WO2014162789A1 - 複合材軽量継手 - Google Patents

複合材軽量継手 Download PDF

Info

Publication number
WO2014162789A1
WO2014162789A1 PCT/JP2014/053861 JP2014053861W WO2014162789A1 WO 2014162789 A1 WO2014162789 A1 WO 2014162789A1 JP 2014053861 W JP2014053861 W JP 2014053861W WO 2014162789 A1 WO2014162789 A1 WO 2014162789A1
Authority
WO
WIPO (PCT)
Prior art keywords
reinforcing fiber
joint
composite material
reinforcing
fiber bundle
Prior art date
Application number
PCT/JP2014/053861
Other languages
English (en)
French (fr)
Inventor
俊 開米
石橋　正康
広川　哲朗
田那村　武司
Original Assignee
シキボウ株式会社
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by シキボウ株式会社 filed Critical シキボウ株式会社
Priority to BR112015024786A priority Critical patent/BR112015024786A2/pt
Priority to CN201480019571.8A priority patent/CN105102829B/zh
Priority to EP14779598.3A priority patent/EP2982871A4/en
Priority to CA2912250A priority patent/CA2912250A1/en
Priority to US14/779,594 priority patent/US20160052233A1/en
Publication of WO2014162789A1 publication Critical patent/WO2014162789A1/ja

Links

Images

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/304—In-plane lamination by juxtaposing or interleaving of plies, e.g. scarf joining
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06—Fibrous reinforcements only
    • B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • B29C70/347—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation combined with compressing after the winding of lay-ups having a non-circular cross-section, e.g. flat spiral windings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/545—Perforating, cutting or machining during or after moulding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/04—Reinforcing macromolecular compounds with loose or coherent fibrous material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2793/00—Shaping techniques involving a cutting or machining operation
    • B29C2793/0045—Perforating
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
    • B29K2105/10—Cords, strands or rovings, e.g. oriented cords, strands or rovings
    • B29K2105/101—Oriented
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2009/00—Layered products
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/737—Articles provided with holes, e.g. grids, sieves
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/02—Composition of the impregnated, bonded or embedded layer
    • B32B2260/021—Fibrous or filamentary layer
    • B32B2260/023—Two or more layers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/04—Impregnation, embedding, or binder material
    • B32B2260/046—Synthetic resin
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form
    • B32B3/26—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
    • B32B3/266—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by an apertured layer, the apertures going through the whole thickness of the layer, e.g. expanded metal, perforated layer, slit layer regular cells B32B3/12
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/02—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
    • Y10T428/24074—Strand or strand-portions
    • Y10T428/24083—Nonlinear strands or strand-portions
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24273—Structurally defined web or sheet [e.g., overall dimension, etc.] including aperture
    • Y10T428/24322—Composite web or sheet

Definitions

  • the present invention relates to a composite lightweight joint formed of a composite material obtained by impregnating and curing a matrix in a laminate in which a plurality of reinforcing fiber layers are laminated.
  • the joint is used to connect a plurality of members, and is used in various places such as transportation equipment such as airplanes and automobiles and buildings such as buildings and bridges.
  • bolts 110 are respectively inserted into the pair of through holes 101 and the through holes of the members A and B provided at both ends of the joint 100.
  • the nut 111 is screwed to the tip of the bolt 110.
  • stress in the tensile direction is applied to the joint 100 (see the arrow in FIG. 6B)
  • the end side region 102 (the region indicated by the dotted points) of the through hole 101 of the joint 100 is connected via the bolt 110.
  • a large stress is applied. For this reason, it is important to increase the strength of the periphery of the through hole 101 of the joint 100, particularly the end side region 102.
  • a plurality of reinforcing fiber layers made of reinforcing fibers aligned in a predetermined direction are laminated, and this laminate is impregnated with a matrix such as a resin and cured.
  • a composite lightweight joint formed of a composite material is known. Since the composite lightweight joint has a high strength per unit weight (specific strength), it is particularly suitable for a joint for transport equipment (particularly, one that moves or rotates at high speed) that requires weight reduction.
  • the composite lightweight joint is formed by laminating reinforcing fiber layers 103a to 103d having different fiber orientation directions, for example, as shown in FIG.
  • Forming a through hole 101 by forming a composite material by impregnating and solidifying a matrix in which the reinforcing fiber layers 103a to 103d are laminated, and then drilling the composite material with a drill or the like. Can do.
  • the reinforcing fibers of all the reinforcing fiber layers 103a to 103d are cut by the drilling process, the strength around the through hole 101 of the joint 100, particularly the tensile strength of the end region 102 is reduced. End up.
  • the reinforcing fiber layer 103b (see FIG. 7B) in which fibers are oriented in the direction in which the stress is applied should transmit this stress.
  • the fiber since the fiber is divided by the through hole 101, stress cannot be transmitted only by the reinforcing fiber layer 103b. Accordingly, the stress must be transmitted in cooperation with the other reinforcing fiber layers, and the reinforcing fiber layers may be separated from each other due to the tensile stress, thereby reducing the strength of the joint.
  • Patent Document 1 shows a joint in which fibers are arranged in an arc along the periphery of a through hole.
  • the fiber curved in the arc shape is not cut by the formation of the through hole. And since it is possible to transmit the tensile stress applied to the joint without cooperating with the other reinforcing fiber layers by the reinforcing fiber layer having the fibers curved in the arc shape, Peeling is prevented.
  • the strength of the joint particularly the strength around the through hole can be increased.
  • FIG. 8 shows a reinforcing fiber layer 200 in which a band-shaped reinforcing fiber bundle 201 is arranged along the periphery of the through hole 210.
  • the circumferential length is different between the inner periphery and the outer periphery of the fiber bundle 201.
  • the diameter of the through hole 210 decreases, as shown in FIG.
  • the resin 202 enters and hardens in the portion where the reinforcing fiber 201b on the inner peripheral side is waved and lifted.
  • Matrix such as resin is much lower in strength than reinforced fiber, so if many parts (resin rich part) made of almost resin alone are formed inside the composite material, the strength of the joint will decrease. End up. In particular, as shown in FIG.
  • the tensile strength of the reinforced wave 201b and the amount of the resin portion 202 that enters the waved part of the reinforced fiber 201b are as follows. It varies from product to product. For this reason, the strength of the joint varies greatly from product to product.
  • each reinforcing fiber bundle For example, if the width of each reinforcing fiber bundle is reduced, the difference between the inner peripheral length and the outer peripheral length in the round portion is reduced, and the waviness of the inner peripheral fibers can be suppressed. However, if the width of each fiber bundle is reduced, the number of fibers constituting each fiber bundle is reduced. Therefore, it is necessary to increase the number of fiber bundles in order to secure the total number of fibers, and the number of steps for supplying the fiber bundles increases. Productivity.
  • the problem to be solved by the present invention is to reduce the cost and weight of the composite lightweight joint by suppressing the decrease in strength and dispersion of the composite lightweight joint without reducing the productivity.
  • the composite lightweight joint according to the present invention which has been made to solve the above problems, is composed of a composite material obtained by impregnating and curing a matrix in a laminate in which a plurality of reinforcing fiber layers are laminated, and the thickness direction of the reinforcing fiber layers
  • a light-weight composite joint having a through-hole penetrating through the at least one of the plurality of reinforcing fiber layers, wherein a plurality of reinforcing fibers are arranged in a band shape around the through-hole.
  • a reinforcing fiber bundle having a round part along the line is provided, and the round part of the reinforcing fiber bundle is twisted.
  • the matrix that enters the raised portion is reduced, so that the matrix rich portion in the composite material, particularly the matrix rich portion in the end side region of the joint It is possible to suppress the formation and prevent the fixing accuracy of the joint from being lowered due to the destruction of the matrix. Furthermore, since the state of the fiber for each product can be stabilized by suppressing the undulation of the fiber, variation in strength between products can be suppressed.
  • the production of the joint can be facilitated by twisting the entire reinforcing fiber bundle, that is, by twisting not only the round part but also the straight part.
  • the fiber orientation direction Q is inclined with respect to the direction P in which tensile stress is applied to the reinforcing fiber bundle, so that the tensile strength of the joint is lowered. .
  • twisting the reinforcing fiber bundle has been regarded as a taboo.
  • the composite material lightweight joint according to the present invention since the undulation of the reinforcing fiber in the inner periphery of the round portion can be suppressed, the decrease and variation in joint strength due to this can be suppressed, and the use of the reinforcing fiber can be suppressed.
  • the amount can be reduced to reduce cost and weight.
  • FIG. 3 is an enlarged plan view of a reinforcing fiber layer shown in FIG.
  • FIG. 4 is an enlarged plan view around a through hole in FIG. 3.
  • FIG. 9 is an enlarged plan view around the through hole in FIG. 8.
  • the composite light weight joint 1 (hereinafter also simply referred to as a joint 1) has a cylindrical through hole 2 for inserting a pin (for example, a bolt) as shown in FIG.
  • the joint 1 includes a plurality of reinforcing fiber layers 3 formed by aligning reinforcing fibers, and a matrix (not shown) impregnated and cured in a laminate in which the plurality of reinforcing fiber layers 3 are stacked.
  • the reinforcing fiber for example, carbon fiber, glass fiber, ceramic fiber or the like is used.
  • the matrix for example, a resin (organic substance) or an inorganic substance is used.
  • the reinforcing fiber layer 3 is formed by arranging a plurality of reinforcing fiber bundles in which a large number of fibers are arranged in a band shape in a single sheet shape.
  • the joint 1 has a plurality of types of reinforcing fiber layers 3 having different fiber orientation directions, and the fiber orientation directions of adjacent reinforcing fiber layers 3 intersect each other.
  • the fibers are in the 0 ° direction and the round direction.
  • Reinforced fiber layer 3a see FIG. 2 (a)
  • reinforced fiber layer 3b see FIG.
  • the reinforcing fiber layer 3 a in which fibers are oriented in the 0 ° direction + round direction shown in FIG. 2A is along the periphery of the through hole 2 as shown in an enlarged view in FIG. 3.
  • the reinforcing fiber bundle 4 having the round part 4a and the straight part 4b, and the reinforcing fiber bundle 5 including only the straight part are provided.
  • the reinforcing fiber bundle 4 at least the round part 4a is twisted.
  • the band-shaped reinforcing fiber bundle 4 is twisted by about 180 ° in the round part 4a, and the narrowest part (referred to as the narrow part 6) in plan view is within the range of the round part 4a (in the illustrated example, the round part is round). Near the center of the portion 4a).
  • the inner peripheral fiber and the outer peripheral fiber of the round part 4a are interchanged.
  • the reinforcing fibers 4 a 1 arranged on the outer peripheral side at one end portion C (left end portion in FIG. 4) in the circumferential direction of the round portion 4 a of each reinforcing fiber bundle 4 are round. It arrange
  • the reinforcing fiber 4a2 (shown by a thick line) arranged on the inner peripheral side at the end portion C on one side in the circumferential direction of the round portion 4a of each reinforcing fiber bundle 4 is an end portion D on the other side in the circumferential direction of the round portion 4a. In the outer peripheral side.
  • the fiber length difference between the two reinforcing fibers 4a1 and 4a2 is reduced by switching the fibers on the inner circumferential side and the fibers on the outer circumferential side from the center in the width direction of the round portion 4a of the reinforcing fiber bundle 4.
  • the fiber length difference between the two reinforcing fibers 4a1 and 4a2 is substantially canceled by replacing the fibers on the inner circumferential side and the fibers on the outer circumferential side from the center in the width direction of the reinforcing fiber bundle 4 at both circumferential ends of the round part 4a.
  • the fiber lengths of all the fibers constituting the round portion 4a are approximately equal, and the undulation of the fibers on the inner peripheral side is suppressed. Accordingly, the inner peripheral side fibers can effectively contribute to the strength of the joint 1 as a whole, so that the strength of the joint 1 is improved.
  • the undulation of the fibers is suppressed, the matrix entering the portion where the fibers are undulated and lifted is suppressed, so that formation of a matrix rich portion inside the composite material is suppressed, and the strength of the joint 1 is further improved. In particular, as shown in FIG.
  • the corrugation of the inner peripheral fiber of the round portion 4a is more likely to occur as the radius r of the through hole 2 of the joint 1 is smaller and as the width w of the reinforcing fiber bundle 4 is larger. Therefore, as the ratio (w / r) of the width w of the reinforcing fiber bundle 4 to the radius r of the through hole 2 is larger, it becomes more effective to twist the round portion 4a as described above. Specifically, for example, when w / r is 0.1 or more, particularly 0.3 or more, it is extremely effective to twist the round portion.
  • the width w of the reinforcing fiber bundle is about 3 to 5 mm and the radius r of the through hole 2 is 30 mm or less, particularly 20 mm or less, further 10 mm or less, it is particularly effective to twist the round part. Become.
  • the reinforcing fiber bundle 4 may be twisted in advance at a predetermined pitch, and the reinforcing fiber bundle 4 may be arranged along the periphery of the through hole 2. At this time, if the twisting pitch of the reinforcing fiber bundle 4 (that is, the pitch of the narrow portion 6) is made equal to the circumferential length L of the round portion 4a, one narrow portion 6 is arranged in the round portion 4a. Can do.
  • the orientation direction Q of each fiber is inclined with respect to the direction P (0 ° direction) in which a tensile load is applied to the reinforcing fiber bundle 4, so that the tensile strength of the joint 1 is lowered.
  • the effect of improving the strength and suppressing the variation by twisting the round portion 4a and suppressing the undulation of the fiber on the inner peripheral side is greater than the strength reduction caused by twisting the reinforcing fiber bundle 4. The strength of the whole 1 can be increased.
  • the method of twisting the round part 4a is not limited to the above.
  • the round part 4 a may be twisted by twisting the reinforcing fiber bundle 4 while being arranged along the periphery of the through hole 2.
  • the above-described composite lightweight joint 1 can be used, for example, as a joint 100 for connecting a plurality of separately formed members A and B as shown in FIG.
  • at least the region facing the through hole 101 in the radial direction on the outer peripheral surface of the pin may be a cylindrical surface in order to increase the contact area with the through hole 101.
  • said composite material lightweight joint 1 can also be used as a joint which is provided in one member A integrally, and connects with the other member B through a pin.
  • the pin inserted into the through hole 2 may be one that fixes the joint 1 and the other member (fixed joint), or allows relative rotation around the pin of the joint 1 and the other member. A thing (rotary joint) may be sufficient.
  • the present invention is not limited to this, and the reinforcing fiber bundle 4a may be twisted in the round part 4a.
  • the effect of reducing the difference in fiber length can be obtained. For example, you may make it reduce the difference of the length of each reinforced fiber which comprises the round part 4a by twisting the round part 4a of the reinforcing fiber bundle 4 several times (greater than 180 degrees).
  • the composite material lightweight joint 1 as described above can be used for transportation equipment such as airplanes and automobiles, and buildings such as buildings and bridges.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Composite Materials (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Materials Engineering (AREA)
  • Health & Medical Sciences (AREA)
  • Manufacturing & Machinery (AREA)
  • Medicinal Chemistry (AREA)
  • Polymers & Plastics (AREA)
  • Organic Chemistry (AREA)
  • Moulding By Coating Moulds (AREA)
  • Connection Of Plates (AREA)
  • Laminated Bodies (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Reinforced Plastic Materials (AREA)

Abstract

　本発明の複合材軽量継手は、複数の強化繊維層３のうちの少なくとも一つの強化繊維層３ａが、多数の強化繊維を帯状に引き揃えてなり、貫通穴２の周囲に沿ったラウンド部４ａを有する強化繊維束４を備え、強化繊維束４のラウンド部４ａに撚りをかけたものである。

Description

複合材軽量継手
　本発明は、複数の強化繊維層を積層した積層体にマトリクスを含浸・硬化させた複合材で形成された複合材軽量継手に関する。
　継手は、複数の部材を連結するために用いられるものであり、例えば航空機、自動車等の輸送機器や、建物、橋梁等の建築物など、様々な箇所に使用される。例えば図６に示すように、部材Ａと部材Ｂとを継手１００を用いて連結する場合、継手１００の両端に設けられた一対の貫通穴１０１及び部材Ａ，Ｂの貫通穴にそれぞれボルト１１０を挿通し、このボルト１１０の先端にナット１１１をネジ固定する。この継手１００に対し、引張方向の応力が加わると（図６（ｂ）の矢印参照）、ボルト１１０を介して、継手１００の貫通穴１０１の端部側領域１０２（散点で示す領域）に大きな応力が加わる。このため、継手１００の貫通穴１０１の周囲、特に端部側領域１０２の強度を高めることが重要となる。　
　ところで、継手の一種として、所定方向に引き揃えた強化繊維（以下、単に「繊維」とも言う。）からなる複数の強化繊維層を積層し、この積層体に樹脂等のマトリクスを含浸・硬化させてなる複合材で形成された複合材軽量継手が知られている。複合材軽量継手は、単位重量当たりの強度（比強度）が高いため、軽量化が要求される航空機等の輸送機器用（特に、高速で移動あるいは回転するもの）の継手に特に適している。
　複合材軽量継手は、例えば図７に示すように、繊維配向方向の異なる強化繊維層１０３ａ～１０３ｄを積層して形成される。このような強化繊維層１０３ａ～１０３ｄを積層した積層体にマトリクスを含浸固化させて複合材を形成した後、この複合材にドリル等で穴開け加工を施すことにより、貫通穴１０１を形成することができる。しかし、この場合、穴開け加工により全ての強化繊維層１０３ａ～１０３ｄの強化繊維が切断されるため、継手１００の貫通穴１０１の周囲の強度、特に端部側領域１０２の引張強度が低下してしまう。具体的に、上記のような継手に引張方向の応力が加わった場合、応力が加わる方向に繊維を配向させた強化繊維層１０３ｂ（図７（ｂ）参照）がこの応力を伝達すべきであるが、繊維が貫通穴１０１で分断されているため、この強化繊維層１０３ｂだけでは応力を伝達することができない。従って、他の強化繊維層と協働して応力を伝達せざるを得ず、引張応力により強化繊維層同士が剥離して継手の強度が低下する恐れがある。
　例えば特許文献１には、貫通穴の周囲に沿って繊維を円弧状に配した継手が示されている。この円弧状に湾曲した繊維は、貫通穴の形成により切断されない。そして、この円弧状に湾曲した繊維を有する強化繊維層単独で、他の強化繊維層と協働することなく、継手に加わる引張応力を伝達することができるため、引張応力による強化繊維層同士の剥離が防止される。以上より、継手の強度、特に貫通穴の周囲の強度を高めることができる。
特公平７－８１２２５号公報
　しかし、上記特許文献１のように、貫通穴の周囲に沿って強化繊維を円弧状に配した複合材軽量継手は、必要とされる性能が得られず、現在のところ実用化には至っていない。その原因は、以下のようなことにあると考えられる。
　強化繊維層を形成する場合には、通常、多数の強化繊維（フィラメント）を帯状に引き揃えた強化繊維束（トウ）が用いられる。図８は、帯状の強化繊維束２０１を貫通穴２１０の周囲に沿って配した強化繊維層２００を示す。この場合、各強化繊維束２０１のうち、貫通穴２１０の周囲に沿って円弧状に湾曲したラウンド部２０１ａでは、繊維束２０１の内周と外周とで周方向長さが異なる。特に、貫通穴２１０の径が小さくなると、図９に示すように、各強化繊維束２０１のラウンド部２０１ａの内周長Ｌ１と外周長Ｌ２との比（Ｌ２／Ｌ１）が大きくなる。このため、内周側の強化繊維２０１ｂが波打って繊維層の積層方向（図９の紙面直交方向）に浮き上がってしまう。このように波打った強化繊維は継手の強度にほとんど寄与しないため、継手の強度低下を招く。
　また、上記のような強化繊維層を含む積層体に樹脂等のマトリクスを含浸させると、内周側の強化繊維２０１ｂが波打って浮き上がった部分に樹脂２０２（散点で示す）が入り込んで硬化する。樹脂等のマトリクスは強化繊維と比べてはるかに強度が低いため、複合材の内部において、ほぼ樹脂のみで形成された部分（樹脂リッチ部）が多く形成されると、継手の強度が低下してしまう。特に、図９に示すように、貫通穴２１０に樹脂２０２が多く露出していると、貫通穴２１０に挿通されたピン（ボルト等、図示省略）が樹脂２０２と直接接触するため、ピンから受ける負荷によって樹脂２０２が破壊されやすい。このように、樹脂リッチ部が破壊されると、ピンと貫通穴２１０との軸心位置がずれて、継手の強度が低下してしまう。
　また、上記のような内周側の強化繊維２０１ｂの波打ち具合は製品ごとに異なるため、波打った強化繊維２０１ｂの引張強度や、強化繊維２０１ｂが波打った部分に入り込む樹脂部２０２の量は製品ごとにばらつく。このため、継手の強度は製品ごとに大きくばらつくことになる。
　以上のように、継手の強度の低下やばらつきが生じると、強化繊維の使用量を増やして強度を確保する必要があるため、コスト高を招く上、軽量化を達成することができない。　
　例えば、各強化繊維束の幅を小さくすれば、ラウンド部における内周長と外周長との差が小さくなり、内周の繊維の波打ちを抑えることができる。しかし、各繊維束の幅を小さくすると、各繊維束を構成する繊維本数が減じられるため、繊維の総数を確保するために繊維束の数を増やす必要が生じ、繊維束を供給する工数が増えて生産性が低下する。
　本発明が解決すべき課題は、生産性を低下させることなく、複合材軽量継手の強度の低下やばらつきを抑え、低コスト化及び軽量化を図ることにある。
　前記課題を解決するためになされた本発明に係る複合材軽量継手は、複数の強化繊維層を積層した積層体にマトリクスを含浸・硬化させた複合材からなり、前記強化繊維層の厚さ方向に貫通する貫通穴を有する複合材軽量継手であって、前記複数の強化繊維層のうちの少なくとも一つの強化繊維層が、多数の強化繊維を帯状に引き揃えてなり、前記貫通穴の周囲に沿ったラウンド部を有する強化繊維束を備え、前記強化繊維束のラウンド部に撚りをかけたものである。
　このように、貫通穴の周囲に沿って配される強化繊維束のラウンド部に撚りをかけることにより、ラウンド部の内周側の繊維と外周側の繊維とが入れ替わるため、ラウンド部の繊維を平行に引き揃えた場合と比べて、ラウンド部の内外周長差に起因した繊維長の差を小さくことができる。これにより、ラウンド部の内周側の繊維が波打って浮き上がる事態が抑えられ、貫通穴の周囲（端部側領域）における継手の強度が向上する。また、内周側の繊維の波打ちによる浮き上がりが抑えられることで、浮き上がった部分に入り込むマトリクスが低減されるため、複合材中におけるマトリクスリッチ部、特に、継手の端部側領域におけるマトリクスリッチ部の形成を抑え、マトリクスの破壊に伴う継手の固定精度の低下を防止できる。さらに、繊維の波打ちを抑えることで、製品ごとの繊維の状態を安定させることができるため、製品ごとの強度のばらつきを抑えることができる。
　上記のラウンド部を有する強化繊維束が、さらに直線部を有する場合、ラウンド部のみに撚りをかけることは難しい。そこで、強化繊維束全体に撚りをかけることで、すなわち、ラウンド部だけでなく直線部にも撚りをかけることで、継手の製造を容易化できる。このように強化繊維束に撚りをかけると、図５に示すように、強化繊維束に引張応力が加わる方向Ｐに対して、繊維の配向方向Ｑが傾斜するため、継手の引張強度が低下する。このため、従来、強化繊維束に撚りをかけることはタブー視されていた。しかし、ラウンド部を有する強化繊維束については、強化繊維束に撚りをかけることによる強度の低下よりも、ラウンド部に撚りをかけて内周側の繊維の波打ちを抑えることによる強度の向上やばらつき抑制の効果が大きいため、継手全体の強度を高めることができる。
　以上のように、本発明に係る複合材軽量継手によれば、ラウンド部の内周における強化繊維の波打ちが抑えられるため、これに起因した継手強度の低下やばらつきが抑えられ、強化繊維の使用量を低減して低コスト化及び軽量化を図ることができる。
本発明の一実施形態に係る複合材軽量継手の平面図である。 上記複合材軽量継手の断面図である。 上記複合材軽量継手を構成する強化繊維層の平面図である。 上記複合材軽量継手を構成する強化繊維層の平面図である。 上記複合材軽量継手を構成する強化繊維層の平面図である。 上記複合材軽量継手を構成する強化繊維層の平面図である。 上記複合材軽量継手を構成する強化繊維層の平面図である。 図２（ａ）に示す強化繊維層の拡大平面図である。 図３の貫通穴周辺の拡大平面図である。 強化繊維束に撚りをかけた状態を示す平面図である。 従来の継手の断面図である。 上記従来の継手の平面図である。 従来の複合材軽量継手を構成する強化繊維層の平面図である。 従来の複合材軽量継手を構成する強化繊維層の平面図である。 従来の複合材軽量継手を構成する強化繊維層の平面図である。 従来の複合材軽量継手を構成する強化繊維層の平面図である。 ラウンド部を有する強化繊維束を含む強化繊維層の平面図である。 図８の貫通穴周辺の拡大平面図である。
　以下、本発明の実施形態を図面に基づいて説明する。
　本実施形態に係る複合材軽量継手１（以下、単に継手１とも言う）は、図１に示すように、ピン（例えばボルト）を挿通するための円筒面状の貫通穴２を有する。継手１は、強化繊維を引き揃えてなる複数の強化繊維層３と、複数の強化繊維層３を積層した積層体に含浸・硬化されたマトリクス（図示省略）とからなる。強化繊維としては、例えば炭素繊維、ガラス繊維、セラミックス繊維等が使用される。マトリクスとしては、例えば樹脂（有機物）や無機物等が使用される。
　強化繊維層３は、多数の繊維を帯状に引き揃えてなる複数の強化繊維束を、一枚のシート状に並べて形成される。継手１は、繊維の配向方向の異なる複数種の強化繊維層３を有し、隣り合う強化繊維層３の繊維配向方向は交差している。本実施形態では、継手１に引張荷重が加わる方向（図２の左右方向）を０°方向とし、貫通穴２の周囲に沿った方向をラウンド方向としたとき、０°方向及びラウンド方向に繊維を配向させた強化繊維層３ａ（図２（ａ）参照）、４５°方向に繊維を配向させた強化繊維層３ｂ（図２（ｂ）参照）、０°方向に繊維を配向させた強化繊維層３ｃ（図２（ｃ）参照）、１３５°方向に繊維を配向させた強化繊維層３ｄ（図２（ｄ）参照）、９０°方向に繊維を配向させた強化繊維層３ｅ（図２（ｅ）参照）の順に積層される。
　各強化繊維層３のうち、図２（ａ）に示す０°方向＋ラウンド方向に繊維を配向させた強化繊維層３ａは、図３に拡大して示すように、貫通穴２の周囲に沿って配されたラウンド部４ａ及び直線部４ｂを有する強化繊維束４と、直線部のみからなる強化繊維束５とを備える。強化繊維束４のうち、少なくともラウンド部４ａには撚りがかかっている。図示例では、帯状の強化繊維束４がラウンド部４ａにおいて約１８０°捩られており、平面視で最も細くなる部分（幅狭部６と言う）がラウンド部４ａの範囲内（図示例ではラウンド部４ａの中央部付近）に配されている。
　このように、強化繊維束４のラウンド部４ａに撚りをかけることで、ラウンド部４ａの内周の繊維と外周の繊維とが入れ替わる。具体的には、図４に示すように、各強化繊維束４のラウンド部４ａの周方向一方の端部Ｃ（図４の左側端部）において外周側に配された強化繊維４ａ１は、ラウンド部４ａの周方向他方側の端部Ｄ（図４の右側端部）において内周側に配される。一方、各強化繊維束４のラウンド部４ａの周方向一方側の端部Ｃにおいて内周側に配された強化繊維４ａ２（太線で示す）は、ラウンド部４ａの周方向他方側の端部Ｄにおいて外周側に配される。このように、強化繊維束４のラウンド部４ａの幅方向中央より内周側の繊維と外周側の繊維とが入れ替わることで、両強化繊維４ａ１，４ａ２の繊維長差が小さくなる。特に、ラウンド部４ａの周方向両端において、強化繊維束４の幅方向中央より内周側の繊維と外周側の繊維とが入れ替わることで、両強化繊維４ａ１，４ａ２の繊維長差がほぼ相殺される。
　これにより、ラウンド部４ａを構成する全ての繊維の繊維長がおおよそ等しくなり、内周側の繊維の波打ちが抑えられる。従って、内周側の繊維が継手１全体の強度に有効に寄与することができるため、継手１の強度が向上する。また、繊維の波打ちが抑えられることで、繊維が波打って浮き上がった部分に入り込むマトリクスが抑えられるため、複合材の内部におけるマトリクスリッチ部の形成が抑えられ、継手１の強度がさらに向上する。特に、図４に示すように、貫通穴２に面する部分、すなわち貫通穴２に挿入されるピンと直接接触する部分におけるマトリクスリッチ部の形成が抑えられるため、マトリクスの破壊による継手の強度低下を防止できる。さらに、ラウンド部４ａの内周側の繊維の波打ちを抑えることで、製品ごとの繊維の状態を安定させることができ、製品ごとの強度のばらつきが抑えられる。
　また、ラウンド部４ａの内周の繊維の波打ちは、継手１の貫通穴２の半径ｒが小さいほど、また、強化繊維束４の幅ｗが大きいほど生じやすい。従って、貫通穴２の半径ｒに対する強化繊維束４の幅ｗの比（ｗ／ｒ）が大きいほど、上記のようにラウンド部４ａに撚りをかけることが有効となる。具体的には、例えばｗ／ｒが０．１以上、特に０．３以上の場合、ラウンド部に撚りをかけることが極めて有効となる。例えば、強化繊維束の幅ｗを３～５ｍｍ程度であり、貫通穴２の半径ｒが３０ｍｍ以下、特に２０ｍｍ以下、さらには１０ｍｍ以下である場合に、ラウンド部に撚りをかけることが特に有効となる。
　ラウンド部４ａに撚りをかけるためには、例えば、強化繊維束４に予め所定ピッチで撚りをかけておき、この強化繊維束４を貫通穴２の周囲に沿って配すればよい。このとき、強化繊維束４の撚りのピッチ（すなわち幅狭部６のピッチ）を、ラウンド部４ａの周長Ｌと等しくしておけば、ラウンド部４ａに一つの幅狭部６を配することができる。
　このように、強化繊維束４に所定ピッチで撚りをかけると、ラウンド部４ａだけでなく、直線部４ｂにも撚りが生じる。この場合、図５に示すように、強化繊維束４に引張荷重が加わる方向Ｐ（０°方向）に対して各繊維の配向方向Ｑが傾斜するため、継手１の引張強度が低下する。しかし、強化繊維束４に撚りをかけることによる強度の低下よりも、ラウンド部４ａに撚りをかけて内周側の繊維の波打ちを抑えることによる強度の向上やばらつき抑制の効果が大きいため、継手１全体の強度を高めることができる。
　ラウンド部４ａに撚りをかける方法は上記に限られない。例えば、強化繊維束４を貫通穴２の周囲に沿って配しながら捩ることにより、ラウンド部４ａに撚りをかけてもよい。　
　上記の複合材軽量継手１は、例えば、図６に示すような別個に形成された複数の部材Ａ，Ｂを接続する継手１００として使用できる。このとき、図示のように、ピン（ボルト１１０）の外周面のうち、少なくとも貫通穴１０１と半径方向で対向する領域は、貫通穴１０１との接触面積を大きくするために円筒面とすることが好ましい。この他、図示は省略するが、上記の複合材軽量継手１を、一方の部材Ａに一体に設け、他方の部材Ｂとピンを介して接続する継手として使用することもできる。また、貫通穴２に挿入されるピンは、継手１と他部材とを固定するもの（固定継手）であってもよいし、継手１と他部材とのピンを中心とした相対回転を許容するもの（回転継手）であってもよい。
　上記の実施形態では、強化繊維束４のラウンド部４ａを一回（１８０°）捩った場合を示したが、これに限らず、ラウンド部４ａにおいて強化繊維束４ａに撚りがかかってさえいれば、繊維長の差を小さくする効果を得ることができる。例えば、強化繊維束４のラウンド部４ａを複数回（１８０°より大きく）捩ることにより、ラウンド部４ａを構成する各強化繊維の長さの差を縮小するようにしてもよい。
　以上のような複合材軽量継手１は、航空機や自動車等の輸送機器や、建物や橋梁等の建築物などに使用することができる。
１     複合材軽量継手
２     貫通穴
３（３ａ～３ｅ）     強化繊維層
４     強化繊維束
４ａ   ラウンド部
４ａ１，４ａ２       強化繊維
４ｂ   直線部
５     強化繊維束
６     幅狭部

Claims (3)

  1. 　複数の強化繊維層を積層した積層体にマトリクスを含浸・硬化させた複合材からなり、前記強化繊維層の厚さ方向に貫通する貫通穴を有する複合材軽量継手であって、
    　前記複数の強化繊維層のうちの少なくとも一つの強化繊維層が、多数の強化繊維を帯状に引き揃えてなり、前記貫通穴の周囲に沿ったラウンド部を有する強化繊維束を備え、前記強化繊維束のラウンド部に撚りをかけた複合材軽量継手。
  2. 　前記ラウンド部の周方向両端において、内周側の強化繊維と外周側の強化繊維とを入れ替えた請求項１に記載の複合材軽量継手。
  3. 　前記強化繊維束が直線部をさらに有し、前記直線部にも撚りをかけた請求項１又は２に記載の複合材軽量継手。
PCT/JP2014/053861 2013-04-05 2014-02-19 複合材軽量継手 WO2014162789A1 (ja)

Priority Applications (5)

Application Number Priority Date Filing Date Title
BR112015024786A BR112015024786A2 (pt) 2013-04-05 2014-02-19 acoplamento de peso leve de compósito
CN201480019571.8A CN105102829B (zh) 2013-04-05 2014-02-19 复合材料轻型连接器
EP14779598.3A EP2982871A4 (en) 2013-04-05 2014-02-19 LIGHTWEIGHT COUPLING OF COMPOSITE MATERIAL
CA2912250A CA2912250A1 (en) 2013-04-05 2014-02-19 Composite lightweight fitting
US14/779,594 US20160052233A1 (en) 2013-04-05 2014-02-19 Composite lightweight fitting

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2013-079902 2013-04-05
JP2013079902 2013-04-05

Publications (1)

Publication Number Publication Date
WO2014162789A1 true WO2014162789A1 (ja) 2014-10-09

Family

ID=51658093

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/JP2014/053861 WO2014162789A1 (ja) 2013-04-05 2014-02-19 複合材軽量継手

Country Status (7)

Country Link
US (1) US20160052233A1 (ja)
EP (1) EP2982871A4 (ja)
JP (1) JP6180969B2 (ja)
CN (1) CN105102829B (ja)
BR (1) BR112015024786A2 (ja)
CA (1) CA2912250A1 (ja)
WO (1) WO2014162789A1 (ja)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2017118578A1 (de) * 2016-01-06 2017-07-13 Wobben Properties Gmbh Faserverbundbauteil und strukturbauteil sowie herstellungsverfahren
CN112677511A (zh) * 2019-10-17 2021-04-20 三菱重工业株式会社 带强化纤维束的复合材料以及螺栓联接构造体

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6750949B2 (ja) * 2016-01-26 2020-09-02 株式会社Ｓｕｂａｒｕ 繊維強化樹脂構造体の製造方法及び繊維強化樹脂構造体
ES2875018T3 (es) 2016-12-28 2021-11-08 Vestas Wind Sys As Unión para conectar una pala de rotor de aerogenerador a un buje de rotor y métodos asociados
JP7112950B2 (ja) * 2018-12-05 2022-08-04 三菱重工業株式会社 複合材の設計方法および複合材
JP7149028B1 (ja) 2022-06-27 2022-10-06 株式会社エルボーション 引き戸及び操作部構造

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0781225B2 (ja) 1990-08-27 1995-08-30 株式会社豊田自動織機製作所 結合部材用三次元織物
JP2012061672A (ja) * 2010-09-15 2012-03-29 Nikkiso Co Ltd 繊維強化プラスチック部品

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3362252A (en) * 1965-10-21 1968-01-09 Bendix Corp Redundant connecting link
US4775563A (en) * 1985-03-27 1988-10-04 Kaempen Charles E Composite spring-lock coupling
US5406033A (en) * 1992-09-02 1995-04-11 Maclean-Fogg Company Insulator structure and method of construction
WO1995033109A1 (fr) * 1994-05-27 1995-12-07 Nippon Steel Corporation Materiau de renforcement composite a base de resine renforcee par fibres, et son procede de production
JP4845525B2 (ja) * 2006-02-08 2011-12-28 ユニ・チャーム株式会社 清掃体及び清掃用具
EP2155476B1 (fr) * 2007-06-12 2011-09-14 Hexcel Reinforcements Procede de fabrication d'un materiau composite dans lequel au moins un fil torsade est depose et materiau composite ainsi obtenu
JP5660563B2 (ja) * 2010-03-31 2015-01-28 広島県 繊維強化熱可塑性樹脂プリプレグの積層方法
JP5460544B2 (ja) * 2010-09-30 2014-04-02 グローブライド株式会社 釣糸ガイド及び釣竿

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0781225B2 (ja) 1990-08-27 1995-08-30 株式会社豊田自動織機製作所 結合部材用三次元織物
JP2012061672A (ja) * 2010-09-15 2012-03-29 Nikkiso Co Ltd 繊維強化プラスチック部品

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP2982871A4

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2017118578A1 (de) * 2016-01-06 2017-07-13 Wobben Properties Gmbh Faserverbundbauteil und strukturbauteil sowie herstellungsverfahren
US11285688B2 (en) 2016-01-06 2022-03-29 Wobben Properties Gmbh Fiber composite component, structural component, and production method
CN112677511A (zh) * 2019-10-17 2021-04-20 三菱重工业株式会社 带强化纤维束的复合材料以及螺栓联接构造体

Also Published As

Publication number Publication date
CN105102829A (zh) 2015-11-25
EP2982871A4 (en) 2016-11-16
BR112015024786A2 (pt) 2017-07-18
EP2982871A1 (en) 2016-02-10
JP6180969B2 (ja) 2017-08-16
JP2014211231A (ja) 2014-11-13
CN105102829B (zh) 2016-12-28
CA2912250A1 (en) 2014-10-09
US20160052233A1 (en) 2016-02-25

Similar Documents

Publication Publication Date Title
JP6180969B2 (ja) 複合材軽量継手
US7731593B2 (en) Composite transmission shaft joint
KR102048508B1 (ko) 3축 섬유 강화된 복합 라미네이트
US9481442B2 (en) Dry preform, annular structure made of a composite material, and manufacturing method for the annular structure
US20110143082A1 (en) Ply drops modifications for composite laminate materials and related methods
US20100122606A1 (en) Tie rod and force transmitting assembly for a tie rod
WO2015146690A1 (ja) 複合材構造体、これを備えた航空機翼および航空機胴体、並びに複合材構造体の製造方法
EP2636509B1 (en) Joint structure for fiber reinforced resin and metal, and joining method for fiber reinforced resin and metal
US20230204071A1 (en) Composite lug with enhanced performance
US10030712B2 (en) Torque disc
CN112739618B (zh) 肘节
JPH05106629A (ja) 繊維強化プラスチツク製荷重伝達軸
WO2017099029A1 (ja) サンドイッチパネル，一方向プリプレグの製造方法及びサンドイッチパネルの製造方法
JP6961531B2 (ja) Ｆｒｐ円筒及びその製造方法
JP2003001717A (ja) プロペラシャフト用のｆｒｐ製パイプ
US9157462B2 (en) Bolted joint structure
CN111271361A (zh) 一种硫化机用紧固螺杆及其制备方法和硫化机
EP3991955B1 (en) Composite component system, use of a composite component system and method for repairing a composite component system
JP7365847B2 (ja) 補強繊維束付き複合材、及びボルト締結構造体
US20220205233A1 (en) Iso-truss structure and coupling mechanism for iso-truss structure
KR102439649B1 (ko) 고박장치용 라싱바 및 이의 제조 방법
JPH0791435A (ja) プロペラシャフトおよびその製造方法
EP3769944A1 (en) Composite drive shaft under dominant unidirectional torque
KR20220087016A (ko) 고박장치용 라싱바
WO2013191232A1 (ja) 強化繊維複合材料及び強化繊維複合材料の製造方法

Legal Events

Date Code Title Description
WWE Wipo information: entry into national phase

Ref document number: 201480019571.8

Country of ref document: CN

121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 14779598

Country of ref document: EP

Kind code of ref document: A1

WWE Wipo information: entry into national phase

Ref document number: 14779594

Country of ref document: US

ENP Entry into the national phase

Ref document number: 2912250

Country of ref document: CA

NENP Non-entry into the national phase

Ref country code: DE

WWE Wipo information: entry into national phase

Ref document number: 2014779598

Country of ref document: EP

REG Reference to national code

Ref country code: BR

Ref legal event code: B01A

Ref document number: 112015024786

Country of ref document: BR

ENP Entry into the national phase

Ref document number: 112015024786

Country of ref document: BR

Kind code of ref document: A2

Effective date: 20150928