Abstract:
The disclosure provides a multi-dimensional weaving shaping machine of composite materials, including: a guide template including a plurality of cylindrical guiders arranged according to the geometrical shape of a prefabricated member; an electrical control three-dimensional motion mechanism including: a control signal receiving terminal configured to receive motion control signals corresponding to the geometrical shape of the prefabricated member; and a three-dimensional motion output terminal configured to form a motion track according to the motion control signals; a weaving needle being connected with the three-dimensional motion output terminal and making weave fibers distribute among the cylindrical guiders according to the geometrical shape of the prefabricated member. The multi-dimensional weaving shaping machine of composite materials of the disclosure utilizes the cylindrical guiders and the electrical control three-dimensional motion mechanism to make the weaving needle to drive braided cords to distribute among the cylindrical guiders along the motion track to form the guide template. The disclosure is applicable to multi-dimensional weaving shaping of large-scale and complicated materials and capable of improving the interlaminar strength of composite materials. The shaping machine applies a rapid shaping technology to multi-dimensional weaving shaping of composite materials and the technical processes are automatic.

Description:
TECHNICAL FIELD OF THE INVENTION 
       [0001]    The disclosure relates to the technical field of weaving shaping of composite materials, and more particularly to a multi-dimensional weaving shaping machine of composite materials. 
       BACKGROUND OF THE INVENTION 
       [0002]    As part of strategic emerging industries in China, high-strength fibers including carbon fibers, aramid fibers, polyethylene and fiberglass and the composite material products thereof have the advantages of light weight, high strength, corrosion resistance and unique concealment performance etc. Composite materials, which are widely applied in fields including wind energy, aeronautics and astronautics, automobiles, railway communication, buildings, weapons, armors, ships, chemical engineering and sports etc., have been an important fiercely-competitive industry that is developed by countries all over the world as a priority. Composite materials are basic key materials in sophisticated industries including aeronautics and astronautics etc. For example, composite material technology are the most critical technology in the competition between Boeing and Airbus as well as one of the major bottlenecks of civil aircraft projects in China. The composite materials used in Boeing 787 already account for more than 50% of the total mass of the plane. Shells of stealth fighters are basically made of microwave absorbing composite materials. In the meanwhile, composite materials are one of the basic factors for stealth of planes and naval vessels. Although having many excellent performances, the following disadvantages need to be overcome to expand the application of composite materials: 
         [0003]    1. Easy Interlaminar Cracking 
         [0004]    Most existing fiber composite materials are produced by superimposing fiber sheets including fiber cloth and prepregs etc. to a certain thickness and cure the fiber sheets by resin substrates. Thanks to the ultra-high strength fibers on the surfaces in 2 dimensions of the sheets, strength of the sheets are several times stronger than that of steel and may reach above 3000 MPa. However, there are resin plastic substrates among the sheets, and the interlaminar strength are extremely low at just 100 MPa. The difference between the fiber strength in the layers and the plastic strength among the layers is as much as more than 30 times. Therefore, easy interlaminar cracking is an intrinsic disadvantage of fiber composite materials. Because of the weak interlaminar strength, as well as the relatively low impact strength and compressive strength, interlaminar cracking is the main failure of composite materials, especially when impacted and compressed to cause fatigue. 
         [0005]    Methods including interlaminar stitching, three-dimensional spinning and three-dimensional weaving etc. may be applied in order to improve the interlaminar strength of composite materials. Although some achievements have been made in the research and development, these technologies have complicated processes together with very high cost and limited use. Nevertheless, broadly-applied multi-axial warp knitted composite materials fail to obtain three-dimensional structures due to the thickness limitation. So, interlaminar cracking is the major disadvantage that harasses the performance of composite materials. Therefore, it&#39;s been a problem in the world to enhance the interlaminar strength of composite materials at low costs. 
         [0006]    2. Low Lamination Efficiency and High Labor Costs 
         [0007]    Usually, if long staples are required to be used as structural materials, fiber sheets are manufactured by yarns and composite material plates or products are produced by superimposing layers of fiber sheets to a certain thickness. Processes of production of yarns, fabrics, plies/composites are necessary in the application of long staples as materials. However, only the process of fabricating yarns into fabrics can be realized efficiently by spinning techniques in the whole production process of fiber composite material products. Since fiber sheets can be hardly operated automatically and mechanically, expensive automatic fiber orientation devices can be applied only in sophisticated industries that require very high lamination accuracy of fiber sheets, such as aircraft manufacturing. Therefore, fiber sheets are mostly laminated into plates and products manually in the industry of composite materials, which is low in production efficiency and high in labor cost, wherein the low manual lamination efficiency has always been the main bottleneck of the production process of composite materials. 
         [0008]    3. Expensive High-Strength Fibers Including Carbon Fibers, Aramid Fibers and High-Modulus Polyethylene Etc. 
         [0009]    The low interlaminar strength, the low lamination efficiency and the high labor costs of lamination processes of fiber composite materials result in limited application of composite materials and limited demands of high-strength fibers including carbon fibers, aramid fibers and high-modulus polyethylene etc. that are mainly used in high-end products in the market. Along with the technical monopoly of developed countries on carbon fibers, aramid fibers and high-modulus polyethylene, these high-strength fibers are naturally very expensive. The good news is that production problems of carbon fibers and high-modulus polyethylene have been solved in China in recent years to realize localization, and aramid fibers will be produced at home soon. 
         [0010]    If the interlaminar strength of composite materials are improved and composite materials can be laminated automatically at low costs, the application demands of composite materials will increase inevitably, the yields of carbon fibers, aramid fibers and high-modulus polyethylene will be also increased greatly and their manufacturing costs are expected to decrease. 
       SUMMARY OF THE INVENTION 
       [0011]    The objective of the disclosure is to provide a multi-dimensional weaving shaping machine of composite materials to solve the technical problem of the lack of highly-automatic manufacturing devices capable of fabricating high-strength composite materials in the prior art. 
         [0012]    To realize the objective above, the disclosure provides a multi-dimensional weaving shaping machine of composite materials, including: a guide template including a plurality of cylindrical guiders arranged according to the geometrical shape of a prefabricated member; an electrical control three-dimensional motion mechanism located above the guide template, and including: a control signal receiving terminal configured to receive motion control signals corresponding to the geometrical shape of the prefabricated member; and a three-dimensional motion output terminal configured to form a motion track according to the motion control signal; a weaving mechanism including: a weaving needle being connected with the three-dimensional motion output terminal for driving weave fibers to move among the cylindrical guiders along the motion track so that the weave fibers are distributed among the cylindrical guiders according to the geometrical shape of the prefabricated member. 
         [0013]    Further, the guide template includes a weaving plate, on which a plurality of uniformly-distributed first through holes are provided; a perforated plate is set below the weaving plate; a plurality of guide columns of which the heights are adjustable heights are set below the perforated plate; the perforated plate is provided with a plurality of second through holes coaxially corresponding to the first through holes; the guide columns pass through the first through holes and the second through holes; the cylindrical guiders are cylindrical sleeves which are sleeved on the guide columns and provided with optional heights. 
         [0014]    Further, a pneumatic chuck for clamping the weaving needle, the cylindrical guiders and/or the guide columns is set on the three-dimensional motion output terminal. 
         [0015]    Further, each of the guide columns is provided with clamping grooves distributed axially at equal intervals. A moveable adjusting plate is set below the perforated plate. A guide column support plate that is static relative to the perforated plate is set below the moveable adjusting plate. The moveable adjusting plate is capable of sliding relative to the perforated plate. A plurality of elongated and round apertures opposite to the second through holes of the perforated plate are set on the moveable adjusting plate. The guide columns pass through the elongated and round apertures and move in the elongated and round apertures with the movement of the moveable adjusting plate. 
         [0016]    Further, locking members matched with the clamping grooves are set on the moveable adjusting plate. The moveable adjusting plate has a locking position to match the locking members with the clamping grooves so as to lock the heights of the guide columns and an unlocking position to separate the locking members and the clamping grooves. 
         [0017]    Further, the locking member is a leaf spring set at an end of the extension direction of the elongated and round aperture and obliquely extending to the guide column located in the elongated and round aperture. The clamping grooves are formed by the conical portions of the guide column and flanges set on the small-diameter ends of the conical portions. 
         [0018]    Further, a first support framework is set below the moveable adjusting plate. The first support frame is provided with a first support frame located on the periphery of the moveable adjusting plate. A locating plate is set on the first support frame. The side face of the locating plate is provided with an adjusting screw rod extending horizontally. The first end of the adjusting screw rod is fixedly connected with the moveable adjusting plate. 
         [0019]    Further, the bottom surface of the moveable adjusting plate is provided with a shifting yoke. The first end of the adjusting screw rod is fixedly connected with the moveable adjusting plate through the shifting yoke, and the second end of the adjusting screw rod is provided with an adjusting handle. 
         [0020]    Further, a connecting hole configured to connect the first support frame is further set on the locating plate. 
         [0021]    Further, the first support framework includes four first support legs, and the guide column support plate is located between the four first support legs. 
         [0022]    Further, a plurality of locating sleeves coaxially matched with the second through holes are further provided on the perforated plate, and the guide columns pass through the locating sleeves. 
         [0023]    Further, the upper end of the guide column is provided with first annular platform extending outwards along the radial direction. 
         [0024]    Further, the periphery of the cylindrical guider is provided with a plurality of layers of ring grooves for limiting the positions of the weave fibers. 
         [0025]    Further, the upper end of the cylindrical guider is provided with a second annular platform extending outwards along the radial direction. 
         [0026]    Further, the electrical control three-dimensional motion mechanism further includes: an X axis motion unit including an X supporter extending along a first direction; an X axis guide rail set on the X axis supporter; an X axis synchronous belt motion mechanism set along the X axis guide rail and provided with an X axis slider; a Y axis motion unit including: a Y axis supporter connected with the X axis slider and extending along a second direction vertical to the first direction; a Y axis guide rail set on the Y axis supporter; a Y axis synchronous belt motion mechanism set along the Y axis guide rail and provided with a Y axis slider; a Z axis motion unit including: a Z axis supporter extending along a third direction vertical to the plane formed by the first direction and the second direction; a Z axis guide rail set on the Z axis supporter; a Z axis synchronous belt motion mechanism set along the Z axis guide rail and provided with a Z axis slider; the Z axis slider is fixedly connected with the Y axis slider, wherein a three-dimensional motion output terminal is formed at the lower end of the Z axis supporter. 
         [0027]    Further, the X axis supporter includes a first supporter and a second supporter in parallel. The X axis guide rail includes a first guide rail and a second guide rail set on the first supporter and the second supporter, respectively. The X axis synchronous belt motion mechanism is set on the first supporter. The synchronous belt of the X axis synchronous belt motion mechanism is connected with the first end of the Y axis supporter. The X axis slider includes a first slider located on the first guide rail and a second slider located on the second guide trail. The first slider and the second slider are located below the first end and the second end of the Y axis supporter, respectively. 
         [0028]    Further, the multi-dimensional weaving shaping machine of composite materials in the disclosure further includes a cylindrical guider storage shelf located at the first side of the guide template. The cylindrical guider storage shelf includes a guider storage support bracket and a storage plate set on the guider storage support bracket. A plurality of cylindrical guiders with different heights are pre-stored on the storage plate. 
         [0029]    Further, a plurality of uniformly-distributed threaded holes are provided on the storage plate. Storage support rods for supporting the cylindrical guiders are provided in the threaded holes. The lower ends of the storage support rods are provided with external threads matched with the threaded holes. 
         [0030]    Further, the weaving mechanism further includes a fiber yarn feeding and tensioning mechanism located at the second side of the guide template. 
         [0031]    Further, the fiber yarn feeding and tensioning mechanism includes: a third bracket; a fiber roll installation bracket set on a support beam of the third bracket and provided with support rods for supporting fiber rolls; tension pulley base plates set on the support beam of the third bracket. A tension pulley for providing fiber yarns to the weaving needle and a guide pulley are provided on each of the tension pulley base plate. 
         [0032]    Further, the fiber yarn feeding and tensioning mechanism further comprises a weaving needle base for storing the weaving needle and the weaving needle base is located on one side of the tension pulley base plate. 
         [0033]    The Disclosure has the Following Beneficial Effect: 
         [0034]    The multi-dimensional weaving shaping machine of composite materials of the disclosure utilizes the cylindrical guiders and the electrical control three-dimensional motion mechanism to make the weaving needle to drive braided cords to distribute among the cylindrical guiders along the motion track to form the guide template. The machine is applicable to multi-dimensional weaving shaping of large-scale and complicated materials and capable of improving the interlaminar strength of composite materials. The shaping machine applies a rapid shaping technology to multi-dimensional weaving shaping of composite materials and the technical processes are automatic. 
         [0035]    Besides the objectives, characteristics and advantages described above, the disclosure has other objectives, characteristics and advantages. The disclosure will be described in details below with reference to the drawings. 
     
    
     
       BRIEF DESCRIPTION OF THE DRAWINGS 
         [0036]    The accompanying drawings that constitute a part of the application are used for providing further understanding to the disclosure. The exemplary embodiments of the disclosure and the illustrations thereof are used for explaining the disclosure, instead of constituting an improper limitation to the disclosure. In the accompanying drawings: 
           [0037]      FIG. 1  is a schematic diagram illustrating a stereo structure of a multi-dimensional weaving shaping machine of composite materials in a preferred embodiment of the disclosure; 
           [0038]      FIG. 2  is a schematic diagram illustrating a composition structure of a guide template in a preferred embodiment of the disclosure; 
           [0039]      FIG. 3  is a structural diagram illustrating a guider support rod in a preferred embodiment of the disclosure; 
           [0040]      FIG. 4  is a schematic diagram illustrating a surface structure of a cylindrical guider in a preferred embodiment of the disclosure; 
           [0041]      FIG. 5  is a schematic diagram illustrating an adjusting structure of a moveable adjusting plate below a guide template in a preferred embodiment of the disclosure; 
           [0042]      FIG. 6  is a schematic diagram illustrating a position relation between a locking member and a clamping groove during free falling of a guider support rod after weaving; 
           [0043]      FIG. 7  is a schematic diagram illustrating a position relation between a locking member and a clamping groove when a moveable adjusting plate is located in a locking position; 
           [0044]      FIG. 8  is a structural diagram of an electrical control three-dimensional motion mechanism in a preferred embodiment of the disclosure; 
           [0045]      FIG. 9  is a schematic diagram illustrating an enlarged structure of Part II in  FIG. 8 ; 
           [0046]      FIG. 10  is a structural diagram of an X axis motion unit in an embodiment of the disclosure; 
           [0047]      FIG. 11  is a structural diagram illustrating partial enlargement in an A direction in  FIG. 10 ; 
           [0048]      FIG. 12  is a structural diagram of a Y axis motion unit in a preferred embodiment of the disclosure; 
           [0049]      FIG. 13  is a structural diagram in a B direction in  FIG. 12 ; 
           [0050]      FIG. 14  is a structural diagram illustrating partial enlargement of  30   a  in  FIG. 8 ; and 
           [0051]      FIG. 15  is a schematic diagram illustrating partial enlargement of a fiber yarn feeding and tensioning mechanism in a preferred embodiment of the disclosure. 
       
    
    
     DETAILED DESCRIPTION OF THE EMBODIMENTS 
       [0052]    The embodiments of the disclosure will be described below in combination with the accompanying drawings. However, the disclosure can be implemented by many different methods limited and covered by the claims. 
         [0053]    As shown in  FIG. 1 , the disclosure provides a multi-dimensional weaving shaping machine of composite materials, including: a guide template  60 , wherein the guide template  60  includes a plurality of cylindrical guiders  62  arranged according to the geometrical shape of prefabricated member; an electrical control three-dimensional motion mechanism  30  located above the guide template  60 , wherein the electrical control three-dimensional motion mechanism  30  includes: a control signal receiving terminal configured to receive motion control signals; a three-dimensional motion output terminal  30   a  configured to form a motion track according to the motion control signals. The multi-dimensional weaving shaping machine of composite materials of the disclosure further includes: a weaving mechanism  50 . The weaving mechanism  50  includes: a weaving needle  14  connected with the three-dimensional motion output terminal  30   a  and driving weave fibers to distribute among the cylindrical guiders  62  along the motion track. 
         [0054]    As shown in  FIG. 2 , in order to shape the guide template  60 , the guide template  60  includes a weaving plate  60   a . A plurality of uniformly-distributed first through holes are provided on the weaving plate  60   a . The weaving plate  60   a  is supported by a rectangular frame  59 . A perforated plate  65  is set below the weaving plate  60   a . The weaving plate  60   a  is provided with a plurality of second through holes coaxially corresponding to the first through holes. A plurality of guide columns  61  with adjustable heights are set below the perforated plate  65 . The upper ends of the guide columns  61  pass through the first through holes and the second through holes to locate above the weaving plate  60   a . The cylindrical guiders  62  are cylindrical sleeves which are sleeved on the guide columns  61  and provided with optional heights. 
         [0055]    As shown in  FIG. 3 , a guide column  61  is provided with clamping grooves  61   a  distributed axially at equal intervals. The clamping grooves  61   a  may be formed by the conical portions of the guide column  61  and flanges set on the small-diameter ends of the conical portions. The upper end of the guide column  61  are provided with a first annular platform  61   c  extending outwards along the radial direction. The portion below the first annular platform  61   c  may be grabbed by a clamping device to move the guide column  61 . 
         [0056]    As shown in  FIG. 4 , in order to locate the weave fibers to the surfaces of a cylindrical guider  62 , the peripheries of the cylindrical guider  62  are provided with a plurality of layers of ring grooves  62   a  for limiting the positions of the weave fibers. Each ring groove  62   a  is formed by a plurality of flanges extending outwards along the radial direction on the cylindrical guider  62 . In order to grab the cylindrical guider  62  conveniently, the upper end of the cylindrical guider  62  may be provided with a second annular platform  62   c  extending outwards along the radial direction, and the portion below the second annular platform  62   c  may be clamped by a chuck to clamp the cylindrical guider  62 . 
         [0057]    As shown in  FIG. 5 , a moveable adjusting plate  68  is set below the perforated plate  65 . A guide column support plate  64  that is static relative to the perforated plate  65  is set below the moveable adjusting plate  68 . When all the guide columns  61  fall (see  FIG. 2 ), the lower ends of the guide columns  61  are located on the guide column support plate  64 . The moveable adjusting plate  68  is sliding relative to the perforated plate  65 . A plurality of elongated and round apertures  72  (see  FIG. 6 ) opposite to the through holes of the perforated plate  65  are set on the moveable adjusting plate  68 . The guide columns  61  pass through the elongated and round apertures  72  and move in the elongated and round apertures  72  with the movement of the moveable adjusting plate  68 . 
         [0058]    locking members matched with the clamping grooves  61   a  are set on the moveable adjusting plate  68 . The moveable adjusting plate  68  is provided with alocking position to match the locking members with the clamping grooves  61   a  so as to lock the heights of the guide columns  61  and an unlocking position to separate the locking members and the clamping grooves  61   a  so as to continue to adjust the heights of the guide columns  61 . 
         [0059]    A first support framework  58  (see  FIG. 2 ) is set below the moveable adjusting plate  68 . The first support frame  58  is provided with a first support frame  58   a  located on the periphery of the moveable adjusting plate  68 . See  FIG. 5 , a locating plate  63  is set on the first support frame  58   a . Internal threaded holes are set on the locating plate  63 . Adjusting screw rod  69  matched with one of the internal threaded holes are provided in the internal threaded hole. The telescopic end of the adjusting screw rod  69  are fixedly connected with the moveable adjusting plate  65 . 
         [0060]    As shown in  FIG. 6  and  FIG. 7 , the locking member may be a leaf spring  71  set at an end of the extension direction of the elongated and round aperture  72  and obliquely extending to the guide column  61  located in the elongated and round aperture  72 . 
         [0061]    See  FIG. 5 , the bottom surface of the moveable adjusting plate  68  is fixed with a shifting yoke  70 . The first end of the adjusting screw rod  69  are fixedly connected with the shifting yoke  70  and the second end of the adjusting screw rod  69  are provided with adjusting handle  69   a . The adjusting screw rod  69  are rotated by using the adjusting handle  69   a , and the adjusting screw rod  69  stretch in the internal threaded hole of the locating plate  63  to drive the shifting yoke  70  to move to further drive the moveable adjusting plate  68  to move so that the leaf springs  71  is matched with the clamping grooves  61   a  to lock the guide columns  61 . For the time being, the guide columns  61  can be only elevated and cannot be lowered. After weaving a component, the relative linear motion of the adjusting screw rod  69  and the locating plate  63  drives the moveable adjusting plate  68  to move in a straight line so that the guide columns  61  can fall freely onto the guide column support plate  64  instead of being clamped tightly by the leaf springs  71 . 
         [0062]    A plurality of connecting holes  63   a  configured to connect the first support frame  58   a  is further set on the locating plate  63 . 
         [0063]    See  FIG. 2 , the first support framework  58  includes four first support legs  58   c , and the guide column support plate  64  is located between the four first support legs  58   c.    
         [0064]    A plurality of locating sleeves  66  (see  FIG. 2  and  FIG. 5 ) coaxially matched with the second through holes are further provided on the perforated plate  65 , and the guide columns  61  pass through the locating sleeves  66 . 
         [0065]    The layout size or shape of the cylindrical guiders  62  in the guide template  60  may be changed according to the external feature of a pre-woven component. The heights of the guide columns  61  for supporting the cylindrical guiders  62  can be adjusted according to the external feature of the pre-woven component. The perforated plate  65  is fixed on the first support framework  58 . locating sleeves  66  sleeved on the periphery of the guide columns  61  are installed on the perforated plate  65  to improve the rigidity of the guide columns  61 . The moveable adjusting plate  68  is suspended below the perforated plate  65  by a plurality of perforated plate mounting bases  67  (see  FIG. 5 ) fixed with the perforated plate  65 , and may make a linear motion relative to the perforated plate  65 . The leaf springs  71  are matched with the elongated and round apertures  72  on the moveable adjusting plate  68  to clamp or release the guide columns  61 . 
         [0066]    The cylindrical guiders  62  with different heights can be stored on a cylindrical guider storage plate  83  (see  FIG. 1 ). The cylindrical guiders  62  with different heights are selected and sleeved on the matrix of the guide columns  62  according to the external features of the woven component to perform approximate weaving. 
         [0067]    As shown in  FIG. 8 , the electrical control three-dimensional motion mechanism  30  further includes: an X axis motion unit including an X supporter extending along a first direction and an X axis guide rail set on the X axis supporter and an X axis synchronous belt motion mechanism set along the X axis guide rail and provided an X axis slider; a Y axis motion unit including a Y axis supporter  12  connected with the X axis slider and extending along a second direction vertical to the first direction and a Y axis guide rail  11  set on the Y axis supporter  12  and a Y axis synchronous belt motion mechanism set along the Y axis guide rail  11  and provided with a Y axis slider  31 ; a Z axis motion unit including a Z axis supporter  8  extending along a third direction vertical to the plane formed by the first direction and the second direction and a Z axis guide rail  9  set on the Z axis supporter  8  and a Z axis synchronous belt motion mechanism set along the Z axis guide rail  9  and provided with a Z axis slider  33  which is fixedly connected with the Y axis slider  31 , wherein a three-dimensional motion output terminal  30   a  is formed at the lower end of the Z axis supporter  8 . 
         [0068]    In order to improve the support strength of the electrical control three-dimensional motion unit, the X axis supporter may include a first supporter  3  and a second supporter  6  in parallel. The X axis guide rail includes a first guide rail  5  and a second guide rail  7  set on the first supporter  3  and the second supporter  6 , respectively. A first synchronous belt motion mechanism and a second synchronous belt motion mechanism are set on the first guide rail  5  and the second guide rail  7 , respectively. The first synchronous belt motion mechanism and the second synchronous belt motion mechanism are provided with a first slider  17  (see  FIG. 11 ) and a second slider  27  (see  FIG. 9 ), respectively. The two ends of the Y axis supporter  12  are connected with the first slider  17  and the second slider  27 , respectively. 
         [0069]    Actually, motion units that are more multi-dimensional, including a four-axis motion unit or a five-axis motion unit etc. can be also applied so as to realize multi-dimensional weaving of composite materials. 
         [0070]    More specifically, the X axis motion system includes the first guide rail  5  and the second guide rail  7  in parallel. The first guide rail is supported by the first supporter  3  and the second guide rail  7  is supported by the second supporter  6 . There is a predetermined distance between the first supporter  3  and the second supporter  6 . The distance between the first supporter  3  and the second supporter  6  can be determined by the width of the guide template  60  (see  FIG. 1 ). The distance between the first supporter  3  and the second supporter  6  may be set relatively long and the size of the guide template  60  is increased correspondingly to adapt to the space required to weave a large component. The first slider  17  is set on the first guide rail  5 . The second slider  27  is set on the second guide rail  7 . The first supporter  3  and the second supporter  6  are connected by a transverse connecting rod  13  (see  FIG. 8 ). One end of the Y axis supporter  12  can be connected with the first slider  17  by an XY connecting plate  18  (see  FIG. 11 ). The X axis synchronous belt  21  in the X axis synchronous belt mechanism is connected to the other end of the Y axis supporter  12  by an X axis synchronous belt fixing plate  26 . 
         [0071]    As shown in  FIG. 10 , an X axis driving synchronous belt wheel  22  is connected with an X axis decelerator  24  fixed on the first supporter  3  by a rolling bearing. An X driven synchronous belt wheel  19  is installed on an X axis driven wheel spindle  50  by a bearing and a retainer ring at the end of the bearing. The X axis driven wheel spindle  50  is tightened on the first supporter  3  by threads. The X axis motion unit takes an X axis motor  25  and the X axis decelerator  24  as the power units drives the X axis driving synchronous belt wheel  22  to function as a drive unit by the X axis motor  25  so as to drive the first slider  17  and the second slider  27  to move on the first guide rail  5  and the second guide rail  7 . 
         [0072]    As shown in  FIG. 12 , the Z axis motion unit includes the Z axis guide rail  9 . The Z axis guide rail  9  is supported by the Z axis supporter  8 . The Z axis slider  33  is set on the Z axis guide rail  9 . The Z axis slider  33  is connected with the Y axis slider  31  by a YZ orthogonal connecting plate  10 . A Y axis synchronous belt joint pressing plate  38  in the Y axis synchronous belt mechanism presses the Y axis synchronous belt  32  on a Y axis synchronous belt fixing plate  39  and is fixed on the YZ orthogonal connecting plate  10 . A Y axis driving synchronous belt wheel  35  is connected with a Y axis decelerator  36  on the Y axis supporter  12  by a rolling bearing. A Y axis driven synchronous belt wheel  29  is installed on a Y axis driven wheel spindle  49  by a bearing and a retainer ring at the end of the bearing. The Y axis driven wheel spindle  49  is secured on the Y axis supporter  12  (see  FIG. 9 ). The Y axis motion system takes a Y motor  37  and the Y axis decelerator  36  as the power units, and takes the Y axis motor  37  and the Y axis driving synchronous belt wheel  35  as the drive units so as to drive the Y axis slider  31  to move on the Y axis guide rail  11 . 
         [0073]    As shown in  FIG. 13 , a Z axis driving synchronous belt wheel base  42  is fixed on the orthogonal connecting plate  10 . A Z axis driving synchronous belt wheel  47  is connected with a Z axis decelerator  40  fixed on the Z axis driving synchronous belt wheel base  42  by a rolling bearing. The direction of Z axis driving synchronous belt wheel  47  is changed by a synchronous belt pulley  45 . The synchronous belt pulley  45  is installed on a synchronous belt pulley shaft  48  by a bearing and a retainer ring at the end of the bearing. The synchronous belt pulley shaft  48  is secured on the Z axis driving synchronous belt wheel base  42  by threads. 
         [0074]    See  FIG. 1 , the multi-dimensional weaving shaping machine of composite materials of the disclosure further includes: a cylindrical guider storage shelf  80  located at the first side of the guide template  60 . The cylindrical guider storage shelf  80  includes a guider storage support bracket  81  and a storage plate  83  set on the guider storage support bracket  81 . A plurality of cylindrical guiders  62  with different heights are pre-stored on the storage plate  83 . 
         [0075]    A plurality of uniformly-distributed threaded holes are provided on the storage plate  83 . Storage support rods (not shown in the figure) for supporting the cylindrical guiders  62  are provided in the threaded holes. The lower ends of the storage support rods are provided with external threads matched with the threaded holes. 
         [0076]    As shown in  FIG. 14 , a pneumatic chuck  15  for clamping the weaving needle and the cylindrical guiders  62  pre-stored on the storage plate  83  is set on the three-dimensional motion output terminal  30   a . The pneumatic chuck  15  may apply an existing standard component. 
         [0077]    See  FIG. 1 , a weaving mechanism  50  of the multi-dimensional weaving shaping machine of composite materials of the disclosure further includes a fiber yarn feeding and tensioning mechanism located at the second side of the guide template  60 . 
         [0078]    As shown in  FIG. 15 , the fiber yarn feeding and tensioning mechanism includes: a third bracket  57 ; a fiber roll installation bracket  56  set on a support beam  57   a  of the third bracket  57  and provided with support rods for supporting fiber rolls  55 ; tension pulley base plates  52  set on a support beam  57   a  and located on the top of the ramp of the fiber roll installation bracket  56 . A tension pulley  53  for providing fiber yarns to the weaving needle and a guide pulley  54  are provided on each of the tension pulley base plates. The fiber roll installation bracket  56  is installed on the support beam  57   a  by bolts. The fiber rolls  55  are placed transversely on the fiber roll installation bracket  56 . The tension pulley base plates  52  and a weaving needle base  51  are installed on another support beam  57   a  by bolts. The tension pulley  53  and the guide pulley  54  are installed on each of the tension pulley base plates  52 . After being guided by the guide pulley  54 , the fiber yarns of the fiber roll  55  are tensioned by the tension pulley  53  and carried by the weaving needle  14  (see  FIG. 1 ) to be woven. 
         [0079]    The above are only the preferred embodiments of the disclosure and not intended to limit the disclosure. For those skilled in the art, the disclosure may have various modifications and changes. Any modifications, equivalent replacements and improvements etc. made within the spirit and principle of the disclosure shall be included in the protection scope of the disclosure.