KR101652708B1 - Reconfigurable deployble tubes with superelastic materials - Google Patents
Reconfigurable deployble tubes with superelastic materials Download PDFInfo
- Publication number
- KR101652708B1 KR101652708B1 KR1020150082807A KR20150082807A KR101652708B1 KR 101652708 B1 KR101652708 B1 KR 101652708B1 KR 1020150082807 A KR1020150082807 A KR 1020150082807A KR 20150082807 A KR20150082807 A KR 20150082807A KR 101652708 B1 KR101652708 B1 KR 101652708B1
- Authority
- KR
- South Korea
- Prior art keywords
- shape memory
- tube body
- tube
- memory member
- shape
- Prior art date
Links
- 239000000463 material Substances 0.000 title claims abstract description 35
- 239000003351 stiffener Substances 0.000 claims abstract description 26
- 239000013013 elastic material Substances 0.000 claims description 18
- 238000000034 method Methods 0.000 claims description 15
- 239000002041 carbon nanotube Substances 0.000 claims description 10
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 9
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 9
- 239000004917 carbon fiber Substances 0.000 claims description 9
- 229910021393 carbon nanotube Inorganic materials 0.000 claims description 9
- 239000002245 particle Substances 0.000 claims description 7
- 239000002759 woven fabric Substances 0.000 claims description 7
- 229910001285 shape-memory alloy Inorganic materials 0.000 claims description 3
- 229910052710 silicon Inorganic materials 0.000 claims description 3
- 239000010703 silicon Substances 0.000 claims description 3
- 229920002050 silicone resin Polymers 0.000 claims description 3
- 230000004044 response Effects 0.000 claims description 2
- 229920000431 shape-memory polymer Polymers 0.000 description 18
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 8
- 238000005452 bending Methods 0.000 description 7
- 239000002131 composite material Substances 0.000 description 7
- 238000011161 development Methods 0.000 description 6
- 230000009477 glass transition Effects 0.000 description 5
- 230000002441 reversible effect Effects 0.000 description 5
- 238000005516 engineering process Methods 0.000 description 4
- 239000010408 film Substances 0.000 description 4
- 229920000642 polymer Polymers 0.000 description 4
- 229920005989 resin Polymers 0.000 description 3
- 239000011347 resin Substances 0.000 description 3
- 239000012781 shape memory material Substances 0.000 description 3
- 238000003860 storage Methods 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000000835 fiber Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 230000003446 memory effect Effects 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 239000010409 thin film Substances 0.000 description 2
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 229920001971 elastomer Polymers 0.000 description 1
- 230000001747 exhibiting effect Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 230000006870 function Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000001151 other effect Effects 0.000 description 1
- 229920002635 polyurethane Polymers 0.000 description 1
- 239000004814 polyurethane Substances 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000012827 research and development Methods 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 230000000930 thermomechanical effect Effects 0.000 description 1
- 230000036962 time dependent Effects 0.000 description 1
- 239000013585 weight reducing agent Substances 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/66—Arrangements or adaptations of apparatus or instruments, not otherwise provided for
-
- B64G2001/224—
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
Abstract
Disclosed is a variable opening type tube using a superelastic material. The variable opening type tube of the present invention comprises a tube body which is hollow inside and a tube extending in the longitudinal direction inside the tube body, And a plurality of stiffeners that are disposed with the stiffener disposed therebetween.
Description
The present invention relates to a variable deployment tube using a superelastic material.
Recently, the meteorological environment is rapidly changing around the world, and it is attempted to develop satellites having high performance for precise and rapid prediction of global weather. Specifically, research on ultra-large space structures for advanced satellite mission and maximizing performance has been conducted mainly in developed countries such as the United States, Europe, and Japan.
In particular, the structure technology that develops in space orbit is a core technology required for all space structures such as communication / image opening antenna, solar panel and so on. However, since the conventional unfolded space structure mostly follows the mechanical expansion method, the weight of the expansion device takes a relatively large proportion, and the deployment mechanism parts may occupy 90% or more of the total structure.
According to such a conventional mechanical expansion method, excessive weight problems and a problem of securing a storage space existed. To cope with such problems, enormous research and development costs were forced to be put into. The background technology of the present application is disclosed in Korean Patent Laid-Open Publication No. 2011-0133756.
SUMMARY OF THE INVENTION The present invention has been made in order to solve the problems of the prior art described above and to provide a variable expansion type tube that can be folded into a small volume that can be accommodated in a small space and uses a superelastic material that can be deployed without additional mechanical devices do.
The present invention also provides a variable deployment tube using a superelastic material that can be repeatedly accommodated and deployed.
The present invention also provides a variable deployment type tube made of a thin composite material excellent in non-rigidity and non-rigidity so that an additional expansion device is not required, and which is light in weight and can be carried and moved freely using a super elastic material.
The present invention also provides a variable expansion type tube using a superelastic material, which can control the speed and shape of the self-expanding shape by controlling the temperature of the shape memory polymer composite material.
The present invention also provides a variable deployment type tube using a superelastic material capable of improving durability and reliability in a space environment.
It is to be understood, however, that the technical scope of the present invention is not limited to the above-described technical problems, and other technical problems may exist.
According to an aspect of the present invention, there is provided a variable expansion type tube using a super elastic material, the tube including a hollow tube body and a tube body extending in the longitudinal direction in the tube body, And a plurality of stiffeners disposed at intervals along the circumference of the tube body.
According to one example of this embodiment, the plurality of stiffeners may have a pair arranged in mutually symmetrical manner when viewed in cross section.
According to an example of this embodiment, the stiffener may be a wire having a superelastic material.
According to one example of this embodiment, the super elastic material may be a material including shape memory alloys.
According to one embodiment of the present invention, the super elastic material may be a material having elastic restoring force that is easily deformed without damage and residual deformation of the material corresponding to the external force, and is restored to the shape before the deformation.
According to one embodiment of the present invention, the tube body may be made of a material including a TWF (Triaxially Woven Fabric Silicon) including TWF carbon fiber and silicone resin.
According to one example of this embodiment, a capton film may be formed on the surface of the tube body.
According to one embodiment of the present embodiment, the cross-sectional surface may be formed in a shape, and the shape memory member may be disposed inside the tube body so as to extend in the longitudinal direction.
According to an embodiment of the present invention, the shape memory member includes an upper flange and a lower flange, which are disposed so as to be in contact with the inner circumference of the tube body and spaced apart from each other by a predetermined distance, . ≪ / RTI >
According to one example of this embodiment, the upper flange or the lower flange and the web may be at right angles to each other.
According to the example of this embodiment, the plurality of stiffeners may be provided in an area where the upper and lower flanges of the shape memory member are not disposed.
According to an example of this embodiment, the shape memory member may further include a heat unit for providing a predetermined heat.
According to one example of this embodiment, the heat unit may include a heat line that is placed in contact with at least one of upper and lower flanges and webs of the shape memory member, and a power source unit that is electrically connected to the heat line.
According to an example of this embodiment, the heat unit may include carbon nanotube particles included in the shape memory member.
According to an embodiment of the present invention, the carbon nanotube particle can heat the shape memory member by a microwave provided from the outside.
The above-described task solution is merely exemplary and should not be construed as limiting the present disclosure. In addition to the exemplary embodiments described above, there may be additional embodiments described in the drawings and the detailed description of the invention.
According to the above-described task solution of the present invention, it is possible to fold in a compact shape (volume) that can be stored in a small space, and it is possible to self-expand according to need without using a mechanical expansion structure, The storage efficiency can be greatly improved and the development system can be simplified by the self development method, so that the manufacturing cost can be reduced and the reliability in the development process can be greatly improved.
In addition, high torsional rigidity can be ensured through the tube structure, and by combining the tube structure with the stiffeners arranged along the circumference of the tube structure, the moment of inertia can be maximized and high bending rigidity can be ensured.
In addition, the present invention is made of a thin film composite material excellent in non-strength and non-rigidity so that an additional expansion device is not necessary, so that it is light in weight and can be carried and moved freely.
Further, by using the shape memory member which has the characteristic of super elasticity that can be easily deformed at a predetermined temperature or more and can be restored to the initial shape, it is possible to control the self-developed speed and shape through temperature control on the shape memory member .
Further, by forming a capton film coated with aluminum on the surface of the tube body, it is possible to shield the UV in a space environment and prevent extreme temperature changes, thereby improving durability and reliability.
Further, the effects obtainable here are not limited to the effects mentioned above, and other effects not mentioned can be clearly understood by those skilled in the art from the following description will be.
BRIEF DESCRIPTION OF THE DRAWINGS Figure 1 is a view of a variable deployment tube using a superelastic material according to one embodiment of the present invention.
FIG. 2 is a developed view of a variable deployment type tube using a folded super elastic material. FIG.
3 is a view showing a variable expansion type tube using a superelastic material including a shape memory member.
Hereinafter, embodiments of the present invention will be described in detail with reference to the accompanying drawings so that those skilled in the art can easily carry out the present invention. It should be understood, however, that the present invention may be embodied in many different forms and should not be construed as limited to the embodiments set forth herein. In the drawings, the same reference numbers are used throughout the specification to refer to the same or like parts.
Throughout this specification, when a part is referred to as being "connected" to another part, it is not limited to a case where it is "directly connected" but also includes the case where it is "electrically connected" do.
Throughout this specification, when a member is "on " another member, it includes not only when the member is in contact with the other member, but also when there is another member between the two members.
Throughout this specification, when an element is referred to as "including " an element, it is understood that the element may include other elements as well, without departing from the other elements unless specifically stated otherwise.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Hereinafter, the present invention will be described in detail with reference to the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS Figure 1 is a view of a variable deployment tube using a superelastic material according to one embodiment of the present invention.
As shown in FIG. 1, the
The variable
The variable
The variable
Hereinafter, the structure of the
Referring to FIG. 1, a
The
The
TWFS has the property of superelasticity that it can withstand high strain without damaging the material and restore the initial shape after deformation by elastic restoring force. By combining the tube
Also, a capton film (not shown) coated with aluminum may be formed on the surface of the tube
Further, the variable
The plurality of
And the plurality of
The plurality of
As described above, according to the present invention, by organically combining a plurality of
FIG. 2 is a developed view of a variable deployment type tube using a folded super elastic material. FIG. As shown in FIG. 2, the variable
It is preferable that the plurality of
3 is a view showing a variable expansion type tube using a superelastic material including a shape memory member. As shown in FIG. 3, the
The
At this time, the upper and
In addition, the upper and
The
For reference, a shape memory polymer (SMP) is a polymer that stores an initial shape and returns to its original shape from a deformed shape when the temperature exceeds a glass transition temperature. The mechanism to restore strain is a change in entropy resulting from the elasticity of the shape memory polymer. The molecular structure of the shape memory polymer is similar to the network structure, and the cross-link molecular chains and reversible molecules connecting the molecular structures are complex. The molecular chain serves as a non-reversible phase that can not go back once it is cured and prevents free movement.
On the other hand, the reversible phase takes a large part in the shape memory polymer and plays an elastic role in deformation and recovery. When the temperature exceeds a certain temperature, the reversible phase becomes fluid and flowability is improved. This temperature is called the glass transition temperature (Tg). When the external force is applied above the glass transition temperature, the molecular chains of the shape memory polymer are aligned and the entropy is reduced. At this time, when the temperature is rapidly lowered to below the glass transition temperature, the unstable reversible phase is stabilized again and the modified form is maintained.
In addition, if heat is applied at a temperature above the glass transition temperature, the molecular chains move through the stored strain energy and return to the original shape.
The thermo-mechanical properties of shape memory polymers change with temperature and time. That is, there is a temperature dependent shape memory effect (SME: Shape Memory Effect) and time-dependent viscoelasticity characteristic.
The shape memory polymer composite material (SMPC) including the shape memory polymer has a superelasticity elastic restoring force capable of large deformation due to a very low rigidity of the material at a specific temperature (Tg) or higher and restored to its initial shape, And has a characteristic of storing the shape before deformation.
A manufacturing process of the shape memory polymer composite material (SMPC) will be described below as an example.
Shape memory polymer (SMP) is made of polyurethane material and DiALEX MP4510 / MP5510 of Mitsubishi Heavy Industries, Ltd. can be used. The resin and the curing agent are mixed and cured in a weight ratio of 2: 3.
The carbon fiber may be T-300 class woven fabric manufactured by Toray Co., Ltd. of Japan. The carbon fiber is laminated in a mold, the mixed shape memory polymer is poured on it, and a vacuum pressure is applied to induce the shape memory polymer to be impregnated into the entire fiber.
While holding the vacuum pressure, put in an oven and cure at 70 ° C for 2 hours. At this time, since the curing rate of the SMPC is very fast within 3 minutes, bubbles are generated on the surface or a solidification phenomenon occurs. Therefore, the process must be changed so that the air bubbles can pass through the fibers.
A breather that uniformly distributes vacuum pressure was attached to the side of the carbon fiber. The liquid shape memory polymer was poured on the carbon fiber and pushed to the breather by the rubber stopper to prevent the occurrence of the core. Thus, a more stable state of the synthetic memory polymer composite material can be produced, which has a function of absorbing surplus resin by making a path to escape of bubbles.
In addition, by impregnating carbon nanotubes (CNTs) in the synthetic memory polymer, the temperature of the synthetic memory polymer can be controlled by using a micro-wave.
On the other hand, the
Then, at the temperature lower than the preset temperature, the elastic restoring force of the
That is, the
The
FIG. 2 is a developed view of a variable deployment type tube using a folded super elastic material. FIG. Referring to FIG. 2, the bendable
On the other hand, the
The heat unit can provide a predetermined heat to the
As the heat is supplied to the
Also, as another embodiment of the heat unit, the heat unit may be a carbon nanotube (CNT) particle contained in the
It will be understood by those of ordinary skill in the art that the foregoing description of the embodiments is for illustrative purposes and that those skilled in the art can easily modify the invention without departing from the spirit or essential characteristics thereof. It is therefore to be understood that the above-described embodiments are illustrative in all aspects and not restrictive. For example, each component described as a single entity may be distributed and implemented, and components described as being distributed in a similar fashion may also be implemented.
The scope of the present invention is defined by the appended claims rather than the detailed description, and all changes or modifications derived from the meaning and scope of the claims and their equivalents should be construed as being included within the scope of the present invention.
100: Variable expansion tube using ultra-elastic material
10: tube body
20: Shape memory member
30: Stiffener
Claims (14)
A tube body having a hollow interior;
A plurality of stiffeners extending in the longitudinal direction within the tube body, the plurality of stiffeners being spaced along the circumference of the tube body; And
And a shape memory member having a cross section formed in an I-shape and extending in the longitudinal direction within the tube body,
Wherein the stiffener is a wire having a superelastic material.
Wherein the superelastic material comprises shape memory alloys.
The ultra-elastic material may be,
Wherein the deformable tube is made of a material having elastic restoring force that is easily deformed without damage and residual deformation of the material in response to an external force and restored to the shape before the deformation.
Wherein the tube body is made of a material comprising a TWF (Triaxially Woven Fabric Silicon) including TWF carbon fibers and a silicone resin.
And a capton film is formed on the surface of the tube body.
The shape memory member
An upper flange and a lower flange disposed to face the inner circumference of the tube body and disposed to face each other with a predetermined distance therebetween; And
And a web connecting said upper flange and said lower flange.
Wherein the upper flange or the lower flange and the web are at right angles to each other.
Further comprising a heat unit for providing a predetermined heat to the shape memory member.
The thermal unit may include:
A heat wire arranged in contact with at least one of an upper flange, a lower flange and a web of the shape memory member; And
And a power supply unit electrically connected to the heat line.
Wherein the heat unit includes carbon nanotube (CNT) particles included in the shape memory member.
Wherein the carbon nanotube particles are heated by a microwave provided from the outside to increase the temperature of the shape memory member.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020150082807A KR101652708B1 (en) | 2015-06-11 | 2015-06-11 | Reconfigurable deployble tubes with superelastic materials |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020150082807A KR101652708B1 (en) | 2015-06-11 | 2015-06-11 | Reconfigurable deployble tubes with superelastic materials |
Publications (1)
Publication Number | Publication Date |
---|---|
KR101652708B1 true KR101652708B1 (en) | 2016-08-31 |
Family
ID=56877533
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
KR1020150082807A KR101652708B1 (en) | 2015-06-11 | 2015-06-11 | Reconfigurable deployble tubes with superelastic materials |
Country Status (1)
Country | Link |
---|---|
KR (1) | KR101652708B1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106995050A (en) * | 2017-04-14 | 2017-08-01 | 哈尔滨工业大学 | One kind is used for Thin-Wall Cylindrical Shells dynamic stiffness actively enhanced SMA actuator |
CN107152603A (en) * | 2016-12-07 | 2017-09-12 | 航天特种材料及工艺技术研究所 | A kind of bistable state shell structure and its manufacture method |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6560942B2 (en) * | 2000-06-06 | 2003-05-13 | Foster-Miller, Inc. | Open lattice, foldable, self deployable structure |
US20050022465A1 (en) * | 1999-11-09 | 2005-02-03 | Warren Peter A. | Flexible, deployment rate damped hinge |
-
2015
- 2015-06-11 KR KR1020150082807A patent/KR101652708B1/en active IP Right Grant
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20050022465A1 (en) * | 1999-11-09 | 2005-02-03 | Warren Peter A. | Flexible, deployment rate damped hinge |
US6560942B2 (en) * | 2000-06-06 | 2003-05-13 | Foster-Miller, Inc. | Open lattice, foldable, self deployable structure |
Non-Patent Citations (2)
Title |
---|
김학인 외 3인, 형상기억폴리머 복합재료 붐 구조물의 굽힘 및 전개 시험, 한국항공우주학회 학술발표집 논문집, 301-303,(2014)* * |
김혜정, 외 6인, 형상기억폴리머의 열-기계적 특성 연구, 한국항공우주학회 학술발표집 논문집, 1682-1685(2012)* * |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107152603A (en) * | 2016-12-07 | 2017-09-12 | 航天特种材料及工艺技术研究所 | A kind of bistable state shell structure and its manufacture method |
CN106995050A (en) * | 2017-04-14 | 2017-08-01 | 哈尔滨工业大学 | One kind is used for Thin-Wall Cylindrical Shells dynamic stiffness actively enhanced SMA actuator |
CN106995050B (en) * | 2017-04-14 | 2019-07-02 | 哈尔滨工业大学 | A kind of SMA actuator actively enhanced for Thin-Wall Cylindrical Shells dynamic stiffness |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
KR101652707B1 (en) | Reconfigurable deployble tubes with shape memory materials | |
Li et al. | Progress of shape memory polymers and their composites in aerospace applications | |
Liu et al. | Shape memory polymers and their composites in aerospace applications: a review | |
Murphey et al. | High strain composites | |
US9975652B2 (en) | Boxed unwindable solar generator | |
US20120167943A1 (en) | Unwindable Flat Solar Generator | |
JP5694144B2 (en) | Shape-changing structural member with embedded spring | |
JP5694143B2 (en) | Shape change structure with superelastic foam material | |
US6910308B2 (en) | Inflatable rigidizable boom | |
US7009578B2 (en) | Deployable antenna with foldable resilient members | |
CN101847786B (en) | Reflecting surface of deployable antenna based on shape memory polymer and manufacturing method of skeleton structure thereof | |
WO2003062565A1 (en) | Open-lattice, foldable, self-deployable structure | |
KR101652708B1 (en) | Reconfigurable deployble tubes with superelastic materials | |
Im et al. | Prospects of large deployable reflector antennas for a new generation of geostationary Doppler weather radar satellites | |
Lin et al. | Shape memory rigidizable inflatable (RI) structures for large space systems applications | |
CN111555012A (en) | Satellite inflatable antenna | |
Murphey et al. | Deployable booms and antennas using bi-stable tape-springs | |
CN109760855A (en) | A kind of flexible space solar energy sailboard | |
JP7359370B2 (en) | Deployable reflector for antenna | |
EP3333420B1 (en) | Reconfigurable structure using dual-matrix composite material | |
Lin et al. | An inflatable microstrip reflectarray concept for Ka-band applications | |
Datashvili | Multifunctional and dimensionally stable flexible fibre composites for space applications | |
CN116247410B (en) | Repeatable sector-shaped unfolding mechanism based on shape memory alloy driving | |
Murphey | Historical perspectives on the development of deployable reflectors | |
Campbell et al. | Development of a novel, passively deployed roll-out solar array |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
E701 | Decision to grant or registration of patent right | ||
GRNT | Written decision to grant |