<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE article  PUBLIC "-//NLM//DTD Journal Publishing DTD v3.0 20080202//EN" "http://dtd.nlm.nih.gov/publishing/3.0/journalpublishing3.dtd"><article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" dtd-version="3.0" xml:lang="en" article-type="research article"><front><journal-meta><journal-id journal-id-type="publisher-id">MSA</journal-id><journal-title-group><journal-title>Materials Sciences and Applications</journal-title></journal-title-group><issn pub-type="epub">2153-117X</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/msa.2013.412098</article-id><article-id pub-id-type="publisher-id">MSA-40532</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Chemistry&amp;Materials Science</subject></subj-group></article-categories><title-group><article-title>
 
 
  3D Braided Material Based on Space Group &lt;i&gt;R&lt;/i&gt;3 Symmetry
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>ensuo</surname><given-names>Ma</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Dongdong</surname><given-names>Yin</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>School of Mechatronics Engineering, Henan University of Science and Technology, Luoyang, China</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>mawensuo@126.com(EM)</email>;<email>yin-dong-dong@163.com(DY)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>06</day><month>12</month><year>2013</year></pub-date><volume>04</volume><issue>12</issue><fpage>773</fpage><lpage>779</lpage><history><date date-type="received"><day>August</day>	<month>31,</month>	<year>2013</year></date><date date-type="rev-recd"><day>October</day>	<month>2,</month>	<year>2013</year>	</date><date date-type="accepted"><day>October</day>	<month>27,</month>	<year>2013</year></date></history><permissions><copyright-statement>&#169; Copyright  2014 by authors and Scientific Research Publishing Inc. </copyright-statement><copyright-year>2014</copyright-year><license><license-p>This work is licensed under the Creative Commons Attribution International License (CC BY). http://creativecommons.org/licenses/by/4.0/</license-p></license></permissions><abstract><p>
 
 
   A unit cell geometrical structure was found with the use of symmetry operations corresponding to the point group C3. Based on the symmetry of space group R3, a 3D braided geometrical structure was obtained by transforming the unit-cell. The features corresponding to this braided structure were studied. The fiber volume percentage and variational tendencies of the material were predicted by establishing a geometric model.  
    
 
</p></abstract><kwd-group><kwd>Point Group C3; Space Group &lt;i&gt;R&lt;/i&gt;3; 3D Braided Geometrical Structure</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>3D braided composites with the excellent mechanical properties are widely used in the aerospace, defense and medical industries [<xref ref-type="bibr" rid="scirp.40532-ref1">1</xref>]. At present, most of the researches have focused on the four-step and two-step braiding methods.</p><p>Four-step braiding method was invented by Florentin invention in 1982, and the two-step braiding method was first invented by Poper and McConnell in 1987 [<xref ref-type="bibr" rid="scirp.40532-ref2">2</xref>]. The four-step three-dimensional braiding method has successfully been used in braiding the rocket nozzle and satellite enhanced phase with the structure of the support pieces. Mesoscopic structure and mechanical properties of the four-step 3D braided composites have been researched a lot [3-9]. Based on the four-step multi-dimensional braiding method, it has been applied to industrial processes successfully [5-9]. The three-dimensional multi-directional braiding process increased axial yarn in braided direction or the other two directions which are perpendicular to braided direction. At present the braided processing of three-dimensional five direction [5-7], six direction [5,8] and seven direction [5,9] has been in successful application. Li Jialu studied the structure and performance of the two-step square 3D braided material [<xref ref-type="bibr" rid="scirp.40532-ref10">10</xref>]. Two-step braiding method 3D braided material is not widely used in practical engineering projects.</p><p>Owing to the constraints of the processing technology, there exist too few varieties of three-dimensional braided composites, low processing efficiency and high cost of the process, which go against a better overall performance of 3D braided materials [<xref ref-type="bibr" rid="scirp.40532-ref11">11</xref>]. Thus there is an urgent need to develop a more three-dimensional processing. The new three-dimensional woven prediction research is still in its infancy [<xref ref-type="bibr" rid="scirp.40532-ref12">12</xref>].</p><p>Different lattice structures of the crystal showed the different properties, and crystal geometry can be classified by crystal symmetry group [<xref ref-type="bibr" rid="scirp.40532-ref13">13</xref>]. With reference to the research methods of symmetry group, researches on unit cell geometry of braided materials can be summarized. According to the space group and the space group, symmetry operations can be deduced from a large number of new three-dimensional yarn crossover methods [<xref ref-type="bibr" rid="scirp.40532-ref12">12</xref>]. A new geometry structure of 3D braided material was deduced by using space point S6 corresponding to symmetry operations and the symmetry of space group P3, and author researched its processing and properties [<xref ref-type="bibr" rid="scirp.40532-ref14">14</xref>]. Under the condition of satisfying all space point group <img src="3-7701077\2b670e14-058b-4426-830f-f63a8d4f0da9.jpg" /> [<xref ref-type="bibr" rid="scirp.40532-ref13">13</xref>] symmetry operations, a new unit-cell with yarn-cross structures is deduced. A kind of cross geometry structure with continuous yarn can be obtained by putting the unit-cell into space lattice content with its symmetry. A new 3D braiding method can be obtained by researching its processing.</p></sec><sec id="s2"><title>2. 3D Braided Geometry Structure Unit Cell Content with Point Group C3 Symmetry</title><p>Let z axis as a rotation axis in the three-dimensional coordinate system xyz. In space group C3 group elements are<img src="3-7701077\bbd96633-ad9f-4f15-acab-85a376a3dfec.jpg" />, Group of generators is<img src="3-7701077\68aeb93c-49e3-49a7-801c-d2064141ae83.jpg" />. Space group C3 is a pure rotation symmetry group. Group element <img src="3-7701077\a753e162-2d3f-4002-88b7-ab9eb9e8add1.jpg" /> represents a 120˚ rotation around the z-axis; <img src="3-7701077\7f22535a-2bce-40ff-968c-12797f592bab.jpg" />represents a 240˚ rotation around the z-axis. <img src="3-7701077\32c27945-457d-498a-9b25-6d08a6d73729.jpg" />represents a 360˚ rotation around an axis or non-rotation.</p><p>Point group C3 group of elements corresponding to symmetry operation can be expressed as</p><p><img src="3-7701077\18859700-2a6e-4d65-bf69-29ce463e26c6.jpg" /></p><p><img src="3-7701077\11cca26c-baee-48f6-a221-ca2a9f350d36.jpg" /></p><p><img src="3-7701077\1850f089-0c6e-4fe2-9dc0-ff25c382fac1.jpg" /></p><p><img src="3-7701077\d12fd984-d2bc-494b-8acd-333ec7eb00f6.jpg" />represents the symmetry operation that a point <img src="3-7701077\5cffe975-0407-4a8b-b539-634274c41a57.jpg" /> in a yarn segment is converted into a point after equal sign.</p><p>Applying symmetry operations of point group C to the yarn segment shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>(a), a kind of combination of yarn segment, as shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>(b), can be obtained, which is the representative volume unit for deriving new 3D braided geometry structure.</p></sec><sec id="s3"><title>3. 3D Braided Geometry Structure Content with Space Group Symmetry</title><sec id="s3_1"><title>3.1. Space Simple Hexagonal Lattice Corresponding to Space Group R3</title><p>A simple hexagonal lattice (shown in <xref ref-type="fig" rid="fig2">Figure 2</xref>) described by crystal symmetry group is coordinated with the space group C3. The deduced unit cell (shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>(b)) as a lattice point is put into the hexagonal lattice, and a new cross geometry structure (shown in <xref ref-type="fig" rid="fig3">Figure 3</xref>) with continuous yarn can be obtained considering the continuity of the yarn.</p></sec><sec id="s3_2"><title>3.2. Translation Symmetry Operations Corresponding to Space Group R3</title><p>In the xyz coordinate system, translation symmetry operation is<img src="3-7701077\e470caf1-b9ce-4f7d-9f9c-1175227d9a78.jpg" />.</p><p>4. Geometry Structure and Processing of the New Three-Dimensional Braided Material Corresponding to the Space Group R3 Symmetry New unit cell of three-dimensional braided geometric structure can be deduced by Space group symmetry operations. The internal geometric structure of possible three-dimensional braid can be obtained by translational symmetry operation for the unit cell. In the actual braided process, boundary yarn is continuous. After considering its rules, a new three-dimensional braided geometric structure can be grasped (shown in <xref ref-type="fig" rid="fig4">Figure 4</xref>).</p><p>To get this new three-dimensional woven material, the motion law of braided yarn carriers must be researched.</p><p>Point position shown in <xref ref-type="fig" rid="fig5">Figure 5</xref> is arranged with movably braided yarn carriers, the basic braided yarn array is composed of braided yarn carriers.</p><p>Braided yarn carriers in the same orbit are in a group. There are two groups in total, named as a and b respectively. In the braiding process, the trajectory of yarn carrier in the same orbit does not change. Once all yarn carriers in a group move along the arrow direction, a braiding cycle is finished.</p><p>The axis of each group of yarns in the three-dimensional braid is straight, and only bending at the boundary (<xref ref-type="fig" rid="fig6">Figure 6</xref>).</p><p>Different groups of yarns cross in space eventually form a new three-dimensional braided geometry structure.</p></sec></sec><sec id="s4"><title>5. The Geometric Analysis Model of the New Three-Dimensional Braided Materials</title><p>The new 3D-braided geometric structure is expected for the production of a new three-dimensional braided composite perform, as a new three-dimensional braided material, its performance prediction is an important part of basic research.</p><p>The properties of braided materials can be used in different geometric analysis model. In 1990s, the equivalent theory of 3D braided materials microstructure geometry was an effective solution to the problems in engineering applications. Ko et al. proposed the Fabric Geometric Model(FGM) [<xref ref-type="bibr" rid="scirp.40532-ref15">15</xref>]; Ma et al. proposed the “*”-type model of a representative unit cell [<xref ref-type="bibr" rid="scirp.40532-ref16">16</xref>]; Yang et al. proposed fiber tilt model based on laminate theory [<xref ref-type="bibr" rid="scirp.40532-ref17">17</xref>]; Du et al. gave the division of the unit cell under different assumptions and model structure. After in depth study of mesoscopic geometric structure of the unit cell [17,18]; Wu Delong proposed three-cell model [<xref ref-type="bibr" rid="scirp.40532-ref19">19</xref>]. Based on the geometric structure of the unit cell the analysis model is widely used and to achieve the ideal predicted results on mechanical properties.</p><p>The new three-dimensional braided material is the unit cell deduced according to space group symmetry operation. And the unit cell geometrical analysis model is more reasonable to analyze its performance. Slight difference of unit cell division method with the traditional method: full yarns are used in unit cell boundary in the geometric model of the new fabric; adjacent unit cell consists of full yarns mosaic instead of the traditional yarn center line segmentation (shown in <xref ref-type="fig" rid="fig7">Figure 7</xref>). The advantage of the method of this division is: maintenance of the full symmetry of the unit cell on the premise of non-affect to the geometry described; group representation theory to study the mechanical properties of the material can be used in the follow-up study.</p><sec id="s4_1"><title>5.1. Basic Hypothesis</title><p>1) The cross section of braided yarn in braided materials is rhombus (<xref ref-type="fig" rid="fig8">Figure 8</xref>) and the braided yarn is sufficiently supple.</p><p>The geometric distortion can be generated with the change in load.</p><p>2) Braiding process is stable and braiding geometry is consistent.</p><p>3) Internal unit cells account for the vast majority of the braided materials; as the cross-sectional size increases, the influence of the surface structure should be ignored.</p><p>4) Internal unit cell, the final cross-section of each yarn is extruded as shown in <xref ref-type="fig" rid="fig9">Figure 9</xref> geometry by the lateral loads from different directions. The degree of lateral compression will affect the size of the fiber volume percent.</p><p>In extreme cases, the lateral extrusion of yarn will reach congestion (shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>0), and at this time fiber volume percentage of the 3D braided will reach the highest. But this time, there exists difficulty in substrate penetration, which is not conducive to improving the performance of the material, and thus three-dimensional woven composite fiber volume percentage should have the best range.</p></sec><sec id="s4_2"><title>5.2. Geometry Model of 3D Braided Materials and the Fiber Volume Percentage</title><p>1) Rhombohedron conventional unit cell volume<img src="3-7701077\b85eb527-d7ac-4643-9635-a4a057765456.jpg" />, Cartesian coordinates of the reference to <xref ref-type="fig" rid="fig1">Figure 1</xref>1, set a unit cell side length L, z direction diagonal length 4H (H is unit-cell height along the symmetry axis of the direction), braid angle as <img src="3-7701077\e4169161-38da-42b6-ac4e-f365fda0a30a.jpg" /> (i.e. yarn axis and the Z-axis angle), Rhombohedron conventional unit cell volume calculated as follows:</p><disp-formula id="scirp.40532-formula86092"><label>(1)</label><graphic position="anchor" xlink:href="3-7701077\6220970a-5d66-42f3-aec7-d853cbcc6f53.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.40532-formula86093"><label>(2)</label><graphic position="anchor" xlink:href="3-7701077\a9c43981-3521-4059-82e9-061a2e6ae1fa.jpg"  xlink:type="simple"/></disp-formula><p>2) Yarn factor ε and the cross-sectional area of the reduction factor λ;</p><p>Yarn factor ε reflects the size of the yarn fiber volume percentage. Cross-section reduction factor λ represent yarn geometry deformation on the influence degree of the equivalent cross section by yarn braiding processing.</p><p>Yarn matter factor is defined as:</p><disp-formula id="scirp.40532-formula86094"><label>(3)</label><graphic position="anchor" xlink:href="3-7701077\486c9646-9588-4068-88a9-4b986d517c4b.jpg"  xlink:type="simple"/></disp-formula><p><img src="3-7701077\76f9a960-52ce-4cf8-b0b3-f78c635d75a9.jpg" />represents the radius of the circular knitting section of yarn, and</p><disp-formula id="scirp.40532-formula86095"><label>(4)</label><graphic position="anchor" xlink:href="3-7701077\8216cd5a-2f7b-41ee-beb6-13052bacb8c1.jpg"  xlink:type="simple"/></disp-formula><p>It is determined by the yarn linear density (<img src="3-7701077\2695d845-4241-44a1-a8f3-b3dada17e018.jpg" />= Texy/1000) and the fiber density <img src="3-7701077\919f8a6e-03de-403a-bc92-0dd0c58ec435.jpg" /> (g/cm<sup>3</sup>) [<xref ref-type="bibr" rid="scirp.40532-ref5">5</xref>]</p><p>To untwisted yarn and different twist yarn, the numerical is different. Twistless yarn fiber volume percent maximum is:</p><disp-formula id="scirp.40532-formula86096"><label>(5)</label><graphic position="anchor" xlink:href="3-7701077\89b4bb0f-de9e-471e-a71e-4a4cfa163638.jpg"  xlink:type="simple"/></disp-formula><p>A represents the yarn reduction sectional area, after the geometry changes in braided materials, assume a circular cross section of the yarn in the braiding process only has sliding between the fibers, before and after deformation of the fiber cross-sectional area of the yarn does not change, the percentage remains constant, and a crosssectional view of the yarn is not changed, there is</p><disp-formula id="scirp.40532-formula86097"><label>(6)</label><graphic position="anchor" xlink:href="3-7701077\2b92ce68-0444-4745-aca9-9edf1f966532.jpg"  xlink:type="simple"/></disp-formula><p>A is the two diagonal length of yarn diamond cross section In the Rhombohedral space area, with the matter load increasing and Yarn deformation, the deformation of the gap will eventually be filled up, and at that time the fiber volume percent maximize. Reflected in the yarn crosssection reduction coefficient λ.</p><disp-formula id="scirp.40532-formula86098"><label>(7)</label><graphic position="anchor" xlink:href="3-7701077\fc7ce85f-7a0c-4664-8432-90687f36c6e5.jpg"  xlink:type="simple"/></disp-formula><p>3) Rhombohedral unit cell edge length L and yarns volume in unit cell <img src="3-7701077\a2c6d5db-19e0-4391-97e3-a0ffc66844e9.jpg" /></p><p>From <xref ref-type="fig" rid="fig1">Figure 1</xref>1 the following relation can be deduced,</p><p><img src="3-7701077\1e3f2c91-6b87-43ae-82b2-2e94984dbcd9.jpg" />, &#160;&#160;&#160;&#160;&#160;&#160;<img src="3-7701077\583421e0-e904-46b7-b8c9-95f47f45e1ba.jpg" />,</p><p><img src="3-7701077\e9be8629-649f-4c1c-a219-80979acdcde7.jpg" />,</p><p><img src="3-7701077\1aafda5d-93e0-42bc-8510-17e97197a677.jpg" />,</p><p><img src="3-7701077\0d4c8d9b-59df-4c29-8de5-0ff85c2eaf6e.jpg" /></p><p><img src="3-7701077\9f2b0fe2-6bdb-4673-b57e-95c515e7b6f0.jpg" /></p><disp-formula id="scirp.40532-formula86099"><label>(8)</label><graphic position="anchor" xlink:href="3-7701077\37a43795-6fb9-4ed7-b766-4b31ccf207b8.jpg"  xlink:type="simple"/></disp-formula><p>Rhombohedral unit cell edge length can be assumed as L,</p><disp-formula id="scirp.40532-formula86100"><label>(9)</label><graphic position="anchor" xlink:href="3-7701077\3d758931-8bb7-4308-a3ce-9124b57c99cf.jpg"  xlink:type="simple"/></disp-formula><p>The total volume of the 12 yarn segments in the rhombohedral unit cell can be assumed as<img src="3-7701077\a3a6eafd-3ac3-4080-b8ec-16b2dc4d96fd.jpg" />,</p><disp-formula id="scirp.40532-formula86101"><label>(10)</label><graphic position="anchor" xlink:href="3-7701077\21d7642c-bf44-4ce0-a14e-a2b848ef5c25.jpg"  xlink:type="simple"/></disp-formula><p>Yarn fiber volume percentage can be assumed as<img src="3-7701077\4e6afbd6-340c-43d3-9e00-1bcf2baf38a7.jpg" />, The total volume of the fibers is</p><disp-formula id="scirp.40532-formula86102"><label>(11)</label><graphic position="anchor" xlink:href="3-7701077\5bdf8243-df80-4892-8105-4da84a4e18aa.jpg"  xlink:type="simple"/></disp-formula><p>4) yarn geometric parameters after deformation a, b and <img src="3-7701077\472ba2da-efff-4eb4-a789-b129af8cde4f.jpg" /></p><p>According to previous assumptions: the yarn is supple enough; matter force is sufficient; different braid angle <img src="3-7701077\da8f3ad3-c05e-4e57-b457-a005340d35db.jpg" /> corresponds to the same kind of cross-sectional geometry with different cross-sectional dimension (<xref ref-type="fig" rid="fig1">Figure 1</xref>2).</p><p>Reference to <xref ref-type="fig" rid="fig1">Figure 1</xref>3, the parameters A and B can be derived. <xref ref-type="fig" rid="fig1">Figure 1</xref>3(b) is the cross-section of a rhombohedral unit cell perpendicular to the Z-axis direction, this figure meets the symmetry of point group<img src="3-7701077\c384b1a0-0972-45f8-bd6b-889f4ddf816f.jpg" />.</p><p>The relationship between A and B is derived as follows:</p><disp-formula id="scirp.40532-formula86103"><label>(12)</label><graphic position="anchor" xlink:href="3-7701077\d6c7d34e-ffaf-4c75-998e-86b2bdd596d2.jpg"  xlink:type="simple"/></disp-formula><p>Braiding angle <img src="3-7701077\92dd39a8-a8e2-4c64-a639-3a849eaab063.jpg" /> of braided yarn (<xref ref-type="fig" rid="fig1">Figure 1</xref>3(c)). So</p><disp-formula id="scirp.40532-formula86104"><label>(13)</label><graphic position="anchor" xlink:href="3-7701077\f29dd9d0-7a48-42d4-b3d2-16ba974d2b1b.jpg"  xlink:type="simple"/></disp-formula><p>The relationship of the parameters a and b</p><disp-formula id="scirp.40532-formula86105"><label>(14)</label><graphic position="anchor" xlink:href="3-7701077\4611715b-da03-40dd-a1db-8364477dada7.jpg"  xlink:type="simple"/></disp-formula><p>5) The fiber volume percentage<img src="3-7701077\f5d93b1c-d06c-4d06-baec-10e9b4d2e7d3.jpg" />. It can be expressed as:&#160;&#160;&#160;&#160;&#160;</p><disp-formula id="scirp.40532-formula86106"><label>(15)</label><graphic position="anchor" xlink:href="3-7701077\a20202b0-528c-4554-af9a-dc6c56ca800b.jpg"  xlink:type="simple"/></disp-formula><p><img src="3-7701077\1264b753-7bc5-4646-92f3-a2c2fb070c1a.jpg" />is the maximum of the fiber volume percentage.</p><p>When the circular cross section of the yarn did not change, the volume percent of the fibers is at minimum</p><disp-formula id="scirp.40532-formula86107"><label>(16)</label><graphic position="anchor" xlink:href="3-7701077\c93ae20e-8b4a-4789-ba58-0b3d15a3af91.jpg"  xlink:type="simple"/></disp-formula><p>6) The value of the percent fiber volume<img src="3-7701077\1bce2007-9102-4fa6-941a-b2e5dc867db4.jpg" />:</p><p>The smaller the braid angle is, the more difficult the matter process is to achieve. The braiding process also need to maintain a certain tension, corresponding to the percentage of lower fiber volume, in fact, this situation is difficult to form a dense braid. The greater the braid angle corresponds to a higher percentage of fiber volume. Fiber volume percentage will not achieve unidirectional yarn aggregate value B under limit congestion state, while according to the formula (6 - 10) we can see, the yarn cross-section reduction factor in the limit state A is 0.8. Braid angle take a value close to A, the yarn is difficult to bending deformation and difficult to achieve the congestion state; Decreases with the braid angle, yarn is prone to bending, but difficult to achieve the process of packing, the braided material is only dependent on the yarn tension weaving, the corresponding braided material because of its loose structure, the percentage of fiber volume is low. Increasing the braid angle, the braided material is not only easy to achieve the process of packing , but also easy to achieve a higher percentage of fiber volume. In the same packing force, the percentage of fiber volume increases with the braid angle.</p><p>As shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>4, fiber volume percentage results of the new three-dimensional braided material is derived by the formula (15). If the yarn cross-section reduction factor is not changed, the percentage of fiber volume almost does not change with the braid angle variation. Taking into account the yarn cross-sectional will change during the actual packing process, the curve in the figure is the simulation results with the consideration of the above factors.</p><p>According to the above analysis, this curve is the trend of the fiber volume percentage with the change of braid angle. The shaded area is the range of possible values for the percentage of volume of the composite fiber.</p></sec></sec><sec id="s5"><title>6. Conclusion</title><p>A novel geometry structure of unit cell is deduced from the point group <img src="3-7701077\636a49cb-c787-405d-9125-e5d07c3253c9.jpg" /> corresponding to symmetry operations. By transforming the unit cell with symmetry of space group R3, A new 3D braided geometry structure is obtained. The braided technology corresponding to this geometry structure is studied. 3D braided material fiber volume percentage and its variation tendencies are predicted by means of the established geometric model. Some new 3D braided preforms with a high performance could be obtained by optimizing the geometric parameters which have higher fiber volume percentage than traditional three-dimensional braided material. Prelimi-</p><p>nary studies indicate that its geometry structure is stabler, and that the mechanical properties of corresponding braided material are better than those of the traditional three-dimensional braided material.</p></sec><sec id="s6"><title>REFERENCES</title></sec></body><back><ref-list><title>References</title><ref id="scirp.40532-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">A. P. Mouritz, M. K. Bannister, P. J. Falzon, et al., “Review of Applications for Advanced Three-Dimensional Fibre Textile Composites,” Composites: Part A, Vol. 30, No. 12, 1999, pp. 1445-1461. http://dx.doi.org/10.1016/S1359-835X(99)00034-2</mixed-citation></ref><ref id="scirp.40532-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">X. M. Wang and Y. F. 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