CN104816660A - High-strength thermoplastic composite plastic seat part and manufacturing method thereof - Google Patents
High-strength thermoplastic composite plastic seat part and manufacturing method thereof Download PDFInfo
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- CN104816660A CN104816660A CN201510214956.6A CN201510214956A CN104816660A CN 104816660 A CN104816660 A CN 104816660A CN 201510214956 A CN201510214956 A CN 201510214956A CN 104816660 A CN104816660 A CN 104816660A
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- Prior art keywords
- continuous fiber
- fiber
- composite plastic
- seat
- thermoplastic
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
- B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
- B60N2/68—Seat frames
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- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
- B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
- B60N2/62—Thigh-rests
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
- B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
- B60N2/64—Back-rests or cushions
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Laminated Bodies (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Abstract
The invention discloses a high-strength thermoplastic composite plastic seat part and a manufacturing method thereof. The high-strength thermoplastic composite plastic seat part comprises a part face portion and reinforcing ribs of the supporting part face portion, wherein fiber in the part face portion includes at least one layer of continuous fiber, and the fiber in the reinforcing ribs is long fiber. The manufacturing method of the high-strength thermoplastic composite plastic seat part comprises the steps of cutting a continuous fiber piece soaked with thermoplastic resin and matched with the seat part in shape and weight, cutting a long fiber thermoplastic resin piece matched with the seat part in shape and weight, heating the fiber piece and arranging the heated continuous fiber thermoplastic resin piece and the long fiber thermoplastic resin piece in a mold for mold pressure in a superposed. Compared with a traditional production process, the manufacturing method is low in energy consumption, high in production efficiency and lower in cost, and the size accuracy of the high-strength thermoplastic composite plastic seat part is also improved.
Description
Technical field
The invention belongs to automotive field, be specifically related to a kind of high-strength thermoplastic composite plastic seat component and preparation method thereof.
Background technology
Along with the requirement of auto trade product weight-saving, the weight of client to product it is also proposed stricter requirement.The backrest frames overwhelming majority that automobile chair on market uses is metal backrest, and manufacturing procedure is complicated, spends more man-hour, energy resource consumption aspect, produces raw materials for plastics production than producing raw material metal and can save the more energy.The cost again utilized is less, pollutes hardly environment.The density that it has is little, the linear expansion factor of thermoplastic composite is less, the advantages such as the shrinkage percentage (precision of product size can be improved) in product molding process can be reduced and greatly extend composite material use in daily life, alternative metals and timber gradually, as the metal parts on car.But the intensity ratio intensity of plastics, specific modulus and shock resistance are strong, the product of preparation often service life shorter.The applying date is on November 27th, 2009, application number is the Chinese patent of 200910199483. 1, disclose a kind of car seat back frame of plastic material, described skeleton is integrated by plastic material, and described skeleton has the shell extended along its circumference, the horizontal sentence cross section of described shell is " n " type, and the inner side of the shell of described n tee section has cellular reinforced rib.Although reinforced rib be arranged on the service life that improve product to a certain extent, also differ greatly compared with the intensity of plastics and metalwork and impact property.
Summary of the invention
The object of this invention is to provide a kind of lightweight, a kind of high-strength thermoplastic composite plastic seat component that molding cycle is short and preparation method thereof.
For achieving the above object, the present invention is by the following technical solutions:
A kind of high-strength thermoplastic composite plastic seat component, comprise the reinforced rib that parts are facial and support component is facial, the fiber in parts face comprises at least one deck continuous fiber, and the fiber in reinforced rib is long fibre.
Described continuous fiber is one deck.
Described continuous fiber is at least two-layer, between continuous fiber layer adjacent every or continuous fiber layer between sandwiched long fibre layer.
Described continuous fiber is thermoplastic resin impregnated continuous unidirectional fibre, the two-way fiber of intersection laying, or at least one in fabric.
Described parts are back of seat, seat sitting face or back of seat and the integrated chair top of seat sitting face.
The thermoplastic base resin that the thermoplastic base resin of described continuous fiber dipping and long fibre flood is same resin.
The thermoplastic base resin that the thermoplastic base resin of described continuous fiber dipping and long fibre flood is different resins.
The preparation method of high-strength thermoplastic composite plastic seat component, comprises the steps:
Step one, cuts out the thermoplastic resin impregnated continuous fiber sheet with seat component shape and weight-matched;
Step 2, cuts out the long fiber thermoplastic resin sheet with seat component shape and weight-matched;
Step 3, heats the continuous fiber sheet of step one, and is heated by the long fiber thermoplastic resin sheet of step 2, or the long fibre material mated with seat component is heated in preparation separately, and heating-up temperature is 200-240 DEG C;
Step 4, the continuous fiber thermoplastic resin sheet heat step 3 and long fiber thermoplastic resin sheet lamination are inserted in mould, or by the continuous fiber thermoplastic resin sheet heated described in step 3 and long fibre material is stacked inserts in mould, the wherein cavity body of mould in the corresponding seat part side portion of continuous fiber thermoplastic resin sheet, long fibre sheet or long fibre material corresponding be reinforced rib cavity body of mould;
Step 5, compression molding, die pressure 1500-1800T/M
2, patrix temperature 30-80 DEG C, counterdie temperature 30-80 DEG C, dwell time 40-90s.
Preparation process of the present invention is simple, production efficiency is high.By dipping and die press technology for forming, make seat component have higher strength-to-density ratio and specific modulus, product has the feature such as designability, lower density; Layout and the orientation of two kinds of fibers complement each other, and use long fibre in reinforced rib, avoid the phenomenon that in compressing process, fiber easily ruptures, and substantially increase the strength-to-density ratio of product, specific modulus and impact resistance.The present invention has compared with traditional production technology that energy consumption is little, production efficiency is high, and cost is lower, and the dimensional accuracy of product have also been obtained raising.
Accompanying drawing explanation
The structural representation of Fig. 1 back of seat.
In Fig. 2 Fig. 2 AA to section drawing in the structural representation of back of seat face sandwiched long fibre layer.
In Fig. 3 Fig. 2 AA to section drawing in back of seat face be the structural representation of long fibre layer.
The structural representation of Fig. 4 seat sitting face.
In Fig. 5 Fig. 4 CC to section drawing in the structural representation of seat sitting face continuous fiber layer sandwiched long fibre layer.
In Fig. 6 Fig. 4 CC to section drawing in seat sitting face continuous fiber layer be the structural representation of individual layer.
The structural representation of Fig. 7 seat sitting face, back of seat one.
Fig. 8 seat sitting face, back of seat face lays the structural representation of one deck continuous fiber.
Fig. 9 seat sitting face, back of seat face lays the structural representation of double layer continuous fiber.
Detailed description of the invention
A kind of high-strength thermoplastic composite plastic seat component, parts are cushion frame, back of seat, seat sitting face or back of seat and the integrated chair top of cushion frame.Comprise the reinforced rib that parts are facial and support component is facial, the fiber in parts face comprises at least one deck continuous fiber, and the fiber in reinforced rib is long fibre.As shown in Figure 1, the integrated back of seat of reinforced rib 12 of back of seat face 11 and support seat back face.As shown in Figure 2,3, the continuous fiber 21 of back of seat face can be one deck, also can be prepared into two-layer or multilayer as required, be separated by between continuous fiber layer or sandwiched long fibre layer 23 between continuous fiber layer, the fiber in reinforced rib is long fibre layer 22.Continuous fiber is thermoplastic resin impregnated continuous unidirectional fibre, the two-way fiber of intersection laying, or at least one in fabric; As shown in Figure 4, the integrated seat cushions of reinforced rib 42 of seat sitting face 41 and supporting chair seat surface.As shown in Figure 5, seat sitting face is continuous fiber layer 51, and the continuous fiber layer on seat sitting face surface is individual layer, sandwiched long fibre layer 52 between two-layer continuous fiber individual layer, and reinforced rib is long fibre layer 52; As shown in Figure 6, the continuous fiber layer 61 on seat sitting face surface is double-deck.As shown in Figure 7, the reinforced rib of back of seat face 71, seat sitting face 72, supporting chair sitting face and the reinforced rib 73 of back of seat face are formed in one.As shown in Figure 8, seat sitting face and back of seat face are continuous fiber layer 81, can sandwiched long fibre layer 82 between continuous fiber layer 81, and the reinforced rib in seat back-rest framework is long fibre layer 82; As shown in Figure 9, seat sitting face and back of seat face are continuous fiber layer 91 is bilayer, also can be prepared into multilayer.The thermoplastic base resin that the thermoplastic base resin of continuous fiber dipping and long fibre flood is same resin, or different resins.Continuous fiber reinforced thermoplastic plastic is similar to Long-fiber-reinforced thermoplastics preparation method, and just continuous fiber reinforced thermoplastic plastic is uninterrupted along its length, can infinitely extend.Long-fiber-reinforced thermoplastics is the rectangular of fully being flooded by resin of obtaining after resin dedicated dipping of long fibre, is then cut into the length of needs as required, is generally 20-30cm;
The preparation method of high-strength thermoplastic composite plastic seat component, comprises the steps:
Step one, cuts out the thermoplastic resin impregnated continuous fiber sheet with seat component shape and weight-matched;
Step 2, cuts out the long fiber thermoplastic resin sheet with seat component shape and weight-matched;
Step 3, heats the continuous fiber sheet of step one, and is heated by the long fiber thermoplastic resin sheet of step 2, or the long fibre material mated with seat component is heated in preparation separately, and heating-up temperature is 200-240 DEG C;
Step 4, the continuous fiber thermoplastic resin sheet heat step 3 and long fiber thermoplastic resin sheet lamination are inserted in mould, or by the continuous fiber thermoplastic resin sheet heated described in step 3 and long fibre material is stacked inserts in mould, the wherein cavity body of mould in the corresponding seat part side portion of continuous fiber thermoplastic resin sheet, long fibre sheet or long fibre material corresponding be reinforced rib cavity body of mould;
Step 5, compression molding, die pressure 1500-1800T/M
2, patrix temperature 30-80 DEG C, counterdie temperature 30-80 DEG C, dwell time 40-90s.
Claims (8)
1. a high-strength thermoplastic composite plastic seat component, comprise the reinforced rib that parts are facial and support component is facial, it is characterized in that: the fiber in parts face comprises at least one deck continuous fiber, the fiber in reinforced rib is long fibre.
2. high-strength thermoplastic composite plastic seat component according to claim 1, is characterized in that: described continuous fiber is one deck.
3. high-strength thermoplastic composite plastic seat component according to claim 1, is characterized in that: described continuous fiber is at least two-layer, between continuous fiber layer adjacent every or continuous fiber layer between sandwiched long fibre layer.
4. high-strength thermoplastic composite plastic seat component according to claim 2, is characterized in that: described continuous fiber is thermoplastic resin impregnated continuous unidirectional fibre, the two-way fiber of intersection laying, or at least one in fabric.
5. high-strength thermoplastic composite plastic seat component according to claim 3, is characterized in that: described parts are back of seat, seat sitting face or back of seat and the integrated chair top of seat sitting face.
6. high-strength thermoplastic composite plastic seat component according to claim 4, is characterized in that: the thermoplastic base resin that the thermoplastic base resin of described continuous fiber dipping and long fibre flood is same resin.
7. high-strength thermoplastic composite plastic seat component according to claim 4, is characterized in that: the thermoplastic base resin that the thermoplastic base resin of described continuous fiber dipping and long fibre flood is different resins.
8. the preparation method of high-strength thermoplastic composite plastic seat component according to claim 1, is characterized in that comprising the steps:
Step one, cuts out the thermoplastic resin impregnated continuous fiber sheet with seat component shape and weight-matched;
Step 2, cuts out the long fiber thermoplastic resin sheet with seat component shape and weight-matched;
Step 3, heats the continuous fiber sheet of step one, and is heated by the long fiber thermoplastic resin sheet of step 2, or the long fibre material mated with seat component is heated in preparation separately, and heating-up temperature is 200-240 DEG C;
Step 4, the continuous fiber thermoplastic resin sheet heat step 3 and long fiber thermoplastic resin sheet lamination are inserted in mould, or by the continuous fiber thermoplastic resin sheet heated described in step 3 and long fibre material is stacked inserts in mould, the wherein cavity body of mould in the corresponding seat part side portion of continuous fiber thermoplastic resin sheet, long fibre sheet or long fibre material corresponding be reinforced rib cavity body of mould;
Step 5, compression molding, die pressure 1500-1800T/M
2, patrix temperature 30-80 DEG C, counterdie temperature 30-80 DEG C, dwell time 40-90s.
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Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105128244A (en) * | 2015-10-23 | 2015-12-09 | 南车株洲电力机车有限公司 | Fiberglass seat die for railway vehicle |
CN105235119A (en) * | 2015-10-23 | 2016-01-13 | 南车株洲电力机车有限公司 | Machining method of urban rail vehicle glass fiber reinforced plastic seat |
CN105881929A (en) * | 2016-02-25 | 2016-08-24 | 中航复合材料有限责任公司 | Continuous fiber fabric and LFT composite wallboard structure manufacturing method |
CN107031480A (en) * | 2016-02-04 | 2017-08-11 | 安道拓卢森堡控股有限公司 | Equipment part and the method for manufacturing equipment part |
CN110116522A (en) * | 2018-02-05 | 2019-08-13 | 富尔西亚排气系统公司 | Pre-preg component comprising main layer and enhancement layer |
CN113226717A (en) * | 2018-10-15 | 2021-08-06 | 阿里斯复合材料有限公司 | Method and apparatus for molding composite ribs and rib-sheet |
CN114364572A (en) * | 2019-07-11 | 2022-04-15 | Sabic环球技术有限责任公司 | Hybrid seat structure and vehicle including the same |
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CN105128244A (en) * | 2015-10-23 | 2015-12-09 | 南车株洲电力机车有限公司 | Fiberglass seat die for railway vehicle |
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CN105881929A (en) * | 2016-02-25 | 2016-08-24 | 中航复合材料有限责任公司 | Continuous fiber fabric and LFT composite wallboard structure manufacturing method |
CN110116522A (en) * | 2018-02-05 | 2019-08-13 | 富尔西亚排气系统公司 | Pre-preg component comprising main layer and enhancement layer |
CN110116522B (en) * | 2018-02-05 | 2021-06-11 | 富尔西亚排气系统公司 | Prepreg part comprising a main layer and a reinforcement layer |
CN113226717A (en) * | 2018-10-15 | 2021-08-06 | 阿里斯复合材料有限公司 | Method and apparatus for molding composite ribs and rib-sheet |
CN114364572A (en) * | 2019-07-11 | 2022-04-15 | Sabic环球技术有限责任公司 | Hybrid seat structure and vehicle including the same |
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CN114364572B (en) * | 2019-07-11 | 2024-04-16 | Sabic环球技术有限责任公司 | Hybrid seat structure and vehicle including the same |
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