CN211869709U - Special case of constant temperature aviation - Google Patents

Special case of constant temperature aviation Download PDF

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Publication number
CN211869709U
CN211869709U CN201922381655.9U CN201922381655U CN211869709U CN 211869709 U CN211869709 U CN 211869709U CN 201922381655 U CN201922381655 U CN 201922381655U CN 211869709 U CN211869709 U CN 211869709U
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CN
China
Prior art keywords
special case
constant temperature
container body
thermostated container
aviation
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Expired - Fee Related
Application number
CN201922381655.9U
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Chinese (zh)
Inventor
邓静怡
黄若婷
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Jiangxi Normal University
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Jiangxi Normal University
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Priority to CN201922381655.9U priority Critical patent/CN211869709U/en
Application granted granted Critical
Publication of CN211869709U publication Critical patent/CN211869709U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a special case of constant temperature aviation relates to special case technical field of aviation, specifically is a special case of constant temperature aviation, including the thermostated container body, one side of thermostated container body articulates there is the chamber door, the fixed surface of thermostated container body is connected with the heat preservation, the side fixedly connected with of thermostated container body is located the shock attenuation piece on heat preservation surface. This special case of constant temperature aviation, use through the mounting panel with the cooperation of placing board and L shape sliding tray, utilize the mounting panel to cup joint placing the board, the messenger places the board and can remove on the mounting panel, be convenient for adjust storing space, the single nonadjustable problem in traditional special case of constant temperature aviation storing space has been avoided, utilize the use of L shape sliding tray simultaneously, slide at L shape sliding tray inside through the carriage, and then utilize the traveller to transport heavier article, the physical demands of carrying sparingly, the practicality of this special case of constant temperature aviation has been improved.

Description

Special case of constant temperature aviation
Technical Field
The utility model relates to a special case technical field of aviation specifically is a special case of constant temperature aviation.
Background
Case is placed to special case of constant temperature aviation is a luggage that often uses when aviation flies, traditional special case of constant temperature aviation is owing to use the removal wheel to support when placing, stability is relatively poor, simultaneously traditional special case of constant temperature aviation is owing to luggage is placed comparatively densely when the delivery, mutual extrusion often leads to special case of constant temperature aviation to warp between the aviation case, and traditional special case of constant temperature aviation inside storage space can not adjust, the storing range is comparatively single, simultaneously to heavier article, it is comparatively inconvenient to carry, therefore we have proposed a special case of constant temperature aviation.
SUMMERY OF THE UTILITY MODEL
Not enough to prior art, the utility model provides a special case of constant temperature aviation has solved the problem of proposing among the above-mentioned background art.
In order to achieve the above purpose, the utility model discloses a following technical scheme realizes: the utility model provides a special case of constant temperature aviation, includes the thermostated container body, one side of thermostated container body articulates there is the chamber door, the fixed surface of thermostated container body is connected with the heat preservation, the side fixedly connected with of thermostated container body is located the shock attenuation piece on heat preservation surface, the both sides fixed mounting of thermostated container body lower surface has a section of thick bamboo that cup joints, the both sides fixed mounting of thermostated container body lower surface has the removal wheel, it is located the inboard of a section of thick bamboo that cup joints to remove the wheel, the sliding tray has been seted up to the upper surface of thermostated container body, the both sides fixedly connected with mounting panel.
Optionally, the spring is dragged to the inner chamber fixedly connected with of a cover sleeve section of thick bamboo, the support column has been cup jointed in the inner chamber activity of a cover sleeve section of thick bamboo, the one end fixedly connected to of support column drags the one end of spring, the inside fixedly connected with of support column promotes the spring, the one end fixed mounting who promotes the spring has spacing post, spacing post extends to the outside of a cover sleeve section of thick bamboo, the lower fixed surface of support column is connected with supporting baseplate.
Optionally, one side of the damping sheet is fixedly connected with a contact plate.
Optionally, the inner cavity joint of sliding tray has the sliding block, the top activity of sliding block has cup jointed the push-and-pull rod.
Optionally, the placing plates are movably sleeved on two sides of the mounting plate, the surface of the mounting plate is provided with fixing holes, inner cavities of the fixing holes are movably sleeved with fixing columns, the fixing columns extend to the outside of the placing plates, and the bottom of the mounting plate is provided with an L-shaped sliding groove.
Optionally, the inner cavity of the L-shaped sliding groove is movably sleeved with a transportation frame, and the inside of the transportation frame is movably sleeved with a rolling column.
Optionally, the middle part of the box door is fixedly provided with two pieces of toughened glass, and a gap between the two pieces of toughened glass is in a vacuum state.
The utility model provides a special case of constant temperature aviation possesses following beneficial effect:
1. this special case of constant temperature aviation, use through the mounting panel with the cooperation of placing board and L shape sliding tray, utilize the mounting panel to cup joint placing the board, the messenger places the board and can remove on the mounting panel, be convenient for adjust storing space, the single nonadjustable problem in traditional special case of constant temperature aviation storing space has been avoided, utilize the use of L shape sliding tray simultaneously, slide at L shape sliding tray inside through the carriage, and then utilize the traveller to transport heavier article, the physical demands of carrying sparingly, the practicality of this special case of constant temperature aviation has been improved.
2. This special case of constant temperature aviation uses through the cooperation of a cover section of thick bamboo and support column and supporting baseplate, when this special case of constant temperature aviation was placed, through taking out the support column and make supporting baseplate and ground contact, and then supports the thermostated container body, has avoided using to remove the wheel and has carried out single support and place and lead to the unstable problem of thermostated container body to appear, has improved the stability of this special case of constant temperature aviation.
Drawings
FIG. 1 is a schematic structural view of the present invention;
fig. 2 is a schematic top view of the present invention;
FIG. 3 is a schematic view of the structure of the door of the present invention;
fig. 4 is a schematic structural view of the placing plate of the present invention;
FIG. 5 is a schematic structural view of the transportation frame of the present invention;
fig. 6 is a schematic structural view of the supporting bottom plate of the present invention.
In the figure: 1. a thermostat body; 2. a box door; 3. fixing a column; 4. mounting a plate; 5. a damping sheet; 6. tempering the glass; 7. a contact plate; 8. a rolling post; 9. a transport rack; 10. pulling the spring; 11. a limiting column; 12. a support pillar; 13. a support base plate; 14. a moving wheel; 15. a heat-insulating layer; 16. an L-shaped sliding groove; 17. a push spring; 18. sleeving a sleeve; 19. placing the plate; 20. a fixing hole; 21. a push-pull rod; 22. a slider; 23. a sliding groove.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.
Referring to fig. 1 to 6, the present invention provides a technical solution: the utility model provides a special case of constant temperature aviation, including thermostated container body 1, one side of thermostated container body 1 articulates there is chamber door 2, thermostated container body 1's fixed surface is connected with heat preservation 15, thermostated container body 1's side fixedly connected with is located the shock attenuation piece 5 on heat preservation 15 surface, the both sides fixed mounting of thermostated container body 1 lower surface has a socket 18, the both sides fixed mounting of thermostated container body 1 lower surface has removal wheel 14, it is located the inboard of socket 18 to remove wheel 14, sliding tray 23 has been seted up to the upper surface of thermostated container body 1, the both sides fixedly connected with mounting panel 4 of thermostated container body 1 inner chamber.
Wherein, the inner cavity of the sleeve 18 is fixedly connected with a pulling spring 10, the inner cavity of the sleeve 18 is movably sleeved with a supporting column 12, one end of the supporting column 12 is fixedly connected to one end of the pulling spring 10, the inside of the supporting column 12 is fixedly connected with a pushing spring 17, one end of the pushing spring 17 is fixedly provided with a limiting column 11, the limiting column 11 extends to the outside of the sleeve 18, the lower surface of the supporting column 12 is fixedly connected with a supporting bottom plate 13, the sleeve 18 is arranged at the bottom of the incubator body 1, the supporting column 12 is sleeved by the sleeve 18, when the constant temperature aviation special case is placed, the supporting column 12 is pulled out by pressing the supporting bottom plate 13, the limiting column 11 is popped out under the elastic force of the sleeve 18 to fix the supporting column 12, at the moment, the supporting bottom plate 13 is contacted with the ground, and further the traditional constant temperature aviation special case is prevented from being, place unstable problem, improved the stability of this special case of constant temperature aviation, utilize simultaneously to pull spring 10 and stimulate support column 12, it is more convenient when putting to receive support column 12.
Wherein, one side fixedly connected with contact plate 7 of shock attenuation piece 5 uses through the cooperation of shock attenuation piece 5 and contact plate 7, utilizes contact plate 7 to contact external object, utilizes the deformation of shock attenuation piece 5 to make contact plate 7 shrink simultaneously, and then plays the effect of preventing extrudeing, shape, anticollision, has improved the stability of this special case of constant temperature aviation.
Wherein, the inner chamber joint of sliding tray 23 has sliding block 22, sliding block 22's top activity has cup jointed push-and-pull rod 21, sliding tray 23 is seted up through the top at thermostated container body 1, utilize sliding tray 23 to carry out the joint to sliding block 22, cup joint push-and-pull rod 21 through sliding block 22, utilize sliding block 22 can rotate and then can adjust the direction of push-and-pull rod 21 at the middle part of sliding tray 23, avoided because aircraft storing passageway is narrower, it is comparatively inconvenient to switch aviation case direction, lead to the inconvenient problem of push-and-pull constant temperature aviation special case operation, the practicality of this constant temperature aviation special case has been improved.
Wherein, the board 19 of placing has been cup jointed in the both sides activity of mounting panel 4, fixed orifices 20 have been seted up on the surface of mounting panel 4, fixed column 3 has been cup jointed in the inner chamber activity of fixed orifices 20, fixed column 3 extends to the outside of placing board 19, L shape sliding tray 16 has been seted up to the bottom of mounting panel 4, use through the cooperation of fixed orifices 20 with fixed column 3, make and place board 19 and remove the back on mounting panel 4, utilize fixed column 3 to pass the inner chamber of placing board 19 and fixed orifices 20 and then fix placing board 19, can make and place board 19 and carry out position control at the certain extent, the problem that traditional special incasement portion of constant temperature aviation placed board unadjustable has been avoided, it is more practical to make this special case of constant temperature aviation carry out the storing.
Wherein, the transportation frame 9 has been cup jointed in the inner chamber activity of L shape sliding tray 16, the roll post 8 has been cup jointed in the inside activity of transportation frame 9, cup joint transportation frame 9 through L shape sliding tray 16, make transportation frame 9 slide in L shape sliding tray 16, when pulling transportation frame 9 to the inner chamber one end of L shape sliding tray 16, transportation frame 9 can the downward sloping, and then with the ground contact, utilize simultaneously roll post 8 can carry some very heavy article, place article, it can extrude fixedly to the top of article to utilize and place board 19 simultaneously, the convenience of use of this special case of constant temperature aviation has been improved.
Wherein, the middle part fixed mounting of chamber door 2 has toughened glass 6, and toughened glass 6's quantity is two, and the clearance between two toughened glass 6 is vacuum state, through set up toughened glass 6 on chamber door 2, is convenient for observe the article of 1 inner chamber of thermostated container body through toughened glass 6, utilizes the clearance between two toughened glass 6 to be vacuum state simultaneously, and then plays the heat preservation effect, has improved the practicality of this special case of constant temperature aviation.
To sum up, this special case of constant temperature aviation, during the use, at first according to the size of goods reciprocate place board 19, then use fixed column 3 to place board 19 and fix, when carrying big article, outwards pull out transportation frame 9, utilize the rolling post 8 to carry out the cargo handling, load the goods after, close chamber door 2, then move push-and-pull rod 21 to the middle part of sliding tray 23, rotate, select suitable pulling direction, when placing, use the sole to step on and press supporting baseplate 13, step on supporting baseplate 13 and press the department and contact with ground, spacing post 11 is released under the elastic force effect that promotes spring 17 and is connected with socket 18 mutually, put push-and-pull rod 21 into the inner chamber of sliding tray 23, can.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.

Claims (7)

1. The utility model provides a special case of constant temperature aviation, includes thermostated container body (1), its characterized in that: one side of thermostated container body (1) articulates there is chamber door (2), the fixed surface of thermostated container body (1) is connected with heat preservation (15), the side fixedly connected with of thermostated container body (1) is located shock attenuation piece (5) on heat preservation (15) surface, the both sides fixed mounting of thermostated container body (1) lower surface has a socket (18), the both sides fixed mounting of thermostated container body (1) lower surface has removal wheel (14), remove wheel (14) and be located the inboard of socket (18), sliding tray (23) have been seted up to the upper surface of thermostated container body (1), the both sides fixedly connected with mounting panel (4) of thermostated container body (1) inner chamber.
2. The special case of constant temperature aviation of claim 1, characterized in that: the inner chamber fixedly connected with of a cover sleeve section of thick bamboo (18) pulls spring (10), the inner chamber activity of a cover sleeve section of thick bamboo (18) has cup jointed support column (12), the one end fixed connection of support column (12) pulls the one end of spring (10), the inside fixedly connected with of support column (12) promotes spring (17), the one end fixed mounting that promotes spring (17) has spacing post (11), spacing post (11) extend to the outside of a cover sleeve section of thick bamboo (18), the lower fixed surface of support column (12) is connected with supporting baseplate (13).
3. The special case of constant temperature aviation of claim 1, characterized in that: one side of the shock absorption sheet (5) is fixedly connected with a contact plate (7).
4. The special case of constant temperature aviation of claim 1, characterized in that: the inner cavity joint of sliding tray (23) has sliding block (22), push-and-pull rod (21) has been cup jointed in the top activity of sliding block (22).
5. The special case of constant temperature aviation of claim 1, characterized in that: the mounting plate is characterized in that the placing plate (19) is movably sleeved on two sides of the mounting plate (4), fixing holes (20) are formed in the surface of the mounting plate (4), fixing columns (3) are movably sleeved in inner cavities of the fixing holes (20), the fixing columns (3) extend to the outside of the placing plate (19), and L-shaped sliding grooves (16) are formed in the bottom of the mounting plate (4).
6. The special case of constant temperature aviation of claim 5, wherein: the inner cavity of the L-shaped sliding groove (16) is movably sleeved with a transportation frame (9), and the inside of the transportation frame (9) is movably sleeved with a rolling column (8).
7. The special case of constant temperature aviation of claim 1, characterized in that: the middle part of the box door (2) is fixedly provided with two pieces of toughened glass (6), and the gap between the two pieces of toughened glass (6) is in a vacuum state.
CN201922381655.9U 2019-12-26 2019-12-26 Special case of constant temperature aviation Expired - Fee Related CN211869709U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201922381655.9U CN211869709U (en) 2019-12-26 2019-12-26 Special case of constant temperature aviation

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201922381655.9U CN211869709U (en) 2019-12-26 2019-12-26 Special case of constant temperature aviation

Publications (1)

Publication Number Publication Date
CN211869709U true CN211869709U (en) 2020-11-06

Family

ID=73263699

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201922381655.9U Expired - Fee Related CN211869709U (en) 2019-12-26 2019-12-26 Special case of constant temperature aviation

Country Status (1)

Country Link
CN (1) CN211869709U (en)

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CF01 Termination of patent right due to non-payment of annual fee
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Granted publication date: 20201106

Termination date: 20211226