CN106870924A - The space framework and application of carbon fibre composite honeycomb cellular structure member and its preparation - Google Patents

The space framework and application of carbon fibre composite honeycomb cellular structure member and its preparation Download PDF

Info

Publication number
CN106870924A
CN106870924A CN201611267221.0A CN201611267221A CN106870924A CN 106870924 A CN106870924 A CN 106870924A CN 201611267221 A CN201611267221 A CN 201611267221A CN 106870924 A CN106870924 A CN 106870924A
Authority
CN
China
Prior art keywords
composite
carbon fibre
space framework
structure member
carbon fiber
Prior art date
Legal status (The legal status 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 status listed.)
Granted
Application number
CN201611267221.0A
Other languages
Chinese (zh)
Other versions
CN106870924B (en
Inventor
张平
张一平
马钰尧
胡匡
胡一匡
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CN201611267221.0A priority Critical patent/CN106870924B/en
Publication of CN106870924A publication Critical patent/CN106870924A/en
Application granted granted Critical
Publication of CN106870924B publication Critical patent/CN106870924B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16SCONSTRUCTIONAL ELEMENTS IN GENERAL; STRUCTURES BUILT-UP FROM SUCH ELEMENTS, IN GENERAL
    • F16S3/00Elongated members, e.g. profiled members; Assemblies thereof; Gratings or grilles
    • F16S3/02Elongated members, e.g. profiled members; Assemblies thereof; Gratings or grilles composed of two or more elongated members secured together side by side
    • AHUMAN NECESSITIES
    • A47FURNITURE; DOMESTIC ARTICLES OR APPLIANCES; COFFEE MILLS; SPICE MILLS; SUCTION CLEANERS IN GENERAL
    • A47CCHAIRS; SOFAS; BEDS
    • A47C7/00Parts, details, or accessories of chairs or stools
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B62LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62DMOTOR VEHICLES; TRAILERS
    • B62D23/00Combined superstructure and frame, i.e. monocoque constructions
    • B62D23/005Combined superstructure and frame, i.e. monocoque constructions with integrated chassis in the whole shell, e.g. meshwork, tubes, or the like
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B62LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62DMOTOR VEHICLES; TRAILERS
    • B62D29/00Superstructures, understructures, or sub-units thereof, characterised by the material thereof
    • B62D29/04Superstructures, understructures, or sub-units thereof, characterised by the material thereof predominantly of synthetic material
    • B62D29/046Combined superstructure and frame, i.e. monocoque constructions

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Transportation (AREA)
  • General Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Structural Engineering (AREA)
  • Laminated Bodies (AREA)

Abstract

The invention discloses a kind of carbon fibre composite honeycomb cellular structure member, the carbon fibre composite honeycomb cellular structure member is cellular composite material tube prepared by continuous carbon fibre, the honeycomb hole of cellular composite material tube is continuous carbon fibre woven composite pipe or continuous carbon fibre wound composite pipe, at least two compositions are overall a branch of, the position that adjacent carbon fiber woven composite pipe or carbon fiber winding composite material tube contacts with each other links together, so that adjacent composite material tube links together, overall cellular composite material tube is constituted.The present invention is designed according to the thickness and stress of pipe, and very big this performance of pulling force is born so as to be optimal performance carbon fiber;The space framework light weight that is prepared using carbon fibre composite honeycomb cellular structure member, rigidity is high, security is good, can be used as the skeleton of automobile, car and seat.

Description

The space framework and application of carbon fibre composite honeycomb cellular structure member and its preparation
Technical field
The present invention relates to a kind of carbon fibre composite honeycomb cellular structure member and its space framework and the application of preparation.
Background technology
Carbon fiber has high intensity, high temperature resistant, corrosion-resistant, endurance, light weight, can to bear very big pulling force etc. significantly high The characteristic of Yu Gang, aluminium etc., belongs to typical high-performance fiber, has overwhelming advantage relative to traditional metal material.Carbon Fiber is added to resin, metal, ceramics, concrete in addition to alone as heat-insulating material usually as reinforcing material Deng in material, carbon fibre composite is constituted.Reasonable in design being combined is needed when carbon fibre composite is used as structural member Material force structure, can just give full play to carbon fiber can bear very big this advantage of pulling force.
Automobile, the vehicle frame of car are all space framework, and the effect of vehicle frame is subject to load, including automobile itself parts Suffered impact, distortion, inertia force etc. when weight and traveling.In the prior art, Truck Frame Structure is generally fall crossbeam type vehicle frame With bearing-type vehicle frame, fall crossbeam type vehicle frame welds sturdy girder steel or riveted gets up as a steelframe, then in this steelframe Upper installation engine, suspension, the part such as vehicle body, the steel crossbeam quality of fall crossbeam type vehicle frame are heavy, and vehicle frame weight accounts for full car gross weight Considerable part;Bearing-type vehicle frame is by steel(More advanced is aluminium)It is stamped, be welded, to design and produce technique requirement All very high, product quality is difficult to control, and production process is cumbersome, and whole body frame structure for automotive rigid is not enough.
The important topic of automobile industry concern is increasingly becoming with energy-saving and environmental protection, people start to consider the lightweight of automobile Development.The lightweight of automobile can reduce the kerb weight of automobile, can not only save material, and reduce automobile production cost, And fuel oil oil consumption, energy-conserving and environment-protective can also be reduced.Therefore, people were begun attempt to lighter, intensity more preferable composite generation For the material of conventional frame member.
The content of the invention
Carbon fiber maximum feature is can to bear very big pulling force in carbon fibre composite, and resin bears pressure, existing Material is made inner tubular portion and does not support, and is made if tabular, because thickness of slab is too small, produces torque small, does not make full use of carbon Fiber can bear the advantage of very big pulling force, so needing how research gives full play to the side that carbon fiber bears this advantage of pulling force Method.Need for carbon fibre composite to be made the light product of density for this, if being made foam, because continuous fiber cannot Foaming, that is, allow to foaming, and influence can be produced on the performance of resin after foaming, loses original performance, can not bear very big drawing Power, therefore how to realize carbon fibre composite and bear very big pulling force as structural member becoming for very big problem.
The present invention is exactly to solve the above problems, there is provided a kind of carbon fibre composite honeycomb cellular structure member and its preparation Space framework and application.
The present invention uses following technical scheme:A kind of carbon fibre composite honeycomb cellular structure member, the carbon fiber composite Material honeycomb cellular structure member is cellular composite material tube prepared by continuous carbon fibre, and the honeycomb hole of cellular composite material tube is continuous Carbon fiber woven composite pipe or continuous carbon fibre wound composite pipe, at least two constitute overall a branch of, adjacent carbon The position that fibre-woven composite pipe or carbon fiber winding composite material tube contact with each other links together, so that adjacent Composite material tube link together, constitute overall cellular composite material tube.
The filament that the adjacent carbon fiber woven composite pipe contacts with each other mutually is woven together.
The adjacent carbon fiber winding composite material tube is mutually woven together.
Space framework prepared by carbon fibre composite honeycomb cellular structure member, the carbon fiber woven composite pipe or carbon are fine Dimension wound composite pipe constitutes ring-shaped frame corresponding with space framework position, the corresponding ring-shaped frame in each position of space framework Space framework is combined as, the position that a branch of ring-shaped frame of adjacent composition interconnects constitutes carbon fibre composite honeybee Nest structural member.
It is described adjacent to be mutually woven together as a branch of ring-shaped frame.
The application of space framework, the space framework is used for automobile skeleton.
The application of space framework, the space framework is used for Bus Frame.
The application of space framework, the space framework is used for chair framework.
Carbon fiber can bear very big pulling force, and will not deform, but be made as it is solid if, not only can waste of materials, increase Add weight, and performance improves also little, therefore the present invention is designed according to the thickness and stress of pipe, so as to be optimal hair Wave carbon fiber and bear very big this performance of pulling force;The space framework quality prepared using carbon fibre composite honeycomb cellular structure member Gently, rigidity is high, security is good, can be used as the skeleton of automobile, car and seat.
Brief description of the drawings
Fig. 1 is structural representation Fig. 1 of carbon fibre composite honeycomb cellular structure member.
Fig. 2 is structural representation Fig. 2 of carbon fibre composite honeycomb cellular structure member.
Fig. 3 is adjacent carbons fibre-woven composite pipe connecting structure schematic diagram.
Fig. 4 is the structural representation of space framework.
Specific embodiment
The present invention is described in further detail with specific embodiment below in conjunction with the accompanying drawings.
As shown in Figure 1, Figure 2 and Figure 3, a kind of carbon fibre composite honeycomb cellular structure member, the carbon fibre composite honeybee Nest structural member is cellular composite material tube prepared by continuous carbon fibre, and the honeycomb hole of cellular composite material tube is continuous carbon fibre Dimension woven composite pipe 1 or continuous carbon fibre wound composite pipe 2, at least two constitute it is overall a branch of, fibrage or Winding method as the braiding of steel wire in high pressure steel wire sebific duct or winding method, adjacent carbon fiber woven composite pipe 1 The filament for contacting with each other mutually is woven together, and adjacent carbon fiber winding composite material tube 2 is mutually woven together, so that Adjacent composite material tube is linked together, constitute overall cellular composite material tube.
As shown in figure 4, space framework prepared by carbon fibre composite honeycomb cellular structure member, the carbon fiber braiding composite wood Expects pipe 1 or carbon fiber winding composite material tube 2 constitute ring-shaped frame 3 corresponding with space framework position, each position of space framework Corresponding ring-shaped frame 3 is combined as space framework, and the position that a branch of ring-shaped frame 3 of adjacent composition interconnects is constituted Carbon fibre composite honeycomb cellular structure member is adjacent to be mutually woven together as a branch of ring-shaped frame 3.
Above-mentioned space framework light weight, rigidity are high, security is good, can be used in automobile, car and chair framework, for vapour When car, car, the weight in working order of vehicle can be reduced, can not only saved material, reduce vehicle production cost, and can also Reduce fuel oil oil consumption, energy-conserving and environment-protective;During for chair framework, seat-weight can be mitigated, improve seat intensity.
The forming method of space framework prepared by carbon fibre composite honeycomb cellular structure member is:
(1)Draw the three-dimensional drawing of described space framework;
(2)Each ring-shaped frame shape according to space framework makes rubber liner respectively, and rubber liner is what a side disconnected Ring-shaped frame, two ends wherein one end closing of disconnection, the other end is set into outlet passageway, and the position that inner bag disconnects is more long than ring-shaped frame 2.5cm;
(3)External mold is made according to each ring-shaped frame shape respectively;
(4)Selection matches carbon fiber braiding or the wound composite pipe of diameter and length with rubber liner, and carbon fiber is woven Or wound composite pipe carries out pre-preg;
(5)Carbon fiber braiding or wound composite pipe are respectively fitted on inner bag;
(6)The prepreg composite materials pipe of inner bag will be enclosed within to insert in correspondence external mold, then locked mode;
(7)Charged and discharged gas repeatedly to inner bag, make to produce slightly play between braided fiber or winding fiber, preimpregnation is woven or is twined It is adapted to weave or wind the shape of lines around composite material tube, eliminates fibre stress;
(8)Preimpregnation carbon fiber is set to weave or the solidification of wound composite pipe to inner bag pressurized, heated;
(9)Die sinking, mould unloading, make the ring-shaped frame that all one side disconnect respectively;
(10)Each ring-shaped frame is combined, it is adjacent to be mutually woven together as a branch of ring-shaped frame;
(11)The ring-shaped frame grafting closure that each is disconnected.

Claims (8)

1. a kind of carbon fibre composite honeycomb cellular structure member, it is characterised in that:The carbon fibre composite honeycomb cellular structure member is Cellular composite material tube prepared by continuous carbon fibre, the honeycomb hole of cellular composite material tube is compound for continuous carbon fibre weaves Tubes of material or continuous carbon fibre wound composite pipe, at least two constitute overall a branch of, adjacent carbon fiber braiding composite wood The position that expects pipe or carbon fiber winding composite material tube contact with each other links together, so that adjacent composite material tube connects It is connected together, constitutes overall cellular composite material tube.
2. carbon fibre composite honeycomb cellular structure member according to claim 1, it is characterised in that:The adjacent carbon fiber The filament that woven composite pipe contacts with each other mutually is woven together.
3. carbon fiber woven composite honeycomb cellular structure member according to claim 1, it is characterised in that:The adjacent carbon Filament wound composite pipe is mutually woven together.
4. the space framework that prepared by carbon fibre composite honeycomb cellular structure member according to claim 1, it is characterised in that:Institute State carbon fiber woven composite pipe or carbon fiber winding composite material tube constitute ring-shaped frame corresponding with space framework position, The corresponding ring-shaped frame in each position of space framework is combined as space framework, and a branch of ring-shaped frame of adjacent composition is interconnected on one The position risen constitutes carbon fiber woven composite honeycomb cellular structure member.
5. space framework according to claim 4, it is characterised in that:It is described adjacent mutually to be compiled as a branch of ring-shaped frame It is woven in together.
6. the application of space framework according to claim 4, it is characterised in that:The space framework is used for automobile skeleton.
7. the application of space framework according to claim 4, it is characterised in that:The space framework is used for Bus Frame.
8. the application of space framework according to claim 4, it is characterised in that:The space framework is used for chair framework.
CN201611267221.0A 2016-12-31 2016-12-31 The space framework and application of carbon fibre composite honeycomb cellular structure member and its preparation Active CN106870924B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201611267221.0A CN106870924B (en) 2016-12-31 2016-12-31 The space framework and application of carbon fibre composite honeycomb cellular structure member and its preparation

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611267221.0A CN106870924B (en) 2016-12-31 2016-12-31 The space framework and application of carbon fibre composite honeycomb cellular structure member and its preparation

Publications (2)

Publication Number Publication Date
CN106870924A true CN106870924A (en) 2017-06-20
CN106870924B CN106870924B (en) 2019-03-15

Family

ID=59164435

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201611267221.0A Active CN106870924B (en) 2016-12-31 2016-12-31 The space framework and application of carbon fibre composite honeycomb cellular structure member and its preparation

Country Status (1)

Country Link
CN (1) CN106870924B (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108006428A (en) * 2017-11-20 2018-05-08 国网河南省电力公司安阳供电公司 A kind of composite glass fiber winding arrangement part and its bundle structure of preparation
CN108049693A (en) * 2017-11-20 2018-05-18 国网河南省电力公司安阳供电公司 A kind of composite material electric pole of braiding structure
CN108468383A (en) * 2018-05-30 2018-08-31 胡广生 A kind of grid structure skeleton and manufacturing method for building
CN109812686A (en) * 2017-11-20 2019-05-28 国网河南省电力公司安阳供电公司 A kind of composite fibre rod structure part of clamping
CN112757657A (en) * 2020-12-16 2021-05-07 哈尔滨工程大学 Water pressure-resistant light high-strength composite material porous buoyancy material and preparation method thereof
CN117776752A (en) * 2023-12-25 2024-03-29 宜兴市新立织造有限公司 Honeycomb foam sandwich bearing/heat insulation composite material and preparation method thereof

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1111087A (en) * 1994-01-12 1995-11-08 株式会社圆多 Tubular fishing rod and its method of manufacture
JP2002020953A (en) * 2000-05-01 2002-01-23 Mitsubishi Rayon Co Ltd Net shaped article of carbon fiber
CN203322712U (en) * 2013-05-28 2013-12-04 核工业第八研究所 Carbon fiber composite material square-to-round pipe fitting
CN105172216A (en) * 2015-08-13 2015-12-23 山东大学 Winding reinforced composite material automobile plate spring and preparation method thereof

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1111087A (en) * 1994-01-12 1995-11-08 株式会社圆多 Tubular fishing rod and its method of manufacture
JP2002020953A (en) * 2000-05-01 2002-01-23 Mitsubishi Rayon Co Ltd Net shaped article of carbon fiber
CN203322712U (en) * 2013-05-28 2013-12-04 核工业第八研究所 Carbon fiber composite material square-to-round pipe fitting
CN105172216A (en) * 2015-08-13 2015-12-23 山东大学 Winding reinforced composite material automobile plate spring and preparation method thereof

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108006428A (en) * 2017-11-20 2018-05-08 国网河南省电力公司安阳供电公司 A kind of composite glass fiber winding arrangement part and its bundle structure of preparation
CN108049693A (en) * 2017-11-20 2018-05-18 国网河南省电力公司安阳供电公司 A kind of composite material electric pole of braiding structure
CN109812686A (en) * 2017-11-20 2019-05-28 国网河南省电力公司安阳供电公司 A kind of composite fibre rod structure part of clamping
CN108468383A (en) * 2018-05-30 2018-08-31 胡广生 A kind of grid structure skeleton and manufacturing method for building
CN112757657A (en) * 2020-12-16 2021-05-07 哈尔滨工程大学 Water pressure-resistant light high-strength composite material porous buoyancy material and preparation method thereof
CN117776752A (en) * 2023-12-25 2024-03-29 宜兴市新立织造有限公司 Honeycomb foam sandwich bearing/heat insulation composite material and preparation method thereof

Also Published As

Publication number Publication date
CN106870924B (en) 2019-03-15

Similar Documents

Publication Publication Date Title
CN106870924A (en) The space framework and application of carbon fibre composite honeycomb cellular structure member and its preparation
CN105128876B (en) A kind of carbon fibre composite car body and its manufacturing method
CN106828616A (en) Slide fastener is engaged carbon fiber braiding structure part and ring connects space framework and the application of preparation
CN203844839U (en) Detachable auxiliary frame
CN109360919B (en) All-composite material battery box for new energy automobile and manufacturing method thereof
WO2022170663A1 (en) Method for manufacturing lightweight component based on continuous fibers and common fibers, and product
CN109291477A (en) Two-way reinforced composite pipe of thermoplasticity continuous glass-fiber prepreg tape journal axle and preparation method thereof
CN101850694A (en) Carbon fiber rim and manufacturing method thereof
CN105667596A (en) Automobile chassis main load bearing structure made of composite material
CN108266632A (en) Slide fastener is engaged carbon fiber winding structural member and ring connects space framework and the application of preparation
WO2023070990A1 (en) Light-weight large-load commercial vehicle stabilizer bar suspender assembly and preparation method therefor
CN107023419A (en) A kind of Solid Rocket Motor combustion chamber housing lightweight joint
CN108263482A (en) The carbon fiber winding structural member of braiding and its space framework and the application of preparation
CN108263476A (en) Riveting carbon fiber winding structural member and its ring connect space framework and the application of preparation
CN108263493A (en) Riveting carbon fiber braiding structure part and its ring connect space framework and the application of preparation
CN216002108U (en) Light-weight large-load stabilizer bar and suspender assembly of commercial vehicle
CN110492035A (en) A kind of lower box and its preparation method of power battery
CN108263491A (en) Slide fastener is engaged space framework and the application of carbon fiber winding structural member and its preparation
WO2018121789A1 (en) Fibre fabric composite structural component, automobile framework prepared using same, and method
CN205327191U (en) Use car body owner load -bearing structure that combined material made
CN108263481A (en) The carbon fiber braiding structure part of winding and its space framework and the application of preparation
CN108263494A (en) The carbon fiber winding structural member of winding and its space framework and the application of preparation
CN108263490A (en) The carbon fiber braiding structure part of braiding and its space framework and the application of preparation
CN108262976A (en) The method that slide fastener occlusion carbon fiber winding composite material structural member prepares space framework
CN108263002A (en) The method that slide fastener occlusion carbon fiber winding composite material structural member prepares space framework

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant