Classifications

• • 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
  • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
  • F16F1/00—Springs
  • F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
  • F16F1/366—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers made of fibre-reinforced plastics, i.e. characterised by their special construction from such materials
  • F16F1/368—Leaf springs
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B60—VEHICLES IN GENERAL
  • B60G—VEHICLE SUSPENSION ARRANGEMENTS
  • B60G11/00—Resilient suspensions characterised by arrangement, location or kind of springs
  • B60G11/02—Resilient suspensions characterised by arrangement, location or kind of springs having leaf springs only
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B60—VEHICLES IN GENERAL
  • B60G—VEHICLE SUSPENSION ARRANGEMENTS
  • B60G11/00—Resilient suspensions characterised by arrangement, location or kind of springs
  • B60G11/02—Resilient suspensions characterised by arrangement, location or kind of springs having leaf springs only
  • B60G11/10—Resilient suspensions characterised by arrangement, location or kind of springs having leaf springs only characterised by means specially adapted for attaching the spring to axle or sprung part of the vehicle
  • B60G11/12—Links, pins, or bushes
• • 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
  • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
  • F16F1/00—Springs
  • F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
  • F16F1/366—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers made of fibre-reinforced plastics, i.e. characterised by their special construction from such materials
  • F16F1/368—Leaf springs
  • F16F1/3683—Attachments or mountings therefor
  • F16F1/3686—End mountings
• • 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
  • B29C70/40—Shaping or impregnating by compression not applied
  • B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
  • B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
  • B29C70/48—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B60—VEHICLES IN GENERAL
  • B60G—VEHICLE SUSPENSION ARRANGEMENTS
  • B60G2202/00—Indexing codes relating to the type of spring, damper or actuator
  • B60G2202/10—Type of spring
  • B60G2202/11—Leaf spring
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B60—VEHICLES IN GENERAL
  • B60G—VEHICLE SUSPENSION ARRANGEMENTS
  • B60G2204/00—Indexing codes related to suspensions per se or to auxiliary parts
  • B60G2204/10—Mounting of suspension elements
  • B60G2204/12—Mounting of springs or dampers
  • B60G2204/121—Mounting of leaf springs
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B60—VEHICLES IN GENERAL
  • B60G—VEHICLE SUSPENSION ARRANGEMENTS
  • B60G2206/00—Indexing codes related to the manufacturing of suspensions: constructional features, the materials used, procedures or tools
  • B60G2206/01—Constructional features of suspension elements, e.g. arms, dampers, springs
  • B60G2206/40—Constructional features of dampers and/or springs
  • B60G2206/42—Springs
  • B60G2206/428—Leaf springs
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B60—VEHICLES IN GENERAL
  • B60G—VEHICLE SUSPENSION ARRANGEMENTS
  • B60G2206/00—Indexing codes related to the manufacturing of suspensions: constructional features, the materials used, procedures or tools
  • B60G2206/01—Constructional features of suspension elements, e.g. arms, dampers, springs
  • B60G2206/70—Materials used in suspensions
  • B60G2206/71—Light weight materials
  • B60G2206/7101—Fiber-reinforced plastics [FRP]
• • 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
  • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
  • F16F2224/00—Materials; Material properties
  • F16F2224/02—Materials; Material properties solids
  • F16F2224/0241—Fibre-reinforced plastics [FRP]
• • 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
  • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
  • F16F2230/00—Purpose; Design features
  • F16F2230/0005—Attachment, e.g. to facilitate mounting onto confer adjustability
• • 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
  • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
  • F16F2238/00—Type of springs or dampers
  • F16F2238/02—Springs
  • F16F2238/022—Springs leaf-like, e.g. of thin, planar-like metal

Definitions

• the invention relates to a fiber composite component designed as a spring with at least one spring section and with at least one load introduction structure.
• Fiber composite components are used in many applications to replace conventional structural steel components.
• Such structural components may also be spring or spring elements, such as vehicle springs, for example, parts of suspensions, such as handlebars or leaf springs.
• Such fiber composite components are elongated, since the longitudinal extent is greater by a multiple than the extension in the transverse direction thereto, and thus in relation to the width and the height of such a component.
• Such components have at least one load introduction structure. This is usually executed as an eye. In conventionally forged components of the type in question such eyes are closed as a rule. In leaf springs, where the eyes are created by a rolling process, these are sometimes open.
• a load introduction structure can serve in such components, a connection pin which protrudes on one or both sides transverse to the longitudinal extent of the component at one end thereof.
• Fiber composite components of the type in question are already known.
• DE 10 2006 047 412 B1 describes a rod-shaped fiber composite structure with load introduction elements.
• This fiber composite structure is a structural component of a hydraulic actuator.
• This known fiber composite structure is composed of two half-shells, which is surrounded by a bandage with circumferential fiber reinforcement.
• DE 10 2010 009 528 A1 discloses a fiber composite component designed as a leaf spring.
• a load introduction structure a bearing eye is provided in this prior art fiber composite component.
• a sleeve is used as the load introduction element, which is wrapped around the end section of the fiber composite material. is.
• this is cut to size in the region of its end to form a narrower tongue.
• an opening is cut into the prepreg strip used to form the fiber composite component, into which the end-side tongue is inserted after the sleeve has been looped around. The protruding from the opening end portion of the tongue is separated. In this way, the end-side end face of the prepreg strip is returned after wrapping around the sleeve as a load introduction element to the relevant end of the actual spring section.
• the invention is therefore based on the object, a fiber composite component, which not only high loads in a reasonable use of material allows, but also the risk of delamination against a fiber composite component whose load introduction structure is provided by a fiber composite material loop , is reduced.
• an initially mentioned tes, generic fiber composite component in which the fiber composite material of the fiber composite component in which the load introduction element forming or enclosing end portion is divided in a plane transverse to the longitudinal extent of the load introduction structure in at least two fiber composite strands and two adjacent fiber composite strands for training one eye in opposite directions to form a particular over a certain Angled amount extending overlap out and with their mutually facing side surfaces, in the portion in which they are arranged overlapping, are non-positively connected to each other.
• the load introduction structure is formed by at least two fiber composite strands.
• the load introduction structure is typically an eye, which may be designed as an open or closed eye.
• the special feature of the fiber composite component according to the invention is that the wrapping or winding direction of adjacent fiber composite material strands is opposite in direction to the formation of the load introduction structure. This means that, in the event that a first fiber composite strand is guided to form an eye in a clockwise direction, whereas the one or both adjacent fiber composite strands are guided in the opposite wrapping or winding direction and thus to the left.
• the amount of wrap by which the fiber composite strands are guided to form the eye of the load-introducing structure is at least so large that adjacent fiber composite strands are overlapping over a certain angular amount.
• the fiber composite material is divided in the region of its at least one load introduction structure in a plane transverse to the longitudinal extension of his eye.
• the extent of the wrap of the load introduction element is thus dependent solely on the length of the fiber composite material strands.
• the load introduction structure can thus be designed independently of the other components of the fiber composite component. This also applies vice versa for the design of the remaining parts of the fiber composite component with respect to the load introduction structure.
• the overlap with respect to the opposite direction of wrap of adjacent fiber composite strands allows the formation of a particular large-scale An exertan urges two adjacent fiber composite strands.
• the bonding of adjacent fiber composite strands together ensures that high forces can be introduced into the load introduction structure and, moreover, delamination is effectively prevented.
• the large-area bonding of adjacent fiber composite strands contributes to the fact that, when a load introduction element is provided, it is securely accommodated in the fiber composite structure of the load introduction structure.
• a load introduction element which is enclosed by the composite fiber material strands, may be, for example, a metal sleeve.
• Each fiber composite strand preferably forms an eye of more than 270 °.
• the side contact surface of these fiber composite strands then extends over at least 90 °.
• the eyes formed by the fiber composite strands which together form the eye of the load introduction structure, are made closed or approximately closed.
• the end-side impact of the fiber composite material strands is returned to or virtually to the surface of the remaining part of the fiber composite material.
• a particular advantage of such a fiber composite component with its in a plane transverse to the longitudinal extension of the load introduction element end to form a load introduction structure divided fiber composite strands is also that the load introduction structure in terms of their load application characteristics to the needs of the application or in the use of such a fiber composite component can be adjusted. Depending on the expected load, it may well be provided that the cross-sectional area of the sum of the fiber composite strands forming an eye in a first wrapping direction is different than the sum cross-sectional area of the fiber composite strands with which the corresponding eye (s) in the other Strapping direction are formed.
• a load introduction structure can be interpreted symmetrically or asymmetrically with this concept with respect to the central transverse plane of the load introduction structure. An asymmetrical design is suitable, for example, for applications in which torsional loads must be absorbed by the load introduction structure when they intervene from a certain functional direction.
• the number of fiber composite strands with which the eye of a load introduction structure is formed is at least two. Preferably, however, an odd number of fiber composite strands are chosen in order to be able to interpret the alternation of an opposing wrapping direction symmetrically starting from its median transverse plane in both directions. This refers to the alternation and not necessarily to the width of each fiber composite strand.
• undirectionally oriented fibers, fiber strands as well as woven fiber material, nonwoven fabric or the like can be used. If no fiber strands are used, which can be easily divided in their end region into the required fiber composite strands, the end portion at which a load introduction structure is to be formed, divided by one or more cuts in the fiber composite strands required for the opposing wrapping.
• a fiber composite component may have such a load introduction structure at several points. If the fiber composite component is, for example, a leaf spring, it will be equipped at its two ends with such a load introduction structure. In such a fiber composite component may well be a frame, a subframe, a handlebar or the like, which has at least one such load introduction structure.
• a common load introduction element for example a metal sleeve
• a metal sleeve is enclosed by the eyes of the fiber composite strands of such a load introduction structure.
• the cross-sectional area of such a metal sleeve may have a circular cross-sectional area. Due to the embedding of such a load introduction element in the manner described above, the cross-sectional area of such a load introduction element may also deviate from the round shape, for example, be made square.
• the spring characteristic of such a spring produced as a fiber composite component can be adjusted inter alia via the fiber volume content of the fiber composite component.
• the fiber volume content indicates the volumetric fraction of the fibers used, typically glass fibers, on the specific geometry of the component.
• the fiber volume content based on the cross-sectional area of such a fiber-composite component designed as a spring indicates the proportion of fibers relative to the cross-sectional area.
• Such a fiber composite component designed, for example, as a parabolic spring can have a constant fiber volume content via the extent of its spring section, in this case its spring arm.
• the cover layers of the fiber strands are made continuous.
• the fiber volume content can be reduced compared to that in the spring section, that is to say for example in the spring arm.
• the fact that these end sections use less stress in fiber have to endure longitudinal direction and are mainly loaded interlaminar. Rather, it is envisaged that these end portions should not react, at least not appreciably elastic, which is ensured by the increased resin content.
• the lower use of fiber strands has a weight-reducing effect on the fiber composite component.
• the cover layers of the fiber strands are typically continuous.
• An advantage of such a configuration is also that the injection mass can be better distributed in infusion processes even at lower pressure in the form such an end portion forming form. The reason for this is the lower number of fiber strands affecting the flow behavior of the injected mass in the at least one end section. Investigations have shown that in the at least one end section the fiber volume content could be reduced by up to 50% for the same fiber composite component quality. The degree of such a fiber volume content reduction in the at least one end section will be interpreted as a function of the application intended for the fiber composite component.
• fiber volume content in the fiber composite strands may be at least partially different.
• fiber composite strands juxtaposed transversely of the spring may have the same fiber volume content, while the composite fiber strands underlying or above thereof may have a different fiber volume content. It is also possible to arrange in the transverse direction of the fiber composite component fiber composite strands with different fiber volume content.
• FIG. 1 shows a perspective view of a manufactured as a fiber composite component leaf spring for a vehicle
• FIG. 2 is an enlarged partial perspective view of the left load introduction structure of the leaf spring of Figure 1,
• FIG. 3 shows the load introduction structure of FIG. 2 from a different perspective with a partially unwound fiber composite material strand with which a load introduction element is looped
• FIG. 4 shows the load introduction structure of FIG. 3 in the same perspective with which the load introduction element enclosing fiber composite material strand.
• FIG. 1 shows a leaf spring 1 manufactured as an elongated fiber composite component.
• the leaf spring 1 has been brought from a fiber composite material in its shape shown in Figure 1.
• fiber composite material fiber strands have been used in the embodiment of Figure 1.
• the fiber composite leaf spring 1 has been produced by means of a resin injection process known per se (Resin Transfer Molding). In this method, serving as textile semifinished fiber strands are inserted into a mold. In a subsequent step, the resin is injected (injected) into the cavity of the mold in which the fiber strands are arranged in the desired shape.
• the leaf spring shown in FIG. 1 can also be produced by using prepregs.
• the leaf spring 1 carries a load introduction structure 2, 2.1.
• the load introduction structure 2 will be described in more detail.
• the load introduction structure 2.1 is constructed identically in the illustrated embodiment. Therefore, the relevant statements apply equally to the load introduction structure 2.1.
• the load introduction structure comprises as a load introduction element a metal sleeve 3, through which an eye is provided.
• the metal sleeve 3 is enclosed by the fiber composite material along its radial lateral surface.
• Figure 2 shows the load introduction structure 2 of the leaf spring 1 in a section at the end of the actual spring leaf.
• the sleeve 3 is wrapped in the illustrated embodiment of three fiber composite material strands 4, 4.1, 4.2.
• the fiber composite strands 4, 4.1, 4.2 are guided around the sleeve 3 with different Umschlingungsnchtung.
• the fiber composite strand 4 is wound clockwise with respect to Figure 2 around the lateral surface of the sleeve 3.
• the fiber composite strand 4.2 is also performed.
• the fiber composite strand 4.1 located between the two fiber composite material strands 4, 4.2 is guided in the counterclockwise direction and thus in opposite directions to the fiber composite material strands 4, 4.2 around the sleeve 3.
• All three fiber composite strands 4, 4.1, 4.2 are guided approximately 360 ° around the lateral surface of the sleeve 3.
• the remaining gusset between the respective end face, as indicated on the end face 5 of the fiber composite strand 4, and the top of the beginning of the strands 4, 4.1, 4.2 is filled with the resin used for curing.
• This filled with resin gusset is identified in Figure 2 by the reference numeral 6.
• a closed eye is placed around the radial outer surface of the sleeve 3 by each fiber composite material strand 4, 4.1, 4.2 in the illustrated embodiment.
• the fiber composite strands 4, 4.1, 4.2 are divided in the transverse plane of the longitudinal course of the sleeve 3 and thus in the longitudinal direction of the leaf spring 1 to allow the above-described opposing wrapping adjacent fiber composite strands 4, 4.1 and 4.1, 4.2 of the sleeve 3.
• the load introduction structure 2 can be exposed to particularly high loads.
• the load introduction structure 2 acting tensile or shear forces regardless of the direction of their attack proportionately at least always in a leaf spring near section of a fiber composite strand 4, 4.2 or 4.1 initiated.
• Figure 3 shows to illustrate the above-described wrap the load introduction structure 2 with the unwound from the sleeve 3 fiber composite strand 4.
• the composite adjacent fiber composite strands here: the fiber composite strand 4 and the fiber composite strand 4.1, via the adjacent and due to the resin material and thus Since in the illustrated embodiment, the looping of the sleeve 3 through the fiber composite strands 4, 4.1, 4.2 is almost 360 °, the contact surface of two adjacent fiber composite strands is particularly large. It is of interest that due to the opposing wrapping of the sleeve 3 through the fiber composite material strands 4, 4.1, 4.2 these can be solved in a tensile load also only in opposite directions from the lateral surface of the sleeve 3. However, this is effectively prevented by the material bond between the adjacent fiber composite strands 4, 4.1 and 4.1, 4.2.
• the composite is readily sufficiently strong for the resin used to cure the fiber composite component to withstand such shear forces.
• FIG. 4 shows the load introduction structure 2 from the perspective of the representation of FIG. 3 with the fiber composite material strand 4 materially connected to the side face 7.
• the wrap of the metal sleeve 3 is constructed symmetrically with respect to its central transverse plane. This can, if this is required by appropriate requirements, be designed asymmetrically.
• the cross-sectional area of the fiber composite strand 4.1 is greater than the sum of the cross-sectional areas of the fiber composite strand 4, 4.2, in a ratio of about 5: 3.
• each load introduction structure 2, 2.1 can be designed in an optimized way to the respective requirements.
• the load introduction structures 2, 2.1 do not need to be identical, as is the case in the illustrated embodiment. It is quite possible, for example, to design the front in the direction of travel load introduction structure with respect to the interpretation of the wrap of the metal sleeve 3 differently than the rear in the direction of travel load introduction structure.
• the fiber volume content over the length of the leaf spring 1 is constant.

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• Engineering & Computer Science (AREA)
• General Engineering & Computer Science (AREA)
• Mechanical Engineering (AREA)
• Springs (AREA)
• Vehicle Body Suspensions (AREA)

Priority Applications (7)

Applications Claiming Priority (2)

Publications (1)

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Family Applications (1)

Country Status (9)

Families Citing this family (5)

Citations (6)

Family Cites Families (8)

• 2016
  • 2016-06-22 DE DE202016103285.7U patent/DE202016103285U1/de active Active
• 2017
  • 2017-06-07 JP JP2018566973A patent/JP7002479B2/ja active Active
  • 2017-06-07 EP EP17732334.2A patent/EP3475593B1/de active Active
  • 2017-06-07 ES ES17732334T patent/ES2775899T3/es active Active
  • 2017-06-07 US US16/301,037 patent/US11156259B2/en active Active
  • 2017-06-07 WO PCT/EP2017/063783 patent/WO2017220321A1/de not_active Ceased
  • 2017-06-07 CN CN201780034287.1A patent/CN109219710B/zh active Active
  • 2017-06-07 PL PL17732334T patent/PL3475593T3/pl unknown
  • 2017-06-07 MX MX2018015981A patent/MX390853B/es unknown

Patent Citations (6)

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