CN106393902A - Nanometer modified capsule material for high-altitude aerostat and preparation method thereof - Google Patents

Nanometer modified capsule material for high-altitude aerostat and preparation method thereof Download PDF

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Publication number
CN106393902A
CN106393902A CN201610768327.2A CN201610768327A CN106393902A CN 106393902 A CN106393902 A CN 106393902A CN 201610768327 A CN201610768327 A CN 201610768327A CN 106393902 A CN106393902 A CN 106393902A
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layer
nano modification
nano
mechanical structure
envelop materialses
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CN106393902B (en
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郭齐红
张丽娇
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Iridium Gasman Aviation Technology Group Co ltd
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EAGLES MEN AERONAUTIC SCIENCE AND TECHNOLOGY GROUP Co Ltd
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    • 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
    • B32B5/02—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 structural features of a fibrous or filamentary layer
    • B32B5/024—Woven fabric
    • 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
    • B32B27/08—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 synthetic resin
    • 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
    • B32B27/28—Layered products comprising a layer of synthetic resin comprising synthetic resins not wholly covered by any one of the sub-groups B32B27/30 - B32B27/42
    • 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
    • B32B27/40—Layered products comprising a layer of synthetic resin comprising polyurethanes
    • 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
    • B32B33/00—Layered products characterised by particular properties or particular surface features, e.g. particular surface coatings; Layered products designed for particular purposes not covered by another single class
    • 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
    • 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
    • B32B38/00—Ancillary operations in connection with laminating processes
    • 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
    • B32B38/00—Ancillary operations in connection with laminating processes
    • B32B38/0008—Electrical discharge treatment, e.g. corona, plasma treatment; wave energy or particle radiation
    • 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
    • B32B2255/00—Coating on the layer surface
    • B32B2255/10—Coating on the layer surface on synthetic resin layer or on natural or synthetic rubber 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
    • B32B2255/00—Coating on the layer surface
    • B32B2255/26—Polymeric coating
    • 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
    • B32B2307/552—Fatigue strength
    • 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
    • B32B2307/724—Permeability to gases, adsorption
    • B32B2307/7242—Non-permeable
    • 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
    • B32B2605/18—Aircraft

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  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Thermal Sciences (AREA)
  • Laminated Bodies (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)

Abstract

The invention specifically relates to a nanometer modified capsule material for a high-altitude aerostat and a preparation method thereof, belonging to the field of aerospace materials. The capsule material comprises a blocking weather-proof film, a nanometer modified glue solution layer, a mechanical structure layer and a nanometer modified welding glue solution layer, wherein one surface of the mechanical structure layer is connected with the blocking weather-proof film through the nanometer modified glue solution layer while the other surface of the mechanical structure layer is connected with the nanometer modified welding glue solution layer; the mechanical structure layer is a PBO high-strength fiber plain weave fabric; and the nanometer modified welding glue solution layer is a polyurethane hot melt adhesive with a nano-material. The capsule material prepared in the invention has the beneficial effects of high strength, light weight, low helium permeability, good weatherability, strong performance in preventing a capsule from absorption of sun light energy in flight during daytime; and the preparation method is easy to operate and control.

Description

Envelop materialses of high-altitude aerostatics a kind of of nano modification and preparation method thereof
Technical field
The invention belongs to aerospace material field is and in particular to a kind of envelop materialses of the high-altitude aerostatics of nano modification And preparation method thereof.
Background technology
High-altitude aerostatics be a kind of containing propulsion plant, controllable flight, rely on the new near space of uplift work in sky Multi-functional flying platform, working depth height above sea level about 20Km.It is pre- in military surveillance, space that the flight characteristic of aerostatics determines it The fields such as police, communication relay and space exploration have broad application prospects, thus are extensively favored by various countries scientist.But The aloft work environment of aerostatics is very harsh：Temperature is low, day and night temperature is big；Atmospheric density is low；Ultraviolet radiation, ozonization Strongly.Work under this kind of environment, require skin material to have extremely low surface density first, too high material surface density makes floating The uplift of device is greatly lost it is difficult to be raised to advection layer height；In order to resist intensive ultraviolet radiation and ozone oxidation it is desirable to cover Leather material has good weatherability；Aerostatics internal temperature is continually changing, and causes eyelid covering inside and outside differential pressure to increase, to floating during long boat For pocket, overcome the pressure reduction that temperature change causes particularly important；Adopt helium as buoyance lift gas more aerostatics, stay sky for a long time Operating characteristic require skin material must to have splendid resistance helium leakage；Due to aerostatics during its military service eyelid covering Inside and outside have pressure reduction therefore skin material and must have enough mechanical properties；It is to keep aerostatics profile to also need to eyelid covering simultaneously Material possesses excellent creep-resistant property, sewing process and is easy to the characteristic repaired.The skin material of high-altitude aerostatics in order to Meet above-mentioned combination property to require, generally adopt multi-layer compound structure, disclosed is mainly by weathering layer, bearing layer, resistance Interlayer and weld layer glued joint compound multiple structure successively.
Application for a patent for invention publication No. CN103692737 discloses a kind of skin material and its preparation side of high-altitude aerostatics Method.Skin material is a kind of to be aluminized high-resistant diaphragm, bearing layer, the cementing height being composited of weld layer by weathering layer, dual-layer, single-sided Obstruct, high intensity, areal density material.The weathering layer of described high-altitude aerostatics skin material has high-weatherability；Dual-layer, single-sided High-resistant diaphragm of aluminizing realizes the high barrier of material and the absorptivity-emissivity ratio low to solar spectrum, effectively stops visible ray to illiteracy The destruction of leather material；Aromatic polyester fibres tissue layer, as bearing layer, realizes the good mechanical property of skin material after being combined； Machine-shaping by the high-frequency welding functional realiey aerostatics of weld layer.The shortcoming of this invention is that combination property need to carry further High.
Content of the invention
Not enough for prior art, the present invention provides a kind of envelop materialses of the high-altitude aerostatics of nano modification, including resistance Every weathering film layer, nano modification glue layer, mechanical structure layer and nano modification solder paste liquid layer, the one side of mechanical structure layer is passed through Nano modification glue layer is connected with intercepting weathering film layer, and the another side of mechanical structure layer is connected with nano modification solder paste liquid layer Connect, mechanical structure layer is PBO high-intensity fiber plain weave cloth, nano modification solder paste liquid layer is the polyurethane adding nano material PUR.
The described weathering film layer that intercepts is to aluminize TPU membrane through the single-layer double-side of PVDF coating treatment, and thickness is 10～20 μm.
Described nano modification glue layer is the polyurethane glue adding nano material, and the addition of nano material is 0.5%- 1%.
The horizontal radical of described PBO high-intensity fiber plain weave cloth is equal with vertical radical, respectively for 10-15 root/cm.
Intercept weathering layer and pass through the deposited conjunction of dry method coating technique to PBO high-intensity fiber plain weave cloth, nano modification glue layer Transferred to by way of roller coat on PBO high-intensity fiber plain weave cloth.
Described nano modification solder paste liquid layer thickness is 10-20 μm.
The preparation method of envelop materialses of the present invention comprises the following steps：
Step one：Carry out glueing joint compound by laminating machine single-layer double-side is aluminized TPU membrane, after corona, even spread is received After the modified polyurethane glue of rice, fit with the PBO high-intensity fiber plain weave cloth after corona, be combined after finishing, winding, Ripening 24 hours at a temperature of 80 DEG C～100 DEG C, obtains ripening completely Compound Fabric；
Step 2：The Compound Fabric surface blade coating that step one is obtained adds the polyurethane hot melt of nano material, through long Laminating mould release membrance after drying tunnel drying, and wind ripening, obtain described envelop materialses.
Compared with prior art, the invention has the beneficial effects as follows：Achieve described envelop materialses intensity height, light weight, helium Gas permeability is low and the combination property such as little to the absorption of solar energy when good weatherability, utricule flight on daytime, and preparation method is easy to Operation and control.Specifically, the main superior effect of the present invention is embodied in the following aspects：
1st, obstruct weathering layer of the present invention is aluminized TPU membrane using through PVDF coating treatment single-layer double-side, and conventional Double-deck aluminized polyester film is compared, good barrier property, and aluminium coated is difficult to shift, and has the performance of excellent reflected sunlight and excellent Weatherability, reduce the difficulty of technique compared with duplicature, improve the efficiency of processing, beneficial to mass production.
2nd, the polyurethane glue that nano material of the present invention is modified carrys out bonding and intercepts weathering layer and mechanical structure layer, Adhesive property and the rub resistance spread with high-quality are little, about 5-10g/m2.
3rd, mechanical structure layer choosing of the present invention PBO high-intensity fiber plain weave cloth, more conventional vectran fiber has There is density low, intensity is high, gained fabric surface density is only 45～55g/m2, intensity not any weakening, reach light weight high Strong requirement.
4th, solder paste liquid layer of the present invention employs through nano-material modified polyurethane hot melt, has excellent Intercept effect of sunlight, and sweat soldering effect is good.
Brief description
Fig. 1 is the version schematic diagram of envelop materialses of the present invention；
Fig. 2 is the preparation technology flow chart of envelop materialses of the present invention.
Shown in figure：1- intercepts weathering layer, 2- nano modification glue layer, 3- mechanical structure layer, 4- nano modification solder paste Liquid layer.
Specific embodiment
In order to get more information about the structure of described envelop materialses, illustrate below in conjunction with the accompanying drawings.
Embodiment 1
As shown in figure 1, envelop materialses of the present invention include intercepting weathering film layer 1, nano modification glue layer 2, mechanics knot Structure layer 3 and nano modification solder paste liquid layer 4, mechanical structure layer 3 is PBO high-intensity fiber plain weave cloth, the one of mechanical structure layer 3 Face is passed through nano modification glue layer 2 and is connected with intercepting weathering film layer 1, and the another side of mechanical structure layer 3 is welded with nano modification Glue layer 4 is connected, and nano modification solder paste liquid layer 4 is the polyurethane hot melt adding nano material.
Described obstruct weathering film layer 1 is that surface treated single-layer double-side is aluminized TPU membrane, and thickness is 10～20 μm.
Described nano modification glue layer 2 is the polyurethane glue adding nano material, and the addition of nano material is 0.5%-1%.
The horizontal radical of described PBO high-intensity fiber plain weave cloth is equal with vertical radical, respectively for 10-15 root/cm.
Intercept weathering layer 1 and pass through the deposited conjunction of dry method coating technique to PBO high-intensity fiber plain weave cloth, nano modification glue layer 2 are transferred on PBO high-intensity fiber plain weave cloth by way of roller coat.
Described nano modification welding glue 4 thickness degree is 10-20 μm.
Embodiment 2
As shown in Fig. 2 the preparation method of envelop materialses of the present invention comprises the following steps：
Step one：Carry out glueing joint compound by laminating machine single-layer double-side is aluminized TPU membrane, after corona, even spread is received After the modified polyurethane glue of rice, fit with the PBO high-intensity fiber plain weave cloth after corona, be combined after finishing, winding, Ripening one day at a temperature of 80 DEG C～100 DEG C, obtains ripening completely Compound Fabric；
Step 2：The Compound Fabric surface blade coating that step one is obtained adds the polyurethane hot melt of nano material, through long Laminating mould release membrance after drying tunnel drying, and wind ripening, obtain described envelop materialses.
It is combined with PBO high-intensity fiber plain weave cloth using the two-sided aluminizer of TPU in present embodiment, and used warp Cross the adhesive of the polyurethane bicomponent of nano modification, improve the rub resistance energy of described envelop materialses, TPU aluminizes on surface reflection Sunlight ability is strong, and the weatherability of TPU just very excellent skill itself, to realize aerostatics in high outage ultraviolet radiation and ozone Stay sky for a long time under corrosive environment, reduce the complexity of technique, mechanical property is not declined with resistance helium seepage property.That adds receives Rice material can stop the absorption of sunlight and the absorption of energy, reduce the pressure reduction causing due to the temperature difference, improve material Safety coefficient.
It is used PBO high-intensity fiber plain cloth as the mechanical structure layer of described envelop materialses in present embodiment, can reach Purpose to the high-strength light of material.
Application examples
The specific performance evaluation data of described envelop materialses is as follows：
1st, described envelop materialses after being embodied as, according to ASTM D1434 standard, the test resistance leakage experiment of helium draws Result is respectively：60.34ml/(m2·24h·0.1MPa)、69.41ml/(m2·24h·0.1MPa)、89.11ml/(m2· 24h·0.1MPa).
2nd, described envelop materialses after being embodied as, surface density test experiments result such as following table：
It is 80～100g/ that envelop materialses amount to grammes per square metre.
3rd, described envelop materialses after being embodied as, adopt hot weld connection technology to weld with self-control heat seal band, record peel strength Reach 80-110N/80mm.
4th, after being embodied as, the tensile strength test of described envelop materialses is according to GB/T 3820-1997, drawn testing machine Test, the warp-wise tensile strength of envelop materialses is 650N/cm, and broadwise tensile strength is 679N/cm.
Obviously, the above embodiment of the present invention is only intended to clearly illustrate example of the present invention, and is not right The restriction of embodiments of the present invention, for those of ordinary skill in the field, also may be used on the basis of the above description To make other changes in different forms, all of embodiment cannot be exhaustive here, every belong to this Obvious change that bright technical scheme is extended out or change the row still in protection scope of the present invention.

Claims (7)

1. the envelop materialses of the high-altitude aerostatics of a kind of nano modification, including obstruct weathering film layer, nano modification glue layer, mechanics Structure sheaf and nano modification solder paste liquid layer, the one side of mechanical structure layer is passed through nano modification glue layer and is intercepted weathering film layer phase Connect, the another side of mechanical structure layer is connected with nano modification solder paste liquid layer, mechanical structure layer is PBO high-intensity fiber plain weave Woven cloth, nano modification solder paste liquid layer is the polyurethane hot melt adding nano material.
2. according to claim 1 envelop materialses it is characterised in that：Described obstruct weathering film layer is through PVDF coating treatment Single-layer double-side aluminize TPU membrane, thickness is 10～20 μm.
3. according to claim 1 envelop materialses it is characterised in that：Described nano modification glue layer is to add nano material Polyurethane glue, the addition of nano material is 0.5%-1%.
4. according to claim 1 envelop materialses it is characterised in that：The horizontal radical of described PBO high-intensity fiber plain weave cloth Equal with vertical radical, respectively for 10-15 root/cm.
5. according to claim 1 envelop materialses it is characterised in that：Intercept weathering layer to arrive by the deposited conjunction of dry method coating technique PBO high-intensity fiber plain weave cloth, nano modification glue layer transfers to PBO high-intensity fiber plain weave cloth by way of roller coat On.
6. according to claim 1 envelop materialses it is characterised in that：Described nano modification solder paste liquid layer thickness is 10-20 μ m.
7. a kind of method of the envelop materialses of high-altitude aerostatics preparing nano modification, it comprises the following steps：
Step one：Be first by laminating machine single-layer double-side is aluminized TPU membrane carry out glueing joint compound, after corona, even spread After the polyurethane glue of nano modification, fit with the PBO high-intensity fiber plain weave cloth after corona, be combined after finishing, winding, Ripening one day at a temperature of 80 DEG C～100 DEG C, obtains ripening completely Compound Fabric；
Step 2：The Compound Fabric surface blade coating that step one is obtained adds the polyurethane hot melt of nano material, through long drying tunnel Laminating mould release membrance after drying, and wind ripening, obtain described envelop materialses.
CN201610768327.2A 2016-08-30 2016-08-30 A kind of envelop materials and preparation method thereof of the high-altitude aerostatics of nano modification Active CN106393902B (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107039561A (en) * 2017-05-18 2017-08-11 青岛三合兴华科技发展有限公司 The preparation method of the ultralight solar cell substrate of composite
CN107101927A (en) * 2017-05-08 2017-08-29 中国科学院光电研究院 A kind of experimental provision and method for aerostatics envelop materialses testing permeability
WO2019095624A1 (en) * 2017-11-15 2019-05-23 东莞前沿技术研究院 Balloon material, raw material composition thereof, and aerostat
CN111590981A (en) * 2020-05-12 2020-08-28 中国乐凯集团有限公司 Skin material for stratospheric airship and preparation method thereof

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201970524U (en) * 2010-08-12 2011-09-14 郭颀 Light capsule composite material with heat reflecting layer
CN102416739A (en) * 2011-08-19 2012-04-18 北京航空航天大学 Airship sheath material and preparation method thereof
CN104772962A (en) * 2015-03-25 2015-07-15 东莞前沿技术研究院 Stratospheric aerostat skin and production method thereof
CN204640999U (en) * 2015-03-25 2015-09-16 东莞前沿技术研究院 Stratosphere aerostatics covering
CN105173052A (en) * 2015-02-10 2015-12-23 东莞前沿技术研究院 Bag skin material and aerostat
CN105836104A (en) * 2016-05-03 2016-08-10 中国乐凯集团有限公司 Solar unmanned aerial vehicle wing cover material and preparing method thereof

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201970524U (en) * 2010-08-12 2011-09-14 郭颀 Light capsule composite material with heat reflecting layer
CN102416739A (en) * 2011-08-19 2012-04-18 北京航空航天大学 Airship sheath material and preparation method thereof
CN105173052A (en) * 2015-02-10 2015-12-23 东莞前沿技术研究院 Bag skin material and aerostat
CN104772962A (en) * 2015-03-25 2015-07-15 东莞前沿技术研究院 Stratospheric aerostat skin and production method thereof
CN204640999U (en) * 2015-03-25 2015-09-16 东莞前沿技术研究院 Stratosphere aerostatics covering
CN105836104A (en) * 2016-05-03 2016-08-10 中国乐凯集团有限公司 Solar unmanned aerial vehicle wing cover material and preparing method thereof

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
刘军虎: "平流层飞艇蒙皮材料的研究现状", 《信息记录材料》 *
周惠久等: "《新材料辞典》", 31 December 1996, 上海科学技术文献出版社 *
廖双泉等: "《热塑性弹性体及其应用》", 30 April 2014, 中国石化出版社 *

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107101927A (en) * 2017-05-08 2017-08-29 中国科学院光电研究院 A kind of experimental provision and method for aerostatics envelop materialses testing permeability
CN107101927B (en) * 2017-05-08 2024-03-22 中国科学院光电研究院 Experimental device and method for permeability test of aerostat capsule material
CN107039561A (en) * 2017-05-18 2017-08-11 青岛三合兴华科技发展有限公司 The preparation method of the ultralight solar cell substrate of composite
WO2019095624A1 (en) * 2017-11-15 2019-05-23 东莞前沿技术研究院 Balloon material, raw material composition thereof, and aerostat
CN111590981A (en) * 2020-05-12 2020-08-28 中国乐凯集团有限公司 Skin material for stratospheric airship and preparation method thereof

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