[go: up one dir, main page]

CN105500837A - 复合材料制作高铁设备舱裙板的工艺 - Google Patents

复合材料制作高铁设备舱裙板的工艺 Download PDF

Info

Publication number
CN105500837A
CN105500837A CN201510947266.1A CN201510947266A CN105500837A CN 105500837 A CN105500837 A CN 105500837A CN 201510947266 A CN201510947266 A CN 201510947266A CN 105500837 A CN105500837 A CN 105500837A
Authority
CN
China
Prior art keywords
prepreg
retardant
apron board
fiber
skirtboard
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
CN201510947266.1A
Other languages
English (en)
Other versions
CN105500837B (zh
Inventor
朱家强
王滨
张四顺
王明
谢长志
罗剑岚
刘永凯
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.)
SHANGHAI CEDAR COMPOSITES TECHNOLOGY Co Ltd
Original Assignee
SHANGHAI CEDAR COMPOSITES TECHNOLOGY Co Ltd
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 SHANGHAI CEDAR COMPOSITES TECHNOLOGY Co Ltd filed Critical SHANGHAI CEDAR COMPOSITES TECHNOLOGY Co Ltd
Priority to CN201510947266.1A priority Critical patent/CN105500837B/zh
Publication of CN105500837A publication Critical patent/CN105500837A/zh
Priority to JP2018532028A priority patent/JP6615356B2/ja
Priority to SG11201702923YA priority patent/SG11201702923YA/en
Priority to PCT/CN2016/096333 priority patent/WO2017101490A1/zh
Priority to US16/063,250 priority patent/US10828870B2/en
Application granted granted Critical
Publication of CN105500837B publication Critical patent/CN105500837B/zh
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • B32B17/00—Layered products essentially comprising sheet glass, or glass, slag, or like fibres
    • B32B17/02—Layered products essentially comprising sheet glass, or glass, slag, or like fibres in the form of fibres or filaments
    • 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
    • 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
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/725—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined being hollow-walled or honeycombs
    • B29C66/7254—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined being hollow-walled or honeycombs honeycomb structures
    • 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
    • B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
    • B29C70/083—Combinations of continuous fibres or fibrous profiled structures oriented in one direction and reinforcements forming a two dimensional structure, e.g. mats
    • 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
    • B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
    • B29C70/083—Combinations of continuous fibres or fibrous profiled structures oriented in one direction and reinforcements forming a two dimensional structure, e.g. mats
    • B29C70/085—Combinations of continuous fibres or fibrous profiled structures oriented in one direction and reinforcements forming a two dimensional structure, e.g. mats the structure being deformed in a three dimensional configuration
    • 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
    • B29C70/345—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 using matched moulds
    • 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
    • B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/681—Component parts, details or accessories; Auxiliary operations
    • B29C70/682—Preformed parts characterised by their structure, e.g. form
    • 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
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B32B27/06—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • 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
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B32B27/06—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B27/065—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material of foam
    • 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
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B32B27/12—Layered products comprising a layer of synthetic resin next to a fibrous or filamentary layer
    • 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
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B32B27/34—Layered products comprising a layer of synthetic resin comprising polyamides
    • 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 shape; Layered products comprising a layer having particular features of form
    • B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
    • B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
    • 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
    • B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/06—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the heating method
    • 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
    • B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/12—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by using adhesives
    • B32B37/1207—Heat-activated adhesive
    • 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
    • B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/14—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
    • B32B37/146—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers whereby one or more of the layers is a honeycomb structure
    • 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
    • B32B5/18—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 features of a layer of foamed material
    • 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
    • B32B5/245—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 being a foam layer
    • 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
    • B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04—Interconnection of layers
    • B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
    • 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
    • B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
    • B32B9/005—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising one layer of ceramic material, e.g. porcelain, ceramic tile
    • B32B9/007—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising one layer of ceramic material, e.g. porcelain, ceramic tile comprising carbon, e.g. graphite, composite carbon
    • 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
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3064—Trains
    • 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
    • B29L2031/60—Multitubular or multicompartmented articles, e.g. honeycomb
    • B29L2031/608—Honeycomb structures
    • 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
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/02—Synthetic macromolecular fibres
    • B32B2262/0261—Polyamide fibres
    • B32B2262/0269—Aromatic polyamide fibres
    • 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
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10—Inorganic fibres
    • B32B2262/101—Glass fibres
    • 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
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10—Inorganic fibres
    • B32B2262/106—Carbon fibres, e.g. graphite fibres
    • 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
    • B32B2266/00—Composition of foam
    • B32B2266/02—Organic
    • B32B2266/0214—Materials belonging to B32B27/00
    • B32B2266/0264—Polyester
    • 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
    • B32B2305/00—Condition, form or state of the layers or laminate
    • B32B2305/02—Cellular or porous
    • B32B2305/024—Honeycomb
    • 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
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/30—Properties of the layers or laminate having particular thermal properties
    • B32B2307/306—Resistant to heat
    • B32B2307/3065—Flame resistant or retardant, fire resistant or retardant
    • 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
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/50—Properties of the layers or laminate having particular mechanical properties
    • B32B2307/514—Oriented
    • B32B2307/516—Oriented mono-axially
    • 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
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/50—Properties of the layers or laminate having particular mechanical properties
    • B32B2307/558—Impact strength, toughness
    • 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
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/70—Other properties
    • B32B2307/718—Weight, e.g. weight per square meter
    • 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
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/70—Other properties
    • B32B2307/72—Density
    • 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
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/70—Other properties
    • B32B2307/732—Dimensional properties
    • 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
    • B32B2309/00—Parameters for the laminating or treatment process; Apparatus details
    • B32B2309/02—Temperature
    • 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
    • B32B2309/00—Parameters for the laminating or treatment process; Apparatus details
    • B32B2309/04—Time
    • 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
    • B32B2309/00—Parameters for the laminating or treatment process; Apparatus details
    • B32B2309/12—Pressure
    • 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
    • B32B2605/00—Vehicles
    • B32B2605/10—Trains
    • 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
    • B32B2605/00—Vehicles
    • B32B2605/12—Ships
    • 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
    • B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/10—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the pressing technique, e.g. using action of vacuum or fluid pressure

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Composite Materials (AREA)
  • Ceramic Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Laminated Bodies (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)

Abstract

本发明涉及一种复合材料制作高铁设备舱裙板的工艺，本发明用的材料包括：芳纶蜂窝、PET泡沫、3K碳纤维阻燃预浸料、单向碳纤维阻燃预浸料、玻璃纤维阻燃预浸料、芳纶阻燃预浸料、300g/m2单组分中温固化蓝色环氧片胶。工艺包括(1)、制作裙板主板；(2)、制作裙板压条；裙板压条包括两种，每一种两条共四条；(3)、裙板主板和裙板压条五者做成裙板总成；裙板主板的四边中相对的两边的裙板压条为同一种，所有的裙板压条均卡在裙板主板上。本发明经过铺层设计使得该裙板在各个角度都能得到很高的强度，增加芳纶设计提供高强冲击性；裙板主板采用模压成型工艺，压条采用袋压工艺，整体强度好；热压成型工艺使得树脂含量很低，裙板主板的重量轻。

Description

复合材料制作高铁设备舱裙板的工艺
技术领域
本发明涉及一种高铁设备舱裙板的工艺，具体涉及一种能制作很高强度且重量轻的复合材料制作高铁设备舱裙板的工艺。
背景技术
高铁设备舱裙板是标准动车组设备舱的重要组成部分，在实际运用中，裙板承载能力、阻燃能力及抗冲击能力等有一定要求，所以在设计铺层、使用材料、设计工艺方面都需考虑；随着科技不断更新，在设计过程中通过轻量化和平顺化有效降低列车在运行过程中的阻力，从而减少持续的能量消耗。通过使用复合材料替代铝合金材料，在确保综合性能指标的前提下，降低整车的自重，提升整列车的轻量化水平。
发明内容
针对上述问题，本发明的主要目的在于提供一种能制作很高强度且重量轻的复合材料制作高铁设备舱裙板的工艺。
本发明是通过下述技术方案来解决上述技术问题的：一种复合材料制作高铁设备舱裙板的工艺，复合材料制作高铁设备舱裙板的材料包括：
芳纶蜂窝、PET泡沫、3K碳纤维阻燃预浸料、单向碳纤维阻燃预浸料、玻璃纤维阻燃预浸料、芳纶阻燃预浸料、300g/㎡单组分中温固化蓝色环氧片胶；
所述复合材料制作高铁设备舱裙板的工艺包括以下步骤：
(1)、裙板主板的制作；
(2)、裙板压条的制作；裙板压条包括两种，每一种两条共四条；
(3)、裙板主板和裙板压条五者做成裙板总成；
裙板主板的四边中相对的两边的裙板压条为同一种，所有的裙板压条均卡在裙板主板上。
在本发明的一个具体实施例子中，裙板主板按照铺层设计从外到内顺序包括如下：
1层198～200g/㎡的3K纹碳纤维阻燃预浸料；
5～8层300～315g/㎡的玻璃纤维阻燃预浸料；
2层235～240g/㎡的芳纶阻燃预浸料；
2层100～150g/㎡单向碳纤维阻燃预浸料；
1层300g/㎡单组分中温固化蓝色环氧片胶；
2层100～150g/㎡单向碳纤维阻燃预浸料；
1片厚度16.4mm芳纶纸蜂窝芯；
1片厚度为100～150g/㎡单向碳纤维阻燃预浸料；
1层300g/㎡单组分中温固化蓝色环氧片胶；
2层100～150g/㎡单向碳纤维阻燃预浸料；
4层300～315g/㎡的玻璃纤维阻燃预浸料；
1层198～200g/㎡的3K斜纹碳纤维阻燃预浸料；
按照铺层，紧密贴实在模具行腔内，在热压机上成型，温度设定为130-150℃，成型时间为3600-3800s，压力设定为4MPa-6Mpa。
在本发明的一个具体实施例子中，裙板压条铺层工艺包括如下：两件裙板压条采用袋压成型，压条由内向外按照铺层顺序包括如下：
1～2层300～315g/㎡的玻璃纤维阻燃预浸料；
4～6层100～150g/㎡单向碳纤维阻燃预浸料；
1层235～240g/㎡的芳纶阻燃预浸料；
2层100～150g/㎡单向碳纤维阻燃预浸料；
1层235～240g/㎡的芳纶阻燃预浸料；
4～6层100～150g/㎡单向碳纤维阻燃预浸料；
1层198～200g/㎡的3K斜纹碳纤维阻燃预浸料；
按照铺层，紧密贴实在模具行腔内，装好风管,在热压机上成型，温度设定130-150℃，成型时间3600-3800s，热压机压力设定4MPa-6Mpa，风管内压1MPa。
在本发明的一个具体实施例子中，所述芳纶纸蜂窝芯密度要求48～50kg/m3。
在本发明的一个具体实施例子中，所述PET泡沫密度要求59～61kg/m3。
本发明的积极进步效果在于：本发明提供的复合材料制作高铁设备舱裙板的工艺具有以下优点：
1、经过铺层设计使得该裙板在各个角度都能得到很高的强度，增加芳纶设计提供高强冲击性；
2、裙板主板采用模压成型工艺，压条采用袋压工艺，提高压条使用强度,不同工艺适用不同产品部件；
3、热压成型工艺使得树脂含量很低，大大减轻裙板主板的重量；
4、外型设计美观大方，性能强，较铝合金减重35％～40％，有较好的应用前景。
附图说明
图1为本发明的裙板总成拆分图。
图2为本发明的裙板总装图。
图3-1为本发明中第一种压条的截面图。
图3-2为本发明中第二种压条的截面图。
图4为本发明的裙板主板的截面图。
具体实施方式
下面结合附图给出本发明较佳实施例，以详细说明本发明的技术方案。
图1为本发明的整体结构示意图，如图1所示，本发明中复合材料制作高铁设备舱裙板的材料包括：芳纶蜂窝、PET泡沫、3K碳纤维阻燃预浸料、单向碳纤维阻燃预浸料、玻璃纤维阻燃预浸料、芳纶阻燃预浸料、300g/㎡单组分中温固化蓝色环氧片胶。
本发明的复合材料制作高铁设备舱裙板的工艺包括以下步骤：
(1)、裙板主板3的制作；
(2)、裙板压条1、2的制作；裙板压条包括两种，每一种两条共四条；
(3)、裙板主板3和裙板压条1、2五者做成裙板总成；
裙板主板的四边中相对的两边的裙板压条为同一种，所有的裙板压条均卡在裙板主板上。
裙板主板按照铺层设计从外到内顺序包括如下：
1层198～200g/㎡的3K纹碳纤维阻燃预浸料；
5～8层300～315g/㎡的玻璃纤维阻燃预浸料；
2层235～240g/㎡的芳纶阻燃预浸料；
2层100～150g/㎡单向碳纤维阻燃预浸料；
1层300g/㎡单组分中温固化蓝色环氧片胶；
2层100～150g/㎡单向碳纤维阻燃预浸料；
1片厚度16.4mm芳纶纸蜂窝芯；
1片厚度为100～150g/㎡单向碳纤维阻燃预浸料；
1层300g/㎡单组分中温固化蓝色环氧片胶；
2层100～150g/㎡单向碳纤维阻燃预浸料；
4层300～315g/㎡的玻璃纤维阻燃预浸料；
1层198～200g/㎡的3K斜纹碳纤维阻燃预浸料；
按照铺层，紧密贴实在模具行腔内，在热压机上成型，温度设定为130-150℃，成型时间为3600-3800s，压力设定为4MPa-6Mpa。
裙板压条铺层工艺包括如下：两件裙板压条采用袋压成型，压条由内向外按照铺层顺序包括如下：
1～2层300～315g/㎡的玻璃纤维阻燃预浸料；
4～6层100～150g/㎡单向碳纤维阻燃预浸料；
1层235～240g/㎡的芳纶阻燃预浸料；
2层100～150g/㎡单向碳纤维阻燃预浸料；
1层235～240g/㎡的芳纶阻燃预浸料；
4～6层100～150g/㎡单向碳纤维阻燃预浸料；
1层198～200g/㎡的3K斜纹碳纤维阻燃预浸料；
按照铺层，紧密贴实在模具行腔内，装好风管,在热压机上成型，温度设定130-150℃，成型时间3600-3800s，热压机压力设定4MPa-6Mpa，风管内压1MPa。
下面结合实施例对本发明作进一步说明：
实例一
第一步：裙板主板模压成型制作，按照铺层一层200g/㎡的3K斜纹碳纤维阻燃预浸料/6层300g/㎡的玻璃纤维阻燃预浸料/3层235g/㎡的芳纶阻燃预浸料/两层150g/㎡单向碳纤维阻燃预浸料/一层300g/㎡单组分中温固化蓝色环氧片胶/两层150g/㎡单向碳纤维阻燃预浸料/一片厚16.4mm芳纶纸蜂窝芯/一层300g/㎡单组分中温固化蓝色环氧片胶/两层100～150g/㎡单向碳纤维阻燃预浸料/四层300g/㎡的玻璃纤维阻燃预浸料/一层200g/㎡的3K斜纹碳纤维阻燃预浸料，将料片贴合在模具中，设定130℃，成型时间3600s，压力设定4MPa。
第二步：裙板两件压条采用袋压成型,压条由内向外按照铺层设计1层300g/㎡的玻璃纤维阻燃预浸料/6层150g/㎡单向碳纤维阻燃预浸料/1层235g/㎡的芳纶阻燃预浸料/2层150g/㎡单向碳纤维阻燃预浸料/1层235g/㎡的芳纶阻燃预浸料/6层150g/㎡单向碳纤维阻燃预浸料/一层200g/㎡的3K斜纹碳纤维阻燃预浸料，按照铺层，紧密贴实在模具行腔内，装好风管，在热压机上成型，温度设定130℃，成型时间3600s，热压机压力设定4MPa，风管内压1MPa。
第三步：CNC雕刻，胶合部件。
第四步：称重：产品相对实际高铁铝合金裙板,减重51％,单位面积载荷超过2500pa。
实例二
第一步：裙板主板模压成型制作,按照铺层一层200g/㎡的3K斜纹碳纤维阻燃预浸料/7层300g/㎡的玻璃纤维阻燃预浸料/2层235g/㎡的芳纶阻燃预浸料/两层150g/㎡单向碳纤维阻燃预浸料/一层300g/㎡单组分中温固化蓝色环氧片胶/两层150g/㎡单向碳纤维阻燃预浸料/一片厚16.4mm芳纶纸蜂窝芯/一层300g/㎡单组分中温固化蓝色环氧片胶/两层100～150g/㎡单向碳纤维阻燃预浸料/四层300g/㎡的玻璃纤维阻燃预浸料/一层200g/㎡的3K斜纹碳纤维阻燃预浸料，将料片贴合在模具中，设定140℃，成型时间3600s，压力设定4MPa。
第二步：裙板两件压条采用袋压成型，压条由内向外按照铺层设计2层300g/㎡的玻璃纤维阻燃预浸料/4层150g/㎡单向碳纤维阻燃预浸料/1层235g/㎡的芳纶阻燃预浸料/2层150g/㎡单向碳纤维阻燃预浸料/1层235g/㎡的芳纶阻燃预浸料/6层150g/㎡单向碳纤维阻燃预浸料/一层200g/㎡的3K斜纹碳纤维阻燃预浸料，按照铺层，紧密贴实在模具行腔内，装好风管，在热压机上成型，温度设定140℃，成型时间3600s，热压机压力设定5Mpa，风管内压1MPa。
第三步：CNC雕刻，胶合部件。
第四步：称重：产品相对实际高铁铝合金裙板,减重52％,单位面积载荷超过2500pa。
实例三
第一步：裙板主板模压成型制作，按照铺层一层200g/㎡的3K斜纹碳纤维阻燃预浸料/6层300g/㎡的玻璃纤维阻燃预浸料/3层235g/㎡的芳纶阻燃预浸料/两层150g/㎡单向碳纤维阻燃预浸料/一层300g/㎡单组分中温固化蓝色环氧片胶/两层150g/㎡单向碳纤维阻燃预浸料/一片厚16.4mm芳纶纸蜂窝芯/一层300g/㎡单组分中温固化蓝色环氧片胶/两层100～150g/㎡单向碳纤维阻燃预浸料/四层300g/㎡的玻璃纤维阻燃预浸料/一层200g/㎡的3K斜纹碳纤维阻燃预浸料，将料片贴合在模具中，设定150℃，成型时间3600s，压力设定4MPa。
第二步：裙板两件压条采用袋压成型,压条由内向外按照铺层设计1层300g/㎡的玻璃纤维阻燃预浸料/4层150g/㎡单向碳纤维阻燃预浸料/1层235g/㎡的芳纶阻燃预浸料/2层150g/㎡单向碳纤维阻燃预浸料/1层235g/㎡的芳纶阻燃预浸料/8层150g/㎡单向碳纤维阻燃预浸料/一层200g/㎡的3K斜纹碳纤维阻燃预浸料，按照铺层，紧密贴实在模具行腔内，装好风管,在热压机上成型，温度设定150℃，成型时间3600s，热压机压力设定6MPa，风管内压1MPa。
第三步：CNC雕刻，胶合部件。
第四步：称重：产品相对实际高铁铝合金裙板，减重51％，单位面积载荷超过2500pa。
以上显示和描述了本发明的基本原理和主要特征和本发明的优点。本行业的技术人员应该了解，本发明不受上述实施例的限制，上述实施例和说明书中描述的只是说明本发明的原理，在不脱离本发明精神和范围的前提下，本发明还会有各种变化和改进，这些变化和改进都落入要求保护的本发明范围内，本发明要求保护范围由所附的权利要求书及其等效物界定。

Claims (5)

1.一种复合材料制作高铁设备舱裙板的工艺，其特征在于：复合材料制作高铁设备舱裙板的材料包括：
芳纶蜂窝、PET泡沫、3K碳纤维阻燃预浸料、单向碳纤维阻燃预浸料、玻璃纤维阻燃预浸料、芳纶阻燃预浸料、300g/㎡单组分中温固化蓝色环氧片胶；
所述复合材料制作高铁设备舱裙板的工艺包括以下步骤：
(1)、裙板主板的制作；
(2)、裙板压条的制作；裙板压条包括两种，每一种两条共四条；
(3)、裙板主板和裙板压条五者做成裙板总成；
裙板主板的四边中相对的两边的裙板压条为同一种，所有的裙板压条均卡在裙板主板上。
2.根据权利要求1所述的复合材料制作高铁设备舱裙板的工艺，其特征在于：裙板主板按照铺层设计从外到内顺序包括如下：
1层198～200g/㎡的3K纹碳纤维阻燃预浸料；
5～8层300～315g/㎡的玻璃纤维阻燃预浸料；
2层235～240g/㎡的芳纶阻燃预浸料；
2层100～150g/㎡单向碳纤维阻燃预浸料；
1层300g/㎡单组分中温固化蓝色环氧片胶；
2层100～150g/㎡单向碳纤维阻燃预浸料；
1片厚度16.4mm芳纶纸蜂窝芯；
1片厚度为100～150g/㎡单向碳纤维阻燃预浸料；
1层300g/㎡单组分中温固化蓝色环氧片胶；
2层100～150g/㎡单向碳纤维阻燃预浸料；
4层300～315g/㎡的玻璃纤维阻燃预浸料；
1层198～200g/㎡的3K斜纹碳纤维阻燃预浸料；
按照铺层，紧密贴实在模具行腔内，在热压机上成型，温度设定为130-150℃，成型时间为3600-3800s，压力设定为4MPa-6Mpa。
3.根据权利要求1所述的复合材料制作高铁设备舱裙板的工艺，其特征在于：裙板压条铺层工艺包括如下：两件裙板压条采用袋压成型，压条由内向外按照铺层顺序包括如下：
1～2层300～315g/㎡的玻璃纤维阻燃预浸料；
4～6层100～150g/㎡单向碳纤维阻燃预浸料；
1层235～240g/㎡的芳纶阻燃预浸料；
2层100～150g/㎡单向碳纤维阻燃预浸料；
1层235～240g/㎡的芳纶阻燃预浸料；
4～6层100～150g/㎡单向碳纤维阻燃预浸料；
1层198～200g/㎡的3K斜纹碳纤维阻燃预浸料；
按照铺层，紧密贴实在模具行腔内，装好风管,在热压机上成型，温度设定130-150℃，成型时间3600-3800s，热压机压力设定4MPa-6Mpa，风管内压1MPa。
4.根据权利要求1所述的复合材料制作高铁设备舱裙板的工艺，其特征在于：所述芳纶纸蜂窝芯密度要求48～50kg/m3。
5.根据权利要求1所述的复合材料制作高铁设备舱裙板的工艺，其特征在于：所述PET泡沫密度要求59～61kg/m3。
CN201510947266.1A 2015-12-16 2015-12-16 复合材料制作高铁设备舱裙板的工艺 Active CN105500837B (zh)

Priority Applications (5)

Application Number Priority Date Filing Date Title
CN201510947266.1A CN105500837B (zh) 2015-12-16 2015-12-16 复合材料制作高铁设备舱裙板的工艺
JP2018532028A JP6615356B2 (ja) 2015-12-16 2016-08-23 複合材料による高速鉄道車両における設備用キャビンのエプロンプレートを製造するプロセス
SG11201702923YA SG11201702923YA (en) 2015-12-16 2016-08-23 The technique of producing apron boards on high-speed rail equipment cabinet by composite material
PCT/CN2016/096333 WO2017101490A1 (zh) 2015-12-16 2016-08-23 复合材料制作高铁设备舱裙板的工艺
US16/063,250 US10828870B2 (en) 2015-12-16 2016-08-23 Process for manufacturing apron board of high-speed rail equipment cabin using composite material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510947266.1A CN105500837B (zh) 2015-12-16 2015-12-16 复合材料制作高铁设备舱裙板的工艺

Publications (2)

Publication Number Publication Date
CN105500837A true CN105500837A (zh) 2016-04-20
CN105500837B CN105500837B (zh) 2018-01-02

Family

ID=55709313

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510947266.1A Active CN105500837B (zh) 2015-12-16 2015-12-16 复合材料制作高铁设备舱裙板的工艺

Country Status (5)

Country Link
US (1) US10828870B2 (zh)
JP (1) JP6615356B2 (zh)
CN (1) CN105500837B (zh)
SG (1) SG11201702923YA (zh)
WO (1) WO2017101490A1 (zh)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2017101490A1 (zh) * 2015-12-16 2017-06-22 上海晋飞新材料科技有限公司 复合材料制作高铁设备舱裙板的工艺
WO2017101492A1 (zh) * 2015-12-16 2017-06-22 上海晋飞新材料科技有限公司 复合材料制作高铁设备舱底板的工艺
CN107553997A (zh) * 2017-08-18 2018-01-09 航天材料及工艺研究所 一种轨道交通车辆车体裙板结构及其成型方法
CN107933590A (zh) * 2017-11-27 2018-04-20 株洲时代新材料科技股份有限公司 一种蜂窝夹芯结构裙板及其制备方法
CN109016708A (zh) * 2018-08-02 2018-12-18 株洲时代新材料科技股份有限公司 一种轨道车辆裙板
CN109094581A (zh) * 2018-08-28 2018-12-28 中车工业研究院有限公司 一种高速列车用设备舱裙板及其制备方法
CN109774192A (zh) * 2019-03-07 2019-05-21 江苏恒神股份有限公司 一种混杂纤维复合材料磁悬浮客车司机室外罩整体成型工艺
CN112454939A (zh) * 2020-10-27 2021-03-09 中车青岛四方机车车辆股份有限公司 用于安装裙板密封件的固定支架及其成型工艺、裙板组件
CN112590248A (zh) * 2020-12-01 2021-04-02 中车长春轨道客车股份有限公司 一种高速列车用碳纤维复合材料车体成型工艺及车体

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107351485B (zh) * 2017-07-13 2020-04-17 郑州宇通客车股份有限公司 一种用于公交车顶裙板的轻量阻燃复合板
CN112510304B (zh) * 2020-10-26 2023-01-31 新丽(广东)新能源汽车部件有限公司 一种电池防护罩的加工工艺
CN114905769B (zh) * 2022-07-19 2022-10-25 成都泰格尔航天航空科技股份有限公司 一种织物蜂窝成型装置及织物蜂窝成型工艺

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102604329A (zh) * 2012-02-29 2012-07-25 中铁伟业（北京）新技术有限公司 轨道车用增强型复合材料裙板
CN202399610U (zh) * 2011-09-26 2012-08-29 蓝星环境工程有限公司 一种复合材料板
CN103009728A (zh) * 2011-09-26 2013-04-03 蓝星环境工程有限公司 一种复合材料板、制备方法及用途

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5667866A (en) * 1995-05-02 1997-09-16 The Nordam Group, Inc. Multi-layered, unbalanced sandwich panel
EP0820858B1 (en) * 1996-07-22 2000-11-02 Hexcel Corporation Honeycomb core materials with particulate reinforcement
US7951449B2 (en) * 2002-06-27 2011-05-31 Wenguang Ma Polyester core materials and structural sandwich composites thereof
JP3894200B2 (ja) * 2004-04-07 2007-03-14 スターライト工業株式会社 ホットランテーブル用ガイド板
US7507461B2 (en) * 2004-09-01 2009-03-24 Hexcel Corporation Edge coating for honeycomb used in panels with composite face sheets
JP4241656B2 (ja) * 2005-04-07 2009-03-18 川崎重工業株式会社 高速鉄道車両の低騒音車体構造
JP4757650B2 (ja) * 2006-02-09 2011-08-24 東海旅客鉄道株式会社 パンタグラフカバー
JP4278677B2 (ja) * 2006-11-30 2009-06-17 株式会社ジャムコ サンドイッチパネル
JP5151535B2 (ja) * 2007-02-22 2013-02-27 東レ株式会社 サンドイッチ構造体、およびそれを用いた成形体、電子機器筐体
JP4699425B2 (ja) * 2007-06-22 2011-06-08 株式会社ジャムコ サンドイッチパネル
JP2010083080A (ja) * 2008-10-01 2010-04-15 Nippon Zeon Co Ltd ハニカムコア積層体及びその製造方法
CA2813006A1 (en) * 2010-09-20 2012-03-29 Bombardier Transportation Gmbh Lightweight compound cab structure for a rail vehicle
FR2990177B1 (fr) * 2012-05-03 2020-03-13 Alstom Transport Technologies Element structurel de vehicule ferroviaire, du type paroi longitudinale ou plancher
US20150151524A1 (en) * 2012-12-19 2015-06-04 Embraer S.A. Methods for fabricating stabilized honeycomb core composite laminate structures
FR3027273B1 (fr) * 2014-10-17 2018-04-27 Arianegroup Sas Architecture de paroi de face de voiture telle qu'une voiture de train en composite sandwich
CN104742460A (zh) * 2015-04-15 2015-07-01 洛阳双瑞橡塑科技有限公司 一种夹芯结构的客车地板
CN105500837B (zh) * 2015-12-16 2018-01-02 上海晋飞复合材料科技有限公司 复合材料制作高铁设备舱裙板的工艺
CN105584058B (zh) * 2015-12-16 2017-12-19 上海晋飞复合材料科技有限公司 复合材料制作高铁设备舱底板的工艺

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN202399610U (zh) * 2011-09-26 2012-08-29 蓝星环境工程有限公司 一种复合材料板
CN103009728A (zh) * 2011-09-26 2013-04-03 蓝星环境工程有限公司 一种复合材料板、制备方法及用途
CN102604329A (zh) * 2012-02-29 2012-07-25 中铁伟业（北京）新技术有限公司 轨道车用增强型复合材料裙板

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2017101490A1 (zh) * 2015-12-16 2017-06-22 上海晋飞新材料科技有限公司 复合材料制作高铁设备舱裙板的工艺
WO2017101492A1 (zh) * 2015-12-16 2017-06-22 上海晋飞新材料科技有限公司 复合材料制作高铁设备舱底板的工艺
CN107553997A (zh) * 2017-08-18 2018-01-09 航天材料及工艺研究所 一种轨道交通车辆车体裙板结构及其成型方法
CN107553997B (zh) * 2017-08-18 2019-11-12 航天材料及工艺研究所 一种轨道交通车辆车体裙板结构及其成型方法
CN107933590A (zh) * 2017-11-27 2018-04-20 株洲时代新材料科技股份有限公司 一种蜂窝夹芯结构裙板及其制备方法
CN109016708A (zh) * 2018-08-02 2018-12-18 株洲时代新材料科技股份有限公司 一种轨道车辆裙板
CN109094581A (zh) * 2018-08-28 2018-12-28 中车工业研究院有限公司 一种高速列车用设备舱裙板及其制备方法
CN109094581B (zh) * 2018-08-28 2019-11-26 中车工业研究院有限公司 一种高速列车用设备舱裙板及其制备方法
CN109774192A (zh) * 2019-03-07 2019-05-21 江苏恒神股份有限公司 一种混杂纤维复合材料磁悬浮客车司机室外罩整体成型工艺
CN112454939A (zh) * 2020-10-27 2021-03-09 中车青岛四方机车车辆股份有限公司 用于安装裙板密封件的固定支架及其成型工艺、裙板组件
CN112590248A (zh) * 2020-12-01 2021-04-02 中车长春轨道客车股份有限公司 一种高速列车用碳纤维复合材料车体成型工艺及车体

Also Published As

Publication number Publication date
SG11201702923YA (en) 2017-07-28
US10828870B2 (en) 2020-11-10
WO2017101490A1 (zh) 2017-06-22
US20180370192A1 (en) 2018-12-27
JP6615356B2 (ja) 2019-12-04
CN105500837B (zh) 2018-01-02
JP2019502591A (ja) 2019-01-31

Similar Documents

Publication Publication Date Title
CN105500837A (zh) 复合材料制作高铁设备舱裙板的工艺
CN105946327B (zh) 一种双面斜纹立体结构玻璃纤维织物及制备复合材料的方法
CN105253154B (zh) 高速动车复合材料车底设备舱底板
CN104842619A (zh) 高韧性多层结构预浸料制造工艺
CN102241166A (zh) 小型无人机专用蜂窝复合材料
US20170182741A1 (en) Systems and methods of producing a structural and non-structural homogeneous and hybrid composite panels, prepregs, hand layup panels with "basalt" fiber, various composite materials, and additives
CN106427133B (zh) 一种轻质低成本抗冲击性层叠预浸料复合板材
CN101736476A (zh) 一种泡沫填充的立体增强材料
CN114872386B (zh) 一种非对称飞机地板及其制备方法
CN109263156B (zh) 一种轨道交通车辆车体裙板结构及其成型方法
CN105584058B (zh) 复合材料制作高铁设备舱底板的工艺
CN107310082A (zh) 制作航空旅客座椅用碳纤维复合材料制件的方法
CN102658681A (zh) 三维正交机织物增强热固性树脂蜂窝夹层复合材料及制备
CN105799246B (zh) 高阻燃低翘曲碳纤维片材及其制备工艺
CN111844947A (zh) 一种新型设备舱板及其制备方法
CN106476330A (zh) 一种轨道车辆芳纶蜂窝侧顶板及其制备方法
CN109094581B (zh) 一种高速列车用设备舱裙板及其制备方法
CN203046380U (zh) 一种连续纤维增强发泡板材
CN108263406B (zh) 列车结构板材及列车结构板材的制造方法
CN216782709U (zh) 一种具有夹层结构的耐高温尼龙基复合材料
CN106741823B (zh) 由复合材料制备的无人机机体及其制备方法
CN213006894U (zh) 一种新型设备舱板
CN211993703U (zh) 一种芯层增强织物为连续无切口的多曲面壳体用超薄预成型体
CN107984858A (zh) 一种具有隔音功能及阻燃型复合材料地板及其制备方法
CN114407479A (zh) 柔性防火防爆板及其制备方法

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
CB02 Change of applicant information

Address after: 201108 Shanghai, Cao Cao Road, No. 13, No. 1, building C1, floor 2, building F1, No. 14, building 1, Minhang District

Applicant after: Shanghai Cedar Composites Technology Co., Ltd.

Applicant after: Shanghai Jin Fei Polytron Technologies Inc.

Address before: 201108 Shanghai, Cao Cao Road, No. 13, No. 1, building C1, floor 2, building F1, No. 14, building 1, Minhang District

Applicant before: Shanghai Cedar Composites Technology Co., Ltd.

Applicant before: SHANGHAI CEDAR COMPOSITES TECHNOLOGY CO. LTD.

CB02 Change of applicant information
GR01 Patent grant
GR01 Patent grant