JP5994737B2 - INTERMEDIATE SUBSTRATE FOR PRESS MOLDING, PREFORM, AND METHOD FOR PRODUCING MOLDED ARTICLE - Google Patents

Description

  The present invention relates to an intermediate substrate for press molding composed of discontinuous reinforcing fibers and a thermoplastic resin. More specifically, the present invention relates to an intermediate group in which two components containing reinforcing fibers having specific aspect ratios in different proportions are laminated to each other. The present invention relates to a material, a preform obtained by laminating the same, and a method for producing a molded product obtained by press molding these.

In recent years, development of materials and molding techniques has been promoted in various industries in order to realize a low environmental burden society by reducing CO ₂ emissions and the like. In the transportation sector in particular, the adoption of materials with excellent weight reduction performance has been expanding as a technology that reduces the environment, and the most famous example is the application of fiber reinforced composite materials (FRP) to aircraft. This FRP is excellent in specific strength and specific rigidity. Among them, a carbon fiber composite material (CFRP) having excellent performance is being adopted in earnest as an ultralight structural material in the aircraft industry. In recent years, weight reduction has been regarded as important in the automobile industry, and development of CFRP for automobile parts has been activated.

  As examples of application of CFRP to automobiles, members made of prepreg, resin transfer molding (RTM), and filament winding (FW) using thermosetting resins that have a proven record in aircraft and sports materials are on the market. On the other hand, a remarkable growth is CFRP using a thermoplastic resin, which can be mass-produced by high-speed molding and is excellent in recyclability, and thus has attracted attention as an automobile material for mass-produced vehicles. Among them, press molding is highly productive and can be applied to complex shapes and large-area molding, and therefore, there is an increasing expectation as an alternative to metal molding.

  A sheet-like material using discontinuous reinforcing fibers is mainly used as an intermediate substrate for molding used in press molding. Typical examples include a sheet molding compound (SMC) and a glass mat thermoplastic (GMT) (Patent Documents 1 and 2). Any of the intermediate substrates is used for so-called flow stamping molding in which the material flows and fills in the mold cavity, and relatively long reinforcing fibers are chopped strands and / or swirls into the thermoplastic resin. Takes a distributed form. The intermediate base material exhibits excellent formability due to its high fluidity, but on the other hand, the localization and orientation of fibers are likely to occur, the mechanical properties in the molded product are not stable, and the reliability is low. There was a problem. In addition, the end of the fiber bundle is often a weak point, and the fiber reinforcing effect cannot be fully utilized.

  Patent Document 3 proposes a stampable sheet in which a continuous reinforcing fiber layer and a discontinuous short fiber layer are laminated at a specific ratio. According to the intermediate substrate, only the discontinuous fiber layer flows out in press molding, and the fibers are localized in the molded product. Therefore, although an excellent reinforcing effect is exhibited in a portion where continuous fibers are present, the reinforcing effect in other portions is reduced, and there is a problem that a large gap is generated in the characteristics when viewed as a molded product as a whole.

  On the other hand, Patent Document 4 proposes an intermediate base material in which discontinuous reinforcing fibers having a specific fiber length distribution are dispersed in a single fiber shape and impregnated with a thermoplastic resin. According to the intermediate base material, the reinforcing effect of the fibers can be fully utilized, and a highly reliable molded product can be obtained. However, there is a case where the fluidity is insufficient due to the large interference between the fibers and the formability is lowered. is there. For this reason, generally, an intermediate base material having an area close to the mold cavity is arranged and molding is performed. In this case, the shape that can be molded is greatly limited, or high pressure is required for molding. Further, there are cases where post-processing such as reduction in molding yield due to generation of burrs (non-product parts) or trim processing is required.

  In other words, the above-described known technology has not yet developed a technology that satisfies both the formability in press molding, the reliability of the molded product, and the reinforcing effect, and the development of an intermediate substrate that satisfies these requirements is craving. Has been.

JP 2000-141502 A JP 1003-80519 A JP-A-6-47737 Japanese Patent No. 4862913

  Accordingly, the present invention solves the technical problems described above and improves the formability in press molding, while satisfying the reliability and reinforcing effect in the molded product, and the intermediate base for press molding, and the intermediate base An object of the present invention is to provide a method for producing a molded article using a material and a preform.

In order to solve the above problems, the present invention adopts the following configuration.
(1) An intermediate base material in which discontinuous reinforcing fibers are monofilamentally and randomly distributed in a thermoplastic resin, and the following components (I) and (II) are laminated to each other, and the configuration in the intermediate base material The ratio of the component (II) to the total amount of the elements (I) and (II) is 30 to 70% by volume, and the aspect ratio of the reinforcing fiber in each of the following components (I) and (II) is 250 or more and 1000 An intermediate substrate for press molding, wherein VfI and VfII below satisfy 0.8VfI> VfII.
(I) Fiber reinforced thermoplastic resin sheet having a reinforcing fiber ratio VfI of 15% by volume to 40% by volume (II) Fiber reinforced thermoplastic resin having a reinforcing fiber ratio VfII of 5% by volume to less than 15% by volume Resin sheet-like material (2) The ratio of component (II) to the total amount of components (I) and (II) in the intermediate substrate is 40 to 60% by volume, for press molding according to (1) above Intermediate substrate.
(3) The intermediate substrate for press molding according to (1) or (2), wherein an average aspect ratio of the discontinuous reinforcing fibers constituting the constituent elements (I) and (II) is 400 or more and 800 or less.
(4) The intermediate substrate for press molding according to any one of (1) to (3), wherein a proportion VfI of reinforcing fibers of the component (I) is 20% by volume or more and 30% by volume or less.
(5) The intermediate substrate for press molding according to any one of (1) to (4), wherein a ratio Vf of reinforcing fibers in the intermediate substrate for press molding is 10% by volume or more and 30% by volume or less.
(6) The intermediate substrate for press molding according to any one of (1) to (5), wherein the reinforcing fibers constituting the constituent elements (I) and (II) are carbon fibers.
(7) The thermoplastic resin constituting the constituent elements (I) and (II) comprises at least one selected from the group consisting of polyolefin, polyamide, polyarylene sulfide and polyetheretherketone, (1) The intermediate substrate for press molding according to any one of to (6).
(8) A press-molding preform in which a plurality of the press-molding intermediate base materials according to any one of (1) to (7) are laminated.
(9) Molding, in which the intermediate substrate or preform for press molding according to any one of (1) to (8) is placed in a mold cavity at a charge rate of 50% or more and less than 100% and then press-molded. Product manufacturing method.
(10) The method for producing a molded article according to (9), wherein the press molding means is stamping molding or heat and cool molding.
(11) The method for producing a molded product according to (9) or (10), wherein the molded product is used as an automobile interior / exterior, a housing for electric / electronic devices, a bicycle, an aircraft interior material, or a transport box. .

  The intermediate substrate of the present invention is particularly suitable as an automobile member because it can exhibit satisfactory reliability and reinforcing effect in a molded product using the same while exhibiting excellent formability in press molding. It is. Furthermore, according to the method for producing a molded article of the present invention, such a molded article can be produced with satisfactory formability to a satisfactory degree.

The schematic diagram which shows an example of the dispersion | distribution state of the reinforced fiber in the fiber reinforced thermoplastic resin sheet-like material used by this invention. The perspective view which shows an example of embodiment in the intermediate substrate for press molding of this invention. The perspective view which shows an example of the engagement form in the intermediate base material for press molding of this invention. The perspective view which shows an example of the engagement form in the intermediate base material for press molding of this invention. The perspective view which shows an example of the engagement form in the intermediate base material for press molding of this invention. The perspective view which shows an example of the laminated structure in the intermediate base material for press molding of this invention. The perspective view which shows an example of the laminated structure in the intermediate base material for press molding of this invention. The perspective view which shows an example of the laminated structure in the intermediate base material for press molding of this invention. The perspective view which shows an example of the laminated structure in the intermediate base material for press molding of this invention. The perspective view which shows an example of the laminated structure in the intermediate base material for press molding of this invention. The schematic diagram of the molded article obtained by the Example and comparative example of this invention. The schematic diagram which shows the cutting-out method of the bending test piece used by the Example and comparative example of this invention.

  The intermediate substrate of the present invention is an intermediate substrate in which discontinuous reinforcing fibers are monofilamentally and randomly distributed in a thermoplastic resin, and the following components (I) and (II) are laminated to each other, The ratio of the component (II) to the total amount of the components (I) and (II) in the intermediate substrate is 30 to 70% by volume, and the aspect ratio of the reinforcing fiber in each of the components (I) and (II) Is 250 or more and 1000 or less, and the following VfI and VfII satisfy 0.8VfI> VfII. Here, the component (I) is a fiber-reinforced thermoplastic resin sheet (hereinafter also referred to as a CFRTP sheet) having a reinforcing fiber ratio VfI of 15% by volume to 40% by volume. II) is a fiber-reinforced thermoplastic resin sheet having a reinforcing fiber ratio VfII of 5% by volume or more and less than 15% by volume.

  Hereinafter, the structure of the intermediate base material of the present invention will be described in detail.

  The intermediate base material of the present invention comprises the CFRTP sheet-like material shown in the components (I) and (II). Here, the sheet-like object is a planar body having a uniform thickness in the plane direction, and examples thereof include a roll shape continuous in the longitudinal direction and a finite-length board shape cut to a predetermined length. Although there is no restriction | limiting in particular in the thickness of an intermediate base material, From the viewpoint of the lamination | stacking cost at the time of setting it as an intermediate base material, handling property, and a preheating efficiency, it is preferable that the thickness is the range of 0.1 mm or more and less than 5.0 mm.

  The CFRTP sheet used in the present invention comprises discontinuous reinforcing fibers dispersed in a monofilament form. Here, the term “dispersed in a monofilament shape” means a ratio of single fibers having a two-dimensional contact angle of 1 degree or more with respect to reinforcing fibers arbitrarily selected in the constituent elements (hereinafter also referred to as fiber dispersion ratio). Is 80% or more, in other words, in the constituent elements, two or more single fibers are in contact with each other and the bundle in parallel is less than 20%. The two-dimensional contact angle is an angle formed by a single fiber of discontinuous reinforcing fibers and a single fiber that comes into contact with the single fiber. It is defined as the angle on the acute angle side that is less than or equal to degrees. This two-dimensional contact angle will be further described with reference to the drawings. 1 (a) and 1 (b) are schematic diagrams showing an embodiment of the present invention, in which discontinuous reinforcing fibers of a CFRTP sheet are observed from a surface direction (a) and a thickness direction (b). . When the single fiber 1 is used as a reference, the single fiber 1 is observed to intersect with the single fibers 2 to 8 in FIG. 1A, but the single fiber 1 is in contact with the single fibers 6 to 8 in FIG. Not. In this case, with respect to the single fiber 1 serving as a reference, the evaluation targets of the two-dimensional contact angle are the single fibers 2 to 5, and of the two angles formed by the two single fibers in contact, 0 degree or more and 90 degrees The following angle 9 is the acute angle side.

  Since the reinforcing fibers are dispersed in a monofilament shape, stress concentration generated at the fiber ends and defects caused thereby are minimized, so that stable strength is exhibited and the reinforcing effect is excellent. Therefore, the obtained molded product shows high reliability and light weight. When the fiber dispersion ratio is less than 80%, the mechanical properties of the molded product are lowered due to stress concentration and defects generated at the end of the contained fiber bundle, and sufficient reliability and light weight of the molded product cannot be obtained. The fiber dispersion rate is preferably 90% or more, more preferably as it approaches 100%.

  Although there is no restriction | limiting in particular as a method of measuring a two-dimensional contact angle from a CFRTP sheet material, For example, the method of observing the orientation of a reinforced fiber from the surface of a component can be illustrated. In this case, it is preferable to expose the fibers by polishing the surface of the constituent elements because the reinforcing fibers can be more easily observed. Moreover, the method of observing the orientation of the reinforcing fiber using transmitted light can be exemplified. In this case, it is preferable to slice the component thinly because the reinforcing fibers can be more easily observed. Furthermore, a method of photographing the orientation image of the reinforcing fiber by observing the constituent elements by X-ray CT transmission can be exemplified. In the case of reinforcing fibers with high X-ray permeability, it is easier to observe reinforcing fibers by mixing tracer fibers with reinforcing fibers or applying tracer chemicals to reinforcing fibers. preferable. Moreover, when measurement is difficult by the above method, a method of observing the orientation of the reinforcing fibers after removing the resin so as not to destroy the structure of the reinforcing fibers can be exemplified. For example, an intermediate substrate or CFRTP sheet is wrapped with aluminum foil, or sandwiched between metal meshes to burn away the thermoplastic resin component, and the resulting substrate made of reinforcing fibers is observed with an optical microscope or an electron microscope. Can be measured.

  In the present invention, the fiber dispersion rate is measured by the following procedure. Two-dimensional contact angles with all single fibers (single fibers 2 to 5 in FIG. 1) in contact with randomly selected single fibers (single fiber 1 in FIG. 1) are measured. This is performed for 100 single fibers, and the ratio is calculated from the ratio between the total number of all single fibers whose two-dimensional contact angle is measured and the number of single fibers whose two-dimensional contact angle is 1 degree or more.

  Further, in the CFRTP sheet material used in the present invention, the reinforcing fibers are randomly distributed. Here, the fact that the reinforcing fibers are randomly distributed means that the average value of the two-dimensional orientation angles of the reinforcing fibers arbitrarily selected in the constituent elements is 30 to 60 degrees. The two-dimensional orientation angle is an angle formed by a single fiber of a reinforcing fiber and a single fiber intersecting with the single fiber, and the angle formed by the intersecting single fibers is 0 degree or more and 90 degrees or less. It is defined as the angle on the acute angle side. This two-dimensional orientation angle will be further described with reference to the drawings. 1A and 1B, when the single fiber 1 is used as a reference, the single fiber 1 intersects with the other single fibers 2-8. Crossing here means a state in which a single fiber as a reference is observed crossing another single fiber in a two-dimensional plane to be observed, and the single fiber 1 and the single fibers 2 to 8 are not necessarily in contact with each other. It is not necessary to be present, and it is no exception for the state observed when they are projected. That is, when viewed with respect to the reference single fiber 1, all of the single fibers 2 to 8 are the evaluation targets of the two-dimensional orientation angle, and in FIG. Among the two angles to be formed, the angle 9 is an acute angle side of 0 degree or more and 90 degrees or less.

  Since the reinforcing fibers are distributed randomly, it is possible to give isotropic properties to the mechanical properties of the molded product, and in addition, there is no need to consider the directionality in handling the intermediate substrate. This will reduce man-hours and human error. On the other hand, if the average value of the two-dimensional orientation angle of the reinforcing fiber is less than 30 degrees or exceeds 60 degrees, the mechanical properties and physical properties of the resulting molded product will cause unevenness and anisotropy. Damaged. Moreover, it causes distortion and warpage of the molded product, leading to cost increase and yield reduction due to subsequent processing and defective products. The average value of the two-dimensional orientation angle of the reinforcing fibers is preferably 40 to 50 degrees, more preferably closer to 45 degrees which is an ideal angle.

  The method for measuring the two-dimensional orientation angle from the component is not particularly limited. For example, a method for observing the orientation of the reinforcing fiber from the surface of the component can be exemplified, and the method for measuring the two-dimensional contact angle is the same as described above. Can take the means.

  In the present invention, the average value of the two-dimensional orientation angle is measured by the following procedure. The average value of the two-dimensional orientation angles with all the single fibers (single fibers 2 to 8 in FIG. 1) intersecting the randomly selected single fibers (single fiber 1 in FIG. 1) is measured. For example, when there are many other single fibers that cross a certain single fiber, an average value obtained by randomly selecting and measuring 20 other single fibers that intersect may be used instead. The measurement is repeated a total of 5 times based on another single fiber, and the average value is calculated as the average value of the two-dimensional orientation angle.

  In the CFRTP sheet material used in the present invention, the aspect ratio p of the reinforcing fibers contained therein is 250 or more and 1000 or less. Here, the aspect ratio p of the reinforcing fiber is a value (Ln / D) obtained by dividing the average fiber length Ln of the reinforcing fiber by the fiber diameter D. By setting the aspect ratio of the reinforcing fiber within the above range, the excellent mechanical properties of the reinforcing fiber, particularly the strength, can be efficiently reflected in the molded product, and a molded product with a high reinforcing effect and light weight is manufactured. be able to. When the aspect ratio is less than 250, the reinforcing efficiency of the reinforcing fibers decreases. When the aspect ratio is larger than 1000, the interference of the reinforcing fibers becomes strong, and the formability of the intermediate substrate is impaired.

  The aspect ratio of the reinforcing fiber is preferably 400 or more and 800 or less, and the reinforcing effect and the shapeability in the intermediate substrate can be balanced.

  Here, a method for evaluating each parameter necessary for deriving the aspect ratio described above will be described.

  The average fiber length Ln of the reinforcing fibers is obtained by heating the CFRTP sheet material in air at 500 ° C. for 30 minutes, randomly selecting 400 fibers from the remaining reinforcing fibers, and using an optical microscope up to a length of 10 μm. The number average is used as the average fiber length Ln.

  In addition, the fiber diameter D of the reinforcing fiber is used for catalogs and the like that are already known, and for unknown ones, a cross section roughly cut out from the CFRTP sheet is used for a section cut with a scanning electron microscope (SEM). The cross section of the ten reinforcing fibers can be observed in a substantially vertical direction at a magnification of 3000 times, and the average value of the fiber diameters measured from the images can be used as the fiber diameter D of the reinforcing fibers.

  In the CFRTP sheet-like material shown in the constituent elements (I) and (II) in the present invention, the ratio of the reinforcing fibers contained therein needs to be selected within a specific range. Here, the ratio of reinforcing fibers refers to the volume content of reinforcing fibers contained in the CFRTP sheet.

  Hereafter, the detail of component (I) and (II) of this invention is demonstrated in order.

  The component (I) of the present invention is a CFRTP sheet-like material having a reinforcing fiber ratio VfI of 15% by volume or more and 40% by volume or less from the viewpoint of ensuring the reliability and mechanical properties of the molded product. By setting VfI in the above range, a strong reinforcing fiber network structure is formed in the CFRTP sheet material, and exhibits excellent mechanical properties, and at the same time, gives a molded product with little anisotropy and variation.

  Here, VfI is more preferably 20% by volume or more and 30% by volume or less, and when used as an intermediate substrate, the balance between formability and mechanical properties is excellent.

  On the other hand, the component (II) in the present invention is a CFRTP sheet-like material having a reinforcing fiber ratio VfII of 5% by volume or more and less than 15% by volume from the viewpoint of enhancing the formability in press molding. A CFRTP sheet having a VfII in the above range exhibits excellent fluidity and functions as a lubricating layer in the intermediate substrate.

  Here, VfII is more preferably 8% by volume or more and 13% by volume or less, and when used as an intermediate substrate, the balance between formability and mechanical properties is excellent.

As a method for evaluating the volume content of the reinforcing fiber, after measuring the mass W0 of the component, the component is heated in air at 500 ° C. for 30 minutes, and the mass W1 of the remaining reinforcing fiber is measured. The value derived by can be used.
-Ratio of reinforcing fiber (volume%) = (W1 / ρf) / {W1 / ρf + (W0−W1) / ρr} × 100.

In the formula, ρf is the density (g / cm ³ ) of the reinforcing fiber, and ρr is the density (g / cm ³ ) of the thermoplastic resin.

  In the intermediate base material shown in the present invention, the CFRTP sheet-like material shown in the constituent elements (I) and (II) described above needs to satisfy the following requirements.

  First, the ratio of the reinforcing fibers contained in the CFRTP sheet material shown in the constituent elements (I) and (II) is 0.8VfI> VfII. When the ratio of the reinforcing fibers of the CFRTP sheet material satisfies the above relationship, the function of the component (II) as the lubricating layer of the CFRTP sheet material can be effectively reflected in the intermediate substrate, and the formability It leads to improvement. If VfII is 0.8 VfI or more, the difference from VfI is too small, so that satisfactory effect of improving shapeability by including the CFRTP sheet-like material of component (II) cannot be obtained. The lower limit of VfII is not particularly limited as long as it is in the range of 5% by volume or more and less than 15% by volume, but from the viewpoint of enhancing the effect of improving the formability of the component (II) by the CFRTP sheet, VfII is preferably 0.6 times or less, more preferably 0.5 times or less of VfII.

  Moreover, the ratio of component (II) contained in an intermediate base material is 30-70 volume% with respect to the total amount of component (I) and (II). When the proportion of reinforcing fibers is 0.8 VfI> VfII and the proportion of component (II) is 30 to 70% by volume, component (II) effectively functions as a lubricating layer of component (I). In addition, the intermediate substrate exhibits excellent formability, and gives a highly reliable molded product with excellent mechanical properties and uniformity. When the proportion of the constituent element (II) is less than 30% by volume, the function as a lubricating layer is hardly exhibited, and the formability of the intermediate substrate is insufficient. When it is larger than 70% by volume, the component (I) cannot follow the flow of the component (II), and only the component (II) flows, so that the orientation and localization of the reinforcing fibers occur, and the molded product Reliability is impaired. The proportion of component (II) contained in the intermediate substrate is preferably 40 to 60% by volume with respect to the total amount of components (I) and (II).

  The formability index can be evaluated by various measurement methods. For example, a method based on an elongation rate calculated from an area expansion rate when the intermediate base material is press-molded can be exemplified. The elongation ratio R is measured by preparing a preform by laminating an intermediate base material cut into a disk shape having a diameter of 150 mm to a thickness of 3 mm, and forming the preform at a molding temperature (melting point or softening point of the intermediate base material + 30 ° C.). Is subjected to press molding at a mold temperature of 120 ° C. with a molding pressure of 15 MPa. The elongation ratio R is obtained from the ratio of the projected area calculated from the diameter of the obtained molded product and the projected area calculated from the diameter of the preform before molding, and the superiority or inferiority of the fluidity is determined based on the size.

The ratio VII of the CFRTP sheet material of component (II) to the total amount of components (I) and (II) in the intermediate substrate described above is the thickness of the CFRTP sheet material shown in components (I) and (II). The ratio can be obtained. FIG. 2 is a perspective view showing an embodiment of the intermediate substrate of the present invention. The intermediate base material 10 in FIG. 2 is formed by alternately laminating nI sheets of the CFRTP sheet material 11 of the component (I) having the thickness t1 and nII sheets of the CFRTP sheet material 12 of the component (II) having the thickness t2. ing. In this case, the ratio VII (volume%) of the CFRTP sheet material of the component (II) can be obtained by the following equation.
VII = (tII × nII) / (tI × nI + tII × nII) × 100.

  The range of application of the above formula is not limited to the intermediate substrate shown in FIG. 2, and it is no exception even if the laminated structure of the intermediate substrate is different. Here, the ratio VI (volume%) of the CFRTP sheet material of the component (I) is a value obtained by subtracting VII from 100 volume%.

  The intermediate base material of the present invention is obtained by laminating the fiber reinforced thermoplastic resin sheet materials of the constituent elements (I) and (II). The laminated form is not particularly limited as long as the intermediate substrate can be carried, and the respective CFRTP sheet-like materials may be substantially independent or engaged with each other. However, the latter form is preferable from the viewpoint of handleability.

  As for the engagement form of the CFRTP sheet material, each CFRTP sheet material may be engaged over the entire surface in the adjacent surface direction, or may be locally engaged. It can be engaged by a welding means such as a double belt press, a hot plate welder, a dielectric heat welder, an ultrasonic welder, a vibration welder, or a physical joining means such as a needle punch or tufting.

  The engagement form of the CFRTP sheet will be further described with reference to the drawings. 3, 4 and 5 are perspective views showing an embodiment of the intermediate substrate of the present invention. 3, 4, and 5, the intermediate base materials 16, 19, and 22 are the CFRTP sheet-like material 13 of the component (I) and the CFRTP sheet-like material 14 of the component (II) through the engagement portion 15. Stacked and integrated. 3 shows that the CFRTP sheet 13 of the component (I) and the CFRTP sheet 14 of the component (II) are engaged over the entire adjacent surface. In FIG. 4, the CFRTP of the component (I) The sheet-like material 17 and the CFRTP sheet-like material 18 of the component (II) are locally engaged over the entire adjacent surface, and in FIG. 5, the CFRTP sheet-like material 20 and the component of the component (I) are shown. The CFRTP sheet material (II) is locally engaged only at the end of the adjacent surface.

  Next, the laminated structure in the intermediate base material of the present invention will be described. 6 to 10 are perspective views of one embodiment of the intermediate substrate of the present invention. In the intermediate base materials 23 to 27, one CFRTP sheet 28 corresponding to the component (I) has a thickness t1, and one CFRTP sheet 29 corresponding to the component (II) has a thickness t2. The CFRTP sheet 29 of element (II) is contained in a proportion of 50% by volume of VII.

  FIG. 6 shows a configuration in which CFRTP sheets 28 and 29 of components (I) and (II) are alternately stacked, FIGS. 7 and 8 show a sandwich stack configuration, FIG. 9 shows an asymmetric stack configuration, and FIG. Is a symmetrically stacked configuration. The laminated structures shown in FIGS. 6 to 10 are only a part of examples, and are not limited to these, and can be appropriately designed according to the specifications of the CFRTP sheet material to be used and the molded product to be acquired.

  Among these, from the viewpoint of reliability in the molded product, alternating lamination and / or multilayer lamination is preferable, and from the viewpoint of suppressing warpage and distortion of the molded product, symmetrical lamination is preferable. Particularly preferred is a laminated structure of a combination of both.

  The intermediate base material of the present invention preferably has a reinforcing fiber ratio Vf in the range of 15% to 20% by volume.

Here, the ratio Vf of reinforcing fibers in the intermediate base material represents the ratio of reinforcing fibers in the entire intermediate base material, and the reinforcement in the CFRTP sheet material shown in the constituent elements (I) and (II) constituting the intermediate base material. From the fiber ratios VfI and VfII and the ratios VI and VII of each component in the intermediate substrate, the following formula can be used.
Vf = (VfI × VI) + (VfII × VII).

  By setting the ratio Vf of the reinforcing fibers within such a range, in addition to the excellent formability in press molding and the reliability in the molded product, the mechanical properties of the molded product can be expressed in a balanced manner.

  As a method for producing the CFRTP sheet-like material shown in the components (I) and (II) described above, for example, there is a method for producing a reinforcing fiber mat in which reinforcing fibers dispersed in a monofilament form in advance are randomly distributed. The reinforcing fiber mat can be produced by a dry process such as an airlaid method in which reinforcing fibers are dispersed into a sheet of air with an air stream or a carding method in which reinforcing fibers are formed by mechanically scraping the reinforcing fibers. A wet process based on the radrite method in which paper is made by stirring in water can be cited as a known technique. As a means for improving the dispersibility and random orientation of the reinforcing fibers in the above, in the dry process, a method of providing a fiber opening bar, a method of further vibrating the fiber opening bar, a method of further finely forming the card eye, Examples include a method of adjusting the rotation speed. In the wet process, there are a method of adjusting the stirring condition of the reinforcing fiber, a method of diluting the reinforcing fiber concentration of the dispersion, a method of adjusting the viscosity of the dispersion, and a method of suppressing the vortex when the dispersion is transferred. It can be illustrated. It is particularly preferable to manufacture by a wet method, and the weight per unit area of the resulting reinforcing fiber mat can be increased by increasing the concentration of input fibers. Furthermore, the weight per unit area can also be adjusted by adjusting the flow rate (flow rate) of the dispersion and the speed of the mesh conveyor. For example, it is possible to increase the weight per unit area of the reinforcing fiber mat obtained by increasing the flow rate of the dispersion liquid while keeping the speed of the mesh conveyor constant. Conversely, the weight per unit area of the resulting reinforcing fiber mat can be reduced by making the speed of the mesh conveyor constant and reducing the flow rate of the dispersion liquid. Furthermore, the fiber orientation can be controlled by adjusting the speed of the mesh conveyor with respect to the flow rate of the dispersion. For example, by slowing down the mesh conveyor with respect to the flow rate of the dispersion, it becomes difficult to orient the fibers in the resulting reinforcing fiber mat in the take-up direction. Thus, various parameters can be adjusted to produce a reinforcing fiber mat.

  The reinforcing fiber mat may be composed of a reinforcing fiber alone, the reinforcing fiber is mixed with a powder or fiber matrix resin component, the reinforcing fiber is mixed with an organic compound or an inorganic compound, or reinforced The fibers may be sealed with a resin component. These reinforcing fiber mats are melt impregnated with a thermoplastic resin, or the thermoplastic resin components contained in the reinforcing fiber mats are melted and solidified to produce the CFRTP sheet material shown in the constituent elements (I) and (II). can do.

  According to the method, the fiber length of the reinforcing fiber can be kept relatively long, and the adjustment of the reinforcing fiber amount and the thermoplastic resin amount per unit area is easy. And (II) can be applied to the production of CFRTP sheet material.

  Here, the reinforcing fiber used for the intermediate substrate of the present invention will be described in more detail. Examples of reinforcing fibers include metal fibers such as aluminum, brass, and stainless steel, PAN-based, rayon-based, lignin-based, pitch-based carbon fibers, graphite fibers, insulating fibers such as glass, aramid, PBO, and polyphenylene. Examples thereof include organic fibers such as sulfide, polyester, acrylic, nylon, and polyethylene, and inorganic fibers such as silicon carbide and silicon nitride. Moreover, the surface treatment may be given to these fibers. Examples of the surface treatment include a treatment with a coupling agent, a treatment with a sizing agent, and an adhesion treatment of an additive in addition to a treatment for depositing a metal as a conductor. Moreover, these reinforcing fibers may be used individually by 1 type, and may use 2 or more types together. Of these, PAN-based, pitch-based and rayon-based carbon fibers are preferably used from the viewpoints of high specific strength and specific rigidity and a light weight reduction effect. In addition, glass fibers can be preferably used from the viewpoint of improving the economical efficiency of the obtained molded product, and in particular, it is preferable to use carbon fibers and glass fibers in combination from the balance of mechanical properties and economy. Furthermore, aramid fibers can be preferably used from the viewpoint of improving the impact absorbability and formability of the obtained molded article, and it is particularly preferable to use carbon fibers and aramid fibers in combination from the balance of mechanical properties and impact absorbability. In addition, reinforcing fibers coated with a metal such as nickel, copper, or ytterbium can be used from the viewpoint of increasing the conductivity of the obtained molded product. Among these, PAN-based carbon fibers that are excellent in balance between mechanical properties such as strength and elastic modulus and price can be more preferably used.

  Next, the thermoplastic resin used for the intermediate substrate of the present invention will be described in more detail. Examples of the thermoplastic resin used for the intermediate substrate of the present invention include “polyethylene terephthalate (PET), polybutylene terephthalate (PBT), polytrimethylene terephthalate (PTT), polyethylene naphthalate (PEN), liquid crystal polyester, and the like. Polyesters, polyolefins such as polyethylene (PE), polypropylene (PP) and polybutylene, polyarylene sulfides such as polyoxymethylene (POM), polyamide (PA) and polyphenylene sulfide (PPS), polyketones (PK) and polyethers Fluororesin such as ketone (PEK), polyether ether ketone (PEEK), polyether ketone ketone (PEKK), polyether nitrile (PEN), polytetrafluoroethylene, liquid crystal polymer ( CP) "and other crystalline resins, in addition to styrene resins, polycarbonate (PC), polymethyl methacrylate (PMMA), polyvinyl chloride (PVC), polyphenylene ether (PPE), polyimide (PI), polyamideimide (PAI) ), Polyetherimide (PEI), polysulfone (PSU), polyethersulfone, polyarylate (PAR) ", etc., phenolic resin, phenoxy resin, polystyrene, polyolefin, polyurethane And thermoplastic elastomers such as polyester-based, polyamide-based, polybutadiene-based, polyisoprene-based, fluorine-based resin, acrylonitrile-based thermoplastic elastomer and the like, and copolymers and modified products thereof. Among them, polyolefin is preferable from the viewpoint of light weight of the obtained molded product, polyamide is preferable from the viewpoint of strength, amorphous resin such as polycarbonate and styrene resin is preferable from the viewpoint of surface appearance, and heat resistance is preferable. From the viewpoint of continuous use temperature, polyether ether ketone is preferably used.

  The thermoplastic resins exemplified in the above group may contain an impact resistance improver such as an elastomer or a rubber component, and other fillers and additives as long as the object of the present invention is not impaired. Examples of these include inorganic fillers, flame retardants, conductivity imparting agents, crystal nucleating agents, ultraviolet absorbers, antioxidants, vibration damping agents, antibacterial agents, insect repellents, deodorants, anti-coloring agents, heat stabilizers. , Release agents, antistatic agents, plasticizers, lubricants, colorants, pigments, dyes, foaming agents, antifoaming agents, or coupling agents.

  Further, the intermediate substrate of the present invention can be used as a preform in which a plurality of the intermediate substrates are laminated. Here, the preform is a laminate of at least two intermediate substrates, and there is no particular limitation on the form as long as the intermediate substrate can be carried, and each intermediate substrate is substantially independent. They may be engaged with each other.

  Examples of the means for producing the preform include a method of laminating before the intermediate substrate is preheated, and a method of laminating after the intermediate substrate is preheated. Here, the preheat treatment refers to a step of heating the intermediate base material to a temperature equal to or higher than the melting point or softening point of the intermediate base material when subjected to press molding. In other words, to laminate after heat treatment of the intermediate base material is to heat each of the intermediate base materials individually or partially, and then to laminate the intermediate base material that is above the melting point or softening point. The laminate obtained by the above also corresponds to the preform of the present invention. In addition, the amount of lamination and size of a preform can be appropriately adjusted according to the shape of a desired molded product. From the viewpoint of formability and handleability, the thickness of the preform is preferably in the range of 1 mm to 10 mm, more preferably in the range of 3 mm to 5 mm. Moreover, when producing a preform before heat-processing, it is preferable to exist in the range of 1 mm-5 mm from a viewpoint of preheating efficiency, More preferably, it exists in the range of 1 mm-3 mm. The thickness here is the thickness of the preform at room temperature before heating.

  Next, a method for producing a molded product using the intermediate substrate or preform of the present invention will be described.

  The production of the molded product in the present invention is performed by press molding. Press molding is a method of obtaining a molded product by applying deformation such as bending, shearing, compression, etc. to various materials exemplified by metals, plastic materials, ceramic materials, etc. using a processing machine, a mold, a tool, etc. Examples of the forming form include drawing, deep drawing, flange, call gate, edge curling, stamping and the like. Examples of the press molding method include a mold press method in which molding is performed using a mold, a rubber press method (hydrostatic pressure molding method), and the like. Among these, from the viewpoint of the degree of freedom of molding pressure and temperature, a mold pressing method in which molding is performed using a compression molding machine and a metal mold is preferable. That is, the intermediate substrate or preform of the present invention is placed in a mold cavity and then press-molded.

  As the mold pressing method, the mold is heated in advance to the molding temperature of the intermediate substrate or preform, the intermediate substrate or preform is placed in the heated mold, and the mold is clamped. There is a so-called hot press molding method in which a molded product is obtained by pressurizing and then cooling the mold while maintaining the state. In addition, the intermediate base material or preform heated above the molding temperature is placed in a mold held below the solidification temperature of the intermediate base material or preform, clamped and pressurized, and then the state is maintained. However, there are methods for obtaining a molded product by cooling an intermediate substrate or preform, so-called stamping molding or heat and cool molding. Among these press molding methods, stamping molding or heat and cool molding is preferable from the viewpoint of increasing the productivity by increasing the molding cycle.

  In this stamping molding and heat-and-cool molding, as a means for heating the intermediate substrate or preform to a molding temperature or higher, far infrared heater, near infrared heater, halogen heater, dielectric heating, hot air heating, hot plate heating, etc. A well-known heating apparatus can be illustrated. Of these, far-infrared heaters and hot plate heating are preferable because of easy temperature control. The molding temperature here is a temperature at which the intermediate substrate or preform can be shaped, and is preferably equal to or higher than the melting point or softening point of the thermoplastic resin constituting the intermediate substrate.

  As a means for transporting and arranging the heated intermediate base material or preform to the mold, a manual system for manually transporting it or a known transport device such as a belt conveyor, an operating frame, a robot arm, or the like may be used. An automatic system can also be applied. Moreover, in the case of an automatic system, you may provide the temperature control equipment and space equipment which can control temperature on a conveyance path | route. When transporting, since the appearance quality of the molded product may be deteriorated or the formability may be impaired due to the temperature drop of the intermediate base material or the preform, it is preferable to transport quickly. Specifically, it is preferably 30 seconds or less, more preferably 20 seconds or less, particularly preferably after the intermediate base material or preform is taken out from the heating device and before being pressed in the mold. Is 10 seconds or less.

  The pressure applied in the molding die is preferably in the range of 10 to 40 MPa from the viewpoint of ease of shaping the intermediate substrate or preform and ease of thickness control of the molded product. In particular, the range of 15 to 30 MPa is preferable from the viewpoint of the equipment cost of the press molding machine, and more preferably 15 to 20 MPa. The pressure here is a pressure applied per projected area of the molded product.

  As the temperature of the mold, it is easy to shape the intermediate base material or preform that has been plasticized within the range of 30 ° C. to 100 ° C. lower than the solidification temperature of the thermoplastic resin constituting the intermediate base material. From the viewpoint of the surface appearance of the molded product, it is preferable. For example, when a polyamide 6 resin is used as the thermoplastic resin, it is within a range of 120 ° C. to 160 ° C., and when a polypropylene resin is used, it is within a range of 80 ° C. to 120 ° C.

  As a means for taking out the molded product that has been cooled and solidified from the mold, it is possible to use an ejector attached to the molding die as a matter of course, as well as manually. As the ejector, a method of blowing compressed air, a method of pushing up by a mechanical structural member, or the like is preferably used.

  A press mold will be described. Molds are roughly classified into two types, one is a sealed mold used for casting, injection molding, flow press (stamping) molding, etc. The other is for bending molding, deep drawing molding, forging, etc. Open mold used. The closed mold is mainly suitable for a method in which a material is poured into the mold, and the open mold is mainly suitable for a method in which the material is deformed without flowing. Since the intermediate substrate or preform of the present invention is a material particularly suitable for the method of flowing the material into the cavity and filling the cavity, it is preferable to use the former hermetically sealed mold. In a closed mold, it is common to provide a shear edge to block outflow of material.

In the press molding described above, it is important that the charge rate when the intermediate substrate or preform is placed in the mold is 50% or more and less than 100%. The charge rate is a ratio of the projected area of the intermediate base material or preform to the projected area of the mold cavity, and is obtained by the following equation.
Charge rate (%) = (projection area of intermediate substrate or preform) / (projection area of mold cavity) × 100

  By setting the charge rate to 50% or more and less than 100%, the intermediate substrate or preform is filled into the cavity with substantial flow. According to this molding, there is no surplus outside the cavity mold at the stage of charging the intermediate substrate or preform into the cavity, and there is virtually no burr (non-product part) after shaping, so material is wasted. It can be effectively reflected in the product. Therefore, the molding yield is excellent, secondary processing such as trimming is not required, and the manufacturing cost can be reduced. In addition, as described above, the intermediate base material or preform of the present invention is excellent in formability and can suppress the orientation and localization of the reinforcing fibers even when flow is involved. It is suitable for use in the range of the charge rate. The charge rate may be appropriately selected within the above-mentioned range depending on the shape and size of the target molded product, and is preferably 80% or more and less than 100 for a large area and thin molded product, and a small area and thick molding. For products, it is preferably 50% or more and less than 80%.

  In the press molding described above, in addition to the intermediate base material and the preform of the present invention, a skin material and a core material can be used together from the viewpoint of imparting a function to the molded product. Here, it is assumed that the skin material and the core material do not substantially contribute to the flow. That is, in press molding, it is arranged at a charge rate of 100% or more with respect to the projected area of the mold cavity.

  For the purpose of modifying the surface of the molded product as the skin material, it is preferable to dispose a resin film on the outermost layer of the intermediate substrate or preform. As the resin film, the use of a thermoplastic resin is preferable because the processability to the film and the adhesion to the preform are simple, and the use of a thermosetting resin is preferable because the surface smoothness of a primer, paint, gel coat, etc. can be improved. When the obtained molded product is used for an electronic device or the like, the flame retardancy of the film is preferably UL-94 standard VTM-1 or higher, and more preferably VTM-0 or higher.

  Moreover, it is preferable to use at least 1 type selected from a decorative film, a transparent film, and a color tone film from a viewpoint of improving the designability of the molded article obtained. Here, the decorative film can be exemplified as a preferred embodiment in which the film surface has a design and / or a geometric pattern. The transparent film can be exemplified as a preferred embodiment in which a resin having a visible light transmittance of 80 to 100% is used. The color tone film can be exemplified as a preferred embodiment containing an organic and / or inorganic pigment or colorant. In addition, a gloss film, a print film, an antistatic film, a light-shielding film, a heat-resistant film, or the like can be used as a lamination unit as necessary.

  Furthermore, it is preferable to use a resin sheet containing reinforcing fibers from the viewpoint of giving the obtained molded article a FRP texture. Especially, the sheet | seat using the continuous reinforcement fiber with high designability and the expectation of an impact characteristic improvement is preferable, and forms, such as a unidirectional base material, a textiles base material, a mat | matte base material, are mentioned. When using discontinuous reinforcing fibers, it is preferable to use the CFRTP sheet-like material shown in the component (I) of the present invention.

  Next, the core material is preferably disposed on an intermediate substrate or an intermediate layer of a preform for the purpose of ensuring the thickness of the molded product. In addition, from the viewpoint of enhancing lightness, it is preferable to use a material having a lower bulk density than the intermediate substrate of the present invention. For example, a mat substrate including a sheet-like substrate, a porous substrate, a honeycomb material, and reinforcing fibers Etc.

  In addition to those exemplified above, as skin materials and core materials, metal plates, metal foils, metal meshes, graphite sheets, heat dissipation sheets, chemical resistant films, gas barrier films, cold resistant films, antibacterial sheets and films, foam sheets, A rubber sheet or the like may be used. The above lamination units may be used alone or in combination of two or more as required.

  As a method of using a skin material and a core material together in press molding, a method in which a skin material is previously arranged in a cavity and an intermediate base material or a preform is subsequently placed in the cavity, or an intermediate base material is used. Alternatively, a method in which a laminate of a preform and a skin material and / or a core material is preheated at the same time, and a laminate heated to a temperature higher than the molding temperature is disposed in the cavity. Examples include a method in which a skin material and / or a core material are laminated and placed in a cavity after pre-heat treatment of the material or preform.

  Examples of the use of the molded article produced using the intermediate substrate or preform of the present invention include, for example, “PC, display, OA equipment, cellular phone, portable information terminal, facsimile, compact disc, portable MD, portable radio. Cassettes, PDAs (mobile information terminals such as electronic notebooks), video cameras, digital video cameras, optical equipment, audio equipment, air conditioners, lighting equipment, entertainment equipment, toy goods, and other home appliances, trays, chassis, interior components , Or its case "and other electrical and electronic equipment parts," posts, panels, reinforcements "and other civil engineering and building material parts," various members, various frames, various hinges, various arms, various axles, various wheel bearings, Suspension, accelerator, or various beams, propeller shafts, wheels, gearboxes, etc. `` Tearing parts '', `` Hood, roof, door, fender, trunk lid, side panel, rear end panel, upper back panel, front body, underbody, various pillars, various members, various frames, various beams, various supports, various rails, Outer plate or body parts such as various hinges, "" Bumper, bumper beam, molding, under cover, engine cover, current plate, spoiler, cowl louver, aero parts such as aero parts "," instrument panel, seat frame, Interior parts such as door trims, pillar trims, handles, various modules "or" motor parts, CNG tank, gasoline tank, fuel pump, air intake, intake manifold, carburetor main body, carburetor -Fuel systems such as spacers, various pipes, various valves, exhaust systems or intake system parts ", structural parts for motorcycles," others, alternator terminals, alternator connectors, IC regulators, light potentiometer bases, engine cooling Water joint, air conditioning thermostat base, heating hot air flow control valve, radiator motor brush holder, turbine vane, wiper motor related parts, distributor, starter switch, starter relay, window washer nozzle, air conditioner panel switch board, fuel Coil for related electromagnetic valve, battery tray, AT bracket, headlamp support, pedal housing, protector, horn terminal, step motor -Rotor, lamp socket, lamp reflector, lamp housing, brake piston, noise shield, spare tire cover, solenoid bobbin, engine oil filter, ignition device case, scuff plate, fascia ", etc. , Winglets, spoilers, edges, ladders, elevators, failings, ribs "and other aircraft parts. From the viewpoint of mechanical properties, it is preferably used for electrical and electronic equipment casings, civil engineering, building material panels, automotive structural parts, and aircraft parts. In particular, it is preferably used for structural parts for automobiles and motorcycles from the viewpoint of mechanical properties and isotropy.

  Hereinafter, the present invention will be described in more detail with reference to examples.

(1) Fiber dispersion ratio of CFRTP sheet-like material CFRTP sheet-like material is sandwiched between two stainless steel meshes (plain weave shape having 50 meshes per 2.5 cm), and the screws are adjusted so that the prepreg does not move. Fixed. This was heated in air at 500 ° C. for 30 minutes to burn off the resin component. The stainless steel mesh was removed, the resulting fiber mat was observed with a microscope, one single fiber was randomly selected, and the two-dimensional contact angle with another single fiber contacting the single fiber was measured by image observation. . As the two-dimensional contact angle, an angle (acute angle side) of 0 ° or more and 90 ° or less among two angles formed by two single fibers in contact with each other was adopted. The measurement of the two-dimensional contact angle was performed on 100 single fibers, targeting all single fibers that contact the selected single fibers. From the obtained results, the ratio was calculated from the total number of all single fibers whose two-dimensional contact angle was measured and the number of single fibers whose two-dimensional contact angle was 1 degree or more, and the fiber dispersion rate was obtained. .

(2) Two-dimensional orientation angle of discontinuous reinforcing fiber of CFRTP sheet-like material A fiber mat was taken out from the CFRTP sheet-like material in the same manner as (1) above. The obtained fiber mat was observed with a microscope, one single fiber was randomly selected, and the two-dimensional orientation angle with another single fiber intersecting with the single fiber was measured by image observation. Of the two angles formed by the two intersecting single fibers, the angle between 0 ° and 90 ° (acute angle side) was adopted as the orientation angle. The number of measured two-dimensional orientation angles per selected single fiber was n = 20. The same measurement was performed by selecting a total of 5 single fibers, and the average value was taken as the two-dimensional orientation angle.

(3) Average fiber length Ln of discontinuous reinforcing fibers contained in the CFRTP sheet
The CFRTP sheet is heated in air at 500 ° C. for 30 minutes to burn off the thermoplastic resin component, and 400 random pieces are selected from the remaining discontinuous reinforcing fibers, and the length is reduced to the unit of 10 μm with an optical microscope. The average value was measured as the average fiber length Ln.

(4) Fiber diameter D of discontinuous reinforcing fibers contained in the CFRTP sheet
For the fiber diameter D of the discontinuous reinforcing fibers contained in the CFRTP sheet material, the single fiber diameter of the reinforcing fibers used for the production of the CFRTP sheet material was used as the fiber diameter D as it was.

(5) Aspect ratio p of discontinuous reinforcing fiber contained in CFRTP sheet
From the average fiber length Ln and the fiber diameter D obtained in the above (3) and (4), it was calculated by the following formula.
・ P = Ln / D
Ln: Fiber length of discontinuous reinforcing fiber (μm)
D: Fiber diameter (μm) of discontinuous reinforcing fibers.

(6) Ratios of reinforcing fibers contained in the CFRTP sheet material VfI, VfII
After measuring the mass W0 of the CFRTP sheet material, the CFRTP sheet material is heated in air at 500 ° C. for 30 minutes to burn off the thermoplastic resin component, and the remaining discontinuous reinforcing fiber mass W1 is measured. Calculated by the formula.
VfI, VfII (volume%) = (W1 / ρf) / {W1 / ρf + (W0−W1) / ρr} × 100
ρf: density of reinforcing fiber (g / cm ³ )
ρr: density of thermoplastic resin (g / cm ³ ).

(7) Volume ratios VI and VII of components contained in the intermediate substrate for press molding
From the thickness of the CFRTP sheet used for the production of the intermediate substrate, the thickness was calculated by the following formula.
Volume ratio (VI) = (tI × nI) / (tI × nI + tII × nII) × 100
Volume ratio (VII) = (tII × nII) / (tI × nI + tII × nII) × 100
tI: Thickness (mm) of CFRTP sheet-like material of component (I)
tII: Thickness (mm) of CFRTP sheet material of component (II)
nI: Number of laminated CFRTP sheet materials (components) of component (I)
nII: The number of laminated CFRTP sheets (components) of the component (II).

(8) Ratio Vf of reinforcing fibers contained in the intermediate substrate for press molding
From the ratios (VfI, VfII) and volume ratios (VI, VII) of the reinforcing fibers contained in the CFRTP sheet obtained in the above (6) and (7), the following formula was used.
Vf (volume%) = (NI × VI) + (NII × VII).

(9) Elongation ratio R of intermediate substrate for press molding
One or a plurality of disks having a diameter of 150 mm cut out from the intermediate base material were laminated to prepare a preform having a thickness of 3 mm, and then a sample was prepared by stamping. Specifically, the preform is put into a far-infrared heater and heated until the preform center temperature reaches the molding temperature of the thermoplastic resin constituting the intermediate substrate (melting point of the thermoplastic resin + 30 ° C.), Immediately placed in a mold having a flat plate-shaped cavity (cavity surface temperature 120 ° C.) installed in a press molding machine, the mold was closed, and after holding the molding pressure 15 MPa for 60 seconds, the mold was opened and the sample was taken out. It was. The obtained sample was substantially circular, and four diameters were measured at 45 ° intervals from the sample, and the projected area of the sample was derived from the average value. Furthermore, the projected area of the preform was derived with a diameter of 150 mm, and the elongation ratio R was calculated by the following equation.
R (%) = (projected area of sample / projected area of preform) × 100.

As an index of formability in press molding, the following criteria were used for determination based on the obtained elongation rate R.
AA: The elongation ratio R of the intermediate substrate is 330% or more A: The elongation ratio R of the intermediate substrate is 280% or more and less than 330% B: The elongation ratio R of the intermediate substrate is 230% or more and less than 280% Some C: The elongation ratio R of the intermediate substrate is 180% or more and less than 230%. D: The elongation ratio R of the intermediate substrate is less than 180%.

(10) Filling rate of molded product Press molding was performed in the same manner as the measurement of the elongation rate R described above except that the size of the intermediate base material to be cut out was a square having a side of 250 mm. FIG. 11 shows a schematic view of the molded product 30 formed. The top plate 31 is a square having a side of 300 mm, and a vertical wall having a vertical height of 20 mm having a gradient of 63 degrees is provided on each side. The curvature radius of each edge was 1 mm. The cavity projected area Sc of the mold in this shape is 102400 mm ² . The filling rate of the molded product was calculated from the cavity projected area Sc of the mold and the projected area Sm of the molded product by the following equation.
Filling rate of molded product (%) = (Sm / Sc) × 100.

(11) Average bending strength σa and average bending elastic modulus Ea of the molded product
The bending strength and bending elastic modulus of the molded product were evaluated according to ASTM D-790. The test piece was cut out as shown in FIG. A total of 12 test pieces were cut out from the top plate portion of the molded product obtained in (10) above in four directions of 0/90 / ± 45, with an arbitrary direction parallel to the side direction of the molded product top plate being 0 degree. It was. The average value of all the measured values (n = 12) by these test pieces was defined as the bending strength σa and the bending elastic modulus Ea. An “Instron” (registered trademark) universal testing machine 4201 type (Instron) was used as a testing machine.

(12) Variation in bending strength of molded product From the individual value of the bending strength of the molded product obtained in the above (11), it was calculated by the following formula.
Bending strength variation (%) = {Σ (σi−σ) ² / n} ^1/2 / σ × 100
σi: Individual value of bending strength (i = 1, 2,... 12) (MPa)
σa: Average bending strength (MPa)
n: Number of measurement points of bending strength (pieces).

As an index of reliability in a molded product, the following criteria were used for determination based on the obtained variation in bending strength.
AA: Variation in bending strength of molded product is less than 5% A: Variation in bending strength of molded product is 5% or more and less than 8% B: Variation in bending strength of molded product is 8% or more and less than 13% C: Variation in bending strength of molded product is 13% or more and less than 18% D: Variation in bending strength of molded product is 18% or more.

(13) Variation in flexural modulus of molded product The individual value of the flexural modulus of the molded product obtained in (11) above was calculated by the following equation.
Variation in flexural modulus (%) = {Σ (Ei−Ea) ² / n} ^1/2 / Ea × 100
Ei: Individual value of flexural modulus (i = 1, 2,... 9) (GPa)
Ea: Average flexural modulus (GPa)
n: Number of measured flexural modulus (pieces).

As an index of reliability in the molded product, the following criteria were used for determination based on the obtained variation in flexural modulus.
AA: Variation in flexural modulus of molded product is less than 5% A: Variation in flexural modulus of molded product is 5% or more and less than 8% B: Variation in flexural modulus of molded product is 8% or more 13 C: less than% C: variation in the flexural modulus of the molded product is 13% or more and less than 18% D: variation in the flexural modulus of the molded product is 18% or more.

(14) Density of molded product ρ
The density ρ of the molded product was measured in accordance with Method A (underwater substitution method) described in 5 of JIS K 7112 (1999). A 2 cm × 2 cm sample was cut out from the test piece subjected to the measurement in (11) above, vacuum-dried at a temperature of 50 ° C. for 12 hours, and then cooled to room temperature in a desiccator was used as the test piece. Ethanol was used as the immersion liquid, measurement was performed for n = 5, and the average value was defined as the density ρ of the molded product.

(15) Specific bending strength of molded product The average bending strength σ of the molded product obtained in the above (11) and (14) and the density ρ of the molded product were calculated by the following equation.
・ Specific bending strength of molded product = σ ^1/2 / ρ
σ: Average bending strength of molded product (MPa)
ρ: Density of molded product (g / cm ³ )

As an index of the reinforcing efficiency of the reinforcing fiber and the weight reduction effect of the molded product, the determination was made based on the following criteria based on the specific bending strength of the molded product obtained.
A: Specific bending strength of molded product is 16 or more A: Specific bending strength of molded product is 15 or more and less than 16 B: Specific bending strength of molded product is 14 or more and less than 15 C: Specific bending of molded product The strength is 13 or more and less than 14 D: The specific bending strength of the molded product is less than 13.

[Carbon fiber 1]
Spinning and firing were performed from a polymer containing polyacrylonitrile as a main component to obtain continuous carbon fibers having a total filament number of 12,000. Further, the continuous carbon fiber was subjected to electrolytic surface treatment and dried in heated air at 120 ° C. to obtain carbon fiber 1. The characteristics of this carbon fiber 1 were as follows.
Density: 1.8 g / cm ³
Single fiber diameter: 7μm
Tensile strength: 4.9 GPa
Tensile modulus: 230 GPa

[Carbon fiber 2]
Spinning and firing were performed from a polymer containing polyacrylonitrile as a main component to obtain continuous carbon fibers having a total filament number of 12,000. Further, the continuous carbon fiber was subjected to electrolytic surface treatment and dried in heated air at 120 ° C. to obtain carbon fiber 2. The characteristics of the carbon fiber 2 were as follows.
Density: 1.8 g / cm ³
Single fiber diameter: 5 μm
Tensile strength: 5.9 GPa
Tensile modulus: 294 GPa

[Resin sheet 1]
90% by mass of unmodified polypropylene resin (manufactured by Prime Polymer Co., Ltd., “Prime Polypro” (registered trademark) J106MG) and acid-modified polypropylene resin (manufactured by Mitsui Chemicals, Inc., “Admer” (registered trademark) QE800) 10 A sheet having a basis weight of 90 g / m ² was produced using a polypropylene master batch composed of mass%.

[Resin sheet 2]
A sheet was obtained in the same manner as the resin sheet 1 except that the basis weight was adjusted to 158 g / m ² .

[Resin sheet 3]
A sheet was obtained in the same manner as the resin sheet 1 except that the basis weight was adjusted to 203 g / m ² .

[Resin sheet 4]
A sheet was obtained in the same manner as the resin sheet 1 except that the basis weight was adjusted to 214 g / m ² .

[Resin sheet 5]
A sheet was obtained in the same manner as the resin sheet 1 except that the basis weight was adjusted to 113 g / m ² .

[Resin sheet 6]
A sheet was obtained in the same manner as the resin sheet 1 except that the basis weight was adjusted to 120 g / m ² .

[Resin sheet 7]
A sheet having a basis weight of 112 g / m ² was prepared using a polyamide master batch made of polyamide 6 resin (manufactured by Toray Industries, Inc., “Amilan” (registered trademark) CM1001).

[Resin sheet 8]
A sheet was obtained in the same manner as the resin sheet 7 except that the basis weight was adjusted to 197 g / m ² .

[Resin sheet 9]
A sheet was obtained in the same manner as the resin sheet 7 except that the basis weight was adjusted to 253 g / m ² .

[Resin sheet 10]
A sheet was obtained in the same manner as the resin sheet 7 except that the basis weight was adjusted to 141 g / m ² .

[Carbon fiber mat 1]
Carbon fiber 1 was cut to 6 mm with a cartridge cutter to obtain chopped carbon fiber. 100 liters of a dispersion having a concentration of 1.5% by mass composed of water and a surfactant (manufactured by Kojun Pharmaceutical Co., Ltd., sodium n-dodecylbenzenesulfonate) (product name) was prepared. The chopped carbon fiber was added to the dispersion and stirred for 10 minutes, and then poured into a papermaking tank having a papermaking surface of 500 mm × 500 mm. The dispersion was dehydrated and removed, and only the carbon fiber content was taken out. Further, the carbon fiber mat 1 was obtained by drying in a drying furnace at 150 ° C. for 2 hours. The basis weight of the obtained carbon fiber mat 1 was 90 g / m ² .

[Carbon fiber mat 2]
A carbon fiber mat 2 was obtained in the same manner as the carbon fiber mat 11 except that the carbon fiber 1 was cut to 1 mm with a cartridge cutter. The obtained carbon fiber mat 2 had a basis weight of 90 g / m ² .

[Carbon fiber mat 3]
A carbon fiber mat 3 was obtained in the same manner as the carbon fiber mat 11 except that the carbon fiber 1 was cut to 3 mm with a cartridge cutter. The basis weight of the obtained carbon fiber mat 3 was 90 g / m ² .

[Carbon fiber mat 4]
A carbon fiber mat 4 was obtained in the same manner as the carbon fiber mat 1 except that the carbon fiber 1 was cut to 9 mm with a cartridge cutter. The basis weight of the obtained carbon fiber mat 4 was 90 g / m ² .

[Carbon fiber mat 5]
A carbon fiber mat 5 was obtained in the same manner as the carbon fiber mat 1 except that the carbon fiber 1 was cut to 6 mm with a cartridge cutter and the basis weight of the carbon fiber mat was 90 g / m ² .

[Carbon fiber mat 6]
A carbon fiber mat 6 was obtained in the same manner as the carbon fiber mat 1 except that the carbon fiber 2 was cut to 9 mm with a cartridge cutter. The obtained carbon fiber mat 6 had a basis weight of 90 g / m ² .

(Reference Example 1) CFRTP sheet 1
A laminate was prepared using one carbon fiber mat 1 and two resin sheets 1. The above laminate is placed in a mold cavity and the mold is closed. After holding the pressure of 5 MPa at a temperature of 210 ° C. for 120 seconds, the cavity temperature is cooled to 50 ° C. while maintaining the pressure, and the mold is Was opened to obtain a CFRTP sheet 1. Properties of the obtained CFRTP sheet 1 are shown in Table 1-1.

(Reference Example 2) CFRTP sheet 2
A CFRTP sheet-like material 2 was obtained in the same manner as in Reference Example 1 except that a laminate was prepared using 3 carbon fiber mats 1 and 2 resin sheets 2 and the pressure applied was 7 MPa. . The characteristics of the obtained CFRTP sheet-like material 2 are shown in Table 1-1.

(Reference Example 3) CFRTP sheet 3
A CFRTP sheet-like material 3 was obtained in the same manner as in Reference Example 1 except that a laminate was prepared using one carbon fiber mat 1 and two resin sheets 3. Properties of the obtained CFRTP sheet-like material 3 are shown in Table 1-1.

Reference Example 4 CFRTP sheet 4
A CFRTP sheet-like material 4 was obtained in the same manner as in Reference Example 1 except that a laminate was produced using one carbon fiber mat 1 and five resin sheets 2. Properties of the obtained CFRTP sheet 4 are shown in Table 1-1.

(Reference Example 5) CFRTP sheet material 5
A CFRTP sheet-like material 5 was obtained in the same manner as in Reference Example 1 except that a laminate was prepared using 4 carbon fiber mats 1 and 3 resin sheets 1 and the pressure applied was 10 MPa. . Properties of the obtained CFRTP sheet 5 are shown in Table 1-1.

(Reference Example 6) CFRTP sheet 6
A CFRTP sheet-like product 6 was obtained in the same manner as in Reference Example 5 except that a laminate was prepared using 4 carbon fiber mats 4 and 3 resin sheets 1. Properties of the obtained CFRTP sheet 6 are shown in Table 1-1.

(Reference Example 7) CFRTP sheet 7
A CFRTP sheet 7 was obtained in the same manner as in Reference Example 1 except that a laminate was prepared using three carbon fiber mats 4 and two resin sheets 2. Properties of the obtained CFRTP sheet 7 are shown in Table 1-1.

(Reference Example 8) CFRTP sheet material 8
A CFRTP sheet-like product 8 was obtained in the same manner as in Reference Example 1 except that a laminate was prepared using one carbon fiber mat 4 and two resin sheets 3. Properties of the obtained CFRTP sheet-like material 8 are shown in Table 1-1.

(Reference Example 9) CFRTP sheet material 9
A CFRTP sheet-like material 9 was obtained in the same manner as in Reference Example 1 except that a laminate was prepared using three carbon fiber mats 3 and two resin sheets 2. Properties of the obtained CFRTP sheet 9 are shown in Table 1-1.

(Reference Example 10) CFRTP sheet 10
A CFRTP sheet 10 was obtained in the same manner as in Reference Example 1 except that a laminate was prepared using one carbon fiber mat 3 and two resin sheets 3. Properties of the obtained CFRTP sheet 10 are shown in Table 1-1.

Reference Example 11 CFRTP sheet 11
A CFRTP sheet material 11 was obtained in the same manner as in Reference Example 1 except that a laminate was prepared using three carbon fiber mats 6 and two resin sheets 2. Properties of the obtained CFRTP sheet 11 are shown in Table 1-2.

Reference Example 12 CFRTP sheet 12
A CFRTP sheet 12 was obtained in the same manner as in Reference Example 1 except that a laminate was prepared using one carbon fiber mat 6 and two resin sheets 3. The characteristics of the obtained CFRTP sheet 12 are shown in Table 1-2.

Reference Example 13 CFRTP sheet 13
A CFRTP sheet-like product 13 was obtained in the same manner as in Reference Example 1, except that a laminate was prepared using three carbon fiber mats 2 and two resin sheets 2. The characteristics of the obtained CFRTP sheet 13 are shown in Table 1-2.

Reference Example 14 CFRTP sheet 14
A CFRTP sheet-like material 14 was obtained in the same manner as in Reference Example 1 except that a laminate was prepared using one carbon fiber mat 2 and two resin sheets 3. Properties of the obtained CFRTP sheet-like material 14 are shown in Table 1-2.

Reference Example 15 CFRTP sheet 15
A CFRTP sheet-like material 15 was obtained in the same manner as in Reference Example 1 except that a laminate was prepared using 5 carbon fiber mats 1 and 2 resin sheets 5 and the applied pressure was 15 MPa. . Properties of the obtained CFRTP sheet 15 are shown in Table 1-2.

Reference Example 16 CFRTP sheet 16
A CFRTP sheet-like material 16 was obtained in the same manner as in Reference Example 1-2, except that a laminate was produced using two carbon fiber mats 5 and three resin sheets 6. The properties of the obtained CFRTP sheet 16 are shown in Table 1.

Reference Example 17 CFRTP sheet 17
The polypropylene masterbatch used for the adjustment of the resin sheet 1 and the carbon fiber 1 were melt-kneaded with a twin-screw extruder to produce a short fiber masterbatch having a carbon fiber ratio of 30% by volume. The short fiber master batch was processed into a sheet shape to produce a CFRTP sheet material 17 having a basis weight of 293 g / m ² . Properties of the obtained CFRTP sheet 17 are shown in Table 1-2.

Reference Example 18 CFRTP sheet 18
The polypropylene masterbatch used for the adjustment of the resin sheet 1 and the carbon fiber 1 were melt-kneaded with a twin screw extruder to prepare a short fiber masterbatch having a carbon fiber ratio of 10% by volume. The short fiber master batch was processed into a sheet shape to produce a CFRTP sheet material 18 having a basis weight of 248 g / m ² . The characteristics of the obtained CFRTP sheet 18 are shown in Table 1-2.

Reference Example 19 CFRTP sheet 19
Glass fiber reinforced thermoplastic resin (GMT)
“Unisheet” (registered trademark) P4038-BK31 manufactured by Quadrant was used as the CFRTP sheet material 19. The characteristics are shown in Table 1-2.

Reference Example 20 CFRTP sheet 20
Thermoplastic sheet molding compound (SMC)
The carbon fiber 1 was melt-impregnated with a master batch adjusted with the resin sheet 1 with an impregnation die to produce a carbon fiber tape in which the ratio of the carbon fibers was adjusted to 50% by volume. The carbon fiber tape was cut with a cartridge cutter to produce a chopped tape having a tape length of 35 mm, and the chopped tape was randomly dispersed by free fall to form a sheet. Further, the formed sheet is placed in a mold cavity installed in a press molding machine, the mold is closed, and after maintaining a pressure of 5 MPa at a temperature of 210 ° C. for 120 seconds, the cavity temperature is adjusted while maintaining the pressure. After cooling to 50 ° C., the mold was opened to obtain a CFRTP sheet 20. The characteristics of the obtained CFRTP sheet 20 are shown in Table 1-2.

Reference Example 21 CFRTP sheet 21
A laminate was prepared using one carbon fiber mat 1 and two resin sheets 7. The laminate is placed in the mold cavity and the mold is closed. After maintaining the pressure of 5 MPa at a temperature of 240 ° C. for 120 seconds, the cavity temperature is cooled to 50 ° C. while maintaining the pressure, and the mold is And CFRTP sheet 21 was obtained. Properties of the obtained CFRTP sheet 21 are shown in Table 4-1.

Reference Example 22 CFRTP sheet material 22
A CFRTP sheet-like material 22 was obtained in the same manner as in Reference Example 21 except that a laminate was produced using three carbon fiber mats 1 and two resin sheets 8 and the pressure applied was 7 MPa. . Properties of the obtained CFRTP sheet material 22 are shown in Table 4-1.

Reference Example 23 CFRTP sheet material 23
A CFRTP sheet-like material 23 was obtained in the same manner as in Reference Example 21 except that a laminate was prepared using one carbon fiber mat 1 and two resin sheets 9. Properties of the obtained CFRTP sheet material 23 are shown in Table 4-1.

Reference Example 24 CFRTP sheet material 24
A CFRTP sheet-like material 24 was obtained in the same manner as in Reference Example 21, except that a laminate was prepared using one carbon fiber mat 1 and five resin sheets 8. Properties of the obtained CFRTP sheet material 24 are shown in Table 4-1.

Reference Example 25 CFRTP sheet 25
A CFRTP sheet-like material 25 was obtained in the same manner as in Reference Example 21, except that a laminate was prepared using 4 carbon fiber mats 1 and 3 resin sheets 7 and the pressure applied was 10 MPa. . Properties of the obtained CFRTP sheet 25 are shown in Table 4-1.

Reference Example 26 CFRTP sheet 26
A CFRTP sheet-like material 26 was obtained in the same manner as in Reference Example 25 except that a laminate was prepared using 4 carbon fiber mats 4 and 3 resin sheets 7. Properties of the obtained CFRTP sheet material 26 are shown in Table 4-1.

Reference Example 27 CFRTP sheet 27
A CFRTP sheet 27 was obtained in the same manner as in Reference Example 21 except that a laminate was produced using three carbon fiber mats 4 and two resin sheets 8. Properties of the obtained CFRTP sheet 27 are shown in Table 4-1.

Reference Example 28 CFRTP sheet 28
A CFRTP sheet-like product 28 was obtained in the same manner as in Reference Example 21 except that a laminate was produced using one carbon fiber mat 4 and two resin sheets 9. The characteristics of the obtained CFRTP sheet 28 are shown in Table 4-1.

Reference Example 29 CFRTP sheet material 29
A CFRTP sheet-like material 29 was obtained in the same manner as in Reference Example 21 except that a laminate was prepared using three carbon fiber mats 3 and two resin sheets 8. Properties of the obtained CFRTP sheet material 29 are shown in Table 4-1.

(Reference Example 30) CFRTP sheet 30
A CFRTP sheet-like material 30 was obtained in the same manner as in Reference Example 21 except that a laminate was produced using one carbon fiber mat 3 and two resin sheets 9. The characteristics of the obtained CFRTP sheet 30 are shown in Table 4-1.

Reference Example 31 CFRTP sheet material 31
A CFRTP sheet-like product 31 was obtained in the same manner as in Reference Example 21 except that a laminate was prepared using three carbon fiber mats 6 and two resin sheets 8. The characteristics of the obtained CFRTP sheet 31 are shown in Table 4-2.

Reference Example 32 CFRTP sheet 32
A CFRTP sheet-like material 32 was obtained in the same manner as in Reference Example 21 except that a laminate was prepared using one carbon fiber mat 6 and two resin sheets 9. Properties of the obtained CFRTP sheet material 32 are shown in Table 4-2.

Reference Example 33 CFRTP sheet 33
A CFRTP sheet-like material 33 was obtained in the same manner as in Reference Example 21 except that a laminate was prepared using three carbon fiber mats 2 and two resin sheets 8. Properties of the obtained CFRTP sheet 33 are shown in Table 4-2.

Reference Example 34 CFRTP sheet 34
A CFRTP sheet-like product 34 was obtained in the same manner as in Reference Example 21 except that a laminate was prepared using one carbon fiber mat 2 and two resin sheets 9. The characteristics of the obtained CFRTP sheet 34 are shown in Table 4-2.

Reference Example 35 CFRTP sheet 35
A CFRTP sheet-like material 35 was obtained in the same manner as in Reference Example 21 except that a laminate was prepared using 5 carbon fiber mats 1 and 2 resin sheets 10 and the pressure applied was 15 MPa. . Properties of the obtained CFRTP sheet 35 are shown in Table 4-2.

Reference Example 36 CFRTP sheet 36
The polyamide masterbatch used for the adjustment of the resin sheet 7 and the carbon fiber 1 were melt-kneaded by a twin screw extruder to produce a short fiber masterbatch having a carbon fiber ratio of 30% by volume. The short fiber master batch was processed into a sheet shape to produce a CFRTP sheet material 36 having a basis weight of 365 g / m ² . The characteristics of the obtained CFRTP sheet 36 are shown in Table 4-2.

Reference Example 38 CFRTP sheet 37
The polyamide masterbatch used in the adjustment of the resin sheet 7 and the carbon fiber 1 were melt-kneaded with a twin screw extruder to produce a short fiber masterbatch having a carbon fiber ratio of 10% by volume. The short fiber masterbatch was processed into a sheet shape to produce a CFRTP sheet material 37 having a basis weight of 309 g / m ² . Properties of the obtained CFRTP sheet 37 are shown in Table 4-2.

Example 1
A laminate was prepared using one CFRTP sheet-like material 2 of Reference Example 2 as the component (I) and one CFRTP sheet-like material 3 of Reference Example 3 as the component (II). The laminate is placed in the mold cavity and the mold is closed. After holding the pressure of 3 MPa at a temperature of 180 ° C. for 120 seconds, the cavity temperature is cooled to 50 ° C. while maintaining the pressure, and the mold is Opened to obtain an intermediate substrate. The properties of the obtained intermediate substrate are shown in Table 2.

  A preform in which three intermediate substrates were laminated was prepared, put into a far infrared heater, and heated until the preform center temperature reached 210 ° C. Take out from the heater, immediately place in a mold with a flat plate-shaped cavity (cavity projection area 300mm x 300mm, cavity surface temperature 120 ° C) installed in the press molding machine at a charge rate of 70%, close the mold, After holding the molding pressure of 15 MPa for 60 seconds, the mold was opened and the molded product was taken out. The obtained molded product was 100% filled in the cavity. Table 2 shows the characteristics of the molded product.

(Example 2)
Example except that a laminate was produced using two CFRTP sheet-like materials 1 of Reference Example 1 as the component (I) and one CFRTP sheet-like material 3 of Reference Example 3 as the component (II) In the same manner as in Example 1, an intermediate substrate was obtained. The properties of the obtained intermediate substrate are shown in Table 2.

  A molded product was obtained by molding in the same manner as in Example 1 except that three preforms were laminated to prepare a preform. The obtained molded product was 100% filled in the cavity. Table 2 shows the characteristics of the molded product.

(Example 3)
Example 1 except that a laminate was prepared using one CFRTP sheet-like material 6 of Reference Example 6 as component (I) and one CFRTP sheet-like material 3 of Reference Example 3 as component (II) In the same manner as in Example 1, an intermediate substrate was obtained. The properties of the obtained intermediate substrate are shown in Table 2.

  A molded product was obtained by molding in the same manner as in Example 1 except that three preforms were laminated to prepare a preform. The obtained molded product was 94% filled in the cavity. Table 2 shows the characteristics of the molded product.

Example 4
Example except that a laminate was prepared using one CFRTP sheet-like material 5 of Reference Example 5 as component (I) and one CFRTP sheet-like material 8 of Reference Example 8 as component (II) In the same manner as in Example 1, an intermediate substrate was obtained. The properties of the obtained intermediate substrate are shown in Table 2.

  A molded product was obtained by molding in the same manner as in Example 1 except that three preforms were laminated to prepare a preform. The obtained molded product was 100% filled in the cavity. Table 2 shows the characteristics of the molded product.

(Example 5)
Example except that a laminate was prepared using one CFRTP sheet-like material 9 of Reference Example 9 as component (I) and one CFRTP sheet-like material 10 of Reference Example 10 as component (II) In the same manner as in Example 1, an intermediate substrate was obtained. The properties of the obtained intermediate substrate are shown in Table 2.

  A molded product was obtained by molding in the same manner as in Example 1 except that three preforms were laminated to prepare a preform. The obtained molded product was 100% filled in the cavity. Table 2 shows the characteristics of the molded product.

(Example 6)
Example except that a laminate was prepared using one CFRTP sheet 7 of Reference Example 7 as component (I) and one CFRTP sheet 8 of Reference Example 8 as component (II) In the same manner as in Example 1, an intermediate substrate was obtained. The properties of the obtained intermediate substrate are shown in Table 2.

  A molded product was obtained by molding in the same manner as in Example 1 except that three preforms were laminated to prepare a preform. The obtained molded product was 99% filled in the cavity. Table 2 shows the characteristics of the molded product.

(Example 7)
Except that a laminate was prepared using four CFRTP sheet-like materials 1 of Reference Example 1 as the component (I) and four CFRTP sheet-like materials 3 of Reference Example 3 as the component (II). In the same manner as in Example 1, an intermediate substrate was obtained. The properties of the obtained intermediate substrate are shown in Table 2.

  A molded product was obtained by molding in the same manner as in Example 1 except that one intermediate substrate was used. The obtained molded product was 100% filled in the cavity. Table 2 shows the characteristics of the molded product.

(Example 8)
Example except that a laminate was prepared using 8 CFRTP sheet-like materials 1 of Reference Example 1 as the component (I) and 2 CFRTP sheet-like materials 3 of Reference Example 3 as the component (II) In the same manner as in Example 1, an intermediate substrate was obtained. The properties of the obtained intermediate substrate are shown in Table 2.

  A molded product was obtained by molding in the same manner as in Example 1 except that one intermediate substrate was used. The obtained molded product was 95% filled in the cavity. Table 2 shows the characteristics of the molded product.

Example 9
A laminate was prepared using one CFRTP sheet material of Reference Example 22 as the component (I) and one CFRTP sheet material of Reference Example 23 as the component (II). The laminate is placed in the mold cavity and the mold is closed. After maintaining the pressure of 3 MPa at a temperature of 240 ° C. for 120 seconds, the cavity temperature is cooled to 50 ° C. while maintaining the pressure, and the mold is Opened to obtain an intermediate substrate. The properties of the obtained intermediate substrate are shown in Table 5.

  A preform in which three intermediate substrates were laminated was prepared, put into a far infrared heater, and heated until the preform center temperature reached 250 ° C. Take out from the heater, immediately place it in a mold with a flat plate-shaped cavity (cavity projection area 300 mm x 300 mm, cavity surface temperature 140 ° C) installed in the press molding machine at a charge rate of 70%, close the mold, After holding the molding pressure of 15 MPa for 60 seconds, the mold was opened and the molded product was taken out. The obtained molded product was 100% filled in the cavity. Table 5 shows the characteristics of the molded product.

(Example 10)
Example 9 except that a laminate was prepared using two CFRTP sheet-like materials of Reference Example 21 as component (I) and one CFRTP sheet-like material of Reference Example 23 as component (II). Similarly, an intermediate substrate was obtained. The properties of the obtained intermediate substrate are shown in Table 5.

  A molded product was obtained by molding in the same manner as in Example 9 except that three preforms were laminated to prepare a preform. The obtained molded product was 100% filled in the cavity. Table 5 shows the characteristics of the molded product.

(Example 11)
Example 9 except that a laminate was prepared using one CFRTP sheet-like material of Reference Example 26 as component (I) and one CFRTP sheet-like material of Reference Example 23 as component (II). Similarly, an intermediate substrate was obtained. The properties of the obtained intermediate substrate are shown in Table 5.

  A molded product was obtained by molding in the same manner as in Example 9 except that three preforms were laminated to prepare a preform. The obtained molded product was 94% filled in the cavity. Table 5 shows the characteristics of the molded product.

(Example 12)
Example 9 except that a laminate was prepared using one CFRTP sheet-like material of Reference Example 25 as component (I) and one CFRTP sheet-like material of Reference Example 28 as component (II). Similarly, an intermediate substrate was obtained. The properties of the obtained intermediate substrate are shown in Table 5.

  A molded product was obtained by molding in the same manner as in Example 9 except that three preforms were laminated to prepare a preform. The obtained molded product was 100% filled in the cavity. Table 5 shows the characteristics of the molded product.

(Example 13)
Example 9 except that a laminate was prepared using one CFRTP sheet material 29 of Reference Example 29 as the component (I) and one CFRTP sheet material of Reference Example 30 as the component (II). In the same manner, an intermediate substrate was obtained. The properties of the obtained intermediate substrate are shown in Table 5.

  A molded product was obtained by molding in the same manner as in Example 9 except that three preforms were laminated to prepare a preform. The obtained molded product was 100% filled in the cavity. Table 5 shows the characteristics of the molded product.

(Example 14)
Example 9 except that a laminate was produced using one CFRTP sheet-like material of Reference Example 27 as the component (I) and one CFRTP sheet-like material of Reference Example 28 as the component (II). Similarly, an intermediate substrate was obtained. The properties of the obtained intermediate substrate are shown in Table 5.

  A molded product was obtained by molding in the same manner as in Example 9 except that three preforms were laminated to prepare a preform. The obtained molded product was 99% filled in the cavity. Table 5 shows the characteristics of the molded product.

(Example 15)
Example 9 except that a laminate was prepared using four CFRTP sheet-like materials of Reference Example 21 as component (I) and four CFRTP sheet-like materials of Reference Example 23 as component (II). Similarly, an intermediate substrate was obtained. The properties of the obtained intermediate substrate are shown in Table 5.

  A molded product was obtained by molding in the same manner as in Example 9 except that one intermediate substrate was used. The obtained molded product was 100% filled in the cavity. Table 5 shows the characteristics of the molded product.

(Example 16)
Example 9 except that a laminate was prepared using 8 CFRTP sheet-like materials of Reference Example 21 as component (I) and 2 CFRTP sheet-like materials of Reference Example 23 as component (II). Similarly, an intermediate substrate was obtained. The properties of the obtained intermediate substrate are shown in Table 5.

  A molded product was obtained by molding in the same manner as in Example 9 except that one intermediate substrate was used. The obtained molded product was 95% filled in the cavity. Table 5 shows the characteristics of the molded product.

(Comparative Example 1)
The CFRTP sheet 1 of Reference Example 1 was used as it was as an intermediate substrate. The properties of the intermediate substrate are shown in Table 3.

  A molded product was obtained by molding in the same manner as in Example 1 except that 12 preforms of the intermediate substrate were laminated to produce a preform. The obtained molded product was 92% filled in the cavity. The characteristics of the molded product are shown in Table 3-1.

(Comparative Example 2)
The CFRTP sheet 2 of Reference Example 2 was used as it was as an intermediate substrate. The properties of the intermediate substrate are shown in Table 3-1.

  A molded product was obtained by molding in the same manner as in Example 1 except that a preform was prepared by laminating six intermediate substrates. The obtained molded product was 84% filled in the cavity. The characteristics of the molded product are shown in Table 3-1.

(Comparative Example 3)
The CFRTP sheet material 19 of Reference Example 19 was used as it was as an intermediate substrate. The properties of the intermediate substrate are shown in Table 3-1.

  A molded product was obtained by molding in the same manner as in Example 1 except that one intermediate substrate was used. The obtained molded product was 100% filled in the cavity. The characteristics of the molded product are shown in Table 3-1.

(Comparative Example 4)
The CFRTP sheet material 20 of Reference Example 20 was used as it was as an intermediate substrate. The properties of the intermediate substrate are shown in Table 3-1.

  A molded product was obtained by molding in the same manner as in Example 1 except that one intermediate substrate was used. The obtained molded product was 100% filled in the cavity. The characteristics of the molded product are shown in Table 3-1.

(Comparative Example 5)
Except that a laminate was prepared using one CFRTP sheet-like material 11 of Reference Example 11 as the lamination unit (I) and one CFRTP sheet-like material 12 of Reference Example 12 as the lamination unit (II), Example In the same manner as in Example 1, an intermediate substrate was obtained. The properties of the obtained intermediate substrate are shown in Table 3-1.

  A molded product was obtained by molding in the same manner as in Example 1 except that three preforms were laminated to prepare a preform. The obtained molded product was 71% filled in the cavity. The characteristics of the molded product are shown in Table 3-1.

(Comparative Example 6)
Except that the laminate was prepared using two CFRTP sheet-like materials 17 of Reference Example 17 as the laminate unit (I) and two CFRTP sheet-like materials 18 of Reference Example 18 as the laminate unit (II). In the same manner as in Example 1, an intermediate substrate was obtained. The properties of the obtained intermediate substrate are shown in Table 3-1.

  A molded product was obtained by molding in the same manner as in Example 1 except that three preforms were laminated to prepare a preform. The obtained molded product was 100% filled in the cavity. The characteristics of the molded product are shown in Table 3-1.

(Comparative Example 7)
Example 1 except that a laminate was prepared using one CFRTP sheet 13 of Reference Example 13 as the laminate unit (I) and one CFRTP sheet of Reference Example 14 as the laminate unit (II). In the same manner, an intermediate substrate was obtained. The properties of the obtained intermediate substrate are shown in Table 3-1.

  A molded product was obtained by molding in the same manner as in Example 1 except that three intermediate substrates were used. The obtained molded product was 84% filled in the cavity. The characteristics of the molded product are shown in Table 3-1.

(Comparative Example 8)
Except that a laminate was prepared using one CFRTP sheet-like material 2 of Reference Example 2 as the lamination unit (I) and two CFRTP sheet-like materials 1 of Reference Example 1 as the lamination unit (II). In the same manner as in Example 1, an intermediate substrate was obtained. The characteristics of the obtained intermediate substrate are shown in Table 3-2.

  A molded product was obtained by molding in the same manner as in Example 1 except that three intermediate substrates were used. The obtained molded product was 86% filled in the cavity. The characteristics of the molded product are shown in Table 3-2.

(Comparative Example 9)
The same procedure as in Example 1 was conducted except that a laminate was prepared using one CFRTP sheet-like material 2 of Reference Example 2 as the laminate unit (I) and five resin sheets 1 as the laminate unit (II). A substrate was obtained. The characteristics of the obtained intermediate substrate are shown in Table 3-2.

  A molded product was obtained by molding in the same manner as in Example 1 except that three intermediate substrates were used. The obtained molded product was 100% filled in the cavity. The characteristics of the molded product are shown in Table 3-2.

(Comparative Example 10)
Example except that a laminate was prepared using one CFRTP sheet-like material 4 of Reference Example 4 as the laminate unit (I) and two CFRTP sheet-like materials 3 of Reference Example 3 as the laminate unit (II). In the same manner as in Example 1, an intermediate substrate was obtained. The characteristics of the obtained intermediate substrate are shown in Table 3-2.

  A molded product was obtained by molding in the same manner as in Example 1 except that two intermediate substrates were used. The obtained molded product was 100% filled in the cavity. The characteristics of the molded product are shown in Table 3-2.

(Comparative Example 11)
Except that a laminate was prepared using one CFRTP sheet 15 of Reference Example 15 as the laminate unit (I) and two CFRTP sheet 1 of Reference Example 1 as the laminate unit (II). In the same manner as in Example 1, an intermediate substrate was obtained. The characteristics of the obtained intermediate substrate are shown in Table 3-2.

  A molded product was obtained by molding in the same manner as in Example 1 except that three intermediate substrates were used. The obtained molded product was 76% filled in the cavity. The characteristics of the molded product are shown in Table 3-2.

(Comparative Example 12)
Except that the laminate was prepared using two CFRTP sheet-like materials 1 of Reference Example 1 as the lamination unit (I) and one CFRTP sheet-like material 16 of Reference Example 16 as the lamination unit (II). In the same manner as in Example 1, an intermediate substrate was obtained. The characteristics of the obtained intermediate substrate are shown in Table 3-2.

  A molded product was obtained by molding in the same manner as in Example 1 except that three intermediate substrates were used. The obtained molded product was 95% filled in the cavity. The characteristics of the molded product are shown in Table 3-2.

(Comparative Example 13)
Except that a laminate was prepared using two CFRTP sheet-like materials 2 of Reference Example 2 as the lamination unit (I) and five CFRTP sheet-like materials 3 of Reference Example 3 as the lamination unit (II). In the same manner as in Example 1, an intermediate substrate was obtained. The characteristics of the obtained intermediate substrate are shown in Table 3-2.

  A molded product was obtained by molding in the same manner as in Example 1 except that one intermediate substrate was used. The obtained molded product was 100% filled in the cavity. The characteristics of the molded product are shown in Table 3-2.

(Comparative Example 14)
Except that a laminate was prepared using 10 CFRTP sheet-like materials 2 of Reference Example 2 as the lamination unit (I) and 1 CFRTP sheet-like material 3 of Reference Example 3 as the lamination unit (II). In the same manner as in Example 1, an intermediate substrate was obtained. The characteristics of the obtained intermediate substrate are shown in Table 3-2.

  A molded product was obtained by molding in the same manner as in Example 1 except that one intermediate substrate was used. The obtained molded product was 89% filled in the cavity. The characteristics of the molded product are shown in Table 3-2.

(Comparative Example 15)
The CFRTP sheet material of Reference Example 21 was used as it was as an intermediate substrate. Table 6 shows the characteristics of the intermediate substrate.

  A molded product was obtained by molding in the same manner as in Example 9 except that 10 preforms of the intermediate substrate were laminated to prepare a preform. The obtained molded product was 92% filled in the cavity. Table 6 shows the characteristics of the molded product.

(Comparative Example 16)
The CFRTP sheet material of Reference Example 22 was used as it was as an intermediate substrate. Table 6 shows the characteristics of the intermediate substrate.

  A molded product was obtained by molding in the same manner as in Example 9 except that a preform was produced by laminating six intermediate substrates. The obtained molded product was 84% filled in the cavity. Table 6 shows the characteristics of the molded product.

(Comparative Example 17)
Example 9 except that a laminate was prepared using one CFRTP sheet-like material of Reference Example 31 as the lamination unit (I) and one CFRTP sheet-like material of Reference Example 32 as the lamination unit (II). Similarly, an intermediate substrate was obtained. The properties of the obtained intermediate substrate are shown in 6.

  A molded product was obtained by molding in the same manner as in Example 9 except that three preforms were laminated to prepare a preform. The obtained molded product was 71% filled in the cavity. Table 6 shows the characteristics of the molded product.

(Comparative Example 18)
Example 9 except that a laminate was prepared using one CFRTP sheet material of Reference Example 33 as the laminate unit (I) and one CFRTP sheet material of Reference Example 34 as the laminate unit (II). Similarly, an intermediate substrate was obtained. The properties of the obtained intermediate substrate are shown in Table 6.

  A molded product was obtained by molding in the same manner as in Example 9 except that three intermediate substrates were used. The obtained molded product was 84% filled in the cavity. Table 6 shows the characteristics of the molded product.

(Comparative Example 19)
Example 9 except that a laminate was prepared using one CFRTP sheet material of Reference Example 22 as the laminate unit (I) and two CFRTP sheet materials of Reference Example 21 as the laminate unit (II). Similarly, an intermediate substrate was obtained. The properties of the obtained intermediate substrate are shown in Table 6.

  A molded product was obtained by molding in the same manner as in Example 9 except that three intermediate substrates were used. The obtained molded product was 86% filled in the cavity. Table 6 shows the characteristics of the molded product.

(Comparative Example 20)
An intermediate group was prepared in the same manner as in Example 9 except that a laminate was produced using one CFRTP sheet-like material of Reference Example 22 as the laminate unit (I) and five resin sheets 7 as the laminate unit (II). I got the material. The properties of the obtained intermediate substrate are shown in Table 6.

  A molded product was obtained by molding in the same manner as in Example 9 except that three intermediate substrates were used. The obtained molded product was 100% filled in the cavity. Table 6 shows the characteristics of the molded product.

(Comparative Example 21)
Example 9 except that a laminate was prepared using one CFRTP sheet-like material of Reference Example 24 as the laminate unit (I) and two CFRTP sheet-like materials of Reference Example 23 as the laminate unit (II). Similarly, an intermediate substrate was obtained. The properties of the obtained intermediate substrate are shown in Table 6.

  A molded product was obtained by molding in the same manner as in Example 9 except that two intermediate substrates were used. The obtained molded product was 100% filled in the cavity. Table 6 shows the characteristics of the molded product.

(Comparative Example 22)
Example 9 except that a laminate was prepared using one CFRTP sheet-like material of Reference Example 35 as the laminate unit (I) and two CFRTP sheet-like materials of Reference Example 21 as the laminate unit (II). Similarly, an intermediate substrate was obtained. The properties of the obtained intermediate substrate are shown in Table 6.

  A molded product was obtained by molding in the same manner as in Example 9 except that three intermediate substrates were used. The obtained molded product was 76% filled in the cavity. Table 6 shows the characteristics of the molded product.

(Comparative Example 23)
Example 9 except that a laminate was prepared using two CFRTP sheet-like materials of Reference Example 22 as the lamination unit (I) and four CFRTP sheet-like materials of Reference Example 23 as the lamination unit (II). Similarly, an intermediate substrate was obtained. The properties of the obtained intermediate substrate are shown in Table 6.

  A molded product was obtained by molding in the same manner as in Example 9 except that one intermediate substrate was used. The obtained molded product was 100% filled in the cavity. Table 6 shows the characteristics of the molded product.

(Comparative Example 24)
Example 9 except that a laminate was prepared using six CFRTP sheet-like materials of Reference Example 22 as the lamination unit (I) and one CFRTP sheet-like material of Reference Example 23 as the lamination unit (II). Similarly, an intermediate substrate was obtained. The properties of the obtained intermediate substrate are shown in Table 6.

  A molded product was obtained by molding in the same manner as in Example 9 except that one intermediate substrate was used. The obtained molded product was 89% filled in the cavity. Table 6 shows the characteristics of the molded product.

  In Examples 2, 7, and 8, as compared with Comparative Examples 1, 13, and 14, the satisfactory effect of improving the shapeability due to the inclusion of the CFRTP sheet material of component (II) is recognized. In addition, the molded product thus obtained has small variations in strength and elastic modulus, and has a high specific strength, so that a molded product excellent in reliability and reinforcing effect can be obtained.

  In Example 7, since the ratio of the component (II) contained in the intermediate base material was larger than the others, the elongation rate (R) was high and the shapeability was particularly excellent. In Example 6, since the proportion of the constituent element (II) was smaller than the others, variations in strength and elastic modulus were small, and a highly reliable molded product was obtained. In Comparative Example 13, since the proportion of the constituent element (II) contained in the intermediate base material is too large, the shapeability is excellent, but the strength and the elastic modulus in the molded product vary greatly. Low. On the contrary, in Comparative Example 14, since the proportion of the constituent element (II) contained in the intermediate base material was too small, the effect of improving the shapeability by containing the constituent element (II) was hardly seen.

  Next, when Examples 1, 5, 6 and Comparative Example 2 are compared, the elongation rate (R) increases due to the inclusion of the CFRTP sheet material of component (II) at any level. It can be seen that the shape is improved. In Example 5, since the aspect ratios of the constituent elements (I) and (II) were moderately small, the effect of improving the formability was excellent as compared with Example 1. In Example 6, since the aspect ratios of the constituent elements (I) and (II) are large, the reliability of the molded product is high and the reinforcing effect is excellent as compared with Example 1.

  On the other hand, for Comparative Examples 5, 6, 7, 8, and 9, which are the same VfI and VfII as Example 1, and VI and VII, Comparative Example 5 has the aspect ratios of the components (I) and (II). Since it was too large, the formability was greatly reduced. In Comparative Example 6, since the aspect ratios of the constituent elements (I) and (II) were too small, the shapeability was excellent, but the specific strength and reliability of the molded product were reduced. Since Comparative Example 7 has a larger aspect ratio than Comparative Example 6, recovery in specific strength and reliability of the molded product can be seen, but it remains a low aspect ratio and is a satisfactory molded product. Was not obtained. In Comparative Example 8, VfII of the component (II) was too large, so that the effect of improving the shapeability by including the component (II) was not seen. On the contrary, in Comparative Example 9, since VfII of the component (II) was too small, a molded product satisfying the specific strength and reliability of the molded product could not be obtained.

  Further, regarding Comparative Examples 10, 11, and 12, since VfI was too small in Comparative Example 10, the reliability of the molded product was impaired. On the contrary, in Comparative Example 11, VfI was too large, so that the elongation rate was lowered and satisfactory shapeability could not be expressed. In Comparative Example 12, VfI and VfII were too close to each other, so that the effect of improving the shapeability by including the component (II) was not recognized.

  In Examples 3 and 4, a high Vf CFRTP sheet is used as the component (I), but in Examples 3 and 4, VfI is in an appropriate range, so that the effect of improving formability is achieved. Was recognized.

  For each of Comparative Examples 3 and 4, since the reinforcing fibers are dispersed in a bundle, a single fiber network is not formed, and the shapeability is excellent, but the localization of the reinforcing fibers accompanying press molding and Due to the orientation, the reliability of the molded product was low. Further, since the reinforcing fibers are dispersed in a bundle shape, the reinforcing effect of the molded product is inferior.

  Even in the case where a polyamide resin is used as the matrix resin, in Examples 9 to 16 in which VfI and VfII are in an appropriate range in the same manner as described above, compared with Comparative Examples 15 to 24 in which VfI and VfII are not in an appropriate range. In addition, it was possible to obtain a molded product having improved formability, specific strength of the molded product and excellent reliability, and the effects of the present invention were sufficiently recognized. Furthermore, the strength and elastic modulus of the matrix resin itself were reflected, and a molded product having a high absolute value of bending strength and elastic modulus could be obtained.

  According to the intermediate substrate for press molding of the present invention, excellent formability is expressed in press molding. Moreover, since the molded product by this has high reliability and a reinforcement effect, it can apply to wide uses, such as a vehicle interior / exterior, a housing | casing of an electric / electronic device, a bicycle, an aircraft interior material, and a transport box.

1, 2, 3, 4, 5, 6, 7, 8 Single fiber 9 Two-dimensional contact angle, two-dimensional orientation angle 10, 16, 19, 22, 23, 24, 25, 26, 27 Intermediate substrate for press molding 11, 12, 13, 14, 17, 18, 20, 21, 28, 29 Fiber reinforced thermoplastic resin sheet 15 Engagement portion 30 Molded product 31, 33 Top plate portion 32 Bending test piece

Claims (11)

An intermediate base material in which discontinuous reinforcing fibers are monofilamentally and randomly distributed in a thermoplastic resin, wherein the following constituent elements (I) and (II) are laminated together, and the constituent elements (I ) And (II) with respect to the total amount of component (II) is 30 to 70% by volume, and the aspect ratio of the reinforcing fiber in each of the following components (I) and (II) is 250 or more and 1000 or less And the following VfI and VfII satisfy | fill 0.8VfI> VfII, and the thickness of the component (II) of an intermediate base material is in the range of 0.1 mm or more and less than 5.0 mm, The intermediate substrate for press molding.
(I) Fiber reinforced thermoplastic resin sheet having a reinforcing fiber ratio VfI of 15% by volume to 40% by volume (II) Fiber reinforced thermoplastic resin having a reinforcing fiber ratio VfII of 5% by volume to less than 15% by volume Resin sheet The intermediate substrate for press molding according to claim 1, wherein a ratio of the component (II) to the total amount of the components (I) and (II) in the intermediate substrate is 40 to 60% by volume. The intermediate substrate for press molding according to claim 1 or 2, wherein an average aspect ratio of the discontinuous reinforcing fibers constituting the constituent elements (I) and (II) is 400 or more and 800 or less. The intermediate substrate for press molding according to any one of claims 1 to 3, wherein a proportion VfI of reinforcing fibers of the component (I) is 20% by volume or more and 30% by volume or less. The intermediate substrate for press molding according to any one of claims 1 to 4, wherein a ratio Vf of reinforcing fibers in the intermediate substrate for press molding is 10 vol% or more and 30 vol% or less. The intermediate substrate for press molding according to any one of claims 1 to 5, wherein the reinforcing fibers constituting the constituent elements (I) and (II) are carbon fibers. The thermoplastic resin constituting the constituent elements (I) and (II) comprises at least one selected from the group consisting of polyolefin, polyamide, polyarylene sulfide, and polyetheretherketone. An intermediate substrate for press molding according to claim 1. A preform for press molding in which a plurality of intermediate substrates for press molding according to any one of claims 1 to 7 are laminated. Molding, wherein the intermediate substrate for press molding according to any one of claims 1 to 7 or the preform according to claim 8 is placed in a mold cavity at a charge rate of 50% or more and less than 100%, and then press molding is performed. Product manufacturing method. The method for producing a molded product according to claim 9, wherein the press molding means is stamping molding or heat and cool molding. The method for producing a molded product according to claim 9 or 10, wherein the molded product is used as an automobile interior / exterior, an electric / electronic device casing, a bicycle, an aircraft interior material, or a transport box.