O, P - Y 垫 材料号 - Y VOLU: 体积 - Y XC, YC, ZC 结果输出点位置 Y 3 PRES 压P1在节点J, I, L, K上; P2在I, J, N, M上; P3在J, K, O, N上; P4在K, L, P, O上; P5在L, I, M, P上; P6在M, N, O, P上 - Y TEMP 温度T(I), T(J), T(K), T(L), T(M), T(N), T(O), T(P) - Y S:X, Y, Z, XY, YZ, XZ 应力 Y Y S:1, 2, 3 主应力 - Y S:INT 应力强度 - Y S:EQV 等效应力 - Y EPEL:X, Y, Z, XY, YZ, XZ 弹性应变 Y Y EPEL:1, 2, 3 主弹性应变 - Y EPEL:EQV 等效的弹性应变[6] - Y EPTH:X, Y, Z, XY, YZ, XZ 热应变 2 2 EPTH:EQV 等效热的应变[6] 2 2 EPPL:X, Y, Z, XY, YZ, XZ 塑性应变 [7] 1 1 EPPL:EQV 等效的塑性应变[6] 1 1 EPCR:X, Y, Z, XY, YZ, XZ 蠕变 1 1 EPCR:EQV 等效蠕变[6] 1 1 EPTO:X, Y, Z, XY, YZ, XZ 总机械的应变 (EPEL + EPPL + EPCR) Y - EPTO:EQV 总数相等的机械的过度疲劳(EPEL + EPPL + EPCR) Y - NL:EPEQ 积聚的等效塑性应变 1 1 NL:CREQ 积聚等效蠕变 1 1 NL:SRAT 塑性屈从的(1 = 活跃地屈从的, 0 = 不屈从的) 1 1 NL:HPRES 静水力学的压力 1 1 发送:弹性的, 塑性、蠕变 应变能量密度 - 1 LOCI:X, Y, Z 综合点位置 - 4 SVAR:1, 2, ... , N 情形变量 - 5 1. 当材料单元是非线性材料时才能进行非线性求解并输出结果。 2. 当单元有热载荷的时候才能输出求解。 3. 当USERMAT子程序和TB运行时获得。 4. 等效应变用到了柏松比，用户为弹性的和热的材料定义这个值(MP,PRXY); 对于塑性和蠕变材料，这值设置成 0.5。 5. 对于非弹性材料的铝合金，由塑性来表示应变。 在节点I, J, ..., P上的序号数据 表185.2 SOLID185项目和次序号码 输出量名字 ETABLE和ESOL命令输入 项目 I J K L M N O P P1 SMISC 2 1 4 3 - - - - P2 SMISC 5 6 - - 8 7 - - P3 SMISC - 9 10 - - 12 11 - P4 SMISC - - 13 14 - - 16 15 P5 SMISC 18 - - 17 19 - - 20 P6 SMISC - - - - 21 22 23 24 · SOLID185假设和限定 · 单元体不许为零。 · 必须给单元分配号码。如图185.1: "SOLID185几何图形" 或可能有位面IJKL和MNOP交换. 有俩各相分离体积的单元体可能被扭曲，当单元的号码定义的不恰当的时候，这种情况经常发生。 · 所有的单元体都有八个节点。你可以通过定义双重的K和L,双重的O和P节点号码来形成棱柱状的单元体。同样也可以获得四面体 。 · 对于单元体中指定了加强的应变公式的形状退化的单元体，经常使用退化形状功能和一个传统的综合列表。 · 如果使用混合公式，你必须使用稀疏求解器或者是前沿求解器。 · 对于节点循环对称的分析，ANSYS 建议您使用加强的应变公式。 · 屈服应力通常包括非线性的几何分析者通常在线性分析中被忽略了通过 PSTRES命令你可以激活压力 。 SOLID185 输出限定 单元185没有特殊的输出限定。 SOLID185 3-D 8-Node Structural Solid MP ME ST <> <> PR <> <> <> PP ED SOLID185 Element Description SOLID185 is used for the 3-D modeling of solid structures. It is defined by eight nodes having three degrees of freedom at each node: translations in the nodal x, y, and z directions. The element has plasticity, hyperelasticity, stress stiffening, creep, large deflection, and large strain capabilities. It also has mixed formulation capability for simulating deformations of nearly incompressible elastoplastic materials, and fully incompressible hyperelastic materials. See SOLID185 in the ANSYS, Inc. Theory Reference for more details about this element. A higher-order version of the SOLID185 element is SOLID186. Figure 185.1  SOLID185 Geometry SOLID185 Input Data The geometry and node locations for this element are shown in Figure 185.1: "SOLID185 Geometry". The element is defined by eight nodes and the orthotropic material properties. The default element coordinate system is along global directions. You may define an element coordinate system using ESYS, which forms the basis for orthotropic material directions. Element loads are described in Node and Element Loads. Pressures may be input as surface loads on the element faces as shown by the circled numbers on Figure 185.1: "SOLID185 Geometry". Positive pressures act into the element. Temperatures may be input as element body loads at the nodes. The node I temperature T(I) defaults to TUNIF. If all other temperatures are unspecified, they default to T(I). For any other input temperature pattern, unspecified temperatures default to TUNIF. Similar defaults occurs for fluence except that zero is used instead of TUNIF. KEYOPT(6) = 1 sets the element for using mixed formulation. For details on the use of mixed formulation, see Applications of Mixed u-P Formulations in the ANSYS Elements Reference. You can apply an initial stress state to this element through the ISTRESS or ISFILE command. For more information, see Initial Stress Loading in the ANSYS Basic Analysis Guide. Alternately, you can set KEYOPT(10) = 1 to read initial stresses from the user subroutine USTRESS. For details on user subroutines, see the Guide to ANSYS User Programmable Features. As described in Coordinate Systems, you can use ESYS to orient the material properties and strain/stress output. Use RSYS to choose output that follows the material coordinate system or the global coordinate system. For the case of hyperelastic materials, the output of stress and strain is always with respect to the global Cartesian coordinate system rather than following the material/element coordinate system. The effects of pressure load stiffness are automatically included for this element. If an unsymmetric matrix is needed for pressure load stiffness effects, use NROPT,UNSYM. "SOLID185 Input Summary" contains a summary of element input. For a general description of element input, see Element Input. SOLID185 Input Summary Nodes I, J, K, L, M, N, O, P Degrees of Freedom UX, UY, UZ Real Constants None, if KEYOPT(2) = 0, HGSTF - Hourglass Stiffness Scaling factor if KEYOPT(2) = 1 (Default is 1.0; any positive number is valid. If set to 0.0, value is automatically reset to 1.0.) Material Properties EX, EY, EZ, PRXY, PRYZ, PRXZ (or NUXY, NUYZ, NUXZ), ALPX, ALPY, ALPZ (or CTEX, CTEY, CTEZ or THSX, THSY, THSZ), DENS, GXY, GYZ, GXZ, DAMP Surface Loads Pressures --  face 1 (J-I-L-K), face 2 (I-J-N-M), face 3 (J-K-O-N), face 4 (K-L-P-O), face 5 (L-I-M-P), face 6 (M-N-O-P) Body Loads Temperatures --  T(I), T(J), T(K), T(L), T(M), T(N), T(O), T(P) Special Features Plasticity Hyperelasticity Viscoelasticity Viscoplasticity Creep Stress stiffening Large deflection Large strain Initial stress import Automatic selection of element technology Birth and death Supports the following types of data tables associated with the TB command: ANEL, BISO, MISO, NLISO, BKIN, MKIN, KINH, CHABOCHE, HILL, RATE, CREEP, HYPER, PRONY, SHIFT, CAST, SMA, ELASTIC, SDAMP, PLASTIC, and USER. Note See the ANSYS, Inc. Theory Reference for details of the material models. See Automatic Selection of Element Technologies and ETCONTROL for more information on selection of elemet technologies. KEYOPT(2) Element technology: 0 --  Full integration with method 1 --  Uniform reduced integration with hourglass control 2 --  Enhanced strain formulation 3 --  Simplified enhanced strain formulation KEYOPT(6) Element formulation: 0 --  Use pure displacement formulation (default) 1 --  Use mixed formulation KEYOPT(10) User-defined initial stress: 0 --  No user subroutine to provide initial stresses (default). 1 --  Read initial stress data from user subroutine USTRESS Note See the Guide to ANSYS User Programmable Features for user written subroutines. SOLID185 Element Technology SOLID185 uses the method (also known as the selective reduced integration method), the uniform reduced integration method, or the enhanced strain formulation method, as follows: · method (selective reduced integration) Helps to prevent volumetric mesh locking in nearly incompressible cases. This option replaces volumetric strain at the Gauss integration point with the average volumetric strain of the elements. This method cannot, however, prevent any shear locking in bending dominated problems. In such situations, use the enhanced strain formulation of this element. If it is not clear if the deformation is bending dominated, enhanced strain formulation is recommended. For more information, see the ANSYS, Inc. Theory Reference. · Uniform reduced integration Also helps to prevent volumetric mesh locking in nearly incompressible cases. Because it has only one integration point, this option is more efficient than the method (selective reduced integration) option. However, the artificial energy introduced to control the hourglass effect may affect solution accuracy adversely. When using this option, check the solution accuracy by comparing the total energy (SENE label in ETABLE) and the artificial energy (AENE label in ETABLE) introduced by hourglass control. If the ratio of artificial energy to total energy is less than 5%, the solution is generally acceptable. If the ratio exceeds five percent, refine the mesh. You can also monitor the total energy and artificial energy by issuing the OUTPR,VENG command in the solution phase. For more information about uniform reduced integration, see the ANSYS, Inc. Theory Reference. · Enhanced strain formulation Prevents shear locking in bending-dominated problems and volumetric locking in nearly incompressible cases. The formulation introduces 13 internal DOFs (inaccessible to ANSYS users). If mixed u-P formulation is employed with enhanced strain formulation, only 9 DOFs for overcoming shear-locking are used. All internal DOFs are introduced automatically at the element level and condensed out. Because of the extra internal DOFs and static condensation, this option is less efficient than either the method (selective reduced integration) option or the uniform reduced integration option. For more information about enhanced strain formulation, see the ANSYS, Inc. Theory Reference. · Simplified enhanced strain formulation Prevents shear locking in bending-dominated problems. This is a special case of the enhanced strain formulation and always introduces 9 internal DOFs (inaccessible to ANSYS users). Because there are no internal DOFs to handle volumetric locking, this formulation should not be used when the material is nearly incompressible, except when the Mixed u-P formulation is also used. When used with the Mixed u-P formulation, the simplified enhanced strain formulation gives the same results as the enhanced strain formulation. All internal DOFs are introduced automatically at the element level and condensed out. Because of the extra internal DOFs and static condensation, this option is less efficient than either the method (selective reduced integration) option or the uniform reduced integration option, but is more efficient than the enhanced strain formulation due to using fewer internal DOFs. For more information about the simplified enhanced strain formulation, see the ANSYS, Inc. Theory Reference. SOLID185 Output Data The solution output associated with the element is in two forms: · Nodal displacements included in the overall nodal solution · Additional element output as shown in Table 185.1: "SOLID185 Element Output Definitions" Several items are illustrated in Figure 185.2: "SOLID185 Stress Output". See Element Table for Variables Identified By Sequence Number in the ANSYS Basic Analysis Guide and The Item and Sequence Number Table in this manual for more information. Figure 185.2  SOLID185 Stress Output Stress directions shown are for global directions. The Element Output Definitions table uses the following notation: A colon (:) in the Name column indicates the item can be accessed by the Component Name method [ETABLE, ESOL]. The O column indicates the availability of the items in the file Jobname.OUT. The R column indicates the availability of the items in the results file. In either the O or R columns, Y indicates that the item is always available, a number refers to a table footnote that describes when the item is conditionally available, and a - indicates that the item is not available. Table 185.1  SOLID185 Element Output Definitions Name Definition O R EL Element Number - Y NODES Nodes - I, J, K, L, M, N, O, P - Y MAT Material number - Y VOLU: Volume - Y XC, YC, ZC Location where results are reported Y 3 PRES Pressures P1 at nodes J, I, L, K; P2 at I, J, N, M; P3 at J, K, O, N; P4 at K, L, P, O; P5 at L, I, M, P; P6 at M, N, O, P - Y TEMP Temperatures T(I), T(J), T(K), T(L), T(M), T(N), T(O), T(P) - Y S:X, Y, Z, XY, YZ, XZ Stresses Y Y S:1, 2, 3 Principal stresses - Y S:INT Stress intensity - Y S:EQV Equivalent stress - Y EPEL:X, Y, Z, XY, YZ, XZ Elastic strains Y Y EPEL:1, 2, 3 Principal elastic strains - Y EPEL:EQV Equivalent elastic strains [6] - Y EPTH:X, Y, Z, XY, YZ, XZ Thermal strains 2 2 EPTH:EQV Equivalent thermal strains [6] 2 2 EPPL:X, Y, Z, XY, YZ, XZ Plastic strains[7] 1 1 EPPL:EQV Equivalent plastic strains [6] 1 1 EPCR:X, Y, Z, XY, YZ, XZ Creep strains 1 1 EPCR:EQV Equivalent creep strains [6] 1 1 EPTO:X, Y, Z, XY, YZ, XZ Total mechanical strains (EPEL + EPPL + EPCR) Y - EPTO:EQV Total equivalent mechanical strains (EPEL + EPPL + EPCR) Y - NL:EPEQ Accumulated equivalent plastic strain 1 1 NL:CREQ Accumulated equivalent creep strain 1 1 NL:SRAT Plastic yielding (1 = actively yielding, 0 = not yielding) 1 1 NL:HPRES Hydrostatic pressure 1 1 SEND:ELASTIC, PLASTIC, CREEP Strain energy densities - 1 LOCI:X, Y, Z Integration point locations - 4 SVAR:1, 2, ... , N State variables - 5 6. Nonlinear solution, output only if the element has a nonlinear material 7. Output only if element has a thermal load 8. Available only at centroid as a *GET item 9. Available only if OUTRES,LOCI is used 10. Available only if the USERMAT subroutine and TB,STATE are used 11. The equivalent strains use an effective Poisson's ratio: for elastic and thermal this value is set by the user (MP,PRXY); for plastic and creep this value is set at 0.5. 12. For the shape memory alloy material model, transformation strains are reported as plasticity strain EPPL. Table 185.2: "SOLID185 Item and Sequence Numbers" lists output available through ETABLE using the Sequence Number method. See Element Table for Variables Identified By Sequence Number in the ANSYS Basic Analysis Guide and The Item and Sequence Number Table in this manual for more information. The following notation is used in Table 185.2: "SOLID185 Item and Sequence Numbers": Name output quantity as defined in the Table 185.1: "SOLID185 Element Output Definitions" Item predetermined Item label for ETABLE command I,J,...,P sequence number for data at nodes I, J, ..., P Table 185.2  SOLID185 Item and Sequence Numbers Output Quantity Name ETABLE and ESOL Command Input Item I J K L M N O P P1 SMISC 2 1 4 3 - - - - P2 SMISC 5 6 - - 8 7 - - P3 SMISC - 9 10 - - 12 11 - P4 SMISC - - 13 14 - - 16 15 P5 SMISC 18 - - 17 19 - - 20 P6 SMISC - - - - 21 22 23 24 SOLID185 Assumptions and Restrictions · Zero volume elements are not allowed. · Elements may be numbered either as shown in Figure 185.1: "SOLID185 Geometry" or may have the planes IJKL and MNOP interchanged. The element may not be twisted such that the element has two separate volumes (which occurs most frequently when the elements are not numbered properly). · All elements must have eight nodes. You can form a prism-shaped element by defining duplicate K and L and duplicate O and P node numbers (see Triangle, Prism and Tetrahedral Elements). A tetrahedron shape is also available. · For the degenerated shape elements where the or enhanced strain formulations are specified, degenerated shape functions and a conventional integration scheme are used. · If you use the mixed formulation (KEYOPT(6) = 1), you must use either the sparse solver (default) or the frontal solver. · For modal cyclic symmetry analyses, ANSYS recommends using enhanced strain formulation. · Stress stiffening is always included in geometrically nonlinear analyses (NLGEOM,ON). It is ignored in geometrically linear analyses (NLGEOM,OFF) when specified by SSTIF,ON. Prestress effects can be activated by the PSTRES command. SOLID185 Product Restrictions There are no product-specific restrictions for this element. PAGE 1