CN214608141U - Oil pipeline mobile device is failed to aviation oil - Google Patents
Oil pipeline mobile device is failed to aviation oil Download PDFInfo
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- CN214608141U CN214608141U CN202023139057.XU CN202023139057U CN214608141U CN 214608141 U CN214608141 U CN 214608141U CN 202023139057 U CN202023139057 U CN 202023139057U CN 214608141 U CN214608141 U CN 214608141U
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Abstract
The application provides an aviation oil delivery pipe moving device, which comprises a support, a first support and a second support, wherein the support comprises a first cross rod and a second cross rod, the first cross rod and the second cross rod are connected with two vertical rods, the first cross rod is arranged at one end of the two vertical rods, and the second cross rod is arranged at the other end close to the two vertical rods; the moving assembly comprises two wheel assemblies and a connecting rod connected with the two wheel assemblies, and each wheel assembly is rotatably connected with one vertical rod. Place on the support through the body with defeated oil pipe, defeated oil pipe orificial one end sets up in the other end of montant, defeated oil pipe mouth of pipe and sealing device towards ground direction can block and establish between two montants and second horizontal poles, the staff of being convenient for carries out the operation, only need to separate defeated oil pipe mouth and oil depot mouth when needs remove, just can remove through removing the subassembly, rotate between wheel subassembly and the montant and be connected, the be convenient for accomodate of defeated oil pipe mobile device of aviation oil, also made things convenient for the staff to carry out oil transportation work for the oil depot mouth of the different degree of depth.
Description
Technical Field
The application relates to the technical field of airport oil transportation equipment, in particular to an aviation oil transportation pipe moving device.
Background
With the development of economy, more and more cities and regions own their own airports. When the aircraft in the airport is added with aviation oil, the aircraft is obtained from an oil depot arranged underground. When the underground oil depot is refueled, the aerial oil storage device on the ground is supplemented after being connected with the oil depot opening on the ground through an oil delivery pipe. The pressure of the aviation oil storage device is high when oil is discharged, and a sealing device is required to be arranged at the pipe orifice of the oil delivery pipe, so that the tight connection between the pipe orifice of the oil delivery pipe and the oil depot orifice can be ensured.
The inventor of this application discovers in long-term research and development, and the sealing device of setting is heavier for current defeated oil pipe's of aviation oil outlet one end, and the staff is difficult for removing the one end of defeated oil pipe oil-out when carrying out the operation, and the operation is inconvenient.
SUMMERY OF THE UTILITY MODEL
The application provides an defeated oil pipe mobile device of aviation oil to solve among the prior art staff and be difficult for the problem that removes the one end of defeated oil pipe oil-out when carrying out the operation.
In order to solve the technical problem, the application adopts a technical scheme that: there is provided an aviation oil pipeline moving device, wherein the device comprises:
the support comprises a first cross rod and a second cross rod which are connected with two vertical rods, the first cross rod is arranged at one end of the two vertical rods, and the second cross rod is arranged at the other end close to the two vertical rods;
the moving assembly comprises two wheel assemblies and connecting rods for connecting the two wheel assemblies, and each wheel assembly is rotatably connected with one vertical rod.
Optionally, each wheel assembly comprises a wheel, a wheel seat, a first support rod and a second support rod, two ends of the wheel seat are rotatably connected with one end of the wheel and one end of the first support rod, one end of the second support rod is rotatably connected with one vertical rod, and the other end of the second support rod is connected with the other end of the first support rod; two ends of the connecting rod are connected with the second supporting rods.
Optionally, each wheel assembly includes a shock absorber disposed between the wheel mount and the first strut.
Optionally, the support further comprises a support member, one end of the support member is connected to the first cross bar along a direction perpendicular to the ground, and the other end of the support member faces the ground.
Optionally, the other end of the supporting member is further provided with a wheel assembly.
Optionally, the support further comprises a third cross bar connecting the two vertical bars, and the third cross bar is located between the first cross bar and the second cross bar; two ends of the third cross rod penetrate through the two vertical rods, and one end of each second supporting rod is rotatably connected with one end of the third cross rod.
Optionally, the device further comprises a lifting assembly arranged on one side of one of the vertical rods, the lifting assembly comprises a jack, a wheel connecting rod and a lifting rod, one end of the jack is adjacent to the second supporting rod, the second supporting rod is located between the vertical rod and one end of the jack, and the wheel connecting rod is rotatably connected with one end of the jack and the second supporting rod; and two ends of the lifting rod are respectively connected with one vertical rod and the other end of the jack.
Optionally, the length of the vertical rod connected with the wheel connecting rod is greater than the length of the other vertical rod.
Optionally, the device further comprises a shielding assembly arranged at the other end of each of the two vertical rods, the shielding assembly comprises a limiting assembly and an extension plate which are connected with each other, the limiting assembly is connected with the two vertical rods, and the extension plate is arranged on one side of the limiting assembly, which deviates from the two vertical rods.
Optionally, the limiting assembly comprises a transverse limiting piece and two longitudinal limiting pieces, the two longitudinal limiting pieces are respectively arranged at two ends of the same side of the transverse limiting piece, each longitudinal limiting piece is connected with one end of the vertical rod, and the extension plate is arranged at one end of the transverse limiting piece, which deviates from two ends of the vertical rod.
The beneficial effect of this application is: the device comprises a support, a first transverse rod and a second transverse rod, wherein the first transverse rod and the second transverse rod are connected with two vertical rods; the moving assembly comprises two wheel assemblies and a connecting rod connected with the two wheel assemblies, and each wheel assembly is rotatably connected with one vertical rod. Place on the support through the body with defeated oil pipe, defeated oil pipe orificial one end sets up in the other end of montant, defeated oil pipe mouth of pipe and sealing device towards ground direction can the card establish between two montants and second horizontal poles, the staff of being convenient for carries out the operation, only need to separate defeated oil pipe mouth and oil depot mouth when needs remove, just can remove through removing the subassembly, rotate between wheel subassembly and the montant and be connected, be convenient for accomodate of defeated oil pipe mobile device of aviation oil, also made things convenient for the staff to carry out oil transportation work for the oil depot mouth of the different degree of depth, the problem of the staff one end of defeated oil pipe oil-out difficult removal when carrying out the operation among the prior art has been solved.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the application, the drawings that are needed to be used in the description of the embodiments are briefly introduced below, it is obvious that the drawings in the following description are only some embodiments of the application, and other drawings can be obtained by those skilled in the art without inventive efforts, wherein:
FIG. 1 is a schematic structural diagram of an embodiment of a device for moving an oil pipeline of an aviation;
FIG. 2 is a schematic view of the structure of an aviation oil pipeline;
FIG. 3 is a schematic structural diagram of another embodiment of the apparatus for moving an oil pipeline of the aircraft shown in FIG. 1;
FIG. 4 is a schematic structural view of yet another embodiment of the apparatus for moving an oil pipeline of the aircraft shown in FIG. 1;
fig. 5 is a schematic structural view of still another embodiment of the apparatus for moving an oil pipeline of an aircraft shown in fig. 1.
Detailed Description
The technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application, and it is obvious that the described embodiments are only a part of the embodiments of the present application, and not all of the embodiments. All other embodiments, which can be obtained by a person skilled in the art without making any inventive step based on the embodiments in the present application, are within the scope of protection of the present application.
It should be noted that if directional indications (such as up, down, left, right, front, and back … …) are referred to in the embodiments of the present application, the directional indications are only used to explain the relative positional relationship between the components, the movement situation, and the like in a specific posture (as shown in the drawings), and if the specific posture is changed, the directional indications are changed accordingly.
In addition, if there is a description of "first", "second", etc. in the embodiments of the present application, the description of "first", "second", etc. is for descriptive purposes only and is not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one such feature. In addition, technical solutions between various embodiments may be combined with each other, but must be realized by a person skilled in the art, and when the technical solutions are contradictory or cannot be realized, such a combination should not be considered to exist, and is not within the protection scope of the present application.
Referring to fig. 1 to 5, fig. 1 is a schematic structural diagram of an embodiment of an aviation oil delivery pipe moving device according to the present application, fig. 2 is a schematic structural diagram of an aviation oil delivery pipe, fig. 3 is a schematic structural diagram of another embodiment of the aviation oil delivery pipe moving device shown in fig. 1, fig. 4 is a schematic structural diagram of another embodiment of the aviation oil delivery pipe moving device shown in fig. 1, and fig. 5 is a schematic structural diagram of another embodiment of the aviation oil delivery pipe moving device shown in fig. 1. The displacement device 100 for the aviation oil pipeline 200 disclosed in the present embodiment includes a support 1 and a displacement assembly 3.
Particularly, the support 1 comprises a first cross rod 11 and a second cross rod 12 which are connected with two vertical rods 13, the first cross rod 11 is arranged at one end of the two vertical rods 13, and the second cross rod 12 is arranged at the other end close to the two vertical rods 13. Two montants 13 and two horizontal poles form a rectangular form frame promptly, and one end is for sealing, and the other end is equipped with an opening, and the design can alleviate the weight of support 1 self like this, is convenient for the staff to carry.
The pipe orifice 21 of the aviation oil delivery pipe 200 is approximately perpendicular to the pipe body 22, the sealing device 23 is arranged at one end of the pipe orifice 21, and correspondingly, the sealing device 23 is also approximately perpendicular to the pipe body 22, so that the operation of an underground oil depot opening is facilitated. The aviation oil delivery pipe 200 is erected on the support 1, and the closed end of the long-strip-shaped frame bears one end, far away from the pipe orifice 21, of the pipe body 22 of the aviation oil delivery pipe 200, so that the longer pipe body 22 is prevented from being abraded due to dragging, the material replacement and maintenance cost of the pipe body 22 is reduced, and the economic expenditure is reduced. The mouth of pipe 21 card of defeated tub of frame of aviation oil 200 is located the open end of rectangular form, and second horizontal pole 12 supports defeated tub of 200 mouths of pipe 21 of aviation oil, avoids the action that the staff kept lifting pipe mouth 21 position when the operation, reduces work step, and it is more simple and convenient to operate.
The moving assembly 3 comprises two wheel assemblies 31 and a connecting rod 32 connecting the two wheel assemblies 31, and each wheel assembly 31 is rotatably connected with one vertical rod 13. The moving assembly 3 can be rotatably connected with the bracket 1, so that a worker can conveniently move or operate the device 100 at various angles and directions by using the aviation oil delivery pipe 200.
In a specific embodiment, each wheel assembly 31 includes a wheel 311, a wheel seat 312, a first support 313 and a second support 314, wherein two ends of the wheel seat 312 are rotatably connected to the wheel 311 and one end of the first support 313, one end of the second support 314 is rotatably connected to one of the vertical rods 13, and the other end is connected to the other end of the first support 313. Two second struts 314 are connected to both ends of the connecting rod 32. The connecting rod 32 limits the relative position between the two wheel assemblies 31, so that the control of workers is facilitated.
In a particular embodiment, each wheel assembly 31 includes a shock absorbing member 315, and the shock absorbing member 315 is disposed between the wheel carrier 312 and the first strut 313. The shock absorbing member 315 can reduce the bumpiness of the wheel 311 during movement on the ground, and prevent the aviation oil pipeline 200 from falling off during movement.
In a specific embodiment, the stand 1 further comprises a support member 14, one end of the support member 14 is connected to the first cross bar 11 along a direction vertical to the ground, and the other end faces the ground. When the aviation oil delivery pipe 200 is in operation, the support 1 is supported on the ground by the support piece 14, so that the support effect can be achieved, the aviation oil delivery pipe 200 can be prevented from driving the moving device 100 to move, the sealing device 23 is prevented from being loosened, and the condition that oiling for an underground oil depot can be smoothly carried out is ensured.
In one embodiment, the other end of the support member 14 is also provided with a wheel assembly 31. The three wheel assemblies 31 are triangular in shape, and can maintain the stability of the mobile device 100.
In a particular embodiment, the stand 1 further comprises a third cross bar 15 connecting the two vertical bars 13, the third cross bar 15 being located between the first cross bar 11 and the second cross bar 12. Two ends of the third cross rod 15 penetrate through the two vertical rods 13, and one end of each second supporting rod 314 is rotatably connected with one end of the third cross rod 15.
In one embodiment, the apparatus 100 further comprises a lifting assembly 4 disposed on one side of one of the vertical rods 13, the lifting assembly 4 comprises a jack 41, a wheel connecting rod 42 and a lifting rod 43, one end of the jack 41 is disposed adjacent to the second strut 314, the second strut 314 is disposed between the vertical rod 13 and one end of the jack 41, and the wheel connecting rod 42 is rotatably connected to one end of the jack 41 and the second strut 314. The lifting rod 43 is connected at both ends to a vertical rod 13 and the other end of the jack 41. When the jack 41 of the hoisting component 4 works, the second supporting rod 314 is driven to lift by adjusting the angle of the hoisting rod 43, so that the vertical rod 13 is driven to tilt or fall, the support 1 and the vertical rod 13 move together, the tilting and falling of the opening end are realized, namely, the sealing device 23 and the pipe orifice 21 of the aviation oil delivery pipe 200 are lifted and fallen, the phenomenon that one end of the pipe orifice 21 of the aviation oil delivery pipe 200 needs to be manually held in a long time during operation is avoided, and the manpower is reduced.
In one embodiment, the length of the vertical rod 13 connecting the wheel connecting rods 42 is greater than the length of the other vertical rod 13.
In a specific embodiment, the device 100 further includes a shielding component 5 disposed at the other end of the two vertical rods 13, the shielding component 5 includes a limiting component 51 and an extension board 52 connected to each other, the limiting component 51 connects the two vertical rods 13, and the extension board 52 is disposed at one side of the limiting component 51 away from the two vertical rods 13. The position of the pipe orifice 21 of the aviation oil delivery pipe 200 can be limited by the limiting component 51 of the shielding component 5, the position is prevented from falling, the extension plate 52 can shield the sealing device 23 and the pipe orifice 21 of the aviation oil delivery pipe 200 in rainy and snowy days, a pulling piece is further arranged on the pipe orifice 21 of the aviation oil delivery pipe 200, and the pulling piece can be sleeved on the extension plate 52 to further fix the pipe orifice 21 of the aviation oil delivery pipe 200.
In one embodiment, the limiting component 51 includes a horizontal limiting piece and two vertical limiting pieces, the two vertical limiting pieces are respectively disposed at two ends of the same side of the horizontal limiting piece, each vertical limiting piece is connected to the other end of one of the vertical rods 13, and the extension board 52 is disposed at one end of the horizontal limiting piece away from the two vertical rods 13.
The application provides an defeated oil pipe mobile device of aviation oil, the device include the support, including first horizontal pole and the second horizontal pole of connecting two montants, first horizontal pole sets up in the one end of two montants, and the second horizontal pole sets up in the other end that is close to two montants. The moving assembly comprises two wheel assemblies and a connecting rod connected with the two wheel assemblies, and each wheel assembly is rotatably connected with one vertical rod. Place on the support through the body with defeated oil pipe, defeated oil pipe orificial one end sets up in the other end of montant, defeated oil pipe mouth of pipe and sealing device towards ground direction can block and establish between two montants and second horizontal poles, the staff of being convenient for carries out the operation, only need to separate defeated oil pipe mouth and oil depot mouth when needs remove, just can remove through removing the subassembly, rotate between wheel subassembly and the montant and be connected, the defeated oil pipe mobile device's of aviation oil of being convenient for accomodate, also made things convenient for the staff to carry out oil transportation work for the oil depot mouth of the different degree of depth, can make the staff remove the one end of defeated oil pipe oil-out easily when carrying out the operation.
The above embodiments are merely examples and are not intended to limit the scope of the present disclosure, and all modifications, equivalents, and flow charts using the contents of the specification and drawings of the present disclosure or those directly or indirectly applied to other related technical fields are intended to be included in the scope of the present disclosure.
Claims (10)
1. An aviation oil pipeline moving device, which is characterized in that the device comprises:
the support comprises a first cross rod and a second cross rod which are connected with two vertical rods, the first cross rod is arranged at one end of the two vertical rods, and the second cross rod is arranged at the other end close to the two vertical rods;
the moving assembly comprises two wheel assemblies and connecting rods for connecting the two wheel assemblies, and each wheel assembly is rotatably connected with one vertical rod.
2. The device of claim 1, wherein each wheel assembly comprises a wheel, a wheel seat, a first strut and a second strut, wherein two ends of the wheel seat are rotatably connected with one end of the wheel and the first strut, one end of the second strut is rotatably connected with one vertical rod, and the other end of the second strut is connected with the other end of the first strut; two ends of the connecting rod are connected with the second supporting rods.
3. The apparatus of claim 2, wherein each wheel assembly includes a shock absorber disposed between the wheel mount and the first strut.
4. The apparatus of claim 2, wherein the stand further comprises a support member having one end connected to the first cross bar in a direction perpendicular to the ground and the other end facing the ground.
5. The apparatus of claim 4, wherein the other end of the support member is further provided with a wheel assembly.
6. The device of claim 2, wherein the stand further comprises a third cross bar connecting the two vertical bars, the third cross bar being located between the first cross bar and the second cross bar; two ends of the third cross rod penetrate through the two vertical rods, and one end of each second supporting rod is rotatably connected with one end of the third cross rod.
7. The apparatus of claim 2, further comprising a lifting assembly disposed on one side of one of the vertical rods, the lifting assembly including a jack, a wheel connecting rod and a lifting rod, one end of the jack being disposed adjacent to the second strut, the second strut being disposed between the vertical rod and one end of the jack, the wheel connecting rod being rotatably connected to one end of the jack and the second strut; and two ends of the lifting rod are respectively connected with one vertical rod and the other end of the jack.
8. The apparatus of claim 7, wherein the vertical rod connecting the wheel connecting rods is longer than the other vertical rod.
9. The device of claim 1, further comprising a shielding component disposed at the other end of the two vertical rods, wherein the shielding component comprises a limiting component and an extension plate, the limiting component and the extension plate are connected with each other, the limiting component connects the two vertical rods, and the extension plate is disposed at a side of the limiting component, which faces away from the two vertical rods.
10. The device of claim 9, wherein the limiting component comprises a transverse limiting piece and two longitudinal limiting pieces, the two longitudinal limiting pieces are respectively arranged at two ends of the transverse limiting piece on the same side, each longitudinal limiting piece is connected with the other end of one vertical rod, and the extension plate is arranged at one end of the transverse limiting piece away from the two vertical rods.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023139057.XU CN214608141U (en) | 2020-12-23 | 2020-12-23 | Oil pipeline mobile device is failed to aviation oil |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023139057.XU CN214608141U (en) | 2020-12-23 | 2020-12-23 | Oil pipeline mobile device is failed to aviation oil |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214608141U true CN214608141U (en) | 2021-11-05 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202023139057.XU Active CN214608141U (en) | 2020-12-23 | 2020-12-23 | Oil pipeline mobile device is failed to aviation oil |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214608141U (en) |
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2020
- 2020-12-23 CN CN202023139057.XU patent/CN214608141U/en active Active
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Effective date of registration: 20230718 Address after: 100000 No. 28, Tianzhu Road, Zone A, Tianzhu Airport Industrial Zone, Shunyi District, Beijing Patentee after: China Aviation Oil Group Co.,Ltd. Patentee after: Shenzhen Chengyuan Aviation Oil Co.,Ltd. Address before: 518000 Shenzhen airport, Fuyong Town, Bao'an District, Shenzhen City, Guangdong Province Patentee before: Shenzhen Chengyuan Aviation Oil Co.,Ltd. |