CN210527418U - Container with locking structure of box door for air transportation - Google Patents
Container with locking structure of box door for air transportation Download PDFInfo
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- CN210527418U CN210527418U CN201921601952.3U CN201921601952U CN210527418U CN 210527418 U CN210527418 U CN 210527418U CN 201921601952 U CN201921601952 U CN 201921601952U CN 210527418 U CN210527418 U CN 210527418U
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- groove
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Abstract
The utility model relates to an air transportation technical field specifically is a container of compact structure of case door for air transportation, the power distribution box comprises a box body, one side of box is provided with the chamber door, the chamber door is two open structure, axis of rotation of the equal fixedly connected with in both sides of chamber door, two the equal fixedly connected with box in both ends of axis of rotation, the chamber door is including the A door and the B door of symmetry installation, the locked groove has been seted up to one side of A door, the inside fixedly connected with switch knob of locked groove. This container of compact structure of case door for air transportation, the inside of chamber door is passed through gear and fixed plate cooperation, has reached the purpose of being convenient for to fix, all is provided with the inserted bar through A door and B door and can fixes the chamber door secondary with the box cooperation for it is more firm after the box is closed, and locking structure all is located the box inside and the surface is smooth, and the degree of cut is higher when two boxes or a plurality of boxes are put side by side, and the mutual support is more stable, also can save space.
Description
Technical Field
The utility model relates to an air transportation technical field specifically is a container of case lock compact structure for air transportation.
Background
The air container transportation means that a suitable cargo is loaded in an air container, a circulation mode of transporting by adopting an airplane loading container is adopted, a special airplane appears, the transportation time and distance are shortened to the maximum extent, the air container is not influenced by the terrain conditions of rivers, mountains and the like, the air container can fly across the country and the ground, the air container is the fastest and convenient transportation mode for a shipper needing to transport cargo urgently, the container for air transportation is generally made of materials such as aluminum alloy or high-strength fiber (glass fiber reinforced plastics), heavy corner castings and corner posts are not needed due to the fact that the air container is not influenced by pressure of sea transportation or other loading and unloading operations, the air container is much lighter than an international standard container, the upper part of the air container is generally made into a dome structure, the air container can be consistent with the shape of the corresponding part of an airplane body, the volume of the airplane cargo hold is fully utilized, and the damage to the airplane due to collision or friction is avoided, however, in the transportation process of the currently used air container, the load borne by the door is mainly borne by the hinge and the two middle pin rods, and for a large-size container, the strength of the door with the structure is not enough to bear a large load, so that the door is easy to deform or even damage.
The container of a compact structure of air transportation case door disclosed in chinese utility model patent application publication specification CN2087201676201UU, this compact structure of air transportation case door's container, though, through the enhancement steel pipe that sets up "X" type structure, equally divide the load that the chamber door bore, make chamber door intensity increase, locking lever through inside cross connection for strengthen steel pipe during locking, the locking lever, each structure of chamber door limits each other, the locking of the chamber door of being convenient for, but some following problems still appear in the use of the compact structure of air transportation case door's container that uses at present:
1. according to the container with the box door locking structure for air transportation, the reinforcing pipes of the X-shaped structure are fixed outside the box doors and have the protrusiveness, so that a plurality of containers can be arranged side by side with large gaps, and the containers are easy to collide.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
Not enough to prior art, the utility model provides a container of compact structure of case door for air transportation sets up fixed connection through the inside of chamber door, has solved the problem that proposes among the above-mentioned background art.
(II) technical scheme
In order to achieve the above purpose, the utility model discloses a following technical scheme realizes: a container with a locking structure of a box door for air transportation comprises a container body, wherein one side of the container body is provided with the container door which is of a double-opening structure, two sides of the container door are fixedly connected with a rotating shaft, two ends of the two rotating shafts are fixedly connected with the container body, the container door comprises an A door and a B door which are symmetrically installed, one side of the A door is provided with a locking groove, the inside of the locking groove is fixedly connected with a switch knob, one side of the switch knob, which is close to the inside of the A door, is fixedly connected with a rotating column, the side of the rotating column is sleeved with a rotating shaft, one end of the rotating column, which is far away from the switch knob, is fixedly connected with a rotating gear, the side of the rotating gear is clamped with a fixing plate through a tooth socket which is matched, two corners of the A door, which is close to the B door, are both provided with first F grooves, and two corners of the door B close to the door A are provided with second F grooves, and the tail ends of the second F grooves are fixedly connected with second spring bolts matched with the tail ends of the second F grooves.
Optionally, two ends of the bottom of the box body are provided with inclined plates forcing the structure.
Optionally, one side of the box body close to the rotating shaft is fixedly connected with two baffles.
Optionally, one side of the switch knob, which is far away from the rotary column, is horizontal to the side of the door a, and the two rotating shafts, which are far away from the baffle, are horizontal to the side of the box body.
Optionally, the rotating shaft is fixedly connected to the inside of the a door.
Optionally, one side of the fixing plate penetrating through the door a is movably connected with a clamping groove which is formed in the side surface of the door B and matched with the side surface of the door B, and one end of the fixing plate penetrating through the door a is fixedly connected with a magnet.
Optionally, the first spring bolt penetrates through the top of the door a, the first spring bolt penetrates through a clamping groove which is formed in the side face of the movable connection box body at one end of the first spring bolt far away from the first F groove and is matched with the clamping groove formed in the side face of the movable connection box body at one end of the first spring bolt far away from the first F groove, the second spring bolt penetrates through the top of the door B, and the second spring bolt penetrates through a clamping groove which is formed in the side face of the movable connection box body at one end of the second spring.
(III) advantageous effects
The utility model provides a container of case door locking structure for air transportation possesses following beneficial effect:
1. this container of tight structure of case door lock for air transportation is provided with switch knob, column spinner, rotary gear and fixed plate cooperation through the inside of chamber door, has reached the fixed purpose of being convenient for, all is provided with first F groove, first inserted bar, second F groove and second inserted bar and box cooperation through A door and B door and can be fixed the chamber door secondary for it is more firm after the box is closed.
2. This container of compact structure of case door for air transportation keeps away from one side of column spinner and the side level of A door, two through switch knob the side of baffle and the side level of box are kept away from to the axis of rotation for the side of box is a plane, and the degree of cut is higher when two boxes or a plurality of boxes are put side by side, and mutual support is more stable, also can save space.
Drawings
Fig. 1 is a schematic plan view of the present invention;
FIG. 2 is a schematic view of the internal structure of the lock groove of the present invention;
fig. 3 is a schematic structural view of the door of the present invention.
In the figure: 1-box body, 2-box door, 201-A door, 202-B door, 3-rotating shaft, 4-locking groove, 5-switch knob, 6-rotating column, 7-rotating shaft, 8-rotating gear, 9-fixing plate, 10-first F groove, 11-first spring bolt, 12-second F groove, 13-second spring bolt, 14-baffle and 15-magnet.
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. 1-3, the present invention provides a technical solution: a container with a box door locking structure for air transportation comprises a container body 1, wherein a box door 2 is arranged on one side of the container body 1, the box door 2 is of a double-opening structure, two rotating shafts 3 are fixedly connected to two sides of the box door 2, the two ends of each rotating shaft 3 are fixedly connected with the container body 1, the box door 2 comprises an A door 201 and a B door 202 which are symmetrically installed, adaptive rubber pads can be arranged at the butt joint of the A door 201 and the B door 202 to enable the sealing effect to be better, a locking groove 4 is formed in one side of the A door 201, a switch knob 5 is fixedly connected inside the locking groove 4, a rotary column 6 is fixedly connected to one side, close to the inside of the A door 201, of the switch knob 5, a rotating shaft 7 is sleeved on the side surface of the rotary column 6, a rotating gear 8 is fixedly connected to one end, far away from the switch knob 5, of the rotating gear 8 is clamped with a fixing plate, a door 201 is close to B door 202's both corners department and has all seted up first F groove 10, two the equal fixedly connected with looks adaptation's of the tail end in first F groove 10F first spring bolt 11, B door 202 is close to A door 201's both corners department and has all seted up second F groove 12, two the equal fixedly connected with looks adaptation's of tail end in second F groove 12F second spring bolt 13.
As an optional technical solution of the utility model:
both ends of 1 bottom of box are provided with the swash plate of coercing the structure, and the swash plate structure can better laminate aircraft shape, utilizes the space in the aircraft.
As an optional technical solution of the utility model:
one side of the box body 1 close to the rotating shaft 3 is fixedly connected with a baffle plate 14, and the baffle plate 14 is provided with two baffle plates 14 which have the effect that the sealing is tighter when the box door is closed, and a rubber pad can be added on the baffle plates, so that the sealing is tighter.
As an optional technical solution of the utility model:
the switch knob 5 keeps away from one side of column spinner 6 and the side level of A door 201, two the baffle 14 was kept away from to axis of rotation 3 side and the side level of box 1 for the side of box 1 is a plane, and the degree of cut is higher when two boxes 1 or a plurality of boxes 1 were put side by side, and mutual support is more stable, also can save space.
As an optional technical solution of the utility model:
the rotating shaft 7 is fixedly connected to the inside of the a-door 201, and the rotating shaft 7 is used for facilitating the control of the switch knob 5, the rotating gear 8 and the fixing plate 9.
As an optional technical solution of the utility model:
the fixing plate 9 penetrates through a clamping groove which is formed in one side of the door A201 and is movably connected with the side face of the door B202 in an adaptive mode, the fixing plate 9 penetrates through one end of the door A201 and is fixedly connected with the magnet 15, the fixing plate 9 can be prevented from moving disorderly due to vibration through the magnet 15, and the magnetic force of the magnet 15 is light-grade suction force and does not influence control of the switch knob 5.
As an optional technical solution of the utility model:
two first spring bolt 11 runs through the top of A door 201, two the draw-in groove of the inside looks adaptation of seting up in the one end swing joint box 1 side that first F groove 10 was kept away from to first spring bolt 11, two second spring bolt 13 runs through the top of B door 202, two the draw-in groove of the inside looks adaptation of seting up in the one end swing joint box 1 side that second F groove 12 was kept away from to second spring bolt 13, and spring bolt makes the automatic internal rotation of bolt prevent to drop-through the spring is spacing.
When the user is using, will pack into the box with the goods of needs shipment earlier, then close the chamber door, close the chamber door through switch knob control fixed plate, then carry out the closure of second time through first inserted bar and second inserted bar and make the closure tighter.
In conclusion, this container of air transportation box door locking structure, during the use, be provided with switch knob 5, column spinner 6, rotary gear 8 and fixed plate 9 cooperation through the inside of chamber door 2, reached the fixed purpose of being convenient for, all be provided with first F groove 10, first inserted bar 13, second F groove 12 and second inserted bar 1202 through A door 201 and B door 202 and cooperate with box 1 and can fix chamber door 2 for the second time, make the box more firm after the closure, keep away from one side of column spinner 6 and the side level of A door 201 through switch knob 5, two the side level of baffle 14 and box 1 is kept away from to axis of rotation 3, make the side of box 1 be a plane, the degree of cut is higher when two boxes 1 or a plurality of boxes 1 are put side by side, and mutual support is more stable, also can save space.
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 container of air transportation case door locking structure which characterized in that: the door comprises a box body (1), a box door (2) is arranged on one side of the box body (1), the box door (2) is of a double-opening structure, a rotating shaft (3) is fixedly connected to the two sides of the box door (2), the two ends of the rotating shaft (3) are fixedly connected with the box body (1), the box door (2) comprises an A door (201) and a B door (202) which are symmetrically installed, a locking groove (4) is formed in one side of the A door (201), a switch knob (5) is fixedly connected to the inside of the locking groove (4), a rotary column (6) is fixedly connected to one side, close to the inside of the A door (201), of the switch knob (5), a rotating shaft (7) is sleeved on the side face of the rotary column (6), a rotary gear (8) is fixedly connected to one end, far away from the switch knob (5), of the rotary column (6), and a fixing plate (9) is clamped to the, a two angle departments that door (201) is close to B door (202) have all seted up first F groove (10), two first F groove (10) the equal fixedly connected with looks adaptation of tail end first spring bolt (11), B door (202) are close to two angle departments that door (201) was close to A and have all seted up second F groove (12), two the equal fixedly connected with looks adaptation of tail end second spring bolt (13) of second F groove (12) F.
2. The container with the locking structure of the air transportation box door as claimed in claim 1, wherein the two ends of the bottom of the box body (1) are provided with sloping plates of a stress structure.
3. A container with a door locking structure for an air transportation container as claimed in claim 1, wherein a baffle (14) is fixedly connected to one side of said container body (1) adjacent to said rotation shaft (3), and there are two baffles (14).
4. A container with a door locking structure for an air transportation box door as claimed in claim 1, wherein one side of the switch knob (5) away from the rotary column (6) is horizontal to the side of the a door (201), and the sides of the two rotary shafts (3) away from the baffle (14) are horizontal to the side of the box body (1).
5. A container of an air transportation door locking structure as claimed in claim 1, wherein said rotary shaft (7) is fixedly connected to the inside of the a-door (201).
6. The container with the door locking structure for the air transportation box door is characterized in that the fixing plate (9) penetrates through one side of the A door (201) and is movably connected with a clamping groove formed in the side surface of the B door (202) and matched with the clamping groove, and one end, penetrating through the A door (201), of the fixing plate (9) is fixedly connected with a magnet (15).
7. The container with the locking structure for the door of the air transportation box, according to claim 1, is characterized in that two first spring bolts (11) penetrate through the top of the A door (201), one ends of the two first spring bolts (11), which are far away from the first F groove (10), are movably connected with matched clamping grooves formed in the side surface of the box body (1), two second spring bolts (13) penetrate through the top of the B door (202), and one ends of the two second spring bolts (13), which are far away from the second F groove (12), are movably connected with matched clamping grooves formed in the side surface of the box body (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921601952.3U CN210527418U (en) | 2019-09-24 | 2019-09-24 | Container with locking structure of box door for air transportation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921601952.3U CN210527418U (en) | 2019-09-24 | 2019-09-24 | Container with locking structure of box door for air transportation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210527418U true CN210527418U (en) | 2020-05-15 |
Family
ID=70606606
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921601952.3U Expired - Fee Related CN210527418U (en) | 2019-09-24 | 2019-09-24 | Container with locking structure of box door for air transportation |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210527418U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2022148127A1 (en) * | 2021-01-06 | 2022-07-14 | 滨州学院 | Aircraft container applied to aircraft loading |
| CN118029843A (en) * | 2024-04-11 | 2024-05-14 | 福建中能电气有限公司 | Waterproof three doors of prefabricated cabin |
-
2019
- 2019-09-24 CN CN201921601952.3U patent/CN210527418U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2022148127A1 (en) * | 2021-01-06 | 2022-07-14 | 滨州学院 | Aircraft container applied to aircraft loading |
| GB2607520A (en) * | 2021-01-06 | 2022-12-07 | Univ Binzhou | Aircraft container applied to aircraft loading |
| CN118029843A (en) * | 2024-04-11 | 2024-05-14 | 福建中能电气有限公司 | Waterproof three doors of prefabricated cabin |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 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: 20200515 Termination date: 20200924 |