CN109727556A - A kind of space representation device - Google Patents

A kind of space representation device Download PDF

Info

Publication number
CN109727556A
CN109727556A CN201910001939.2A CN201910001939A CN109727556A CN 109727556 A CN109727556 A CN 109727556A CN 201910001939 A CN201910001939 A CN 201910001939A CN 109727556 A CN109727556 A CN 109727556A
Authority
CN
China
Prior art keywords
locking mechanism
film
display
composite material
shape memory
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
CN201910001939.2A
Other languages
Chinese (zh)
Inventor
刘彦菊
冷劲松
张豆
刘立武
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.)
Harbin Institute of Technology Shenzhen
Original Assignee
Harbin Institute of Technology Shenzhen
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 Harbin Institute of Technology Shenzhen filed Critical Harbin Institute of Technology Shenzhen
Priority to CN201910001939.2A priority Critical patent/CN109727556A/en
Publication of CN109727556A publication Critical patent/CN109727556A/en
Pending legal-status Critical Current

Links

Landscapes

  • Manufacture Of Macromolecular Shaped Articles (AREA)

Abstract

本发明提供了一种空间展示装置,涉及航空航天技术领域。本发明提供一种空间展示机构,包括配重杆、展示膜、锁定机构和激励装置;所述展示膜的上端适于悬挂固定,下端与所述配重杆连接且卷绕于所述配重杆上;所述锁定机构采用形状记忆聚合物复合材料制成,其以收缩形态环绕于卷绕在所述配重杆上的展示膜外侧,适于将所述展示膜固定于所述配重杆上;所述激励装置适于在设定条件下对所述锁定机构进行激励并使所述锁定机构回复,当所述锁定机构回复到展开形态时,所述展示膜在所述配重杆的重力作用下展开。本发明将形状记忆聚合物复合材料和所述配重杆的重力结合到一起,实现了空间展示机构的展示功能。

The invention provides a space display device, which relates to the technical field of aerospace. The invention provides a space display mechanism, comprising a counterweight rod, a display film, a locking mechanism and an excitation device; the upper end of the display film is suitable for hanging and fixing, and the lower end is connected with the counterweight rod and wound around the counterweight on the rod; the locking mechanism is made of shape memory polymer composite material, which wraps around the outside of the display film wound on the counterweight rod in a contracted form, and is suitable for fixing the display film to the counterweight on the rod; the actuating device is adapted to actuate the locking mechanism under set conditions and restore the locking mechanism, and when the locking mechanism is restored to the deployed state, the display film is placed on the counterweight rod unfolded under the force of gravity. The invention combines the shape memory polymer composite material and the gravity of the counterweight rod together to realize the display function of the space display mechanism.

Description

A kind of space representation device
Technical field
The present invention relates to aerospace field, in particular to a kind of space representation device.
Background technique
In field of aerospace technology, spacecraft after reaching specified celestial body, has been needed when executing deep space exploration task At some displaying functions, the opening for showing mechanism is usually completed by artificial movement, and for the expansion under unmanned environment It is difficult to capture, if remote auto is taken to unlock, structure is complex if design, and considers weight issue, and sexual valence is relatively low. In recent years, shape-memory polymer is more and more concerned, and shape-memory polymer has shape memory function, is that one kind can The high molecular material for generating intelligent active deformation, under the action of dynamic excitation, which, which can generate, biggish replys change Shape is converted to unfoldable shape from retracted configuration.
Summary of the invention
In view of this, the present invention is directed to propose a kind of space representation device, utilizes shape memory polymer composite material Shape memory function is designed.
In order to achieve the above objectives, the technical scheme of the present invention is realized as follows:
A kind of space representation mechanism, including weight linear meter, displaying film, locking mechanism and exciting bank;It is described to show the upper of film End is suitable for suspension and fixes, and lower end connect with the weight linear meter and is wound on the weight linear meter;The locking mechanism uses shape Memory composites are made, and are surrounded on the outside of the displaying film on the weight linear meter, are suitable for retracted configuration The displaying film is fixed on the weight linear meter;The exciting bank is suitable for carrying out the locking mechanism under setting condition It motivates and replys the locking mechanism, when the locking mechanism is returned to unfoldable shape, the displaying film is in the counterweight It is unfolded under the gravity of bar.
Optionally, gravity direction is provided with elastic strip on the displaying film, the elastic strip and the displaying film are simultaneously It is wound on the weight linear meter.
Optionally, the elastic strip has two, and two elastic strips are respectively arranged at the left side edge for showing film And right side edge.
Optionally, the exciting bank includes heater circuit, and the heater circuit includes adding thermal resistance, the adding thermal resistance Distribution is set to the surface of the locking mechanism.
Optionally, the heater circuit further includes thermistor, and the thermistor, the adding thermal resistance are connected with power supply In the same circuit.
Optionally, the adding thermal resistance is prepared using laser ablation mode.
Optionally, the exciting bank further include: strain temperature sensor and controller, the strain temperature sensor and The controller is connected, and the strain temperature sensor is suitable for monitoring the strain and temperature of the locking mechanism.
Optionally, the shape memory polymer composite material include shape-memory polymer it is mutually compound with fiber reinforcement and At material.
Optionally, it is 5%- that the fiber reinforcement, which mutually accounts for the volume fraction of the shape memory polymer composite material, 60%.
Optionally, the heater circuit is powered using solar panel.
Compared with the existing technology, space representation device of the present invention has the advantage that
For the present invention when the displaying film roll is around on the weight linear meter, the locking mechanism in contraction state can be with Fixed function is rolls-up onto displaying, avoids scattering for the displaying film;When the displaying film needs to be unfolded, the locking mechanism Unfoldable shape is returned under the action of exciting bank, then the displaying volume carries out under the action of the gravity of the weight linear meter Expansion, the gravity of shape memory polymer composite material and the weight linear meter is combined, space representation mechanism is realized Displaying function.In addition, realizing the reusable of the space representation mechanism by shape memory polymer composite material.
Elastic strip of the present invention can be played to the booster action for showing film edge, avoid the broken of the displaying film It is bad;In addition, by the setting of the elastic strip, it can be to avoid the bonding for showing film;But more main effect is still, Certain resilient urging force is provided, convenient for the expansion for showing film, avoids that the weight linear meter quality is too small to cause the exhibition Show the phenomenon that film can not be unfolded.
Detailed description of the invention
The attached drawing for constituting a part of the invention is used to provide further understanding of the present invention, schematic reality of the invention It applies example and its explanation is used to explain the present invention, do not constitute improper limitations of the present invention.In the accompanying drawings:
Fig. 1 is positive structure schematic after the space representation mechanism opening of the embodiment of the present invention;
Fig. 2 is structure schematic diagram after the space representation mechanism opening of the embodiment of the present invention;
Structural schematic diagram when Fig. 3 is the space representation mechanism locking of the embodiment of the present invention;
Fig. 4 is the heating circuit structure schematic diagram of the embodiment of the present invention;
Fig. 5 is the weight linear meter structural schematic diagram of the embodiment of the present invention.
Description of symbols:
1- weight linear meter, 2- show film, 3- locking mechanism, 4- elastic strip, 5- adding thermal resistance, 6- thermistor, 7- solar energy Solar panel, 8- engraved structure.
Specific embodiment
It should be noted that in the absence of conflict, the feature in embodiment and embodiment in the present invention can phase Mutually combination.
In addition, direction or positional relationship all in the text being previously mentioned in an embodiment of the present invention are the position based on attached drawing Relationship is set, only for facilitating the description present invention and simplifying description, rather than implies or imply that signified device or element must have The specific orientation having, is not considered as limiting the invention.
The present invention will be described in detail below with reference to the accompanying drawings and embodiments.
Embodiment one
A kind of space representation mechanism, as depicted in figs. 1 and 2, including weight linear meter 1, displaying film 2, locking mechanism 3 and excitation dress It sets;The upper end for showing film 2 is suitable for suspension and fixes, and lower end connect with the weight linear meter 1 and is wound on the weight linear meter 1; The locking mechanism 3 is made of shape memory polymer composite material, is surrounded on retracted configuration wound on the counterweight 2 outside of displaying film on bar 1, suitable for the displaying film 2 to be fixed on the weight linear meter 1;The exciting bank is suitable for setting The locking mechanism 3 is motivated under fixed condition and replys the locking mechanism 3, when the locking mechanism 3 is returned to exhibition When open form state, the displaying film 2 is unfolded under the gravity of the weight linear meter 1.
It should be noted that as shown in Fig. 2, the unfoldable shape of the locking mechanism 3 is bar shaped, as shown in Figure 1, the exhibition Show that wherein one end of film 2 is connect by the way of bonding or screw fastening with the weight linear meter 1, as shown in figure 3, manufacturing process In, first by the displaying film 2 on the weight linear meter 1, then by the locking mechanism 3 in retracted configuration along described Weight linear meter 1 circumferentially around it is described show film 2 outside, be fixed on the displayings film 2 on the weight linear meter 1, make described in Show that film 2 is not unfolded.As shown in Figures 2 and 3, it is mounted on the locking mechanism 3 in the left and right sides for showing film 2, To guarantee the symmetry of structure, fixing intensity also can be enhanced.
The upper end for showing film 2 is provided with threaded hole, in such a way that screw fastens with the car body of celestial body vehicle or too Sky calibration object connection hangs on the space representation mechanism on the car body or space calibration object.The excitation Device is connected with controller, when the controller receive expansion instruction when, the exciting bank to the locking mechanism 3 into Row energization replys the locking mechanism 3;When the locking mechanism 3 is returned to unfoldable shape, release to the displaying film 2 Limitation, the displaying film 2 is unfolded under the gravity of weight linear meter 1, to show displaying picture.
Here, the shape memory polymer composite material includes made of shape-memory polymer and fiber-reinforced composite Material.The fiber reinforcement is mutually carbon fiber, glass fibre, spandex fibre, Kafra fiber, aramid fiber, graphene or carbon One of nanotube is a variety of.Wherein the fiber reinforcement mutually accounts for the volume fraction of the shape memory polymer composite material For 5%-60%.Preferably, the volume fraction of fiber reinforcement phase described in the shape memory polymer composite material is 40%. Volume fraction shared by the fiber reinforcement phase can be adjusted according to the demand of coupling mechanism force, when required coupling mechanism force is smaller, The lesser shape memory polymer composite material of the fiber reinforcement phase volume fraction can be selected;When required coupling mechanism force When larger, the biggish shape memory polymer composite material of the fiber reinforcement phase volume can be selected.
The advantages of this arrangement are as follows when the displaying film 2 is wound on the weight linear meter 1, in contraction state The locking mechanism 3 can be rolls-up onto fixed function to displaying, avoid scattering for the displaying film 2;When the displaying film 2 needs When expansion, the locking mechanism 3 is returned to unfoldable shape under the action of exciting bank, and then the displaying volume 2 is matched described It is unfolded under the action of the gravity of weight bar, the gravity of shape memory polymer composite material and the weight linear meter 1 is integrated to Together, the displaying function of space representation mechanism is realized.In addition, realizing the sky by shape memory polymer composite material Between show mechanism it is reusable.
Embodiment two
Place unlike the embodiments above is, as shown in Figure 1, being provided with bullet along the vertical direction on the displaying film 2 Property item 4, the elastic strip 4 and the displaying film 2 are wound in together on the weight linear meter 1.Here upper and lower refers to when described Show direction parallel with gravity after film 2 is unfolded.
In order to avoid the quality of the weight linear meter 1 is excessive, increase transportation cost, weight linear meter 1 described here uses cylinder knot Structure, as shown in figure 5, and avoiding opening up engraved structure 8 in the cylinder.But when the quality of the weight linear meter 1 is too small When, but may with the displaying film 2 can not be unfolded the phenomenon that.Here, the elastic strip 4 can choose stalloy material Matter can also choose organic polymer fibrous material or other elastic materials.The original state of the elastic strip is shown in FIG. 1 Bar shaped state, as depicted in figs. 1 and 2, the elastic strip 4 and front and the back for showing film 2 and being located at the displaying film 2 Face, front refer to that the displaying film 2 draws figuratum side, and the back side refers on the displaying film 2 back to the drafting Figuratum side.In manufacturing process, first the elastic strip 4 and the displaying film 2 are wound in together on the weight linear meter 1, By figuratum side wound on the side close to 1 center of weight linear meter, that is to say, that figuratum side is wound on interior Side;Then the locking mechanism 3 in retracted configuration is shown into the outer of film 2 circumferentially around described along the weight linear meter 1 Side is fixed on the displaying film 2 on the weight linear meter 1, keeps the displaying film 2 not unfolded.As shown in Figures 2 and 3, in institute It states and shows that the left and right sides of film 2 is mounted on the locking mechanism 3, to guarantee the symmetry of structure, also can be enhanced fixed strong Degree.
When the controller receives expansion instruction, the exciting bank motivates the locking mechanism 3, makes institute State the expansion of locking mechanism 3;But in order to avoid gravity deficiency so that the case where displaying film 2 is unfolded, here, described Show that elastic strip 4 is respectively set in the edge of the left and right sides of film 2, what the elastic strip 4 can be fastened by bonding or screw Mode is connect with the displaying film 2.When the locking mechanism 3 expansion after, the elastic strip 4 due to be in tensioning state, Having certain elastic force flicks the displaying film 2, avoids the bonding for showing film 2, after the displaying film 2 is flicked, The displaying film 2 is unfolded under the gravity of weight linear meter 1, to show displaying picture.
The advantages of this arrangement are as follows the elastic strip 4 can be played to the booster action for showing 2 edge of film, keep away Exempt from the destruction for showing film 2;In addition, by the setting of the elastic strip 4, it can be to avoid the bonding for showing film 2;But more Main effect is still, provides certain resilient urging force, convenient for the expansion for showing film 2, avoids the counterweight 1 mass of bar too small the phenomenon that causing the displaying film 2 that can not be unfolded.
Embodiment three
Place unlike the embodiments above is, as shown in figure 4, the exciting bank includes heater circuit, it is described to add Heater circuit includes adding thermal resistance 5, and the adding thermal resistance 5 is distributed the surface for being set to the locking mechanism 3.
Here, as shown in figure 4, the adding thermal resistance 5 is distributed in the table that the locking mechanism 3 is in the part of contraction state Face, that is, the lower half portion of the locking mechanism 3 are down here for the structure in Fig. 4.The adding thermal resistance 5 are prepared in the surface of the locking mechanism 3 using laser ablation mode, and the adding thermal resistance 5 is not contacted with the displaying film 2.
It should be noted that the adding thermal resistance 5 is series among heater circuit with power supply, instructed when receiving expansion Afterwards, the heater circuit work, the adding thermal resistance 5 are generated heat, and thermal excitation are imposed to the locking mechanism 3, due to the locking Mechanism 3 is made of shape memory polymer composite material, when the locking mechanism 3 reaches shape memory polymer composite material When more than glass transition temperature, the locking mechanism 3 is started to spread out.The adding thermal resistance 5 by resistivity such as constantans substantially not The material varied with temperature is made.Wherein, the power supply uses solar panel 7, is institute by the solar panel 7 State heater circuit power supply.Certain power supply can also be battery, and the battery is connect with the solar panel 7, lead to The solar panel 7 is crossed by the energy storage being collected into the battery, is the heating by the battery Circuit power supply.
Example IV
Place unlike the embodiments above is, as shown in figure 4, the heater circuit further includes thermistor 6, it is described Thermistor 6, the adding thermal resistance 5 and power supply are connected in the same circuit.The resistivity of thermistor 6 is increased with temperature and is risen Height, the thermistor 6 are connected with the adding thermal resistance 5.
Since space environment range of temperature is larger, this is one for thermotropic shape memory polymer material A biggish challenge.When the glass transition temperature of shape memory polymer composite material, the locking mechanism 3 is not achieved in temperature It can not be unfolded;But when environment temperature is excessively high, and it will lead to the decomposition of shape memory polymer composite material.The heating electricity The heat generated that is powered of resistance 5 is mainly shed by three kinds of heat transfer, thermal convection and heat radiation modes, and voltage and temperature are changing into It is positively correlated, i.e., voltage is higher, and temperature rise is bigger;Voltage is lower, and temperature rise is smaller.That is, if it is desirable that finally balancing When obtain a certain temperature value if, environment temperature is lower to need bigger voltage value;Environment temperature is higher to need smaller voltage Value.When the adding thermal resistance 5 is heated with changeless power, rapid heat dissipation at low ambient temperatures, in fact it could happen that heating The glass transition temperature of the shape memory polymer composite material is not achieved in temperature, and it is relatively slow to radiate in the high temperature environment, Heating temperature again may be excessively high, leads to the decomposition of the shape memory polymer composite material, leads to the space representation device Damage.
Here, the thermistor 6, the adding thermal resistance 5 and power supply are series in heater circuit, the thermistor 6 use the thermistor of positive temperature coefficient, that is to say, that the resistance of the thermistor 6 is increased with temperature and increased.The heat The selection needs of quick resistance 6 are determined according to the temperature range estimated in advance, it is ensured that electrified regulation under low temperature and hot environment Temperature can be in a reasonable range.When environment temperature is excessively high, the resistance value of the thermistor 6 is bigger, point The supply voltage of load is bigger, and the voltage at 5 both ends of adding thermal resistance then accordingly reduces, and reduces the power of the adding thermal resistance 5, Calorific value is reduced, so as to avoid the generation of the excessively high phenomenon of heating temperature in hot environment;When environment temperature is too low, institute The resistance value for stating thermistor 6 is smaller, and the supply voltage shared is smaller, and the voltage at 5 both ends of adding thermal resistance then accordingly increases Greatly, the power of the adding thermal resistance 5 is increased, calorific value is increased, it is too low so as to avoid heating temperature in low temperature environment Phenomenon occurs.
As shown in figure 4, the thermistor 6 is located at the position of 3 unfoldable shape of locking mechanism, that is, it is located at described The position of the top half of locking mechanism 3, the distance between the thermistor 6 and the adding thermal resistance 5 ensure that the heat Quick resistance 6 is not interfered by the adding thermal resistance 5.By the setting of the thermistor, realize according to environment temperature to described The automatic adjusument of heater circuit, to realize reliable and secure heating at different ambient temperatures.
Embodiment five
Place unlike the embodiments above is, the space representation mechanism further include: strain temperature sensor and control Device processed, the strain temperature sensor are connected with the controller, and the strain temperature sensor is suitable for monitoring the locking The strain and temperature of mechanism 3.
Here, the strain temperature sensor uses flexible electronic device, integrated with composite material in the fabrication process Molding, the strain temperature sensor can simultaneously be monitored the temperature of the locking mechanism 3 and strain.The strain temperature Sensor is using the low-frequency range of frequency spectrum as temperature signal, and high band is as the components of strain, closer one under the premise of assurance function The simplification of the realization structure of step.Wherein, the strain data that the strain temperature sensor is incuded is used to judge the locking machine The expansion degree of structure 3, if the expansion degree of the locking mechanism 3 is not up to setting value, the adding thermal resistance 5 continues to heat, make The temperature of the locking mechanism 3 is in shape expansion temperature range;The temperature data that the strain temperature sensor is incuded For monitoring the temperature of the locking mechanism 3, when the locking mechanism 3 when the temperature is excessively high, it is electric that controller disconnects the heating Road;When glass transition temperature of the temperature lower than the shape memory polymer composite material, then circuit is connected, the heating is made Resistance 5 continues to heat, and when the expansion degree of locking mechanism 3 reaches setting value, controller disconnects heater circuit.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all in essence of the invention Within mind and principle, any modification, equivalent replacement, improvement and so on be should all be included in the protection scope of the present invention.

Claims (10)

1.一种空间展示机构,其特征在于,包括配重杆(1)、展示膜(2)、锁定机构(3)和激励装置;所述展示膜(2)的上端适于悬挂固定,下端与所述配重杆(1)连接且卷绕于所述配重杆(1)上;所述锁定机构(3)采用形状记忆聚合物复合材料制成,其以收缩形态环绕设置于卷绕在所述配重杆(1)上的展示膜(2)的外侧,适于将所述展示膜(2)固定于所述配重杆(1)上;所述激励装置适于在设定条件下对所述锁定机构(3)进行激励并使所述锁定机构(3)回复,当所述锁定机构(3)回复到展开形态时,所述展示膜(2)在所述配重杆(1)的重力作用下展开。1. A space display mechanism, characterized in that it comprises a counterweight rod (1), a display film (2), a locking mechanism (3) and an excitation device; the upper end of the display film (2) is suitable for hanging and fixing, and the lower end is suitable for hanging and fixing. The locking mechanism (3) is made of a shape memory polymer composite material, and is arranged around the winding in a shrinking form On the outside of the display film (2) on the counterweight rod (1), the display film (2) is suitable for fixing the display film (2) on the counterweight rod (1); the excitation device is suitable for setting the The locking mechanism (3) is actuated and the locking mechanism (3) is restored under certain conditions. When the locking mechanism (3) is restored to the unfolded state, the display film (2) is placed on the counterweight bar. (1) unfolded under the action of gravity. 2.根据权利要求1所述的空间展示机构,其特征在于,所述展示膜(2)上沿重力方向设置有弹性条(4),所述弹性条(4)和所述展示膜(2)同时卷绕于所述配重杆(1)上。2. The space display mechanism according to claim 1, characterized in that, elastic strips (4) are provided on the display film (2) along the direction of gravity, the elastic strips (4) and the display film (2) ) are simultaneously wound on the counterweight bar (1). 3.根据权利要求2所述的空间展示机构,其特征在于,所述弹性条(4)有两条,两条所述弹性条(4)分别设置于所述展示膜(2)的左侧边缘和右侧边缘。3 . The space display mechanism according to claim 2 , wherein there are two elastic strips ( 4 ), and the two elastic strips ( 4 ) are respectively arranged on the left side of the display film ( 2 ). 4 . edge and right edge. 4.根据权利要求1所述的空间展示机构,其特征在于,所述激励装置包括加热电路,所述加热电路包括加热电阻(5),所述加热电阻(5)分布设置于所述锁定机构(3)的表面。4. The space display mechanism according to claim 1, characterized in that the excitation device comprises a heating circuit, the heating circuit comprises heating resistors (5), and the heating resistors (5) are distributed and arranged on the locking mechanism (3) surface. 5.根据权利要求4所述的空间展示机构,其特征在于,所述加热电路还包括热敏电阻(6),所述热敏电阻(6)、所述加热电阻(5)与电源串联在同一回路中。5. The space display mechanism according to claim 4, wherein the heating circuit further comprises a thermistor (6), the thermistor (6), the heating resistor (5) and the power supply are connected in series in the same circuit. 6.根据权利要求4所述的空间展示机构,其特征在于,所述加热电阻(5)采用激光刻蚀方式制备。6 . The space display mechanism according to claim 4 , wherein the heating resistor ( 5 ) is prepared by laser etching. 7 . 7.根据权利要求5所述的空间展示机构,其特征在于,所述激励装置还包括:应变温度传感器和控制器,所述控制器与所述应变温度传感器相连接,所述应变温度传感器适于监测所述锁定机构(3)的应变和温度。7 . The space display mechanism according to claim 5 , wherein the excitation device further comprises: a strain temperature sensor and a controller, the controller is connected with the strain temperature sensor, and the strain temperature sensor is adapted to. for monitoring the strain and temperature of the locking mechanism (3). 8.根据权利要求1所述的空间展示机构,其特征在于,所述形状记忆聚合物复合材料包括形状记忆聚合物和纤维增强相复合而成的材料。8 . The space display mechanism according to claim 1 , wherein the shape memory polymer composite material comprises a composite material of shape memory polymer and fiber reinforcement. 9 . 9.根据权利要求8所述的空间展示机构,其特征在于,所述纤维增强相占所述形状记忆聚合物复合材料的体积分数为5%-60%。9 . The space display mechanism according to claim 8 , wherein the volume fraction of the fiber-reinforced phase in the shape memory polymer composite material is 5%-60%. 10 . 10.根据权利要求4所述的空间展示机构,其特征在于,所述加热电路采用太阳能电池板(7)供电。10. The space display mechanism according to claim 4, wherein the heating circuit is powered by a solar panel (7).
CN201910001939.2A 2019-01-02 2019-01-02 A kind of space representation device Pending CN109727556A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910001939.2A CN109727556A (en) 2019-01-02 2019-01-02 A kind of space representation device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910001939.2A CN109727556A (en) 2019-01-02 2019-01-02 A kind of space representation device

Publications (1)

Publication Number Publication Date
CN109727556A true CN109727556A (en) 2019-05-07

Family

ID=66299566

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201910001939.2A Pending CN109727556A (en) 2019-01-02 2019-01-02 A kind of space representation device

Country Status (1)

Country Link
CN (1) CN109727556A (en)

Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2493730Y (en) * 2001-08-04 2002-05-29 贾向海 No hinging integral coiling door
CN101016891A (en) * 2007-03-12 2007-08-15 哈尔滨工业大学 Shape memory composite material hinge driving deploying device
CN201035883Y (en) * 2006-06-26 2008-03-12 傅忠 Scroll advertising device
CN103224037A (en) * 2013-05-17 2013-07-31 哈尔滨工业大学 Multiple-repeated butt joint method of spacecraft space
CN103552696A (en) * 2013-11-08 2014-02-05 哈尔滨工业大学 Frame-type space extensible structure based on shape memory polymer
CN103988244A (en) * 2011-11-10 2014-08-13 严浩燮 Pillar Display
CN105207577A (en) * 2015-11-09 2015-12-30 哈尔滨工业大学 Flexible solar cell array based on shape memory polymer composite material and expansion method of flexible solar cell array
CN105356836A (en) * 2015-11-23 2016-02-24 哈尔滨工业大学 Unfolding method of space flexible solar battery array
CN105974724A (en) * 2016-07-04 2016-09-28 张家港宝视特影视器材有限公司 Projection arc curtain tensioning device
US9786247B2 (en) * 2015-03-03 2017-10-10 Samsung Display Co., Ltd. Wearable display device
CN107919846A (en) * 2017-12-21 2018-04-17 星际漫步(北京)航天科技有限公司 Winding drum type solar battery mechanism for outspreading sailboard and method of deploying
CN108112099A (en) * 2017-12-29 2018-06-01 中国电子科技集团公司第二十七研究所 A kind of anti-ultra-low temperature systems of floating platform
CN108199123A (en) * 2018-02-28 2018-06-22 北京国能电池科技股份有限公司 Heating appliances and systems
CN207869415U (en) * 2018-02-28 2018-09-14 北京国能电池科技股份有限公司 Heating film and heating device

Patent Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2493730Y (en) * 2001-08-04 2002-05-29 贾向海 No hinging integral coiling door
CN201035883Y (en) * 2006-06-26 2008-03-12 傅忠 Scroll advertising device
CN101016891A (en) * 2007-03-12 2007-08-15 哈尔滨工业大学 Shape memory composite material hinge driving deploying device
CN103988244A (en) * 2011-11-10 2014-08-13 严浩燮 Pillar Display
CN103224037A (en) * 2013-05-17 2013-07-31 哈尔滨工业大学 Multiple-repeated butt joint method of spacecraft space
CN103552696A (en) * 2013-11-08 2014-02-05 哈尔滨工业大学 Frame-type space extensible structure based on shape memory polymer
US9786247B2 (en) * 2015-03-03 2017-10-10 Samsung Display Co., Ltd. Wearable display device
CN105207577A (en) * 2015-11-09 2015-12-30 哈尔滨工业大学 Flexible solar cell array based on shape memory polymer composite material and expansion method of flexible solar cell array
CN105356836A (en) * 2015-11-23 2016-02-24 哈尔滨工业大学 Unfolding method of space flexible solar battery array
CN105974724A (en) * 2016-07-04 2016-09-28 张家港宝视特影视器材有限公司 Projection arc curtain tensioning device
CN107919846A (en) * 2017-12-21 2018-04-17 星际漫步(北京)航天科技有限公司 Winding drum type solar battery mechanism for outspreading sailboard and method of deploying
CN108112099A (en) * 2017-12-29 2018-06-01 中国电子科技集团公司第二十七研究所 A kind of anti-ultra-low temperature systems of floating platform
CN108199123A (en) * 2018-02-28 2018-06-22 北京国能电池科技股份有限公司 Heating appliances and systems
CN207869415U (en) * 2018-02-28 2018-09-14 北京国能电池科技股份有限公司 Heating film and heating device

Similar Documents

Publication Publication Date Title
Wu et al. A trimode thermoregulatory flexible fibrous membrane designed with hierarchical core–sheath fiber structure for wearable personal thermal management
CN103552696B (en) The frame-type space deployable structure of Shape-based interpolation memory polymer
Wu et al. Wearable aerogels for personal thermal management and smart devices
He et al. High-performance and long-term stability of MXene/PEDOT: PSS-decorated cotton yarn for wearable electronics applications
JP6438557B2 (en) Coiled and non-coiled nanofiber twisted and polymer fiber torsion and tension actuators
Xiao et al. Electrically driven liquid crystal network actuators
BR102017017897A2 (en) HEATING SET, AND METHOD FOR MAKING A HEATING SET.
US9975652B2 (en) Boxed unwindable solar generator
CN105416613A (en) Repeatable and flexible capture structure based on dielectric elastomer and shape memory polymer and method for capturing space debris
EP3339013A1 (en) Heated floor panels with thermally conductive and electrically insulating fabric
CN107039777B (en) A rib mesh supporting deployable antenna reflector and design method thereof
CN101402399A (en) Intelligent unlocking mechanism of memory alloy
CN105356836B (en) Unfolding method of space flexible solar battery array
CN103303497B (en) Shape memory polymer intelligent torsion releasing mechanism of space unfolding structure
CN116588356A (en) A kind of spacecraft protection system and its protection method
Zanjani et al. Manufacturing of electroactive morphing carbon fiber/glass fiber/epoxy composite: Process and structural monitoring by FBG sensors
CN109592078B (en) A space unlocking device
Yang et al. A flexible carbon fibre-based electrothermal film for fast actuation of shape memory alloy sheets
KR101738069B1 (en) Flexible display device having shape memory alloy
CN209225429U (en) A kind of flexibility sun wing mechanism
Ming et al. Design, fabrication and experimental verification of a drag sail based on thermal-driven controllable bi-stable shape memory polymer composite booms
CN116674763B (en) A Superconducting Thermally Reversible Satellite Structure and Fabrication Method Based on Shape Memory Alloy
BR102017017889A2 (en) HEATING SET, AND METHOD FOR MAKING A HEATING SET
JPH01285498A (en) Panel expanding device for space
CN207833358U (en) A kind of spaceborne temperature regulating device based on thermal conductive wire heat transfer

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
RJ01 Rejection of invention patent application after publication

Application publication date: 20190507