CN212402108U - Antidetonation flight case - Google Patents

Antidetonation flight case Download PDF

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Publication number
CN212402108U
CN212402108U CN202020998833.2U CN202020998833U CN212402108U CN 212402108 U CN212402108 U CN 212402108U CN 202020998833 U CN202020998833 U CN 202020998833U CN 212402108 U CN212402108 U CN 212402108U
Authority
CN
China
Prior art keywords
box
fixedly arranged
box body
elastic cloth
box cover
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.)
Expired - Fee Related
Application number
CN202020998833.2U
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Chinese (zh)
Inventor
肖修谊
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.)
Foshan Jianxiang Performing Arts Equipment Co ltd
Original Assignee
Foshan Jianxiang Performing Arts Equipment Co ltd
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 Foshan Jianxiang Performing Arts Equipment Co ltd filed Critical Foshan Jianxiang Performing Arts Equipment Co ltd
Priority to CN202020998833.2U priority Critical patent/CN212402108U/en
Application granted granted Critical
Publication of CN212402108U publication Critical patent/CN212402108U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses an antidetonation aviation case, the power distribution box comprises a box body, the top swing joint of box has the case lid, the intermediate position fixed mounting of terminal surface has the fixed block before the box, the equal fixed mounting in both sides of fixed block has the lower switch of terminal surface before being located the box to detain, two upper switches are installed to the preceding terminal surface symmetry of case lid and are detained, the both ends fixed mounting of fixed block has the handle, four end angles that the box one side was kept away from to the case lid with the equal fixed mounting in four end angles that the case lid one side was kept away from to the box has the anticollision angle. The utility model discloses a set up elasticity cloth A and elasticity cloth B, wrap up the inside instrument and equipment of box, make through setting up magnetite A and magnetite B and attract each other between elasticity cloth A and the elasticity cloth B, separate the inside instrument of box and the inner wall of case lid and box, thereby avoid touching the antidetonation effect that improves the aviation case.

Description

Antidetonation flight case
Technical Field
The utility model relates to an aviation case technical field specifically is an antidetonation aviation case.
Background
The aviation case is a novel packing product which is produced by replacing transportation and aims at solving the defects that the traditional simple wooden case packing transportation cannot solve the problems that high-tech products cannot be effectively protected and have poor maneuverability in the long-distance transportation process, the traditional simple wooden case packing transportation cannot solve the defects that the high-tech products cannot be effectively protected and have poor maneuverability in the long-distance transportation process, and a new packing product, namely the aviation case, which replaces transportation is produced aiming at the defect. The use and development of the aviation case step into the gold stage by the increasingly frequent transnational trade, and the aviation case is widely applied to the fields of high-tech equipment such as stage lighting equipment, medical instrument equipment, audio-visual system multimedia, photoelectric industry, military transportation package, military equipment transportation and the like.
However, in the use process of the existing aviation case, a gap is often left between the instrument placed in the accommodating cavity and the inner wall of the accommodating cavity, so that the instrument and the inner wall of the accommodating cavity are impacted or rubbed to damage equipment and a case body in the transportation process, and the existing aviation case does not have good shock resistance; therefore, the existing requirements are not met, and an anti-seismic flight box is provided for the requirements.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an antidetonation aviation case to current aviation case that proposes in solving above-mentioned background art often can leave the clearance between the inner wall in holding intracavity and holding chamber is placed to the instrument in the use, and this has just resulted in producing striking or friction between the inner wall in instrument meeting and holding chamber in the transportation and has damaged equipment and box, does not possess good shock resistance scheduling problem.
In order to achieve the above object, the utility model provides a following technical scheme: an anti-seismic aviation case comprises a case body, wherein a case cover is movably connected above the case body, a fixed block is fixedly arranged at the middle position of the front end face of the case body, lower switch buttons positioned at the front end face of the case body are fixedly arranged at the two sides of the fixed block, two upper switch buttons are symmetrically arranged at the front end face of the case cover, handles are fixedly arranged at the two ends of the fixed block, four end angles of the case cover far away from one side of the case body and four end angles of the case body far away from one side of the case cover are fixedly provided with anti-collision angles, an elastic cloth A is arranged in the case cover, a fixed frame A is fixedly arranged at the edge of the elastic cloth A, a storage bin is arranged in the case body, an elastic cloth B is arranged in the storage bin, a fixed frame B is fixedly arranged at the edge of the elastic cloth B, and springs, the equal fixed mounting in the other end of spring has the bottom plate, the equal fixed mounting in outward flange of bottom plate has the rectangle frame, the equal fixed mounting in four end angles that fixed frame A one side was kept away from to elasticity cloth A has magnetite A, the equal fixed mounting in four end angles that fixed frame B one side was kept away from to elasticity cloth B has magnetite B.
Preferably, the magnetic poles of the magnet A and the magnet B are opposite, the magnet A and the magnet B are the same in size, and the top end of the lower switch buckle is clamped into the upper switch buckle.
Preferably, the box cover is connected with the box body through a hinge, and the hinge is located on one end face far away from the upper switch buckle and the lower switch buckle.
Preferably, the rectangular frame and the bottom plate are of an integrally formed structure, the outer edge of the rectangular frame is attached to the inner edge of the fixed frame A, and the height of the rectangular frame is half of the height of the fixed frame A.
Preferably, one end of the spring is fixedly installed at four end corners of the bottom plate, and the other end of the spring is fixedly installed at four end corners of one surface, close to the rectangular frame, of the elastic cloth A and four end corners of one surface, close to the bottom plate, of the elastic cloth B.
Preferably, the fixed block is fixedly installed in the middle position of the front end face formed by the box cover and the box body together, and the positions of the upper switch buckle and the lower switch buckle are vertically corresponding.
Preferably, the bottom plate is fixedly installed on the bottom end face of the storage bin and the top end face of the inner wall of the box cover through bolts.
Compared with the prior art, the beneficial effects of the utility model are that:
1. the utility model discloses a set up elasticity cloth A and elasticity cloth B, wrap up the inside instrument and equipment of box, make through setting up magnetite A and magnetite B and attract each other between elasticity cloth A and the elasticity cloth B, make the inside of case lid and the inside of storing storehouse respectively connected with the fixed frame B in the fixed frame A and the elasticity cloth B outside through setting up the spring, separate the inside instrument of box and the inner wall of case lid and box, thereby avoid touching the antidetonation effect that improves the aviation case.
Drawings
FIG. 1 is an exploded view of the whole of the present invention;
FIG. 2 is a schematic structural view of the overall closed state of the present invention;
FIG. 3 is a schematic structural view of the overall open state of the present invention;
fig. 4 is a side view of the present invention as a whole.
In the figure: 1. a box cover; 2. an anti-collision angle; 3. a switch buckle is arranged; 4. a rectangular frame; 5. a spring; 6. a fixed frame A; 7. a magnet A; 8. a magnet B; 9. a box body; 10. a lower switch buckle; 11. a fixed block; 12. a handle; 13. a storage bin; 14. a base plate; 15. elastic cloth A; 16. elastic cloth B; 17. and a fixing frame B.
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 4, the present invention provides an embodiment: an anti-seismic aviation case comprises a case body 9, a case cover 1 is movably connected above the case body 9, a fixed block 11 is fixedly arranged at the middle position of the front end face of the case body 9, lower switch buckles 10 positioned on the front end face of the case body 9 are fixedly arranged on both sides of the fixed block 11, two upper switch buckles 3 are symmetrically arranged on the front end face of the case cover 1, handles 12 are fixedly arranged at both ends of the fixed block 11, four end corners of one face, away from the case body 9, of the case cover 1 and four end corners of one face, away from the case cover 1, of the case body 9 are respectively and fixedly provided with an anti-collision corner 2, an elastic cloth A15 is arranged inside the case cover 1, a fixed frame A6 is fixedly arranged at the edge of the elastic cloth A15, a storage bin 13 is arranged inside the case body 9, an elastic cloth B16 is arranged inside the storage bin 13, a fixed frame B17 is fixedly arranged at the edge of the elastic cloth B16, springs 5, rectangular frame 4 is all fixed mounting to the outward flange of bottom plate 14, and the equal fixed mounting in four end angles that fixed frame A6 one side was kept away from to elasticity cloth A15 has magnetite A7, and the equal fixed mounting in four end angles that fixed frame B17 one side was kept away from to elasticity cloth B16 has magnetite B8.
Further, the magnetic poles of the magnet a7 and the magnet B8 are opposite, the magnet a7 and the magnet B8 are the same size, and the tip of the lower switch button 10 is engaged with the inside of the upper switch button 3.
By adopting the technical scheme, the magnets A7 and the magnets B8 drive the elastic cloth A15 and the elastic cloth B16 to attract each other.
Further, the box cover 1 is connected with the box body 9 through a hinge, and the hinge is located on one end face far away from the upper switch buckle 3 and the lower switch buckle 10.
By adopting the technical scheme, the box cover 1 is movably connected with the box body 9.
Further, the rectangular frame 4 and the bottom plate 14 are of an integrally formed structure, the outer edge of the rectangular frame 4 is attached to the inner edge of the fixing frame a6, and the height of the rectangular frame 4 is half of the height of the fixing frame a 6.
By adopting the technical scheme, the rectangular frame 4 can be clamped in the fixing frame A6, so that the elastic cloth A15 always leaves a space with the inner wall of the box cover 1, and the elastic cloth B16 always leaves a space with the inner wall of the storage bin 13.
Furthermore, one end of the spring 5 is fixedly arranged at four end corners of the bottom plate 14, and the other end of the spring 5 is fixedly arranged at four end corners of one surface of the elastic cloth A15 close to the rectangular frame 4 and four end corners of one surface of the elastic cloth B16 close to the bottom plate 14.
Through adopting above-mentioned technical scheme to when magnetite A7 and magnetite B8 attract each other, avoid fixed frame A6 and fixed frame B17 can't cause with the internal connection of case lid 1 and storing storehouse 13 and rock.
Further, the fixing block 11 is fixedly installed in the middle position of the front end face formed by the box cover 1 and the box body 9, and the positions of the upper switch buckle 3 and the lower switch buckle 10 correspond to each other up and down.
By adopting the technical scheme, the box cover 1 and the box body 9 are convenient to close.
Further, the bottom plate 14 is fixedly mounted on the bottom end surface of the storage compartment 13 and the top end surface of the inner wall of the box cover 1 by bolts, respectively.
By adopting the technical scheme, the rectangular frame 4 can be fixed on the bottom end surface of the storage bin 13 and the top end surface of the inner wall of the box cover 1.
The working principle is as follows: when the aviation case is used, the case cover 1 is opened through the upper switch buckle 3 and the lower switch buckle 10, instrument equipment needing to be stored is placed in the storage bin 13 in the case body 9, the elastic cloth B16 supports the instrument equipment upwards, the case cover 1 is closed, the magnet A7 and the magnet B8 attract each other, the elastic cloth A15 moves downwards, the elastic cloth B16 moves upwards, the instrument equipment between the elastic cloth A15 and the elastic cloth B16 is wrapped without damaging the instrument equipment, meanwhile, the spring 5 is stretched under the tensile force, the fixing frame A6 is fixed on the top end face of the case cover 1 through the rectangular frame 4, the fixing frame B17 is fixed on the bottom end face of the storage bin 13 through the rectangular frame 4, the case cover 1 and the case body 9 are closed through the upper switch buckle 3 and the lower switch buckle 10, the case cover 1 and the case body 9 are lifted and moved through the handle 12, the aviation case can flexibly adjust the wrapping force according to different sizes of the instrument equipment, make the instrument and equipment be located the centre of storing storehouse 13 all the time, alleviate vibrations simultaneously through spring 5 fixes fixed frame A6 and fixed frame B17, avoid producing the collision with the inner wall of case lid 1 the inner wall of storing storehouse 13 already, possess good antidetonation effect.
It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein.

Claims (7)

1. The utility model provides an antidetonation aviation case, includes the box, its characterized in that: the upper part of the box body is movably connected with a box cover, a fixed block is fixedly arranged at the middle position of the front end face of the box body, lower switch buckles positioned at the front end face of the box body are fixedly arranged at the two sides of the fixed block, two upper switch buckles are symmetrically arranged at the front end face of the box cover, handles are fixedly arranged at the two ends of the fixed block, four end corners of one surface of the box body away from the box cover and four end corners of one surface of the box body away from the box cover are fixedly provided with anti-collision corners, an elastic cloth A is arranged in the box cover, a fixed frame A is fixedly arranged at the edge of the elastic cloth A, a storage bin is arranged in the box body, an elastic cloth B is arranged in the storage bin, a fixed frame B is fixedly arranged at the edge of the elastic cloth B, springs are fixedly arranged in the fixed frame A and the, the equal fixed mounting in outward flange of bottom plate has the rectangle frame, the equal fixed mounting in four end angles that fixed frame A one side was kept away from to elasticity cloth A has magnetite A, the equal fixed mounting in four end angles that fixed frame B one side was kept away from to elasticity cloth B has magnetite B.
2. An anti-seismic flight box according to claim 1, wherein: the magnetic poles of the magnet A and the magnet B are opposite, the magnet A and the magnet B are the same in size, and the top end of the lower switch buckle is clamped into the inner part of the upper switch buckle.
3. An anti-seismic flight box according to claim 1, wherein: the box cover is connected with the box body through a hinge, and the hinge is located on one end face far away from the upper switch buckle and the lower switch buckle.
4. An anti-seismic flight box according to claim 1, wherein: the rectangular frame and the bottom plate are of an integrally formed structure, the outer edge of the rectangular frame is attached to the inner edge of the fixed frame A, and the height of the rectangular frame is half of the height of the fixed frame A.
5. An anti-seismic flight box according to claim 1, wherein: one end of the spring is fixedly installed at four end corners of the bottom plate, and the other end of the spring is fixedly installed at four end corners of one surface, close to the rectangular frame, of the elastic cloth A and four end corners of one surface, close to the bottom plate, of the elastic cloth B.
6. An anti-seismic flight box according to claim 1, wherein: the fixed block is fixedly arranged in the middle of the front end face formed by the box cover and the box body together, and the upper switch buckle and the lower switch buckle are vertically corresponding in position.
7. An anti-seismic flight box according to claim 1, wherein: the bottom plate is fixedly arranged on the bottom end surface of the storage bin and the top end surface of the inner wall of the box cover through bolts respectively.
CN202020998833.2U 2020-06-03 2020-06-03 Antidetonation flight case Expired - Fee Related CN212402108U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202020998833.2U CN212402108U (en) 2020-06-03 2020-06-03 Antidetonation flight case

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202020998833.2U CN212402108U (en) 2020-06-03 2020-06-03 Antidetonation flight case

Publications (1)

Publication Number Publication Date
CN212402108U true CN212402108U (en) 2021-01-26

Family

ID=74409695

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202020998833.2U Expired - Fee Related CN212402108U (en) 2020-06-03 2020-06-03 Antidetonation flight case

Country Status (1)

Country Link
CN (1) CN212402108U (en)

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GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20210126

Termination date: 20210603