CN210134673U - Container classroom - Google Patents
Container classroom Download PDFInfo
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- CN210134673U CN210134673U CN201920232739.3U CN201920232739U CN210134673U CN 210134673 U CN210134673 U CN 210134673U CN 201920232739 U CN201920232739 U CN 201920232739U CN 210134673 U CN210134673 U CN 210134673U
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- classroom
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Abstract
The utility model provides a container classroom, including the classroom main part, the classroom main part includes apron, all-wing aircraft and the skeleton that is the square body, all-wing aircraft includes all-wing aircraft main part and support frame, the one end of all-wing aircraft main part is rotatable to be connected in the top of a side of skeleton, top surface, bottom surface and other sides of skeleton are equipped with the apron respectively, the support frame is rotatable to be connected in the other end of all-wing aircraft main part; can make the all-wing aircraft main part be in the position on parallel ground through rotating the all-wing aircraft main part, rotate the support frame again and support the all-wing aircraft main part and make it keep stable state, can expand the teaching area in classroom, improve the space utilization and the ventilation effect in classroom greatly, improve student's learning environment simultaneously to can judge whether to launch the all-wing aircraft according to actual conditions, the flexibility is high.
Description
Technical Field
The utility model relates to a teaching facility field especially relates to a container classroom.
Background
The container classroom is a place which can be quickly built up for students to study, has low cost and provides great convenience for education of countries or regions which are relatively backward in development. But the container classroom overall structure on the existing market is all heavier, and the leakproofness is stronger, and the ventilation effect is relatively poor, and such learning environment can cause the influence to student's study. In addition, the teaching area of the classroom cannot be expanded generally by the existing container classroom, and the waste of space is caused.
SUMMERY OF THE UTILITY MODEL
In order to overcome the defects of the prior art, the utility model aims to solve the technical problems that: a container classroom can expand the teaching area of the classroom and improve the space utilization rate.
In order to solve the technical problem, the utility model discloses a technical scheme be: a container classroom is characterized by comprising a classroom body;
the classroom main body comprises a cover plate, a flying wing and a square framework;
the flying wing comprises a flying wing main body and a support frame;
one end of the flying wing main body is rotatably connected to the top of one side face of the framework, and the cover plates are respectively arranged on the top face, the bottom face and the other side faces of the framework;
the support frame is rotatably connected to the other end of the flying wing main body.
Furthermore, the classroom main body also comprises a hydraulic hinge;
one side of the hydraulic hinge is connected with the top of one side face of the framework, and the other side of the hydraulic hinge is connected with one end of the flying wing main body.
Further, the number of the flying wings is two;
one end of the flying wing main body of one flying wing can be rotatably connected to the top of the first side surface of the framework, and the flying wing main body of the flying wing is provided with a door and a window;
one end of the flying wing main body of the other flying wing can be rotatably connected to the top of a second side face, opposite to the first side face, in the framework, and the flying wing main body of the other flying wing is provided with a window.
Further, the classroom body also includes a hydraulic rod;
one end of the hydraulic rod is connected with the position, close to the top, of the flying wing main body, and the other end of the hydraulic rod is connected with the position, close to the top, of the framework.
Further, the support frame comprises a support seat, an upper support rod, a lower support rod, a first transverse plate and a second transverse plate;
the top surface of the supporting seat is welded to the other end of the flying wing main body, one end of the upper supporting rod is rotatably connected with the bottom surface of the supporting seat, one end of the lower supporting rod is slidably connected with the other end of the upper supporting rod, and the lower supporting rod is of a channel steel structure;
one end of the first transverse plate is rotatably connected to the inner side of the channel steel supporting the other end of the lower rod, and one end of the second transverse plate is hinged to the other end of the first transverse plate.
Furthermore, the device also comprises a pin shaft;
a first through hole is formed in the position, close to the bottom, of the upper supporting rod, and a second through hole matched with the first through hole is formed in the position, close to the top, of the lower supporting rod;
the pin shaft is respectively matched with the first through hole and the second through hole.
Further, the device also comprises a connecting plate;
the number of the support frames is two;
one end of the connecting plate is connected with the other end of the second transverse plate of one of the support frames, and the other end of the connecting plate is connected with the other end of the second transverse plate of the other support frame.
Furthermore, the solar cell panel is arranged on the top surface of the top cover plate.
Furthermore, a gap is arranged between the solar cell panel and the top cover plate.
The solar cell panel is characterized by further comprising a cell box and a storage battery, wherein the cell box is arranged in a gap between the solar cell panel and the top cover plate, the storage battery is arranged in the cell box, and the storage battery is electrically connected with the solar cell panel.
The beneficial effects of the utility model reside in that: through the one end rotatable coupling that sets up the all-wing aircraft main part in the top of a side of skeleton, support frame rotatable coupling in the other end of all-wing aircraft main part can make the all-wing aircraft main part be in the position on parallel ground through rotating the all-wing aircraft main part, rotates the support frame again and supports the all-wing aircraft main part and make it keep stable state, can expand the teaching area in classroom, has improved the space utilization and the ventilation effect in classroom greatly, has improved student's learning environment simultaneously to can judge whether to launch the all-wing aircraft according to actual conditions, the flexibility is high.
Drawings
Fig. 1 is an exploded view of a container classroom flying wing deployment configuration according to an embodiment of the present invention;
fig. 2 is a perspective view showing a container classroom flying wing deployment mode according to an embodiment of the present invention;
fig. 3 is a front view of the container classroom flying wing deployment configuration according to an embodiment of the present invention;
fig. 4 is a side view of a container classroom winged deployment configuration in accordance with an embodiment of the present invention;
fig. 5 is a top view of the container classroom flyer deployment configuration according to an embodiment of the present invention;
fig. 6 is a perspective view showing a closed configuration of flying wings in a container classroom according to an embodiment of the present invention;
fig. 7 is a front view of a closed configuration of a container classroom flying wing according to an embodiment of the present invention;
fig. 8 is a side view of a container classroom flyer closed configuration in accordance with an embodiment of the present invention;
fig. 9 is a top view of a closed configuration of container classroom flywings in accordance with an embodiment of the present invention;
fig. 10 is a perspective view showing a closed state of the support frame according to the embodiment of the present invention;
fig. 11 is a front view of the closed configuration of the support frame according to the embodiment of the present invention;
fig. 12 is a side view of a closed configuration of a support frame according to an embodiment of the present invention;
fig. 13 is a top view of the closed configuration of the support frame according to the embodiment of the present invention;
fig. 14 is a perspective view showing an expanded form of the support frame according to the embodiment of the present invention;
fig. 15 is a front view of the support frame according to the embodiment of the present invention in an expanded state;
fig. 16 is a side view of the support frame according to the embodiment of the present invention in an expanded configuration;
fig. 17 is a plan view of the support frame according to the embodiment of the present invention in an expanded state;
fig. 18 is a detailed view of a connecting plate of a support frame according to an embodiment of the present invention;
description of reference numerals:
1. a framework;
21. a right flying wing; 22. a left flying wing;
31. a top cover plate; 32. a bottom cover plate; 33. a front cover plate; 34. a rear cover plate;
41. a supporting seat; 42. supporting the upper rod; 43. supporting the lower rod; 44. a first transverse plate; 45. a second transverse plate;
5. hydraulic hinge; 6. a hydraulic lever; 7. a solar panel; 8. a battery case; 9. a storage battery;
10. an air conditioning system; 11. an LED lighting lamp; 12. an electronic whiteboard; 13. a connecting plate.
Detailed Description
In order to explain the technical content, the objects and the effects of the present invention in detail, the following description is made with reference to the accompanying drawings in combination with the embodiments.
The utility model discloses the most crucial design lies in: the stability of the flying wing is kept by rotating the flying wing main body and the supporting frame, and the space utilization rate of a classroom is improved.
Referring to fig. 1 to 17, a container classroom includes a classroom body;
the classroom main body comprises a cover plate, a flying wing and a square framework;
the flying wing comprises a flying wing main body and a support frame;
one end of the flying wing main body is rotatably connected to the top of one side face of the framework, and the cover plates are respectively arranged on the top face, the bottom face and the other side faces of the framework;
the support frame is rotatably connected to the other end of the flying wing main body.
From the above description, the beneficial effects of the present invention are: through the one end rotatable coupling that sets up the all-wing aircraft main part in the top of a side of skeleton, support frame rotatable coupling in the other end of all-wing aircraft main part can make the all-wing aircraft main part be in the position on parallel ground through rotating the all-wing aircraft main part, rotates the support frame again and supports the all-wing aircraft main part and make it keep stable state, can expand the volume in classroom, has improved the space utilization and the ventilation effect in classroom greatly, has improved student's learning environment simultaneously to can judge whether to launch the all-wing aircraft according to actual conditions, the flexibility is high.
Furthermore, the classroom main body also comprises a hydraulic hinge;
one side of the hydraulic hinge is connected with the top of one side face of the framework, and the other side of the hydraulic hinge is connected with one end of the flying wing main body.
From the above description, through setting up hydraulic hinge and being connected with the top and the all-wing aircraft main part of skeleton respectively, can avoid the condition of tong when opening and shutting the all-wing aircraft, improved the security that the all-wing aircraft opened and shut.
Further, the number of the flying wings is two;
one end of the flying wing main body of one flying wing can be rotatably connected to the top of the first side surface of the framework, and the flying wing main body of the flying wing is provided with a door and a window;
one end of the flying wing main body of the other flying wing can be rotatably connected to the top of a second side face, opposite to the first side face, in the framework, and the flying wing main body of the other flying wing is provided with a window.
As can be seen from the above description, the door and the window are provided on one of the flying wing bodies, and the window is provided on the second flying wing body, so that the daily passage, ventilation and lighting of a classroom can be ensured without unfolding the flying wing, and the whole flying wing can be unfolded, the whole flying wing can be closed, or only one flying wing can be unfolded according to actual requirements, so that the flexibility is high.
Further, the classroom body also includes a hydraulic rod;
one end of the hydraulic rod is connected with the position, close to the top, of the flying wing main body, and the other end of the hydraulic rod is connected with the position, close to the top, of the framework.
According to the above description, the hydraulic rods are respectively connected with the position, close to the top, of the flying wing main body and the position, close to the top, of the framework, the power assisting effect can be achieved on the opening and closing of the flying wing, the opening and closing of the flying wing are facilitated, and manpower is saved.
Further, the support frame comprises a support seat, an upper support rod, a lower support rod, a first transverse plate and a second transverse plate;
the top surface of the supporting seat is welded to the other end of the flying wing main body, one end of the upper supporting rod is rotatably connected with the bottom surface of the supporting seat, one end of the lower supporting rod is slidably connected with the other end of the upper supporting rod, and the lower supporting rod is of a channel steel structure;
one end of the first transverse plate is rotatably connected to the inner side of the channel steel supporting the other end of the lower rod, and one end of the second transverse plate is hinged to the other end of the first transverse plate.
From the above description, when in use, the upper supporting rod can be rotated to be perpendicular to the supporting base, the lower supporting rod and the upper supporting rod are stretched to proper positions, then the first transverse plate and the second transverse plate are rotated to be perpendicular to the lower supporting rod, the main body of the flying wing can be firmly supported, the extension and retraction are realized through the sliding of the lower supporting rod, the supporting height of the flying wing can be adjusted as required, and the flexibility is high; when accomodating, rotate the second diaphragm and stack to first diaphragm on, rotate first diaphragm again and accomodate to being the support lower beam of channel-section steel structure in, the shrink supports the lower beam and supports the upper beam, and the rotatory support upper beam is on a parallel with the all-wing aircraft main part and has accomplished accomodating promptly, has not only improved the stability that supports the all-wing aircraft, has reduced the space of bracing piece moreover and has taken up, does not influence the inside space in container classroom.
Furthermore, the device also comprises a pin shaft;
a first through hole is formed in the position, close to the bottom, of the upper supporting rod, and a second through hole matched with the first through hole is formed in the position, close to the top, of the lower supporting rod;
the pin shaft is respectively matched with the first through hole and the second through hole.
From the above description, it can be known that the position of the upper supporting rod close to the bottom and the position of the lower supporting rod close to the top are correspondingly provided with the first through hole and the second through hole, so that the upper supporting rod and the lower supporting rod can be fixed in a pin shaft mode during stretching, and the stability is improved.
Further, the device also comprises a connecting plate;
the number of the support frames is two;
one end of the connecting plate is connected with the other end of the second transverse plate of one of the support frames, and the other end of the connecting plate is connected with the other end of the second transverse plate of the other support frame.
From the above description, can connect two support frames together through the form of connecting plate with the bolt, make the connection structure of the support frame of two support frames more firm, further improved the stability of support.
Furthermore, the solar cell panel is arranged on the top surface of the top cover plate.
As can be seen from the description, the solar cell panel is used for supplying power to the classroom, so that the energy is saved and the environment is protected.
Furthermore, a gap is arranged between the solar cell panel and the top cover plate.
As can be seen from the above description, the gap is arranged between the solar cell panel and the top cover plate, so that the heat insulation of the classroom can be effectively realized, and the temperature in the classroom is reduced.
The solar cell panel is characterized by further comprising a cell box and a storage battery, wherein the cell box is arranged in a gap between the solar cell panel and the top cover plate, the storage battery is arranged in the cell box, and the storage battery is electrically connected with the solar cell panel.
It can be known from the above-mentioned description, can play the guard action to the battery through the battery case, improve the security, save the electric energy that solar cell panel produced through the battery in addition, make things convenient for the classroom also can normally use electricity when not having the sun, improved the utilization of electric energy.
Example one
Referring to fig. 1 to 18, a container classroom includes a classroom body;
the classroom main body comprises a cover plate, a flying wing and a square framework 1;
the flying wing comprises a flying wing main body and a support frame;
one end of the flying wing main body is rotatably connected to the top of one side face of the framework 1, and the cover plates are respectively arranged on the top face, the bottom face and the other side faces of the framework 1;
the support frame is rotatably connected to the other end of the flying wing main body;
the number of the flying wings can be set according to the actual situation, for example, one, two, three or four flying wings can be arranged;
preferably, the number of the flying wings is two, as shown in fig. 1, the flying wings include a left flying wing 22 and a right flying wing 21, and the cover plates include a top cover plate 31, a bottom cover plate 32, a front cover plate 33 and a rear cover plate 34;
one end of the left flying wing main body of the left flying wing 22 is rotatably connected to the top of the first side surface of the framework 1, and the right flying wing main body of the right flying wing 21 is provided with a door and a window, specifically, the door and the window are arranged on the surface of the right flying wing main body;
one end of the left wing main body of the left wing 22 is rotatably connected to the top of a second side surface opposite to the first side surface in the framework 1, and the left wing main body of the left wing 22 is provided with a window, specifically, the window is arranged on the surface of the left wing main body;
wherein, the classroom main body also comprises a hydraulic hinge 5;
one side of the hydraulic hinge 5 is connected with the top of one side of the framework 1, and the other side of the hydraulic hinge 5 is connected with one end of the flying wing main body;
preferably, the hydraulic hinge 5 is a hydraulic damping hinge;
wherein the classroom body further includes a hydraulic rod 6;
one end of the hydraulic rod 6 is connected with the position, close to the top, of the flying wing main body, and the other end of the hydraulic rod 6 is connected with the position, close to the top, of the framework 1;
specifically, the hydraulic rod 6 comprises a piston rod and a pressure rod, and one end of the pressure sensor is slidably connected with one end of the piston rod along the length direction of the piston rod;
as shown in fig. 10 to 17, the supporting frame includes a supporting seat 41, an upper supporting rod 42, a lower supporting rod 43, a first horizontal plate 44 and a second horizontal plate 45;
the top surface of the support base 41 is welded to the other end of the flying wing main body, one end of the upper support rod 42 is rotatably connected to the bottom surface of the support base 41, one end of the lower support rod 43 is slidably connected to the other end of the upper support rod 42, specifically, the diameter of the lower support rod 43 is smaller than that of the upper support rod 42, and one end of the lower support rod 43 is slidably connected to the other end of the upper support rod 42 along the length direction of the upper support rod 42;
specifically, the lower supporting rod 43 is a channel steel structure;
specifically, a limiting member is arranged at the bottom of the supporting seat 41, and the limiting member limits the supporting upper rod 42 to rotate to a position perpendicular to the main body of the flying wing;
one end of the first transverse plate 44 is rotatably connected to the inner side of the channel steel at the other end of the lower supporting rod 43, and one end of the second transverse plate 45 is hinged to the other end of the first transverse plate 44;
the device comprises an upper supporting rod 42, a lower supporting rod 43 and a pin shaft, wherein the upper supporting rod is provided with a first through hole at a position close to the bottom, the lower supporting rod 43 is provided with a second through hole matched with the first through hole at a position close to the top, the pin shaft is respectively matched with the first through hole and the second through hole, and when the lower supporting rod 43 is stretched to a position corresponding to the first through hole and the second through hole, the lower supporting rod and the first through hole can be fixed in a pin shaft mode;
preferably, the rotation directions of the upper support rod 42, the first horizontal plate 44 and the second horizontal plate 45 are all in the direction of the flying wing main body.
Specifically, as shown in fig. 14 to 17, when in use, the upper supporting rod 42 can be rotated to be perpendicular to the supporting base 41, the lower supporting rod 43 and the upper supporting rod 42 are stretched to appropriate positions, and then the first transverse plate 44 and the second transverse plate 45 are rotated to be perpendicular to the lower supporting rod 43, so that the supporting frame is in a spread state, and the main flying wing body can be firmly supported, wherein the stretching positions of the upper supporting rod 42 and the lower supporting rod 43 can be adjusted according to actual requirements, and thus the support for the height of the main flying wing body can be flexibly set; as shown in fig. 10 to 13, when in storage, the second transverse plate 45 is rotated to be stacked on the first transverse plate 44, then the first transverse plate 44 is rotated to be stored in the lower supporting rod 43 in a channel steel structure, the lower supporting rod 43 and the upper supporting rod 42 are contracted, and the upper rotating supporting rod 42 is parallel to the flying wing main body, so that the storage is completed, the stability of supporting the flying wings is improved, the space occupation of the supporting rods is reduced, and the space in a container classroom is not influenced;
as shown in fig. 18, the foldable support frame further comprises two connecting plates 13, one end of each connecting plate 13 is connected to the other end of the second transverse plate 45 of one of the supporting frames, and the other end of each connecting plate 13 is connected to the other end of the second transverse plate 45 of the other supporting frame;
specifically, a first through hole is formed in the surface of the other end of one of the support frames, a second through hole is formed in the surface of the other end of the second transverse plate 45 of the other support frame, and two ends of the connecting plate 13 are respectively connected with the first through hole and the second through hole;
preferably, the first connecting hole and the second connecting hole can be fixedly connected with each other by means of matching the connecting plate 13 with a bolt, so that the stability of the whole structure is improved;
as shown in fig. 2, the connecting structure of the two supporting frames after the first connecting hole and the second connecting hole are connected is U-shaped;
preferably, the rotation directions of the upper supporting rod 42, the first transverse plate 44 and the second transverse plate 45 of the two brackets are set to rotate oppositely;
the solar cell panel is characterized by further comprising a solar cell panel 7, wherein the solar cell panel 7 is arranged on the top surface of the top cover plate 31, and a gap is formed between the solar cell panel 7 and the top cover plate 31;
the solar cell comprises a solar cell panel 7, a top cover plate 31, a battery box 8 and a storage battery 9, wherein the battery box 8 is arranged in a gap between the solar cell panel 7 and the top cover plate 31, the storage battery 9 is arranged in the battery box 8, and the storage battery 9 is electrically connected with the solar cell panel;
further, the LED lamp and the air conditioning system 10 are further included, the LED lamp 11 and the air conditioning system 10 are arranged on the bottom surface of the top cover plate 31, and the LED lamp 11 and the air conditioning system 10 are respectively electrically connected with the storage battery 9;
further, the classroom main body is internally provided with necessary facilities of classrooms such as a seat, an electronic whiteboard 12 and the like so as to ensure normal teaching.
To sum up, the utility model provides a container classroom, through setting up one end rotatable coupling of all-wing aircraft main part in the top of a side of skeleton, the support frame rotatable coupling in the other end of all-wing aircraft main part, can make all-wing aircraft main part be in the position of parallel ground through rotating all-wing aircraft main part, rotate the support frame again and support all-wing aircraft main part and make it keep steady state, can expand the teaching area in classroom, have greatly improved space utilization and ventilation effect in classroom, and can judge whether to launch all-wing aircraft according to the actual conditions, the flexibility is high; by arranging the foldable telescopic support frame, the stability of the flying wing support is improved, the space occupation of the support rod is reduced, and the space in a container classroom is not influenced; wherein through setting up hydraulic pressure hinge respectively with the top and the all-wing aircraft bulk phase of skeleton, improved the security that the all-wing aircraft opened and shut, and set up the space between solar cell panel and top surface cover plate, can effectively insulate against heat to the classroom, reduced the inside temperature in classroom, improved student's learning environment.
The above mentioned is only the embodiment of the present invention, and not the limitation of the patent scope of the present invention, all the equivalent transformations made by the contents of the specification and the drawings, or the direct or indirect application in the related technical field, are included in the patent protection scope of the present invention.
Claims (10)
1. A container classroom is characterized by comprising a classroom body;
the classroom main body comprises a cover plate, a flying wing and a square framework;
the flying wing comprises a flying wing main body and a support frame;
one end of the flying wing main body is rotatably connected to the top of one side face of the framework, and the top face, the bottom face and the side face of the framework are respectively provided with the cover plate;
the support frame is rotatably connected to the other end of the flying wing main body.
2. The container classroom of claim 1 wherein the classroom body further includes hydraulic hinges;
one side of the hydraulic hinge is connected with the top of one side face of the framework, and the other side of the hydraulic hinge is connected with one end of the flying wing main body.
3. The container classroom of claim 1 or 2 wherein the number of said flying wings is two;
one end of the flying wing main body of one flying wing can be rotatably connected to the top of the first side surface of the framework, and the flying wing main body of the flying wing is provided with a door and a window;
one end of the flying wing main body of the other flying wing can be rotatably connected to the top of a second side face, opposite to the first side face, in the framework, and the flying wing main body of the other flying wing is provided with a window.
4. The container classroom of claim 1 or 2 wherein the classroom body further includes a hydraulic ram;
one end of the hydraulic rod is connected with the position, close to the top, of the flying wing main body, and the other end of the hydraulic rod is connected with the position, close to the top, of the framework.
5. The container classroom of claim 1 wherein the support frame includes a support base, an upper support bar, a lower support bar, a first cross plate, and a second cross plate;
the top surface of the supporting seat is welded to the other end of the flying wing main body, one end of the upper supporting rod is rotatably connected with the bottom surface of the supporting seat, one end of the lower supporting rod is slidably connected with the other end of the upper supporting rod, and the lower supporting rod is of a channel steel structure;
one end of the first transverse plate is rotatably connected to the inner side of the channel steel supporting the other end of the lower rod, and one end of the second transverse plate is hinged to the other end of the first transverse plate.
6. The container classroom of claim 5 further comprising a pin;
a first through hole is formed in the position, close to the bottom, of the upper supporting rod, and a second through hole matched with the first through hole is formed in the position, close to the top, of the lower supporting rod;
the pin shaft is respectively matched with the first through hole and the second through hole.
7. The container classroom of claim 5 or 6 further comprising a connection panel;
the number of the support frames is two;
one end of the connecting plate is connected with the other end of the second transverse plate of one of the support frames, and the other end of the connecting plate is connected with the other end of the second transverse plate of the other support frame.
8. The container classroom of claim 1 further comprising a solar panel disposed on a top surface of the cover plate.
9. The container classroom of claim 8 wherein a gap is provided between the solar panel and the cover plate.
10. The container classroom of claim 9 further comprising a battery compartment disposed in the space between the solar panel and the roof deck and a battery disposed within the battery compartment, the battery being electrically connected to the solar panel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920232739.3U CN210134673U (en) | 2019-02-22 | 2019-02-22 | Container classroom |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920232739.3U CN210134673U (en) | 2019-02-22 | 2019-02-22 | Container classroom |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210134673U true CN210134673U (en) | 2020-03-10 |
Family
ID=69702218
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920232739.3U Active CN210134673U (en) | 2019-02-22 | 2019-02-22 | Container classroom |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210134673U (en) |
-
2019
- 2019-02-22 CN CN201920232739.3U patent/CN210134673U/en active Active
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