CN217999269U - Locking structure for preventing self-opening flying wing carriage - Google Patents
Locking structure for preventing self-opening flying wing carriage Download PDFInfo
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- CN217999269U CN217999269U CN202221533698.XU CN202221533698U CN217999269U CN 217999269 U CN217999269 U CN 217999269U CN 202221533698 U CN202221533698 U CN 202221533698U CN 217999269 U CN217999269 U CN 217999269U
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- opening
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Abstract
The utility model provides a prevent from locking structure in all-wing aircraft carriage of opening. A locking structure for preventing a self-opening all-wing vehicle cabin, comprising: mounting a plate; the two connecting plates are respectively and fixedly arranged on two sides of the bottom of the mounting plate; adjusting device rotates to be connected in one side of connecting plate, and adjusting device includes the carriage release lever, and the top of carriage release lever front side is provided with the axis of rotation, the bottom fixedly connected with fixed block of carriage release lever, the bottom fixedly connected with pull rod of fixed block, the spacing spring of top fixedly connected with of fixed block. The utility model provides a prevent from locking structure in all-wing aircraft carriage of opening, it is taut to drive stop device through rotating adjusting device for the limiting plate pastes tight carriage, this device simple structure, and the practicality is strong, the user only need rotate adjusting device can, spacing spring can restrict adjusting device, it is not hard up along with the difficult landing of jolting of vehicle in going.
Description
Technical Field
The utility model relates to a carriage field especially relates to a prevent from locking structure in all-wing aircraft carriage who opens.
Background
The flying wing vehicle is an improvement of a common van vehicle, can open special vehicles of wing plates on two sides of a carriage through a manual device or a hydraulic device, and is a very popular transport tool for modern logistics enterprises due to the advantages of high loading and unloading speed, high efficiency, side loading and unloading and the like.
The flying wing vehicle becomes the best choice of large-scale logistics company transportation, because in recent years, a large amount of light new materials are applied to wingspan vehicle series for carriage dead weight reduces, and the carriage design is pleasing to the eye, and freight transportation safe and reliable in addition, expected to possess a place in high-end logistics transportation market, van-type two wing vehicle principle is through the battery discharge through power pack promotion hydraulic system work reach the effect of lifting. The lifting height can exceed the carriage and approach a 90-degree angle.
At present, most of locking devices of two-wing side plates of all flying wing carriages in the market mostly adopt manual lock catches, the manual lock catches often have the problems of time and labor waste or insecure locking and the like when in use, and the lock catches are easy to loosen along with bumping of the vehicle when the vehicle runs and are unsafe.
Therefore, it is necessary to provide a locking structure of a flying wing car for preventing self-opening to solve the above technical problems.
SUMMERY OF THE UTILITY MODEL
The utility model provides a prevent from locking structure in all-wing aircraft carriage of opening, the locking device who has solved most all-wing aircraft carriage both wings curb plates on the market adopts manual hasp mostly, and manual hasp often has when using to waste time and energy or locks insecure scheduling problem, jolts the hasp along with the vehicle when the vehicle goes and is not hard up easily, unsafe problem.
In order to solve the technical problem, the utility model provides a pair of prevent from locking structure in all-wing aircraft carriage of opening, include: mounting a plate;
the two connecting plates are respectively and fixedly arranged on two sides of the bottom of the mounting plate;
the adjusting device is rotatably connected to one side of the connecting plate and comprises a moving rod, a rotating shaft is arranged at the top of the front side of the moving rod, a fixed block is fixedly connected to the bottom end of the moving rod, a pull rod is fixedly connected to the bottom end of the fixed block, and a limiting spring is fixedly connected to the top of the fixed block;
and the limiting device is arranged on one side of the adjusting device.
Preferably, the limiting device comprises a connecting ring, a steel cable is arranged on one side of the connecting ring, and a limiting plate is fixedly connected to one side of the steel cable.
Preferably, one side fixedly connected with fixed plate of mounting panel bottom, one side fixedly connected with connecting block of fixed plate bottom, the inside of connecting block is provided with limiting device, the opposite side fixed mounting of fixed plate bottom has the installation piece.
Preferably, the limiting device comprises a limiting block, one side of the outer surface of the limiting block is fixedly connected with a squeezing plate, and two sides of the squeezing plate are both provided with sliding holes.
Preferably, the inside of connecting block is provided with the installation cavity, the equal fixed mounting in both sides of installation cavity has the slide bar, the surface cover of slide bar is equipped with extrusion spring.
Preferably, the bottom of one side of the mounting block is provided with a limiting groove.
Compared with the prior art, the utility model provides a pair of prevent from locking structure in all-wing aircraft carriage of opening has following beneficial effect:
the utility model provides a prevent from locking structure in all-wing aircraft carriage of opening, it is taut to drive stop device through rotating adjusting device for the limiting plate pastes tight carriage, this device simple structure, and the practicality is strong, the user only need rotate adjusting device can, spacing spring can restrict adjusting device, it is not hard up along with the difficult landing of jolting of vehicle in going.
Drawings
Fig. 1 is a schematic structural diagram of a first embodiment of a locking structure of a flying wing car for preventing self-opening provided by the present invention;
FIG. 2 is a schematic view of the adjustment device shown in FIG. 1;
fig. 3 is a schematic structural diagram of a second embodiment of a locking structure of a flying wing car for preventing self-opening provided by the present invention;
FIG. 4 is a cross-sectional view of the connector block shown in FIG. 3;
fig. 5 is a schematic view of the restriction device shown in fig. 3.
Reference numbers in the figures: 1. mounting plate, 2, connecting plate, 3, adjusting device, 31, movable rod, 32, axis of rotation, 33, spacing spring, 34, fixed block, 35, pull rod, 4, stop device, 41, connecting ring, 42, cable wire, 43, limiting plate, 5, fixed plate, 6, connecting block, 7, limiting device, 71, limiting block, 72, stripper plate, 73, slide opening, 8, mounting cavity, 9, slide bar, 10, stripper spring, 11, mounting block, 12, limiting groove.
Detailed Description
The present invention will be further described with reference to the accompanying drawings and embodiments.
Please refer to fig. 1 and fig. 2 in combination, wherein fig. 1 is a schematic structural diagram of a first embodiment of a locking structure of a flying wing car for preventing self-opening according to the present invention; fig. 2 is a schematic structural diagram of the adjusting device shown in fig. 1. A locking structure for preventing a self-opening all-wing vehicle cabin comprises: a mounting plate 1;
the two connecting plates 2 are respectively and fixedly arranged on two sides of the bottom of the mounting plate 1;
the adjusting device 3 is rotatably connected to one side of the connecting plate 2, the adjusting device 3 comprises a moving rod 31, a rotating shaft 32 is arranged at the top of the front side of the moving rod 31, a fixed block 34 is fixedly connected to the bottom end of the moving rod 31, a pull rod 35 is fixedly connected to the bottom end of the fixed block 34, and a limiting spring 33 is fixedly connected to the top of the fixed block 34;
and the limiting device 4 is arranged on one side of the adjusting device 3.
The two connecting plates 2 are respectively fixed on the front side and the rear side of the bottom of the mounting plate 1, and the adjusting device 3 is connected between the two connecting plates 2 through a rotating shaft 32.
The limiting spring 33 is sleeved on the outer surface of the moving rod 31, and when the adjusting device 3 rotates to be parallel to the mounting plate 1, the limiting spring 33 keeps a leftward extrusion effect, so that the adjusting device 3 keeps parallel.
The limiting device 4 is arranged on the left side of the adjusting device 3.
Stop device 4 includes go-between 41, one side of go-between 41 is provided with cable wire 42, one side fixedly connected with limiting plate 43 of cable wire 42.
The connecting ring 41 is a U-shaped block, the two sides are rotatably connected with the front side and the rear side of the fixing block 34, the left side of the connecting ring 41 is connected with the steel cable 42, and the steel cable 42 penetrates through the frame hole, so that the limiting plate 43 is pressed on the surface of the carriage.
The general frame surface has set up the intercommunicating pore, and cable 42 passes the intercommunicating pore, and limiting plate 43 is pasting the carriage surface, and can not influence the carriage when limiting plate 43 is horizontal and is turned up, turns over ninety degrees back with limiting plate 43 for limiting plate 43 is pressing carriage and frame simultaneously, thereby restricts the carriage and opens.
The utility model provides a pair of prevent from locking structure in all-wing aircraft carriage who opens's theory of operation as follows:
in operation, the lever 35 is first grasped and pulled to the side away from the limit plate 43, the adjusting device 3 is rotated by the rotating shaft 32, and when the adjusting device 3 is moved to be parallel to the mounting plate 1, the limit device 4 is pulled to the side away from the limit plate 43, so that the limit plate 43 presses the carriage.
When the release is needed, the lever 35 is held and pulled downwards, so that the limiting device 4 moves towards the limiting plate 43, and the carriage is loosened.
Compared with the prior art, the utility model provides a pair of prevent from locking structure in wing carriage of opening has following beneficial effect:
the utility model provides a prevent from locking structure in all-wing aircraft carriage of opening drives stop device 4 through rotating adjusting device 3 taut for limiting plate 43 pastes tight carriage, this device simple structure, and the practicality is strong, the user only need rotate adjusting device 3 can, spacing spring 33 can restrict adjusting device 3, it is not hard up along with the difficult landing of jolting of vehicle in going.
Second embodiment
Referring to fig. 3, 4 and 5, a second embodiment of the present application provides another locking structure for preventing self-opening of an all-wing vehicle cabin based on a locking structure for preventing self-opening of an all-wing vehicle cabin provided by a first embodiment of the present application. The second embodiment is only a preferred mode of the first embodiment, and the implementation of the second embodiment does not affect the implementation of the first embodiment alone.
Specifically, the locking structure that a second embodiment of this application provided prevents from opening all-wing aircraft carriage's difference lies in, a locking structure that prevents from opening all-wing aircraft carriage, one side fixedly connected with fixed plate 5 of mounting panel 1 bottom, one side fixedly connected with connecting block 6 of fixed plate 5 bottom, the inside of connecting block 6 is provided with limiting device 7, the opposite side fixed mounting of fixed plate 5 bottom has installation piece 11.
The fixed plate 5 is arranged on the front side of the right side of the bottom of the mounting plate 1, and the mounting block 11 is arranged on the rear side of the right side of the bottom of the mounting plate 1.
The limiting device 7 comprises a limiting block 71, a pressing plate 72 is fixedly connected to one side of the outer surface of the limiting block 71, and sliding holes 73 are formed in two sides of the pressing plate 72.
The front and rear ends of the restricting block 71 extend out of the outer surfaces of the front and rear sides of the connecting block 6, respectively.
The inside of connecting block 6 is provided with installation cavity 8, the equal fixed mounting in both sides of installation cavity 8 has slide bar 9, the surface cover of slide bar 9 is equipped with extrusion spring 10.
The extrusion plate 72 is arranged in the installation cavity 8 and is sleeved on the outer surface of the sliding rod 9 through the sliding hole 73, the extrusion spring 10 is sleeved on the outer surface of the sliding rod 9, one end of the extrusion spring 10 is connected with the extrusion plate 72, the other end of the extrusion spring is connected with the inner wall of the installation cavity 8, and the extrusion spring 10 is extruded when the extrusion plate 72 moves.
The bottom of one side of the mounting block 11 is provided with a limiting groove 12.
The limiting groove 12 is matched with the limiting block 71.
The utility model provides a pair of prevent from locking structure in all-wing aircraft carriage who opens as follows:
when the device works, firstly, a user holds the limiting block 71 and pulls the limiting block 71 away from the connecting block 6, so that the limiting block 71 drives the extrusion plate 72 to move and extrude the extrusion spring 10, and the limiting block 71 is separated from the limiting groove 12.
The lever 35 is then pulled into the top between the connecting block 6 and the mounting block 11, and then the restricting block 71 is released, and the pressing spring 10 inserts the pressing plate 72 into the restricting groove 12, restricting the lever 35 to the top of the pressing plate 72.
When the lever needs to be turned, the restricting block 71 is pulled out.
Compared with the prior art, the utility model provides a pair of prevent from locking structure in all-wing aircraft carriage of opening has following beneficial effect:
the utility model provides a prevent from locking structure in all-wing aircraft carriage of opening, elasticity promotion limiting device 7 recovers through extrusion spring 10, and during embedding embedded groove 12 was entered in the embedding of limiting device 7, restricted pull rod 35 between connecting block 6 and installation piece 11, this device simple structure, the practicality is strong, has restricted adjusting device 3 for adjusting device 3 can not become flexible stop device 4 of landing, has strengthened the locking effect.
The above-mentioned only be the embodiment of the present invention, not consequently the restriction of the patent scope of the present invention, all utilize the equivalent structure or equivalent flow transform made of the content of the specification and the attached drawings, or directly or indirectly use in other relevant technical fields, all including in the same way the patent protection scope of the present invention.
Claims (6)
1. A locking structure for preventing a self-opening all-wing vehicle compartment, comprising: mounting a plate;
the two connecting plates are respectively and fixedly arranged on two sides of the bottom of the mounting plate;
the adjusting device is rotatably connected to one side of the connecting plate and comprises a moving rod, a rotating shaft is arranged at the top of the front side of the moving rod, a fixed block is fixedly connected to the bottom end of the moving rod, a pull rod is fixedly connected to the bottom end of the fixed block, and a limiting spring is fixedly connected to the top of the fixed block;
and the limiting device is arranged on one side of the adjusting device.
2. The locking structure of a flying wing car capable of preventing self-opening according to claim 1, wherein the limiting device comprises a connecting ring, a steel cable is arranged on one side of the connecting ring, and a limiting plate is fixedly connected to one side of the steel cable.
3. The locking structure of a flying wing car capable of preventing self-opening according to claim 1, wherein a fixing plate is fixedly connected to one side of the bottom of the mounting plate, a connecting block is fixedly connected to one side of the bottom of the fixing plate, a limiting device is arranged inside the connecting block, and a mounting block is fixedly mounted to the other side of the bottom of the fixing plate.
4. The locking structure of a flying wing vehicle cabin capable of preventing self-opening according to claim 3, wherein the limiting device comprises a limiting block, a pressing plate is fixedly connected to one side of the outer surface of the limiting block, and sliding holes are formed in two sides of the pressing plate.
5. The locking structure of a winged vehicle compartment capable of preventing self-opening as claimed in claim 3, wherein a mounting cavity is arranged inside the connecting block, sliding rods are fixedly mounted on both sides inside the mounting cavity, and an extrusion spring is sleeved on the outer surface of each sliding rod.
6. The locking structure of a flying wing vehicle cabin capable of preventing self-opening according to claim 3, wherein a limiting groove is formed at the bottom of one side of the mounting block.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221533698.XU CN217999269U (en) | 2022-06-17 | 2022-06-17 | Locking structure for preventing self-opening flying wing carriage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221533698.XU CN217999269U (en) | 2022-06-17 | 2022-06-17 | Locking structure for preventing self-opening flying wing carriage |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217999269U true CN217999269U (en) | 2022-12-09 |
Family
ID=84293839
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221533698.XU Active CN217999269U (en) | 2022-06-17 | 2022-06-17 | Locking structure for preventing self-opening flying wing carriage |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217999269U (en) |
-
2022
- 2022-06-17 CN CN202221533698.XU patent/CN217999269U/en active Active
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