CN212895263U - Jet type oil engine - Google Patents
Jet type oil engine Download PDFInfo
- Publication number
- CN212895263U CN212895263U CN202021331863.4U CN202021331863U CN212895263U CN 212895263 U CN212895263 U CN 212895263U CN 202021331863 U CN202021331863 U CN 202021331863U CN 212895263 U CN212895263 U CN 212895263U
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- China
- Prior art keywords
- oil
- pipe
- jet type
- type oil
- heat dissipation
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- 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
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- 230000008878 coupling Effects 0.000 claims abstract description 9
- 238000010168 coupling process Methods 0.000 claims abstract description 9
- 238000005859 coupling reaction Methods 0.000 claims abstract description 9
- 238000007789 sealing Methods 0.000 claims description 48
- 230000017525 heat dissipation Effects 0.000 claims description 34
- 239000000956 alloy Substances 0.000 claims description 6
- 229910000838 Al alloy Inorganic materials 0.000 claims description 3
- 229910000881 Cu alloy Inorganic materials 0.000 claims description 3
- 239000004033 plastic Substances 0.000 claims description 3
- 229920003023 plastic Polymers 0.000 claims description 3
- 230000000712 assembly Effects 0.000 claims 1
- 238000000429 assembly Methods 0.000 claims 1
- 239000003921 oil Substances 0.000 abstract description 93
- 238000002347 injection Methods 0.000 abstract description 15
- 239000007924 injection Substances 0.000 abstract description 15
- 239000010687 lubricating oil Substances 0.000 abstract description 6
- 239000002699 waste material Substances 0.000 abstract description 3
- 230000001771 impaired effect Effects 0.000 abstract 1
- 238000010586 diagram Methods 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 238000009940 knitting Methods 0.000 description 3
- 238000003912 environmental pollution Methods 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 239000007921 spray Substances 0.000 description 2
- 230000006978 adaptation Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 239000004753 textile Substances 0.000 description 1
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- Lubrication Of Internal Combustion Engines (AREA)
Abstract
The utility model relates to an injection type oil machine technical field discloses an injection type oil machine, advance oil pipe, rigid coupling on the mounting bracket and spout the oil pipe and set up at the inside oil inlet of advancing oil pipe including injection type oil machine organism, rigid coupling on injection type oil machine organism front surface, one side of advancing oil pipe is connected with seal assembly, and advance the inside of oil pipe and set up with the communicating thread groove of oil inlet, the both sides of injection type oil machine organism all are connected with radiator unit. The utility model discloses a seal assembly can carry out the shutoff to the oil inlet, and through the sealed mode of bilayer formula, the seepage phenomenon that can greatly reduced oil inlet department appears has avoided spilling of oil inlet department lubricating oil and the waste and the polluted environment scheduling problem that lead to, can dispel the heat fast to the inside of injection formula oil machine organism through radiator unit, prevents that the heat is difficult to the effluvium in the injection formula oil machine organism and the impaired problem of components and parts that lead to, has ensured its normal use.
Description
Technical Field
The utility model relates to an injection type oil engine technical field specifically is an injection type oil engine.
Background
When a circular knitting machine of textile machinery runs at a high speed, the needle cylinder knitting needle and the cam track generate friction and generate heat, so that the knitting needle and the cam track are easy to wear and even break, the quality of cloth is affected, and the whole needle cylinder is damaged.
However, in the use process of the existing jet type oil engine, the sealing of the oil inlet is not firm enough, so that the leakage of lubricating oil is easily caused, and meanwhile, the heat dissipation effect of the existing jet type oil engine is not ideal enough, so that the heat dissipation requirement is difficult to be completed in a short time. Accordingly, one skilled in the art provides a jet type oil engine to solve the problems set forth in the background art.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a jet type oil machine to solve the problem that proposes among the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme:
the utility model provides an injection formula oil machine, includes that injection formula oil machine organism, rigid coupling advance oil pipe, embedding on injection formula oil machine organism front surface and install the oil level scale mark on injection formula oil machine organism front surface, rigid coupling at the control panel, manometer and the backup pad of injection formula oil machine organism upper surface, rigid coupling mounting bracket, the spout oil pipe of rigid coupling on the backup pad front surface and set up at the inside oil inlet of advancing oil pipe on the mounting bracket, the one side of advancing oil pipe is connected with seal assembly, and advance the inside of oil pipe and set up with the communicating thread groove of oil inlet, the both sides of injection formula oil machine organism all are connected with radiator unit.
As a further aspect of the present invention: the sealing assembly comprises a threaded head, a sealing plate, a sealing ring and a support plate, wherein the top end of the threaded head is fixedly connected with the support plate, the sealing plate is fixedly sleeved outside the threaded head, the lower surface edge of the support plate is fixedly connected with the sealing ring, and the support plate is connected with the oil inlet pipe through a hanging rope.
As a further aspect of the present invention: the thread head is connected with the thread groove through threads, the sealing plate is located inside the oil inlet, and the sealing plate is matched with the oil inlet.
As a further aspect of the present invention: the sealing plate and the sealing ring are both of annular structures and are rubber components, and the diameter of the sealing plate is smaller than that of the sealing ring.
As a further aspect of the present invention: the thread head and the thread groove are both in a round table shape, and the thread head is a component made of plastic materials.
As a further aspect of the present invention: the heat dissipation assembly comprises a heat dissipation plate, a second heat pipe, a first heat pipe and heat dissipation holes, one end of the first heat pipe is inserted into the jet type oil engine body, the other end of the first heat pipe is fixedly connected with the second heat pipe in an annular mode, the heat dissipation plate is sleeved with the external fixing portion of the first heat pipe, and the heat dissipation holes are formed in four edges of the heat dissipation plate.
As a further aspect of the present invention: the first heat conduction pipe and the second heat conduction pipe are both of cylindrical structures, and the first heat conduction pipe and the second heat conduction pipe are both members made of copper alloy materials.
As a further aspect of the present invention: the heating panel is the cuboid structure, and the heating panel is the component of aluminum alloy material.
Compared with the prior art, the beneficial effects of the utility model are that:
1. the utility model can plug the oil inlet through the sealing component, and can greatly reduce the leakage phenomenon at the oil inlet through the double-layer sealing mode, thereby avoiding the problems of waste, environmental pollution and the like caused by the leakage of the lubricating oil at the oil inlet;
2. the inside of the jet type oil engine body can be rapidly cooled through the cooling assembly, the problem that components are damaged due to the fact that heat in the jet type oil engine body is difficult to diffuse is solved, and normal use of the jet type oil engine body is guaranteed.
Drawings
FIG. 1 is a schematic structural diagram of a jet type oil engine;
FIG. 2 is a schematic diagram of a seal assembly in a jet oil engine;
FIG. 3 is a schematic structural diagram of a heat dissipation assembly in a jet type oil engine;
fig. 4 is a schematic structural diagram of the first heat conducting pipe and the second heat conducting pipe in the jet type oil engine.
In the figure: 1. a mounting frame; 2. an oil spray pipe; 3. a support plate; 4. a pressure gauge; 5. a control panel; 6. a seal assembly; 7. a jet type oil engine body; 8. an oil inlet pipe; 9. oil level scale lines; 10. a heat dissipating component; 11. an oil inlet; 12. a thread groove; 13. a screw head; 14. a sealing plate; 15. a seal ring; 16. a backup plate; 17. a heat dissipation plate; 18. a second heat conductive pipe; 19. a first heat conductive pipe; 20. and (4) heat dissipation holes.
Detailed Description
Referring to fig. 1 to 4, in an embodiment of the present invention, an oil jet machine includes an oil jet machine body 7, an oil inlet pipe 8 fixedly connected to a front surface of the oil jet machine body 7, an oil level scale mark 9 embedded in the front surface of the oil jet machine body 7, a control panel 5 fixedly connected to the upper surface of the oil jet machine body 7, a pressure gauge 4 and a support plate 3, a mounting frame 1 fixedly connected to the front surface of the support plate 3, an oil spray pipe 2 fixedly connected to the mounting frame 1, and an oil inlet 11 provided inside the oil inlet pipe 8, one side of the oil inlet pipe 8 is connected to a sealing assembly 6, and a thread groove 12 communicated with the oil inlet 11 is provided inside the oil inlet pipe 8, the sealing assembly 6 includes a thread head 13, a sealing plate 14, a sealing ring 15 and a backup plate 16, the top end of the thread head 13 is fixedly connected to the backup plate 16, and the sealing plate 14 is fixedly, support the lower surface edge fixedly connected with sealing washer 15 of backup plate 16, support and link to each other through hanging the rope with advancing oil pipe 8 by the backup plate 16, thread head 13 and thread groove 12 pass through threaded connection, closing plate 14 is located the inside of oil inlet 11, and closing plate 14 and 11 looks adaptations of oil inlet, closing plate 14 and sealing washer 15 are the ring structure, and closing plate 14 and sealing washer 15 are the component of rubber material, closing plate 14's diameter is less than the diameter of sealing washer 15, thread head 13 and thread groove 12 are round platform form, thread head 13 is the component of plastics material, can carry out the shutoff to oil inlet 11 through seal assembly 6, and through the sealed mode of bilayer formula, the seepage phenomenon that can greatly reduced oil inlet 11 department appear, avoided spilling of oil inlet 11 department lubricating oil and the extravagant and polluted environment scheduling problem that lead to.
In fig. 1, 3 and 4: the two sides of the jet type oil engine body 7 are both connected with a heat dissipation assembly 10, the heat dissipation assembly 10 comprises a heat dissipation plate 17, a second heat conduction pipe 18, a first heat conduction pipe 19 and heat dissipation holes 20, one end of the first heat conduction pipe 19 is inserted into the jet type oil engine body 7, the other end of the first heat conduction pipe 19 is fixedly connected with the second heat conduction pipe 18 in an annular shape, the heat dissipation plate 17 is fixedly sleeved outside the first heat conduction pipe 19, the heat dissipation holes 20 are formed in four edges of the heat dissipation plate 17, the first heat conduction pipe 19 and the second heat conduction pipe 18 are both of a cylindrical structure, the first heat conduction pipe 19 and the second heat conduction pipe 18 are both made of copper alloy materials, the heat dissipation plate 17 is of a cuboid structure, the heat dissipation plate 17 is made of aluminum alloy materials, the heat dissipation assembly 10 can rapidly dissipate heat inside the jet type oil engine body 7, and the problem that components are damaged due, the normal use of the utility model is guaranteed.
The utility model discloses a theory of operation is: the user injects lubricating oil into the oil inlet 11 first, then aligns the thread head 13 with the thread groove 12 and screws in, at this time, along with the continuous rotation of the thread head 13, when the bottom of the sealing plate 14 is abutted against the oil inlet 11, so as to play a role of primarily sealing the oil inlet 11, meanwhile, along with the continuous screwing of the sealing plate 14, the sealing ring 15 at this time can also be attached to the top edge of the oil inlet pipe 8, so as to play a secondary sealing effect on the periphery of the oil inlet 11, because the sealing plate 14 and the sealing ring 15 are both members made of rubber materials, both have good sealing effects, so as to plug the oil inlet 11 through the sealing component 6, and through the double-layer sealing mode, the leakage phenomenon at the oil inlet 11 can be greatly reduced, and the problems of waste, environmental pollution and the like caused by the leakage of the lubricating oil at the oil inlet 11, when the jet type oil engine body 7 generates heat itself, at this time, the first heat pipe 19 can transmit the heat inside the jet type oil engine body 7 to the second heat pipe 18 and the heat dissipation plate 17 in a heat conduction manner, and then the heat is dissipated to the surroundings through the heat dissipation hole 20 on the heat dissipation plate 17 and the second heat pipe 18, so that the inside of the jet type oil engine body 7 can be quickly dissipated through the heat dissipation assembly 10, the problem that the heat inside the jet type oil engine body 7 is difficult to dissipate and the components are damaged is prevented, and the normal use of the jet type oil engine body is ensured.
The above-mentioned, 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 (8)
1. The utility model provides a jet type oil machine, including jet type oil machine organism (7), the rigid coupling advances oil pipe (8) on jet type oil machine organism (7) front surface, oil level scale mark (9) on jet type oil machine organism (7) front surface are installed in the embedding, control panel (5) of rigid coupling at jet type oil machine organism (7) upper surface, manometer (4) and backup pad (3), mounting bracket (1) of rigid coupling on backup pad (3) front surface, spout oil pipe (2) and set up in advancing the inside oil inlet (11) of oil pipe (8) on mounting bracket (1), its characterized in that: one side of the oil inlet pipe (8) is connected with a sealing assembly (6), a thread groove (12) communicated with the oil inlet (11) is formed in the oil inlet pipe (8), and two sides of the jet type oil engine body (7) are connected with heat dissipation assemblies (10).
2. The jet type oil engine according to claim 1, characterized in that the sealing assembly (6) comprises a threaded head (13), a sealing plate (14), a sealing ring (15) and a support plate (16), the support plate (16) is fixedly connected to the top end of the threaded head (13), the sealing plate (14) is fixedly sleeved on the outer portion of the threaded head (13), the sealing ring (15) is fixedly connected to the edge of the lower surface of the support plate (16), and the support plate (16) is connected with the oil inlet pipe (8) through a hanging rope.
3. The jet oil engine as claimed in claim 2, characterized in that the screw head (13) and the screw groove (12) are connected by screw threads, the sealing plate (14) is positioned inside the oil inlet (11), and the sealing plate (14) is matched with the oil inlet (11).
4. The jet oil engine as claimed in claim 2, characterized in that the sealing plate (14) and the sealing ring (15) are both circular ring structures, the sealing plate (14) and the sealing ring (15) are both rubber components, and the diameter of the sealing plate (14) is smaller than that of the sealing ring (15).
5. The jet type oil engine according to claim 2, characterized in that the thread head (13) and the thread groove (12) are both in a circular truncated cone shape, and the thread head (13) is a member made of plastic.
6. The jet type oil engine according to claim 1, wherein the heat dissipation assembly (10) comprises a heat dissipation plate (17), a second heat conduction pipe (18), a first heat conduction pipe (19) and heat dissipation holes (20), one end of the first heat conduction pipe (19) is inserted into the jet type oil engine body (7), the second heat conduction pipe (18) is fixedly connected to the other end of the first heat conduction pipe (19) in an annular shape, the heat dissipation plate (17) is fixedly sleeved outside the first heat conduction pipe (19), and the heat dissipation holes (20) are formed in four edges of the heat dissipation plate (17).
7. An oil jet engine according to claim 6, characterized in that the first heat conduction pipe (19) and the second heat conduction pipe (18) are both of a cylindrical structure, and the first heat conduction pipe (19) and the second heat conduction pipe (18) are both members made of copper alloy material.
8. The jet type oil engine according to claim 6, characterized in that the heat dissipation plate (17) is of a rectangular parallelepiped structure, and the heat dissipation plate (17) is a member made of an aluminum alloy material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021331863.4U CN212895263U (en) | 2020-07-09 | 2020-07-09 | Jet type oil engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021331863.4U CN212895263U (en) | 2020-07-09 | 2020-07-09 | Jet type oil engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212895263U true CN212895263U (en) | 2021-04-06 |
Family
ID=75285511
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021331863.4U Expired - Fee Related CN212895263U (en) | 2020-07-09 | 2020-07-09 | Jet type oil engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212895263U (en) |
-
2020
- 2020-07-09 CN CN202021331863.4U patent/CN212895263U/en not_active Expired - Fee Related
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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 |
Granted publication date: 20210406 |