CN109687159A - Ultralight high-precision rapid shaping antenna reflective face and preparation method thereof - Google Patents

Ultralight high-precision rapid shaping antenna reflective face and preparation method thereof Download PDF

Info

Publication number
CN109687159A
CN109687159A CN201811614560.0A CN201811614560A CN109687159A CN 109687159 A CN109687159 A CN 109687159A CN 201811614560 A CN201811614560 A CN 201811614560A CN 109687159 A CN109687159 A CN 109687159A
Authority
CN
China
Prior art keywords
precision
pmi foam
antenna reflective
reflective face
preparation
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.)
Pending
Application number
CN201811614560.0A
Other languages
Chinese (zh)
Inventor
徐宏涛
郝旭峰
鞠博文
李秀伟
史耀辉
王晓蕾
刘千立
沈峰
徐小魁
田杰
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 Composite Material Science and Technology Co Ltd
Original Assignee
Shanghai Composite Material Science and 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 Composite Material Science and Technology Co Ltd filed Critical Shanghai Composite Material Science and Technology Co Ltd
Priority to CN201811614560.0A priority Critical patent/CN109687159A/en
Publication of CN109687159A publication Critical patent/CN109687159A/en
Pending legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q15/00Devices for reflection, refraction, diffraction or polarisation of waves radiated from an antenna, e.g. quasi-optical devices
    • H01Q15/14Reflecting surfaces; Equivalent structures
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q15/00Devices for reflection, refraction, diffraction or polarisation of waves radiated from an antenna, e.g. quasi-optical devices
    • H01Q15/14Reflecting surfaces; Equivalent structures
    • H01Q15/141Apparatus or processes specially adapted for manufacturing reflecting surfaces
    • H01Q15/142Apparatus or processes specially adapted for manufacturing reflecting surfaces using insulating material for supporting the reflecting surface
    • H01Q15/144Apparatus or processes specially adapted for manufacturing reflecting surfaces using insulating material for supporting the reflecting surface with a honeycomb, cellular or foamed sandwich structure

Landscapes

  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Aerials With Secondary Devices (AREA)

Abstract

The present invention provides a kind of ultralight high-precision rapid shaping antenna reflective faces and preparation method thereof, and the antenna reflective face includes surface metal-layer, glue-line, PMI foam, and the glue-line is connect with the working face of PMI foam reflecting surface.The present invention is by the PMI foam applications of quickly and easily Transmetallation and light high-stiffness in the preparation of antenna reflector, solve the problems, such as that traditional aluminum honeycomb interlayer composite material reflecting surface needs the autoclave forming process of use cost height, long flow path, compared to traditional honeycomb sandwich construction antenna reflector, not only it has been significantly shorter the process flow of preparation, more by 3 times of its weight saving, and it can guarantee that type face precision is suitable.

Description

Ultralight high-precision rapid shaping antenna reflective face and preparation method thereof
Technical field
The present invention relates to PMI foam material structure functors and preparation method thereof, and in particular to a kind of ultralight high-precision is fast Rapid-result type antenna reflective face and preparation method thereof.
Background technique
Antenna reflective face is the Typical Representative of structure-function integration, and it is logical that the surface precision of working face directly affects antenna Interrogate the authenticity of signal.However, the increasing lightweight of antenna reflective face, high-precision, the demand of low cost, give antenna-reflected Quickly manufacture brings huge challenge to face high-precision.In recent years, American-European countries starts to use foam material in antenna reflective face field Material, in numerous foamed materials, Polymethacrylimide (PMI) foamed material is steady because of its chemistry outstanding and structure size The excellent characteristics such as qualitative, good suitability for secondary processing, specific strength and specific modulus height are widely used.
Existing foam is applied in reflecting surface is used as sandwich material more, such as the utility model of Publication No. CN 206412482U The patent of invention of patent and Publication No. CN103560332B, these reflector type face precision are all grade or submillimeter level, It is unable to satisfy the communication for having reached Terahertz frequency range radio frequency and detection reflector requirement.And traditional Terahertz frequency range antenna Reflecting surface uses the structure of composite material skin aluminum honeycomb interlayer, and product quality is heavier, and composite material skin is needed using heat Tank technological forming is pressed, it is at high cost, process flow is long, in order to meet antenna reflective face lightweight high-precision quickly manufacture demand, adopt The main structure for using PMI foam as antenna reflective face mitigates weight, is guaranteed using thermoforming process and Transmetallation anti- The requirement for penetrating face surface conductivity, and meeting high-precision and quickly manufacturing.
Summary of the invention
For the defects in the prior art, the object of the present invention is to provide a kind of ultralight high-precision rapid shaping antenna-reflecteds Face and preparation method thereof.Guarantee antenna reflective face rigidity, product surface precision to it is micron-sized under the premise of, alleviate product Weight shortens process flow, reduces cost.
The purpose of the present invention is achieved through the following technical solutions:
The present invention provides a kind of ultralight high-precision rapid shaping antenna reflective face, and the antenna reflective face includes setting gradually Metal layer, glue-line and PMI foam reflecting surface;The glue-line is connect with the working face of PMI foam reflecting surface.
Preferably, the PMI foam reflecting surface is made by PMI closed cell rigid foamed material.
Preferably, in the PMI foam reflecting surface, the aperture of PMI foam is that (aperture of PMI foam is tiny by 0.1-0.5mm And uniformly), the density of PMI foam is 50~120kg/m3
Preferably, 20~30 μm of diameter of metallic particles in the metal layer, metal layer with a thickness of 0.05~0.2mm.
Preferably, the glue-line is made by coating normal-temperature curing epoxy resinae adhesive, and the shearing of the glue-line is strong Degree >=20MPa, peel strength >=15N/cm of the glue-line.
The present invention also provides a kind of preparation methods of ultralight high-precision rapid shaping antenna reflective face, include the following steps:
S1, PMI foam reflecting surface blank is prepared using thermoforming process;
S2, the PMI foam reflecting surface blank is processed, PMI foam reflecting surface is made;
S3, metal transfer film, the sprayed metal layer on the metal transfer film, in the gold are coated on high-precision mold Belong to and coats glue-line on layer;
S4, the PMI foam reflecting surface prepared in step S2 is covered on the glue-line, through vacuum solidification and solidifying and setting After demould to get the antenna reflective face.
Preferably, in step S1, the step of thermoforming process includes: that PMI foam is placed on high-precision mold is flat Plate, and make vacuum bag;The high-precision mold for carrying out vacuum bag and PMI foam plate are subjected to hot briquetting.
Preferably, in step S1, the condition of the thermoforming process are as follows: be warming up to foam softening temperature (such as room temperature~ 200 DEG C), it vacuumizes, vacuum pressure is 0.05~0.097MPa, 0.5~1.5h of heat-insulation pressure keeping, furnace cooling.Select this heat The reflecting surface blank of the molding available higher initial precision of technique, reduces subsequent amount of machining, improves efficiency.
Preferably, in step S2, the step of processing includes: by the PMI foam reflecting surface blank from high-precision mould After being demoulded on tool, it is fixed in frost sucker using the method for unstressed clamping, is processed using CNC milling machine;Process obtained institute State PMI foam reflector type face precision RMS0.01~0.05mm.The unstressed installation way for selecting this frost sucker, avoids Influence of the stress generated when tradition machinery clamping to reflector precision.
Preferably, in step S3, the metal transfer film is by 2-30 parts of polyvinyl alcohol, 40-70 parts of distilled water, 10-60 parts Ethyl alcohol, 3-10 part glycerol, 3-10 parts of lauryl sodium sulfate mix.Glycerol and surfactant sodium dodecyl base sulfuric acid is added The purpose of sodium is to reduce the surface tension of metal transfer film, improves transfer liquid in the wetability of die surface, improves transfer film thickness Uniformity is spent, the coating of transfer membrane is improved, improves metal spraying efficiency.
It is highly preferred that the metal transfer film is by 5 parts of polyvinyl alcohol, and 55 parts of distilled water, 40 parts of ethyl alcohol, 5 parts of glycerol, 5 parts Lauryl sodium sulfate composition.
Preferably, in step S3, the step of sprayed metal layer includes: to be sprayed on the surface of metal transfer film using flame The mode sprayed metal layer of painting;The metal that the metal layer uses includes at least one of aluminium, nickel;The flame-spraying is formed 20~30 μm of metallic particles diameter, obtained 0.05~0.2mm of metal layer thickness.If the metallic particles of spraying is excessive, can lead It causes the metal layer porosity formed to increase, reduces the electrical property of reflecting surface.
Preferably, in step S3, described the step of coating glue-line includes: to coat normal-temperature curing epoxy on the surface of metal layer Resin adhesive, glue-spread 200g/m2~250g/m2
Preferably, the normal-temperature curing epoxy Resin adhesive includes J133 normal-temperature curing epoxy Resin adhesive.
It preferably, include: that will process by the step that the PMI foam reflecting surface is covered on the glue-line in step S4 Obtained PMI reflecting surface is placed on high-precision mold, production bag vacuum pressurization sizing, make PMI antenna reflective face with Mold is bonded completely.
Preferably, in step S4, the condition of the vacuum solidification: 20~30 DEG C of solidifications, curing time are 24~48h, at Type pressure is 0.05~0.097MPa.The purpose of vacuum solidification is to keep it complete with mold to PMI reflecting surface certain pressure Fitting.
Preferably, in step S4, the condition of the solidifying and setting are as follows: in 60 DEG C of solidifications, 3~4h or 80 DEG C of 1~2h of solidification.
Compared with prior art, the present invention have it is following the utility model has the advantages that
1, the present invention efficiently solves legacy cellular folder by high performance PMI foam applications in the preparation of antenna reflective face The problems such as layer antenna reflector complex process, long flow path, and significantly reduce the weight of antenna reflective face.
2, present invention uses the reflecting surface blank that the technique of thermoforming has obtained degree of precision, production efficiency is improved; Unstressed clamping is realized using the method for frost sucker clamping, avoids the stress of tradition machinery clamping generation to reflector precision Influence;It joined glycerol and Surfactant SDS in metal transfer film, improve the coating of transfer membrane, Improve metal spraying efficiency.
Detailed description of the invention
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other feature of the invention, Objects and advantages will become more apparent upon:
Fig. 1 is the ultralight high-precision rapid shaping antenna reflective face composition schematic diagram of the present invention;
Wherein: 1- high-precision reflecting surface shaping mould;2- surface metal-layer;3- glue-line;4-PMI foam reflecting surface.
Specific embodiment
The present invention is described in detail combined with specific embodiments below.Following embodiment will be helpful to the technology of this field Personnel further understand the present invention, but the invention is not limited in any way.It should be pointed out that the ordinary skill of this field For personnel, without departing from the inventive concept of the premise, several changes and improvements can also be made.These belong to the present invention Protection scope.
Embodiment 1
The present embodiment provides a kind of ultralight high-precision rapid shaping antenna reflective faces, as shown in Figure 1, including setting gradually Metal layer 2, glue-line 3 and PMI foam reflecting surface 4;The glue-line 3 is connect with the working face of PMI foam reflecting surface 4.
The aperture of the PMI foam reflecting surface is tiny and uniform, and aperture is 0.3~0.5mm, and the density of PMI foam is 110kg/m3
20~30 μm of the diameter of metallic particles in the metal layer, metal layer with a thickness of 0.05~0.2mm.
The adhesive that the glue-line uses is normal temperature cure J133 epoxy resin adhesive, the shear strength of the glue-line >=25MPa, peel strength >=20N/cm are -60~100 DEG C using temperature.
The present embodiment also provides a kind of preparation method of ultralight high-precision rapid shaping antenna reflective face, and specific steps are such as Under:
S1, PMI foam plate is placed on high-precision mold (RMS=8.8 μm), and make vacuum bag;
S2, the high-precision mold for carrying out vacuum bag and PMI foam plate are placed in baking oven, thermoforming process are as follows: room Temperature~200 DEG C, vacuumizes, vacuum pressure 0.097MPa, heat-insulation pressure keeping 1h, furnace cooling;
S3, the good PMI foam antenna reflective face blank of thermoforming is demoulded, is inhaled using the method for unstressed clamping in frost It is clamping in disk, PMI foam antenna reflective face is processed using high-precision milling machine, the type face precision of working face is 37.7 μm;
S4, preparing metal transfer membrane, by 5 parts of polyvinyl alcohol, 55 parts of distilled water, 40 parts of ethyl alcohol, 5 parts of glycerol, 5 parts of dodecanes Base sodium sulphate is uniformly mixed, and is uniformly brushed metal transfer film on high-precision mold (RMS=8.8 μm) using wool brush, It is whole to brush twice;
S5, method spray metal aluminium layer of the high-precision mold surface for brushing metal transfer film using flame-spraying is being applied, Metallic particles diameter≤25 μm that flame-spraying is formed, obtained 0.05~0.2mm of metal layer thickness;
S6, one layer of J133 normal-temperature curing epoxy Resin adhesive is coated on the high-precision mold for sprayed metal layer, apply Glue amount 200g/m2~250g/m2
S7, the PMI foam reflecting surface integral cap for processing S3 make vacuum on coated J133 adhesive Bag vacuumizes, and solidifies at 20~30 DEG C, and curing time is briquetting pressure 0.097MPa for 24 hours, solid after being then placed into baking oven Change sizing, 60 DEG C of solidification 3h;
After S9, demoulding, finally RMS=38.4 μm of surface precision of antenna reflective face obtained, the weight of reflecting surface are 5.7kg, the production cycle 7 days.
Embodiment 2
The present embodiment provides a kind of ultralight high-precision rapid shaping antenna reflective face with and preparation method thereof, the antenna is anti- It is same as Example 1 to penetrate face structure, it is specific the preparation method is as follows:
S1, PMI foam plate is placed on high-precision mold (RMS=8.8 μm), and make vacuum bag;
S2, the high-precision mold for carrying out vacuum bag and PMI foam plate are placed in baking oven, thermoforming system are as follows: room Temperature~200 DEG C, vacuumizes, vacuum pressure 0.097MPa, heat-insulation pressure keeping 1h, furnace cooling;
S3, the good PMI foam antenna reflective face blank of thermoforming is demoulded, is inhaled using the method for unstressed clamping in frost It is clamping in disk, PMI foam antenna reflective face is processed using high-precision milling machine, the type face precision of working face is 37.7 μm;
S4, preparing metal transfer membrane, by 5 parts of polyvinyl alcohol, 55 parts of distilled water, 40 parts of ethyl alcohol, 5 parts of glycerol, 5 parts of dodecanes Base sodium sulphate is uniformly mixed, and is uniformly brushed transfer membrane on high-precision mold (RMS=8.8 μm) using wool brush, whole It brushes twice.
S5, method spray metal aluminium layer of the high-precision mold surface for brushing metal transfer film using flame-spraying is being applied, Metallic particles diameter≤25 μm that flame-spraying is formed, obtained 0.05~0.2mm of metal layer thickness;
S6, one layer of J133 normal-temperature curing epoxy Resin adhesive is coated on the high-precision mold for sprayed metal layer, apply Glue amount 200g/m2~250g/m2
S7, the PMI foam reflecting surface integral cap for processing S3 make vacuum on coated J133 adhesive Bag vacuumizes, and solidifies at 20~30 DEG C, curing time 48h, briquetting pressure 0.05MPa, solid after being then placed into baking oven Change sizing, 80 DEG C of solidification 1h;
S8, RMS=40.3 μm of surface precision for demoulding aft antenna reflecting surface, the weight of reflecting surface are 5.5kg, production cycle 8 days.
Embodiment 3
The present embodiment provides a kind of ultralight high-precision rapid shaping antenna reflective face with and preparation method thereof, the antenna is anti- It is same as Example 1 to penetrate face structure, it is specific the preparation method is as follows:
S1, PMI foam plate is placed on high-precision mold (RMS=8.8 μm), and make vacuum bag;
S2, the high-precision mold for carrying out vacuum bag and PMI foam plate are placed in baking oven, thermoforming system are as follows: room Temperature~200 DEG C, vacuumizes, vacuum pressure 0.05MPa, heat-insulation pressure keeping 1.5h, furnace cooling;
S3, the good PMI foam antenna reflective face blank of thermoforming is demoulded, is inhaled using the method for unstressed clamping in frost It is clamping in disk, PMI foam antenna reflective face is processed using high-precision milling machine, the type face precision of working face is 37.7 μm;
S4, preparing metal transfer membrane, by 30 parts of polyvinyl alcohol, 70 parts of distilled water, 10 parts of ethyl alcohol, 3 parts of glycerol, 10 part 12 Sodium alkyl sulfate is uniformly mixed, and is uniformly brushed transfer membrane on high-precision mold (RMS=8.8 μm) using wool brush, whole Twice of body brushing.
S5, method spray metal aluminium layer of the high-precision mold surface for brushing metal transfer film using flame-spraying is being applied, 20-25 μm of the metallic particles diameter that flame-spraying is formed, obtained 0.05~0.2mm of metal layer thickness;
S6, one layer of J133 normal-temperature curing epoxy Resin adhesive is coated on the high-precision mold for sprayed metal layer, apply Glue amount 200g/m2~250g/m2
S7, the PMI foam reflecting surface integral cap for processing S3 make vacuum on coated J133 adhesive Bag vacuumizes, and solidifies at 20~30 DEG C, and curing time is briquetting pressure 0.097MPa for 24 hours, solid after being then placed into baking oven Change sizing, 60 DEG C of solidification 3-4h;
S8, RMS=44.7 μm of surface precision for demoulding aft antenna reflecting surface, the weight of reflecting surface are 6.2kg, production cycle 7 days.
Embodiment 4
The present embodiment provides a kind of ultralight high-precision rapid shaping antenna reflective face with and preparation method thereof, the antenna is anti- It is same as Example 1 to penetrate face structure;Specific preparation method is substantially the same manner as Example 1, the difference is that only: the present embodiment In step S4, metal transfer film uses 2 parts of polyvinyl alcohol, 40 parts of distilled water, 60 parts of ethyl alcohol, 10 parts of glycerol and 3 parts of dodecyls Sodium sulphate is prepared obtain after evenly mixing.
In the present embodiment, RMS=49.5 μm of surface precision of the antenna reflective face obtained after finally demoulding, the weight of reflecting surface Measuring is 5.8kg, the production cycle 7 days.
Comparative example 1
This comparative example is related to a kind of preparation method of antenna reflective face, specific steps are as follows:
S1, using automatic fiber placement technology, M55J/ cyanogen is coated on high-precision antenna reflector shaping mould (RMS=8.8 μm) Sour rouge hot melt prepreg, laying angle are [+45/0/-45/90]2s
S2, inside and outside covering is utilized into autoclave process curing molding, curing cycle are as follows: room temperature~120 DEG C, pressurization 0.5MPa, 120 DEG C of heat-insulation pressure keeping 8h, pressure release furnace cooling;
S3, the inside panel of forming is placed on high-precision inside panel shaping mould, using aluminum honeycomb as sandwich, is carried out Solidification by cement forms afterwards, briquetting pressure 0.2MPa.
S5, the high-precision inside panel molding mould surface coating aluminum layer in coating metal transfer film, J47C glue film is spread It is overlying on metallic aluminum, by reflection cover on resin, and vacuumizes solidification, 130 DEG C of temperature, vacuum pressure 0.097MPa, Time 3h.
S6, RMS=37.3 μm of surface precision for demoulding aft antenna reflecting surface, reflecting surface weight are 16.4kg, production cycle 20 days.
Comparative example 2
The preparation process of antenna reflective face in this comparative example are as follows:
S1, using automatic fiber placement technology, M55J/ cyanogen is coated on high-precision antenna reflector shaping mould (RMS=8.8 μm) Sour rouge hot melt prepreg, laying angle are [+45/0/-45/90]2s
S2, inside and outside covering is utilized into autoclave process curing molding, curing cycle are as follows: room temperature~120 DEG C, pressurization 0.5MPa, 120 DEG C of heat-insulation pressure keeping 8h, pressure release furnace cooling;
S3, the inside panel of forming is placed on high-precision inside panel shaping mould, using aluminum honeycomb as sandwich, is carried out Solidification by cement forms afterwards, briquetting pressure 0.2MPa.
S5, the high-precision inside panel molding mould surface coating aluminum layer in coating metal transfer film, J47C glue film is spread It is overlying on metallic aluminum, by reflection cover on resin, and vacuumizes solidification, 130 DEG C of temperature, vacuum pressure 0.05MPa, when Between 4h.
S6, RMS=39.6 μm of surface precision for demoulding aft antenna reflecting surface, reflecting surface weight are 16.9kg, production cycle 20 days.
Comparative example 3
This comparative example provides a kind of preparation method of antenna reflective face, and the antenna reflective face structure is same as Example 1; Specific preparation method is substantially the same manner as Example 1, and the difference is that only: in the step S4 of this comparative example, metal transfer film is adopted It is prepared obtained after evenly mixing with 5 parts of polyvinyl alcohol, 55 parts of distilled water, 40 parts of ethyl alcohol, 10 parts of glycerol.
In this comparative example, RMS=58.2 μm of surface precision of the antenna reflective face obtained after finally demoulding, the weight of reflecting surface Measuring is 5.9kg, the production cycle 7 days.
Effect compares:
The size of antenna reflective face RMS value and weight that above-described embodiment and comparative example obtain is as shown in table 1
Table 1
By above embodiments and comparative example it is found that based on PMI foam as main structure reflecting surface surface precision with Aluminum honeycomb sandwich structure reflecting surface is suitable, and the weight of antenna reflective face reduces 3 times, and the production cycle is obviously shortened.
Specific embodiments of the present invention are described above.It is to be appreciated that the invention is not limited to above-mentioned Particular implementation, those skilled in the art can make a variety of changes or modify within the scope of the claims, this not shadow Ring substantive content of the invention.In the absence of conflict, the feature in embodiments herein and embodiment can any phase Mutually combination.

Claims (10)

1. a kind of ultralight high-precision rapid shaping antenna reflective face, which is characterized in that the antenna reflective face includes setting gradually Metal layer, glue-line and PMI foam reflecting surface;The glue-line is connect with the working face of PMI foam reflecting surface.
2. ultralight high-precision rapid shaping antenna reflective face as described in claim 1, which is characterized in that the PMI foam is anti- It penetrates in face, the aperture of PMI foam is 0.1-0.5mm, and the density of PMI foam is 50~120kg/m3
3. ultralight high-precision rapid shaping antenna reflective face as described in claim 1, which is characterized in that golden in the metal layer 20~30 μm of the diameter of metal particles, metal layer with a thickness of 0.05~0.2mm.
4. a kind of preparation method of ultralight high-precision rapid shaping antenna reflective face according to claim 1, feature exist In including the following steps:
S1, PMI foam reflecting surface blank is prepared using thermoforming process;
S2, the PMI foam reflecting surface blank is processed, PMI foam reflecting surface is made;
S3, metal transfer film, the sprayed metal layer on the metal transfer film, in the metal layer are coated on high-precision mold Upper coating glue-line;
S4, the PMI foam reflecting surface prepared in step S2 is covered on the glue-line, is taken off after vacuum solidification and solidifying and setting Mould is to get the antenna reflective face.
5. the preparation method of ultralight high-precision rapid shaping antenna reflective face as claimed in claim 4, which is characterized in that step In S1, the condition of the thermoforming process are as follows: it is warming up to the softening temperature of PMI foam, is vacuumized, vacuum pressure 0.05- 0.097MPa, heat-insulation pressure keeping 0.5-1.5h, furnace cooling.
6. the preparation method of ultralight high-precision rapid shaping antenna reflective face as claimed in claim 4, which is characterized in that step In S2, the step of processing includes: after demoulding the PMI foam reflecting surface blank from high-precision mold, using without answering The method of power clamping is fixed in frost sucker, is processed using CNC milling machine;Process the obtained PMI foam reflector type face Precision RMS 0.01-0.05mm.
7. the preparation method of ultralight high-precision rapid shaping antenna reflective face as claimed in claim 4, which is characterized in that step In S3, the metal transfer film is by 2-30 parts of polyvinyl alcohol, 40-70 parts of distilled water, 10-60 parts of ethyl alcohol, 3-10 parts of glycerol, 3-10 Part lauryl sodium sulfate mixes.
8. the preparation method of ultralight high-precision rapid shaping antenna reflective face as claimed in claim 4, which is characterized in that step In S3, the step of sprayed metal layer includes: the mode using flame-spraying in the surface spray metal of metal transfer film;Institute Stating metal includes at least one of aluminium, nickel;20~30 μm of metallic particles diameter of the flame-spraying formation, obtained metal 0.05~0.2mm of thickness degree.
9. the preparation method of ultralight high-precision rapid shaping antenna reflective face as claimed in claim 4, which is characterized in that step In S3, described the step of coating glue-line includes: to coat normal-temperature curing epoxy Resin adhesive on the surface of metal layer, and glue-spread is 200g/m2~250g/m2
10. the preparation method of ultralight high-precision rapid shaping antenna reflective face as claimed in claim 4, which is characterized in that step In rapid S4, the condition of the vacuum solidification: 20~30 DEG C of solidifications, curing time are 24~48h, briquetting pressure is 0.05~ 0.097MPa;The condition of the solidifying and setting are as follows: in 60 DEG C of solidifications, 3~4h or 80 DEG C of 1~2h of solidification.
CN201811614560.0A 2018-12-27 2018-12-27 Ultralight high-precision rapid shaping antenna reflective face and preparation method thereof Pending CN109687159A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201811614560.0A CN109687159A (en) 2018-12-27 2018-12-27 Ultralight high-precision rapid shaping antenna reflective face and preparation method thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201811614560.0A CN109687159A (en) 2018-12-27 2018-12-27 Ultralight high-precision rapid shaping antenna reflective face and preparation method thereof

Publications (1)

Publication Number Publication Date
CN109687159A true CN109687159A (en) 2019-04-26

Family

ID=66190721

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201811614560.0A Pending CN109687159A (en) 2018-12-27 2018-12-27 Ultralight high-precision rapid shaping antenna reflective face and preparation method thereof

Country Status (1)

Country Link
CN (1) CN109687159A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110474153A (en) * 2019-07-31 2019-11-19 航天材料及工艺研究所 A kind of flexible high-precision parabola antenna and preparation method thereof
CN111864403A (en) * 2020-06-30 2020-10-30 上海复合材料科技有限公司 High-precision reflecting surface forming method

Citations (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1775507A (en) * 2005-10-18 2006-05-24 成都飞机工业(集团)有限责任公司 Thermal forming method for PMI foam laminated structure
CN101227029A (en) * 2008-01-24 2008-07-23 吴豪 Composite material satellite antenna reflection surface and manufacturing process thereof
CN201655975U (en) * 2009-10-21 2010-11-24 中国电子科技集团公司第五十四研究所 High-precision antenna reflector panel with light high-rigidity structure
CN103000995A (en) * 2012-12-12 2013-03-27 洛阳双瑞橡塑科技有限公司 Combined antenna housing
CN103042697A (en) * 2012-12-31 2013-04-17 北京玻钢院复合材料有限公司 Integral forming process of carbon fiber antenna reflecting surface
CN103247864A (en) * 2013-05-10 2013-08-14 中国电子科技集团公司第五十四研究所 High-precision spinning antenna reflecting surface and manufacturing method thereof
CN104162995A (en) * 2014-08-08 2014-11-26 西安拓飞复合材料有限公司 Manufacturing method for carbon fiber antenna surface
AU2013295249A1 (en) * 2012-07-24 2014-11-27 Evonik Operations Gmbh Novel shaping process for PMI foam materials and/or composite components produced therefrom
CN104767035A (en) * 2015-04-20 2015-07-08 中国电子科技集团公司第五十四研究所 High-precision carbon fiber auxiliary reflection face forming method
CN204516903U (en) * 2015-04-20 2015-07-29 中国电子科技集团公司第五十四研究所 A kind of novel high-precision carbon fiber subreflector
CN105034479A (en) * 2015-05-29 2015-11-11 杨建军 Metallized layer dielectric plate of polymethacrylimide foam base material
CN105479753A (en) * 2015-12-30 2016-04-13 中国人民解放军国防科学技术大学 Preparation method and preparation system of curved surface structured foam
CN105633590A (en) * 2015-12-30 2016-06-01 中国电子科技集团公司第三十九研究所 High-precision carbon fiber aluminum honeycomb sandwich structure reflecting surface manufacturing method
CN106739043A (en) * 2017-03-17 2017-05-31 零八电子集团四川天源机械有限公司 PMI foam layers radome of fighter and its manufacture method
CN106785415A (en) * 2016-12-08 2017-05-31 上海复合材料科技有限公司 The polymer matrix composites antenna house of body containing stereoscopic radiation and its forming method
CN206412482U (en) * 2016-12-20 2017-08-15 中国航空工业集团公司雷华电子技术研究所 A kind of two waveband common reflector reflecting surface structure
CN107738457A (en) * 2017-11-02 2018-02-27 中广核俊尔新材料有限公司 A kind of integrated forming technique of unmanned aerial vehicle body

Patent Citations (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1775507A (en) * 2005-10-18 2006-05-24 成都飞机工业(集团)有限责任公司 Thermal forming method for PMI foam laminated structure
CN101227029A (en) * 2008-01-24 2008-07-23 吴豪 Composite material satellite antenna reflection surface and manufacturing process thereof
CN201655975U (en) * 2009-10-21 2010-11-24 中国电子科技集团公司第五十四研究所 High-precision antenna reflector panel with light high-rigidity structure
AU2013295249A1 (en) * 2012-07-24 2014-11-27 Evonik Operations Gmbh Novel shaping process for PMI foam materials and/or composite components produced therefrom
CN108453993A (en) * 2012-07-24 2018-08-28 赢创罗姆有限公司 The new forming method and/or composite component prepared therefrom of PMI foamed materials
US20150174798A1 (en) * 2012-07-24 2015-06-25 Cornelia Zimmermann Novel shaping process for pmi foam materials and/or composite components produced therefrom
CN103000995A (en) * 2012-12-12 2013-03-27 洛阳双瑞橡塑科技有限公司 Combined antenna housing
CN103042697A (en) * 2012-12-31 2013-04-17 北京玻钢院复合材料有限公司 Integral forming process of carbon fiber antenna reflecting surface
CN103247864A (en) * 2013-05-10 2013-08-14 中国电子科技集团公司第五十四研究所 High-precision spinning antenna reflecting surface and manufacturing method thereof
CN104162995A (en) * 2014-08-08 2014-11-26 西安拓飞复合材料有限公司 Manufacturing method for carbon fiber antenna surface
CN104767035A (en) * 2015-04-20 2015-07-08 中国电子科技集团公司第五十四研究所 High-precision carbon fiber auxiliary reflection face forming method
CN204516903U (en) * 2015-04-20 2015-07-29 中国电子科技集团公司第五十四研究所 A kind of novel high-precision carbon fiber subreflector
CN105034479A (en) * 2015-05-29 2015-11-11 杨建军 Metallized layer dielectric plate of polymethacrylimide foam base material
CN105479753A (en) * 2015-12-30 2016-04-13 中国人民解放军国防科学技术大学 Preparation method and preparation system of curved surface structured foam
CN105633590A (en) * 2015-12-30 2016-06-01 中国电子科技集团公司第三十九研究所 High-precision carbon fiber aluminum honeycomb sandwich structure reflecting surface manufacturing method
CN106785415A (en) * 2016-12-08 2017-05-31 上海复合材料科技有限公司 The polymer matrix composites antenna house of body containing stereoscopic radiation and its forming method
CN206412482U (en) * 2016-12-20 2017-08-15 中国航空工业集团公司雷华电子技术研究所 A kind of two waveband common reflector reflecting surface structure
CN106739043A (en) * 2017-03-17 2017-05-31 零八电子集团四川天源机械有限公司 PMI foam layers radome of fighter and its manufacture method
CN107738457A (en) * 2017-11-02 2018-02-27 中广核俊尔新材料有限公司 A kind of integrated forming technique of unmanned aerial vehicle body

Non-Patent Citations (4)

* Cited by examiner, † Cited by third party
Title
吴利英: "复合材料制件表面金属化技术金属喷涂转移法", 《表面技术》 *
吴利英: "复合材料转移法金属化脱模剂工艺研究及应用", 《电子工艺技术》 *
姚卫国: "高分子表面金属化技术", 《化工进展》 *
苏航: "PMI 泡沫的热成型工艺研究及应用分析", 《安徽化工》 *

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110474153A (en) * 2019-07-31 2019-11-19 航天材料及工艺研究所 A kind of flexible high-precision parabola antenna and preparation method thereof
CN110474153B (en) * 2019-07-31 2021-02-09 航天材料及工艺研究所 Flexible high-precision parabolic antenna and preparation method thereof
CN111864403A (en) * 2020-06-30 2020-10-30 上海复合材料科技有限公司 High-precision reflecting surface forming method
CN111864403B (en) * 2020-06-30 2022-05-03 上海复合材料科技有限公司 High-precision reflecting surface forming method

Similar Documents

Publication Publication Date Title
CN106739043B (en) PMI foam sandwich aircraft radome and manufacturing method thereof
CN107134642B (en) The resistance to 450 DEG C of quartz/composite polyimide material antenna house of one kind and preparation method
CN110481059A (en) A kind of composite material foam sandwich construction and its forming method
CN106182801A (en) A kind of aircraft foam core filled composite material rudder face forming method
CN104162994B (en) A kind of manufacture method of carbon fiber parabola antenna
CN105633590B (en) A kind of high-precision carbon fiber aluminum honeycomb sandwich structure reflecting surface manufacture method
CN107538763B (en) A kind of processing method and curved surface honeycomb of curved surface honeycomb
CN104767035B (en) A kind of high-precision carbon fiber subreflector forming method
CN109687159A (en) Ultralight high-precision rapid shaping antenna reflective face and preparation method thereof
CN103407170A (en) Manufacturing method for satellite borne antenna reflecting surface
CN109130336A (en) A kind of high precision high stability composite material antenna reflective face and preparation method thereof
CN103935042B (en) The manufacture method of the hollow rotor of unmanned vehicle and hollow rotor
CN104441685A (en) Method for manufacturing carbon fiber composite S loudspeaker
CN112537047B (en) Forming and assembling method for composite material reflector
CN106867251A (en) A kind of prepreg and the method that honeycomb core is prepared by it
CN110422344A (en) A kind of satellite compound flywheel of large rotating inertia lightweight and preparation method thereof
CN101885215A (en) Forming method of composite material leaf grille for controlling speed of aviation aircraft
CN110216902A (en) A kind of metal rudder core adds the dead size RTM forming method of polymer matrix composites
JPWO2019188195A1 (en) Manufacturing method of fiber reinforced plastic
CN103057128A (en) Automatic heating and pressurization production process for composite material specially used for small-sized unmanned plane
CN105437569B (en) A kind of forming method of composite reflector
CN106881879A (en) A kind of method that use second bonding technique manufactures adhesive bonding of composites structure
CN108620593A (en) A kind of large-size ultra-thin Metal Substrate density gradient material and its preparation method and application
CN111055517B (en) XPS extruded sheet inner core and epoxy resin composite material glider wing and preparation method thereof
CN117341227A (en) High-strength carbon fiber shell forming process for unmanned aerial vehicle body

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
RJ01 Rejection of invention patent application after publication

Application publication date: 20190426

RJ01 Rejection of invention patent application after publication