CN116141651A - Shape memory material-based aircraft emergency slide and manufacturing method thereof - Google Patents
Shape memory material-based aircraft emergency slide and manufacturing method thereof Download PDFInfo
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- CN116141651A CN116141651A CN202310243206.6A CN202310243206A CN116141651A CN 116141651 A CN116141651 A CN 116141651A CN 202310243206 A CN202310243206 A CN 202310243206A CN 116141651 A CN116141651 A CN 116141651A
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- substrate
- shape memory
- crease
- crease group
- emergency slide
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- 239000012781 shape memory material Substances 0.000 title claims abstract description 42
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 17
- 239000000758 substrate Substances 0.000 claims abstract description 77
- 238000000034 method Methods 0.000 claims abstract description 20
- 239000012779 reinforcing material Substances 0.000 claims abstract description 17
- 238000010438 heat treatment Methods 0.000 claims abstract description 13
- 239000000463 material Substances 0.000 claims abstract description 5
- 238000001816 cooling Methods 0.000 claims abstract description 4
- 229920000431 shape-memory polymer Polymers 0.000 claims description 12
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 9
- 239000000835 fiber Substances 0.000 claims description 9
- 239000004593 Epoxy Substances 0.000 claims description 6
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims description 3
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 3
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 3
- 239000004642 Polyimide Substances 0.000 claims description 3
- 239000000853 adhesive Substances 0.000 claims description 3
- 230000001070 adhesive effect Effects 0.000 claims description 3
- 229910052796 boron Inorganic materials 0.000 claims description 3
- 239000006229 carbon black Substances 0.000 claims description 3
- 239000004917 carbon fiber Substances 0.000 claims description 3
- 239000002041 carbon nanotube Substances 0.000 claims description 3
- 229910021393 carbon nanotube Inorganic materials 0.000 claims description 3
- XLJMAIOERFSOGZ-UHFFFAOYSA-M cyanate Chemical compound [O-]C#N XLJMAIOERFSOGZ-UHFFFAOYSA-M 0.000 claims description 3
- 239000003365 glass fiber Substances 0.000 claims description 3
- 229910002804 graphite Inorganic materials 0.000 claims description 3
- 239000010439 graphite Substances 0.000 claims description 3
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 3
- 229920001721 polyimide Polymers 0.000 claims description 3
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 claims description 3
- 229910010271 silicon carbide Inorganic materials 0.000 claims description 3
- 229920001169 thermoplastic Polymers 0.000 claims description 3
- 229920001187 thermosetting polymer Polymers 0.000 claims description 3
- 239000004416 thermosoftening plastic Substances 0.000 claims description 3
- 230000008569 process Effects 0.000 abstract description 9
- 238000012423 maintenance Methods 0.000 abstract description 5
- 230000007246 mechanism Effects 0.000 abstract description 5
- 230000002411 adverse Effects 0.000 abstract description 3
- 230000000694 effects Effects 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 3
- 230000009477 glass transition Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000000638 stimulation Effects 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D25/00—Emergency apparatus or devices, not otherwise provided for
- B64D25/08—Ejecting or escaping means
-
- 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
- B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
- B29C53/02—Bending or folding
- B29C53/04—Bending or folding of plates or sheets
-
- 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
- B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
- B29C53/80—Component parts, details or accessories; Auxiliary operations
- B29C53/84—Heating or cooling
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Aviation & Aerospace Engineering (AREA)
Abstract
The invention provides an aircraft emergency slide based on shape memory materials and a manufacturing method thereof, wherein the method comprises the following steps: taking a substrate, wherein a first crease group and a second crease group are arranged on the substrate, a heating device is arranged at the first crease group and the second crease group, the first crease group of the substrate is heated to soften the first crease group of the substrate, and then the substrate is folded into a slide shape along the first crease group to cool and harden the substrate; the manufacturing materials of the substrate comprise shape memory materials and reinforcing materials; and heating the second crease group of the substrate to soften the second crease group of the substrate, folding the substrate along the second crease group, and cooling and hardening the substrate to obtain the folded airplane emergency slide based on the shape memory material. The shape memory material-based airplane emergency slide provided by the invention has the advantages of simple driving mechanism, stable unfolding process and lower maintenance cost, and can avoid adverse effects caused by the scratch and air leakage of the emergency slide.
Description
Technical Field
The invention relates to the technical field of emergency rescue equipment, in particular to an aircraft emergency slide based on a shape memory material and a manufacturing method thereof.
Background
There are a variety of emergency rescue devices on board an aircraft, one of which is an aircraft emergency slide, which must be released by crew members at a first time upon occurrence of an emergency situation, and which is therefore very important for aviation safety. Each gate and service gate of the aircraft has an emergency slide thereon that needs to be manually operated to help passengers and units escape in emergency situations, however, existing emergency slides are mostly of inflatable construction, and thus are easily scratched or punctured by sharp objects, which has a high probability of affecting the 90 second golden escape time. In addition, the inflatable emergency slide has the problems of complex driving mechanism, unstable unfolding process, air leakage, high maintenance cost and the like.
Disclosure of Invention
The invention solves the technical problems that the existing inflatable emergency slide structure has at least one of the problems of complex driving mechanism, unstable unfolding process, higher maintenance cost, easy breakage, air leakage and the like.
In order to solve the technical problems, the invention adopts the following technical scheme:
a method for manufacturing an aircraft emergency slide based on shape memory materials comprises the following steps:
s1, taking a substrate, wherein a first crease group and a second crease group are arranged on the substrate, a heating device is arranged at the first crease group and the second crease group, the first crease group of the substrate is heated so as to soften the first crease group of the substrate, and then the substrate is folded into a slide shape along the first crease group, so that the substrate is cooled and hardened; wherein, the manufacturing material of the substrate comprises a shape memory material and a reinforcing material;
and S2, heating the second crease group of the substrate to soften the second crease group of the substrate, then folding the substrate along the second crease group, and cooling and hardening the substrate to obtain the folded airplane emergency slide based on the shape memory material.
Preferably, the substrate is rectangular, the first crease group includes two first creases, the first creases are wavy and extend along the length direction of the substrate, and the two first creases are symmetrically distributed relative to the short side symmetry axis of the substrate and have peaks deviating from each other.
Preferably, the second crease group includes a plurality of second creases parallel to the short sides of the substrate, and the plurality of second creases are distributed at equal intervals and have the same length as the short sides of the substrate.
Preferably, the shape memory material comprises at least one of an epoxy thermoplastic shape memory polymer, an epoxy thermoset shape memory polymer, a polyimide shape memory polymer, and a cyanate shape memory polymer.
Preferably, the reinforcing material includes at least one of graphite fiber, carbon fiber, glass fiber, boron fiber, silicon carbide fiber, carbon powder, carbon black, carbon nanotube and nickel powder.
Preferably, the reinforcing material comprises 2% -80% of the total mass of the shape memory material and the reinforcing material.
Preferably, the heating device comprises one of a resistance wire, a conductive adhesive and an electrothermal film.
The invention also provides an aircraft emergency slide based on the shape memory material, which is manufactured by adopting the manufacturing method of the aircraft emergency slide based on the shape memory material.
Preferably, the substrate is rectangular, a third crease group is further arranged on the substrate, the third crease group comprises two third creases, the third creases are straight lines parallel to the long sides of the substrate, and the two third creases are symmetrically distributed relative to the symmetry axis of the short sides of the substrate.
Preferably, the substrate is rectangular, and a fourth crease group is further arranged on the substrate, the fourth crease group comprises a plurality of fourth creases, the fourth creases are elliptical, and the long axes of the fourth creases are coincident with the symmetry axes of the short sides of the substrate.
Compared with the prior art, the aircraft emergency slide based on the shape memory material is made of the shape memory material and the reinforcing material, the emergency slide is made in a paper folding-like mode, the reinforcing material can enable the emergency slide to have high strength, on the basis, the aircraft emergency slide can be unfolded and folded only through thermal stimulation, the emergency slide driving mechanism is simple, the unfolding process is stable, the maintenance cost is low, and because the unfolding process of the aircraft emergency slide does not involve inflation, adverse effects caused by the fact that the emergency slide is scratched and air leakage can be avoided.
Drawings
FIG. 1 is a flow chart of an aircraft emergency slide based on shape memory materials in an embodiment of the invention;
FIG. 2 is a schematic diagram of a substrate according to an embodiment of the invention;
FIG. 3 is a schematic illustration of an aircraft emergency slide based on shape memory materials in an expanded state in an embodiment of the invention;
FIG. 4 is a schematic illustration of an aircraft emergency slide based on shape memory material in a folded state in an embodiment of the invention;
FIG. 5 is a process diagram of an aircraft emergency slide based on shape memory materials from a folded state to an unfolded state in an embodiment of the invention;
FIG. 6 is a schematic illustration of a stretcher made in an embodiment of the invention;
FIG. 7 is a schematic diagram of a unit in an embodiment of the invention;
fig. 8 is a schematic view of a fabricated lifeboat in an embodiment of the present invention.
Reference numerals illustrate:
1. a substrate, 2, a first crease, 3, a second crease, 4, a third crease, 5 and a fourth crease.
Detailed Description
In order that the above objects, features and advantages of the invention will be readily understood, a more particular description of the invention will be rendered by reference to specific embodiments thereof which are illustrated in the appended drawings.
It should be noted that, without conflict, features in the embodiments of the present invention may be combined with each other. It should be noted that the terms "first," "second," and the like in the description and the claims of the present invention and the above figures are used for distinguishing between similar objects and not necessarily for describing a particular sequential or chronological order. It is to be understood that the data so used may be interchanged where appropriate such that the embodiments of the invention described herein may be implemented in sequences other than those illustrated or otherwise described herein. In the present invention, the symmetry axis of the short sides of the substrate 1 is understood to be a straight line passing through the midpoints of the two short sides of the substrate 1 at the same time.
As shown in fig. 1, an embodiment of the present invention provides a method for manufacturing an aircraft emergency slide based on a shape memory material, including:
step S1, taking a substrate 1, wherein a first crease group and a second crease group (shown in fig. 2) are arranged on the substrate 1, heating devices are arranged at the first crease group and the second crease group, the first crease group of the substrate 1 is heated so as to soften the first crease group of the substrate 1, and then the substrate 1 is folded into a slide shape (shown in fig. 3) along the first crease group, so that the substrate 1 is cooled and hardened; wherein, the manufacturing materials of the substrate 1 comprise shape memory materials and reinforcing materials;
and S2, heating the second crease group of the substrate 1 to soften the second crease group of the substrate 1, then folding the substrate 1 along the second crease group, and cooling and hardening the substrate 1 to obtain the folded airplane emergency slide (shown in fig. 4) based on the shape memory material.
When the airplane emergency slide prepared by the method disclosed by the embodiment of the invention is not used, the airplane emergency slide is in a folded state as shown in fig. 4, and the space occupied by the airplane emergency slide is relatively small, so that the airplane emergency slide is convenient to store. When an emergency situation occurs to the aircraft, the second crease group is heated by the heating device, so that the aircraft emergency slide can be opened to the unfolding state shown in fig. 3, and the process of converting the aircraft emergency slide from the folding state to the unfolding state is shown in fig. 5.
Compared with the prior art, the aircraft emergency slide based on the shape memory material is made of the shape memory material and the reinforcing material, the emergency slide is made in a paper folding-like mode, the reinforcing material can enable the emergency slide to have high strength, on the basis, the aircraft emergency slide can be unfolded and folded only through thermal stimulation, the aircraft emergency slide is simple in driving mechanism, stable in unfolding process and low in maintenance cost, and because the unfolding process of the aircraft emergency slide does not involve inflation, adverse effects caused by the fact that the emergency slide is scratched and air leakage can be avoided.
In an embodiment of the present invention, as shown in fig. 2, the substrate 1 is illustratively rectangular, the first crease group includes two first creases 2, the first creases 2 are wavy and extend along the length direction of the substrate 1, and the two first creases 2 are symmetrically distributed relative to the symmetry axis of the short side of the substrate 1 and have peaks facing away. The second crease group comprises a plurality of second creases 3 parallel to the short sides of the substrate 1, and the second creases 3 are distributed at equal intervals and have the same length as the short sides of the substrate 1. Preferably, each of said second folds 3 passes by a crest or trough of said first folds 2.
In an embodiment of the present invention, the shape memory material comprises at least one of an epoxy thermoplastic shape memory polymer, an epoxy thermoset shape memory polymer, a polyimide shape memory polymer, and a cyanate shape memory polymer. The glass transition temperature of the shape memory material is designed by changing the material proportion so as to meet the working requirement. For the aircraft emergency slide, the glass transition temperature can be adjusted to be about 200 ℃.
In an embodiment of the present invention, the reinforcing material includes at least one of graphite fiber, carbon fiber, glass fiber, boron fiber, silicon carbide fiber, carbon powder, carbon black, carbon nanotube and nickel powder. The reinforcing material accounts for 2% -80% of the total mass of the shape memory material and the reinforcing material.
In an embodiment of the invention, the heating device comprises one of a resistance wire, a conductive adhesive and an electrothermal film. Preferably, the heating device is an electrothermal film.
The embodiment of the invention also provides an aircraft emergency slide based on the shape memory material, which is manufactured by adopting the manufacturing method of the aircraft emergency slide based on the shape memory material.
In the embodiment of the present invention, the substrate 1 is rectangular, a third crease group is further disposed on the substrate 1, the third crease group includes two third creases 4, the third creases 4 are straight lines parallel to the long sides of the substrate 1, and the two third creases 4 are symmetrically distributed relative to the symmetry axis of the short sides of the substrate 1. After the aircraft emergency slide is unfolded, the first crease group and the second crease group are heated to soften the first crease group and the second crease group, the aircraft emergency slide is unfolded to be in the initial shape of the substrate 1, then the third crease group of the aircraft emergency slide is heated to soften the third crease group, the aircraft emergency slide is folded along the third crease group, and then the aircraft emergency slide can be folded to be in the stretcher shape (shown in fig. 6). When a large number of stretchers are needed when people suffer from more casualties on the airplane, the airplane emergency slide folded into the stretcher shape can be divided into a plurality of stretchers for rescue.
In the embodiment of the present invention, the substrate 1 is rectangular, and a fourth crease group is further disposed on the substrate 1, where the fourth crease group includes a plurality of fourth creases 5, and the fourth crease 5 is elliptical and has a long axis coincident with a symmetry axis of a short side of the substrate 1. After the aircraft emergency slide is unfolded, the first crease group and the second crease group are heated, so that the first crease group and the second crease group are softened, and the aircraft emergency slide is unfolded into the initial shape of the base plate 1. The aircraft emergency slide is divided into a plurality of units along the length direction (shown in fig. 7), each unit only comprises a fourth crease 5, the fourth crease 5 of the unit is heated to soften the fourth crease 5, the unit is folded along the fourth crease 5, and after the shape is adjusted, the aircraft emergency slide can be folded into the shape of a lifeboat (shown in fig. 8). When the aircraft falls to the barren island due to special conditions, the aircraft emergency slide can be divided into a plurality of units, and then the units are folded to form the lifeboat for escape or lifesaving. In the present invention, the initial shape of the substrate 1, that is, the shape of the substrate 1 when not folded in step S1.
In addition, although the present disclosure is disclosed above, the scope of the present disclosure is not limited thereto. Various changes and modifications may be made by one skilled in the art without departing from the spirit and scope of the disclosure, and these changes and modifications will fall within the scope of the disclosure.
Claims (10)
1. The method for manufacturing the aircraft emergency slide based on the shape memory material is characterized by comprising the following steps of:
s1, taking a substrate (1), wherein a first crease group and a second crease group are arranged on the substrate (1), heating devices are arranged at the first crease group and the second crease group, the first crease group of the substrate (1) is heated so as to soften the first crease group of the substrate (1), and then the substrate (1) is folded into a slide shape along the first crease group, so that the substrate (1) is cooled and hardened; wherein the manufacturing material of the substrate (1) comprises a shape memory material and a reinforcing material;
and S2, heating the second crease group of the substrate (1) to soften the second crease group of the substrate (1), then folding the substrate (1) along the second crease group, and cooling and hardening the substrate (1) to obtain the folded airplane emergency slide based on the shape memory material.
2. The method for manufacturing the airplane emergency slide based on the shape memory material according to claim 1, wherein the base plate (1) is rectangular, the first crease group comprises two first creases (2), the first creases (2) are wavy and extend along the length direction of the base plate (1), and the two first creases (2) are symmetrically distributed relative to the symmetry axis of the short side of the base plate (1) and have wave peaks which are opposite.
3. The method for manufacturing an aircraft emergency slide based on shape memory materials according to claim 2, characterized in that the second crease group comprises a plurality of second creases (3) parallel to the short sides of the substrate (1), wherein the plurality of second creases (3) are distributed at equal intervals and have the same length as the short sides of the substrate (1).
4. The method of claim 1, wherein the shape memory material comprises at least one of an epoxy thermoplastic shape memory polymer, an epoxy thermoset shape memory polymer, a polyimide shape memory polymer, and a cyanate shape memory polymer.
5. The method of claim 1, wherein the reinforcing material comprises at least one of graphite fiber, carbon fiber, glass fiber, boron fiber, silicon carbide fiber, carbon powder, carbon black, carbon nanotubes, and nickel powder.
6. The method of making an aircraft emergency slide based on shape memory materials according to claim 1, wherein the reinforcing material comprises 2% -80% of the total mass of the shape memory material and the reinforcing material.
7. The method of claim 1, wherein the heating device comprises one of a resistive wire, a conductive adhesive, and an electrothermal film.
8. An aircraft emergency slide based on shape memory material, characterized in that it is manufactured by the method for manufacturing an aircraft emergency slide based on shape memory material according to any one of claims 1-7.
9. The aircraft emergency slide based on shape memory materials according to claim 8, characterized in that the base plate (1) is rectangular, a third crease group is further arranged on the base plate (1), the third crease group comprises two third creases (4), the third creases (4) are straight lines parallel to the long sides of the base plate (1), and the two third creases (4) are symmetrically distributed relative to the symmetry axis of the short sides of the base plate (1).
10. The shape memory material based aircraft emergency slide according to claim 8, characterized in that the base plate (1) is rectangular, a fourth crease group is further provided on the base plate (1), the fourth crease group comprises a plurality of fourth creases (5), the fourth crease (5) is elliptical, and the long axis of the fourth crease is coincident with the short side symmetry axis of the base plate (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310243206.6A CN116141651A (en) | 2023-03-14 | 2023-03-14 | Shape memory material-based aircraft emergency slide and manufacturing method thereof |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310243206.6A CN116141651A (en) | 2023-03-14 | 2023-03-14 | Shape memory material-based aircraft emergency slide and manufacturing method thereof |
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| CN116141651A true CN116141651A (en) | 2023-05-23 |
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| CN202310243206.6A Pending CN116141651A (en) | 2023-03-14 | 2023-03-14 | Shape memory material-based aircraft emergency slide and manufacturing method thereof |
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Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101797805A (en) * | 2010-02-01 | 2010-08-11 | 哈尔滨工业大学 | Method for manufacturing inflatable expansion wing skin based on shape memory polymer |
| CN105461946A (en) * | 2015-12-14 | 2016-04-06 | 哈尔滨工业大学 | Deformation-controllable shape memory composite material and deformation method thereof |
| CN108987880A (en) * | 2018-07-25 | 2018-12-11 | 哈尔滨工业大学 | Deployable antenna basic unit, deployable antenna and method for folding based on paper folding |
| CN110843312A (en) * | 2019-11-26 | 2020-02-28 | 哈尔滨工程大学 | Grid-reinforced intelligent paper folding composite material structure design method |
| CN111328182A (en) * | 2018-12-13 | 2020-06-23 | 哈尔滨工业大学 | Deformed circuit board based on shape memory polymer composite material |
| CN112373163A (en) * | 2020-11-26 | 2021-02-19 | 北京航空航天大学 | Air inflation and expansion composite material structure capable of being rigidized |
-
2023
- 2023-03-14 CN CN202310243206.6A patent/CN116141651A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101797805A (en) * | 2010-02-01 | 2010-08-11 | 哈尔滨工业大学 | Method for manufacturing inflatable expansion wing skin based on shape memory polymer |
| CN105461946A (en) * | 2015-12-14 | 2016-04-06 | 哈尔滨工业大学 | Deformation-controllable shape memory composite material and deformation method thereof |
| CN108987880A (en) * | 2018-07-25 | 2018-12-11 | 哈尔滨工业大学 | Deployable antenna basic unit, deployable antenna and method for folding based on paper folding |
| CN111328182A (en) * | 2018-12-13 | 2020-06-23 | 哈尔滨工业大学 | Deformed circuit board based on shape memory polymer composite material |
| CN110843312A (en) * | 2019-11-26 | 2020-02-28 | 哈尔滨工程大学 | Grid-reinforced intelligent paper folding composite material structure design method |
| CN112373163A (en) * | 2020-11-26 | 2021-02-19 | 北京航空航天大学 | Air inflation and expansion composite material structure capable of being rigidized |
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