CN116608350B - Marine system pipeline with vibration reduction structure - Google Patents
Marine system pipeline with vibration reduction structure Download PDFInfo
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- CN116608350B CN116608350B CN202310868075.0A CN202310868075A CN116608350B CN 116608350 B CN116608350 B CN 116608350B CN 202310868075 A CN202310868075 A CN 202310868075A CN 116608350 B CN116608350 B CN 116608350B
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- pipeline
- pneumatic flow
- flow pipeline
- plate
- inner pneumatic
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- 230000006835 compression Effects 0.000 claims abstract description 3
- 238000007906 compression Methods 0.000 claims abstract description 3
- 239000000428 dust Substances 0.000 claims description 33
- 239000012535 impurity Substances 0.000 claims description 24
- 239000000853 adhesive Substances 0.000 claims description 12
- 230000001070 adhesive effect Effects 0.000 claims description 12
- 238000013016 damping Methods 0.000 claims description 12
- 230000007246 mechanism Effects 0.000 claims description 12
- 239000013618 particulate matter Substances 0.000 claims description 11
- 239000002245 particle Substances 0.000 claims description 8
- 238000000034 method Methods 0.000 claims description 5
- 238000012216 screening Methods 0.000 claims description 5
- 230000003139 buffering effect Effects 0.000 claims description 4
- 239000000463 material Substances 0.000 abstract description 43
- 238000005299 abrasion Methods 0.000 abstract description 6
- 239000011797 cavity material Substances 0.000 description 19
- 239000000843 powder Substances 0.000 description 14
- 239000007789 gas Substances 0.000 description 12
- 230000010355 oscillation Effects 0.000 description 5
- 239000008187 granular material Substances 0.000 description 4
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 4
- 230000003670 easy-to-clean Effects 0.000 description 3
- 238000012544 monitoring process Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 230000003116 impacting effect Effects 0.000 description 2
- 238000010030 laminating Methods 0.000 description 2
- 239000003345 natural gas Substances 0.000 description 2
- 239000000758 substrate Substances 0.000 description 2
- 230000001360 synchronised effect Effects 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- TZCXTZWJZNENPQ-UHFFFAOYSA-L barium sulfate Chemical compound [Ba+2].[O-]S([O-])(=O)=O TZCXTZWJZNENPQ-UHFFFAOYSA-L 0.000 description 1
- 229910052601 baryte Inorganic materials 0.000 description 1
- 239000010428 baryte Substances 0.000 description 1
- 230000001680 brushing effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000003208 petroleum Substances 0.000 description 1
- 230000003313 weakening effect Effects 0.000 description 1
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L43/00—Bends; Siphons
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L55/00—Devices or appurtenances for use in, or in connection with, pipes or pipe systems
- F16L55/24—Preventing accumulation of dirt or other matter in the pipes, e.g. by traps, by strainers
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L57/00—Protection of pipes or objects of similar shape against external or internal damage or wear
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L57/00—Protection of pipes or objects of similar shape against external or internal damage or wear
- F16L57/06—Protection of pipes or objects of similar shape against external or internal damage or wear against wear
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Joints Allowing Movement (AREA)
Abstract
The invention discloses a marine system pipeline with a vibration reduction structure, and relates to the field of marine pipelines. According to the invention, the air flow drives the material to flow from the first pipeline, the inner pneumatic flow pipeline and the second pipeline in sequence, the elastic connecting structure has certain elasticity, and when the air flow drives the material to enter the inner pneumatic flow pipeline, the air flow drives the material to push the splice plate compression spring of the inner pneumatic flow pipeline, so that the buffer purpose is realized, the impact force of the air flow and the material on the inner pneumatic flow pipeline is reduced, the vibration of the whole pipeline is reduced, and the abrasion problem of the inner pneumatic flow pipeline is reduced.
Description
Technical Field
The invention relates to the field of marine system pipeline devices, in particular to a marine system pipeline with a vibration reduction structure.
Background
The marine system pipeline comprises a submarine oil and gas gathering and transportation pipeline, a trunk pipeline, an auxiliary pressurizing platform, a main pipe connected with the pipeline and the platform, and the like. The system has the function of collecting oil or natural gas extracted from offshore oil and gas fields, and conveying the oil or natural gas to a single-point mooring of a moored oil ship or to an onshore oil and gas depot. The conveying process of the marine oil and gas pipeline is the same as that of the land pipeline. The marine pipeline engineering is carried out in the sea area, the engineering construction method is different from the land pipeline engineering, along with the development of the marine petroleum industry, the requirements of marine engineering on powder materials such as barite are gradually increased, for the granular materials or powder materials flowing in the airtight marine pipeline along the air flow direction, as the air flow speed is higher in the pipeline, the impact can be caused on the inner wall of the pipeline when the air flow passes through the corner of the pipeline, especially when the air flow drives the granular materials or powder materials to impact the inner wall of the pipeline, the pipeline is caused to vibrate, the inner wall of the pipeline is severely worn, and the corner of the pipeline is most prone to grinding leakage. Therefore, it is necessary to provide a marine pipeline with a vibration damping structure to solve the above problems.
Disclosure of Invention
The invention aims to provide a marine system pipeline with a vibration reduction structure, which solves the problems that the pipeline inner wall is impacted when the airflow passes through the corner of the pipeline due to the high flowing speed of the airflow in the pipeline, particularly the pipeline is vibrated when the airflow drives granular materials or powder to impact the pipeline inner wall, the pipeline inner wall is severely worn, and the pipeline corner is most easily ground and leaked.
In order to achieve the above purpose, the present invention provides the following technical solutions: the marine system pipeline with the vibration reduction structure comprises an outer pneumatic flow pipeline and an inner pneumatic flow pipeline, wherein the inner pneumatic flow pipeline is bent, the outer pneumatic flow pipeline is sleeved outside the inner pneumatic flow pipeline, the outer pneumatic flow pipeline is used as the external protection of the inner pneumatic flow pipeline, the inner pneumatic flow pipeline is communicated between a first pipeline and a second pipeline, the air flow drives materials to flow from the first pipeline, the inner pneumatic flow pipeline and the second pipeline in sequence, a spring is fixedly welded at the outer ring of the inner pneumatic flow pipeline, one end of the spring far away from the outer ring of the inner pneumatic flow pipeline is movably attached to the inner wall of the outer pneumatic flow pipeline, the inner pneumatic flow pipeline comprises at least four inner pneumatic flow pipeline splice plates and an elastic connection structure, the inner pneumatic flow pipeline splice plates are spliced to form a pipeline shape, the elastic connection structure is also provided with a plurality of inner pneumatic flow pipeline splice plates in a one-to-one correspondence mode, the elastic connection structure is connected between the two adjacent inner pneumatic flow pipeline splice plates, the elastic connection structure has a certain elasticity, and when the air flow drives the materials to enter the inner pneumatic flow pipeline to push the inner pneumatic flow pipeline, the air flow pipeline to drive the inner pneumatic flow pipeline to compress the inner pneumatic flow pipeline, so that the problem of the air flow pipeline is reduced, and the impact force of the air flow pipeline is reduced, and the air flow is reduced, and the problem of the air flow is caused by the impact is caused by the air flow and the impact force is reduced, and the impact force of the inner pipeline is caused by the flow and the flow pipeline; because the pressure of the air current when driving the material through interior air force flow pipeline is not invariable, consequently, interior air force flow pipeline splice plate receives the impact force of air current and material also unstable for the spring has compressed and two kinds of states of resilience, thereby makes interior air force flow pipeline splice plate incessantly take place to vibrate, utilizes the vibration of interior air force flow pipeline splice plate to offset the impact force of air current and material, thereby reduces the holistic vibration of pipeline, and also has the weakening effect to the force of air current and material impact interior air force flow pipeline when interior air force flow pipeline splice plate self vibrates.
Preferably, the elastic connection structure comprises first rubber strips, the first rubber strips are arranged in pairs, a pair of first rubber strips are respectively and fixedly arranged on two side surfaces of each inner pneumatic flow pipeline splice plate, which are close to the inner pneumatic flow pipeline splice plates on two sides of the inner pneumatic flow pipeline splice plates, the first rubber strips on one side, which are close to each other, of each adjacent two inner pneumatic flow pipeline splice plates are movably attached, when materials driven by air flow are particles, a spring with proper elasticity is used, so that the maximum thrust generated by the air flow with the animal material flow can only push the spring to compress to a certain extent, and the width of a gap formed when the two adjacent first rubber strips are far away from each other is smaller than the minimum diameter of the particles, thereby avoiding the particles from entering the gap between the inner ring of the outer pneumatic flow pipeline and the outer ring of the inner pneumatic flow pipeline from the gap between the two first rubber strips; based on the intermittent opening and closing of the two first rubber strips, impurities or dust doped in the particles can enter between the inner ring of the outer pneumatic flow pipeline and the outer ring of the inner pneumatic flow pipeline through gaps, so that the purpose of dust removal and screening of the particles in the flow process is achieved.
Preferably, the elastic connection structure comprises a second rubber strip, the second rubber strip is fixedly arranged on one surfaces of the two inner pneumatic flow pipeline splice plates, which are close to each other, when the material flowing by the air flow is powder, the elastic connection structure is arranged as the second rubber strip, when the inner pneumatic flow pipeline splice plates compress the spring, gaps are not formed between the adjacent two inner pneumatic flow pipeline splice plates, so that the purposes of preventing powder leakage and realizing force unloading buffer on the air flow and the powder impact inner pneumatic flow pipeline are achieved, and the abrasion of the inner pneumatic flow pipeline is reduced.
Preferably, the inner wall of the outer pneumatic flow pipeline is fixedly provided with the bonding plate through the screw, the inner wall of the bonding plate is provided with the brush hair, dust entering between the inner ring of the outer pneumatic flow pipeline and the outer ring of the inner pneumatic flow pipeline is easy to adhere to the bonding plate, and impurities are easy to wind on the brush hair, so that the phenomenon that the dust or impurities entering between the inner ring of the outer pneumatic flow pipeline and the outer ring of the inner pneumatic flow pipeline flow back into the inner pneumatic flow pipeline again through a gap is avoided.
Preferably, the outer ring of the inner pneumatic flow pipeline splice plate is fixedly provided with a guide plate, the guide plate is of an arc-shaped plate structure, the guide plate is shielded outside the two first rubber strips which are mutually attached, dust or impurities which enter the space between the inner ring of the outer pneumatic flow pipeline and the outer ring of the inner pneumatic flow pipeline are considered to be not adhered to the adhesive plate or are still likely to flow back into the inner pneumatic flow pipeline through a gap between the two first rubber strips before being wound on bristles, and therefore, the guide plate is provided with a guide plate, and the guide plate has a flow guiding function, and can move along the outer surface of the guide plate after entering the space between the inner ring of the outer pneumatic flow pipeline and the outer ring of the inner pneumatic flow pipeline, so that the dust or impurities are unlikely to enter the gap.
Preferably, the outer pneumatic flow pipeline comprises two pipeline shells with semi-annular radial sections, end fixing plates are fixedly welded on one surfaces of the two pipeline shells, which are close to each other, end fixing rings are fixedly welded on two ends of the two pipeline shells, which are close to the first pipeline and the second pipeline, through screw fixing, the end fixing rings are fixedly connected on corresponding outer rings of the first pipeline and the second pipeline, and dust or impurities between an inner ring of the outer pneumatic flow pipeline and an outer ring of the inner pneumatic flow pipeline are easy to clean regularly based on the detachable arrangement of the outer pneumatic flow pipeline.
Preferably, an annular air cavity is formed between the outer ring of the inner pneumatic flow pipeline and the inner ring of the outer pneumatic flow pipeline, a pressure sensor for monitoring the air pressure in the annular air cavity is fixedly arranged on the inner wall of the outer pneumatic flow pipeline, a pressurizing pump is arranged outside the outer pneumatic flow pipeline, a pressurizing pipeline is arranged on the pressurizing pump, an air pipe is fixedly arranged on one end face of the outer pneumatic flow pipeline, one end of the air pipe is communicated with the annular air cavity, the other end of the air pipe is communicated with the pressurizing pipeline, and the pressurizing pump can sequentially charge the air pressure into the annular air cavity through the pressurizing pipeline and the air pipe when started, so that the air pressure value in the annular air cavity is adjusted, and when the impact force of materials flowing in the inner pneumatic flow pipeline is large, the springs are easy to be excessively compressed, and at the moment, the air pressurizing is charged into the annular air cavity, so that the vibration phenomenon of an splice plate of the inner pneumatic flow pipeline can be reduced, and the splice plate springs are avoided.
Preferably, the two ends of the inner pneumatic flow pipeline splice plate are respectively provided with a locking mechanism, the locking mechanism comprises a locking ring and a locking plate, the two locking rings are respectively movably sleeved at the outer ring of the first pipeline and the outer ring of the second pipeline, the locking plate is fixedly arranged at one surface of the locking ring close to the inner pneumatic flow pipeline splice plate, and a plurality of locking plates are arranged at equal angles along the axis of the locking ring.
Preferably, the locking mechanical system cooperation power unit uses, power unit includes electric putter, adapter sleeve, first base plate and second base plate, power unit is provided with two sets of, and two first base plates are fixed connection respectively in the outer lane department of first pipeline and second pipeline, and two second base plates are fixed welding respectively in the outer lane department of two locking rings, and the one side that corresponds second base plate and first base plate are close to each other is fixed and is provided with the adapter sleeve, electric putter's both ends are all installed between two corresponding adapter sleeves through the screw fixed, promote the second base plate and remove when electric putter starts, because second base plate fixed connection is in the outer lane department of locking ring, locking ring synchronous motion when the second base plate removes to make the locking plate laminating on the locking ring in the outer lane department of interior air flow pipeline splice plate.
Preferably, rubber sections are fixedly arranged at two ends, close to the first pipeline and the second pipeline, of the inner pneumatic flow pipeline splice plate, the rubber sections are conventional common pipe sections capable of being elastically deformed, details are omitted, the rubber sections can be elastically deformed to adapt to vibration of the inner pneumatic flow pipeline splice plate, and tightness of joints between the two ends of the inner pneumatic flow pipeline splice plate and the first pipeline and between the two ends of the inner pneumatic flow pipeline splice plate and the second pipeline is guaranteed.
The invention has the technical effects and advantages that:
1. according to the marine system pipeline with the vibration reduction structure, the airflow drives the material to flow from the first pipeline, the inner pneumatic flow pipeline and the second pipeline in sequence, the elastic connection structure has certain elasticity, and when the airflow drives the material to enter the inner pneumatic flow pipeline, the airflow drives the material to push the inner pneumatic flow pipeline splice plate to compress the spring, so that the purpose of buffering is achieved, the impact force of the airflow and the material on the inner pneumatic flow pipeline is reduced, the vibration of the whole pipeline is reduced, and the abrasion problem of the inner pneumatic flow pipeline is reduced;
2. according to the marine system pipeline with the vibration reduction structure, the pressure of the air flow driving the material to pass through the inner pneumatic flow pipeline is not constant, so that the impact force of the air flow and the material on the inner pneumatic flow pipeline splice plate is unstable, the springs are in two states of compression and rebound, the inner pneumatic flow pipeline splice plate continuously oscillates, the impact force of the air flow and the material is counteracted by the oscillation of the inner pneumatic flow pipeline splice plate, the integral oscillation of the pipeline is reduced, and the force of the air flow and the material impacting the inner pneumatic flow pipeline is weakened when the inner pneumatic flow pipeline splice plate oscillates;
3. when the material driven by the air flow is particulate matters, the marine system pipeline with the vibration reduction structure uses the spring with proper elasticity, so that the maximum thrust generated by the air flow with the material flow can only push the spring to compress to a certain extent, the width of a gap formed when two adjacent first rubber strips are mutually far away is smaller than the minimum diameter of the particulate matters, and the particulate matters are prevented from entering the gap between the two first rubber strips and leaking between the inner ring of the outer pneumatic flow pipeline and the outer ring of the inner pneumatic flow pipeline; based on intermittent opening and closing between the two first rubber strips, impurities or dust doped in the particles can enter between the inner ring of the outer pneumatic flow pipeline and the outer ring of the inner pneumatic flow pipeline through gaps, so that the purpose of dust removal and screening of the particles in the flowing process is realized;
4. according to the marine system pipeline with the vibration reduction structure, the adhesive plate is fixedly arranged on the inner wall of the outer pneumatic flow pipeline through the bolts, the bristles are arranged on the inner wall of the adhesive plate, dust entering between the inner ring of the outer pneumatic flow pipeline and the outer ring of the inner pneumatic flow pipeline is easy to adhere to the adhesive plate, and impurities are easy to wind on the bristles, so that the phenomenon that the dust or impurities entering between the inner ring of the outer pneumatic flow pipeline and the outer ring of the inner pneumatic flow pipeline flow back into the inner pneumatic flow pipeline again through gaps is avoided;
5. according to the marine system pipeline with the vibration reduction structure, the guide plates are fixedly arranged at the outer ring of the inner pneumatic flow pipeline splice plate and are of arc-shaped plate structures, the guide plates are shielded outside the two mutually-attached first rubber strips, the guide plates have a flow guiding effect, and when dust or impurities enter between the inner ring of the outer pneumatic flow pipeline and the outer ring of the inner pneumatic flow pipeline, the dust or impurities move along the outer surface of the guide plates and are not easy to enter into gaps;
6. the marine system pipeline with the vibration reduction structure is easy to clean dust or impurities entering between the inner ring of the outer pneumatic flow pipeline and the outer ring of the inner pneumatic flow pipeline periodically based on the detachable arrangement of the outer pneumatic flow pipeline;
7. according to the marine system pipeline with the vibration reduction structure, when the locking ring moves along the first pipeline or the second pipeline, the locking plate is attached to the outer ring of the inner pneumatic flow pipeline splice plate, the inner pneumatic flow pipeline splice plates are temporarily locked, so that the adjacent two inner pneumatic flow pipeline splice plates are attached to each other, then the outer pneumatic flow pipeline is detached to clean dust or impurities in the annular cavity, dust or impurities can be cleaned under the condition of no shutdown, and the marine system pipeline with the vibration reduction structure is high in practicability;
8. according to the marine system pipeline with the vibration reduction structure, when the material flowing through the air flow is powder, the elastic connection structure is set to be the second rubber strip, and the second rubber strip is fixedly arranged on the surface, close to each other, of the two inner pneumatic flow pipeline splice plates, so that when the inner pneumatic flow pipeline splice plates compress a spring, gaps are not formed between the adjacent two inner pneumatic flow pipeline splice plates, the purposes of preventing powder leakage, and realizing unloading buffer on the air flow and the powder impact on the inner pneumatic flow pipeline are achieved, and abrasion of the inner pneumatic flow pipeline is reduced;
9. according to the marine system pipeline with the vibration reduction structure, when the second rubber strip is arranged between two adjacent inner pneumatic flow pipeline splice plates, the pressure sensor for monitoring the gas pressure in the annular air cavity is fixedly arranged on the inner wall of the outer pneumatic flow pipeline, the pressurizing pump is arranged outside the outer pneumatic flow pipeline, the pressurizing pipeline is arranged on the pressurizing pump, the air pipe is fixedly arranged on one end face of the outer pneumatic flow pipeline, one end of the air pipe is communicated with the annular air cavity, the other end of the air pipe is communicated with the pressurizing pipeline, the gas pressure can be filled into the annular air cavity through the pressurizing pipeline and the air pipe in sequence when the pressurizing pump is started, so that the gas pressure value in the annular air cavity is adjusted, the springs are easy to be excessively compressed when the impact force of materials flowing in the inner pneumatic flow pipeline is large, the gas pressurization is filled into the annular air cavity at the moment, the vibration phenomenon of the inner pneumatic flow pipeline splice plates can be reduced, and the springs are prevented from being excessively compressed by the inner pneumatic flow pipeline splice plates.
Drawings
Fig. 1 is a schematic view of a marine pipeline structure with a vibration damping structure according to embodiment 1 of the present invention.
FIG. 2 is a schematic view of the structure of the splice plate for inner pneumatic flow pipes according to embodiment 1 of the present invention.
FIG. 3 is a schematic view of an inner pneumatic flow duct splice according to an embodiment 1 of the present invention.
Fig. 4 is a cross-sectional view of a marine pipeline having a vibration damping structure according to embodiment 1 of the present invention.
Fig. 5 is another perspective cross-sectional view of a marine pipeline having a vibration damping structure according to embodiment 1 of the present invention.
Fig. 6 is an enlarged schematic view of the structure a in fig. 2 according to the present invention.
Fig. 7 is an enlarged schematic view of the structure B in fig. 4 according to the present invention.
Fig. 8 is an enlarged schematic view of the structure at C in fig. 5 according to the present invention.
Fig. 9 is a schematic view showing a pipe structure of a marine system having a vibration damping structure in embodiment 2 of the present invention.
Fig. 10 is a sectional view of a marine system pipeline having a vibration damping structure in embodiment 2 of the present invention.
Fig. 11 is an enlarged schematic view of the structure at D in fig. 10 according to the present invention.
In the figure: 11. a first pipe; 12. a second pipe; 13. an external pneumatic flow pipeline; 131. an end fixing ring; 132. an end fixing plate; 14. an inner pneumatic flow pipeline splice plate; 141. a spring; 142. a guide plate; 143. a first rubber strip; 144. a second rubber strip; 15. a locking ring; 151. a locking plate; 16. an electric push rod; 161. connecting sleeves; 162. a first substrate; 163. a second substrate; 17. an adhesive sheet; 171. brushing; 21. a pressurizing pump; 22. a pressurized conduit; 23. an air pipe; 31. a pressure sensor.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
In the embodiment 1, in order to solve the problems that the air flow has high flowing speed in the pipeline, the inner wall of the pipeline is impacted when the air flow passes through the corner of the pipeline, particularly, the air flow drives granular materials or powder to impact the inner wall of the pipeline, the pipeline is vibrated, the inner wall of the pipeline is severely worn, and the corner of the pipeline is most prone to grinding and leakage; the marine system pipeline with the vibration reduction structure as shown in the figures 1-11 comprises an outer pneumatic flow pipeline 13 and an inner pneumatic flow pipeline, wherein the inner pneumatic flow pipeline is bent, the outer pneumatic flow pipeline 13 is sleeved outside the inner pneumatic flow pipeline as an outer protecting sleeve of the inner pneumatic flow pipeline, the inner pneumatic flow pipeline is communicated between a first pipeline 11 and a second pipeline 12, and air flow drives materials to flow from the first pipeline 11, the inner pneumatic flow pipeline and the second pipeline 12 in sequence; the spring 141 is fixedly welded at the outer ring of the inner pneumatic flow pipeline, one end of the spring 141, which is far away from the outer ring of the inner pneumatic flow pipeline, is movably attached to the inner wall of the outer pneumatic flow pipeline 13, the inner pneumatic flow pipeline comprises an inner pneumatic flow pipeline splice plate 14 and an elastic connection structure, an annular air cavity is formed between the outer ring of the inner pneumatic flow pipeline and the inner ring of the outer pneumatic flow pipeline 13, at least four inner pneumatic flow pipeline splice plates 14 are arranged, a plurality of inner pneumatic flow pipeline splice plates 14 are spliced to form a pipeline shape, the elastic connection structure corresponds to the plurality of inner pneumatic flow pipeline splice plates 14 one by one, the elastic connection structure is connected between the two adjacent inner pneumatic flow pipeline splice plates 14, the elastic connection structure has certain elasticity, when air flow drives materials to enter the inner pneumatic flow pipeline, the air flow drives the materials to push the inner pneumatic flow pipeline splice plates 14 to compress the spring 141, so that the buffering purpose is achieved, the impact force of the air flow and the materials to the inner pneumatic flow pipeline is reduced, the vibration of the whole pipeline is reduced, and the abrasion problem of the inner pneumatic flow pipeline is reduced.
It should be noted that, because the pressure of the air flow driving the material passing through the inner pneumatic flow pipeline is not constant, the impact force of the air flow and the material on the inner pneumatic flow pipeline splice plate 14 is unstable, so that the spring 141 has two states of being compressed and rebounded, and the inner pneumatic flow pipeline splice plate 14 continuously oscillates, and the oscillation of the inner pneumatic flow pipeline splice plate 14 is utilized to counteract the impact force of the air flow and the material, so that the overall oscillation of the pipeline is reduced, and the force of the air flow and the material impacting the inner pneumatic flow pipeline is weakened when the inner pneumatic flow pipeline splice plate 14 itself oscillates.
The elastic connection structure comprises first rubber strips 143, the first rubber strips 143 are arranged in pairs, a pair of first rubber strips 143 are respectively and fixedly arranged on two sides of each inner pneumatic flow pipeline splice plate 14 close to the inner pneumatic flow pipeline splice plates 14 on two sides of the inner pneumatic flow pipeline splice plates, and the first rubber strips 143 on one side, close to each other, of each two adjacent inner pneumatic flow pipeline splice plates 14 are movably attached to each other.
When the material driven by the air flow is particulate matter, the spring 141 with proper elasticity is used, so that the maximum thrust generated by the air flow with the animal material flow can only push the spring 141 to compress to a certain extent, and the width of a gap formed when two adjacent first rubber strips 143 are mutually far away is smaller than the minimum diameter of the particulate matter, thereby avoiding the particulate matter from entering the gap between the two first rubber strips 143 and leaking between the inner ring of the outer pneumatic flow pipeline 13 and the outer ring of the inner pneumatic flow pipeline; based on intermittent opening and closing between the two first rubber strips 143, impurities or dust doped in the particulate matters can enter between the inner ring of the outer pneumatic flow pipeline 13 and the outer ring of the inner pneumatic flow pipeline through gaps, so that the purpose of dust removal and screening of the particulate matters in the flow process is achieved.
In view of the fact that dust or foreign matter can enter between the inner ring of the outer pneumatic flow tube 13 and the outer ring of the inner pneumatic flow tube, the adhesive plate 17 is fixedly installed on the inner wall of the outer pneumatic flow tube 13 by means of screws, the bristles 171 are arranged on the inner wall of the adhesive plate 17, dust entering between the inner ring of the outer pneumatic flow tube 13 and the outer ring of the inner pneumatic flow tube easily adheres to the adhesive plate 17, foreign matter easily winds around the bristles 171, and therefore the phenomenon that dust or foreign matter entering between the inner ring of the outer pneumatic flow tube 13 and the outer ring of the inner pneumatic flow tube flows back into the inner pneumatic flow tube again through the gaps is avoided.
Considering that dust or impurities entering between the inner ring of the outer pneumatic flow tube 13 and the outer ring of the inner pneumatic flow tube are not adhered to the adhesive plate 17 or are likely to flow back into the inner pneumatic flow tube through the gap between the two first rubber strips 143 before being wound around the bristles 171, the guide plate 142 is fixedly arranged at the outer ring of the inner pneumatic flow tube splice plate 14, the guide plate 142 is in an arc-shaped plate-shaped structure, the guide plate 142 shields the outer parts of the two first rubber strips 143 which are mutually adhered, and the guide plate 142 has a flow guiding function, and when dust or impurities enter between the inner ring of the outer pneumatic flow tube 13 and the outer ring of the inner pneumatic flow tube, the dust or impurities can move along the outer surface of the guide plate 142 and are not easy to enter the gap.
The outer pneumatic flow pipeline 13 comprises two pipeline shells with semi-annular radial sections, end fixing plates 132 are fixedly welded on one surfaces, close to each other, of the two pipeline shells, the two corresponding end fixing plates 132 are fixed through screws, end fixing rings 131 are fixedly welded on two ends, close to the first pipeline 11 and the second pipeline 12, of the two pipeline shells, the end fixing rings 131 are fixedly connected to corresponding outer rings of the first pipeline 11 and the second pipeline 12 through screws, and dust or impurities entering between an inner ring of the outer pneumatic flow pipeline 13 and an outer ring of the inner pneumatic flow pipeline are easy to clean regularly based on the detachable arrangement of the outer pneumatic flow pipeline 13.
According to the invention, the pipeline integrally flows through the air flow, the air force is seriously wasted when the pipeline is stopped because the material flowing through the air flow is usually far away, and the vibration of the inner air force flow pipeline splice plate 14 is influenced when the annular cavity is filled with impurities or dust, therefore, locking mechanisms are arranged at two ends of the inner air force flow pipeline splice plate 14, each locking mechanism comprises a locking ring 15 and a locking plate 151, the two locking rings 15 are respectively and movably sleeved at the outer rings of the first pipeline 11 and the second pipeline 12, the locking plates 151 are fixedly arranged on one surface of the locking rings 15 close to the inner air force flow pipeline splice plate 14, the locking plates 151 are arranged at equal angles along the axis of the locking rings 15, when the locking rings 15 move along the first pipeline 11 or the second pipeline 12, the locking plates 151 are attached to the outer rings of the inner air force flow pipeline splice plate 14, the inner air force flow pipeline splice plate 14 is temporarily locked, so that adjacent two inner air force flow pipelines 14 are attached, and then the outer air force flow pipeline 13 is detached to clean dust or impurities in the annular cavity, and the dust can be cleaned under the condition of no stop or the dust is strong.
In actual use, in order to cooperate with the locking mechanism to be provided with the power mechanism, the power mechanism includes electric putter 16, adapter sleeve 161, first base plate 162 and second base plate 163, the power mechanism is provided with two sets of, two first base plates 162 are fixed connection respectively in the outer lane department of first pipeline 11 and second pipeline 12, two second base plates 163 are fixed welding respectively in the outer lane department of two locking rings 15, the one side that corresponds second base plate 163 and first base plate 162 are close to each other is all fixed and is provided with adapter sleeve 161, the both ends of electric putter 16 are all installed between two corresponding adapter sleeves 161 through the fix with screw, promote the second base plate 163 when electric putter 16 starts to remove, because second base plate 163 fixed connection is in the outer lane department of locking ring 15, locking ring 15 synchronous movement when second base plate 163 removes, thereby make the locking plate 151 laminating on the locking ring 15 in the outer lane department of pneumatic flow pipeline splice plate 14.
In embodiment 2, when the material flowing by the air flow is powder, the elastic connection structure is set as the second rubber strip 144, and the second rubber strip 144 is fixedly arranged on the surface of the two inner pneumatic flow pipeline splice plates 14 close to each other, so that when the inner pneumatic flow pipeline splice plates 14 compress the springs 141, no gap exists between the adjacent two inner pneumatic flow pipeline splice plates 14, thereby not only preventing powder leakage, but also realizing the purpose of unloading and buffering the inner pneumatic flow pipeline due to the impact of the air flow and the powder, and reducing the abrasion of the inner pneumatic flow pipeline.
When the second rubber strip 144 is arranged between two adjacent inner pneumatic flow pipeline splice plates 14, the pressure sensor 31 for monitoring the gas pressure in the annular air cavity is fixedly arranged on the inner wall of the outer pneumatic flow pipeline 13, the pressurizing pump 21 is arranged outside the outer pneumatic flow pipeline 13, the pressurizing pump 21 is provided with the pressurizing pipeline 22, one end face of the outer pneumatic flow pipeline 13 is fixedly provided with the air pipe 23, one end of the air pipe 23 is communicated with the annular air cavity, the other end of the air pipe 23 is communicated with the pressurizing pipeline 22, and when the pressurizing pump 21 is started, the gas pressure can be filled into the annular air cavity through the pressurizing pipeline 22 and the air pipe 23 in sequence, so that the gas pressure value in the annular air cavity can be adjusted, the spring 141 is easy to be excessively compressed when the impact force of the material flowing in the inner pneumatic flow pipeline is large, the gas is pressurized at the moment, the vibration phenomenon of the inner pneumatic flow pipeline splice plates 14 can be reduced, and the spring 141 is prevented from being excessively compressed by the inner pneumatic flow pipeline splice plates 14.
In the invention, since the inner pneumatic flow pipeline splice plate 14 can oscillate to remove the impact force of materials in the air flow, in order to ensure the tightness between the two ends of the inner pneumatic flow pipeline splice plate 14 and the first pipeline 11 and the second pipeline 12, rubber sections are fixedly arranged at the two ends of the inner pneumatic flow pipeline splice plate 14, which are close to the first pipeline 11 and the second pipeline 12, and are common elastically deformable pipe sections, which are not shown in the figure, and are not described in detail herein, the rubber sections can elastically deform to adapt to the oscillation of the inner pneumatic flow pipeline splice plate 14, and the tightness of the joints between the two ends of the inner pneumatic flow pipeline splice plate 14 and the first pipeline 11 and the second pipeline 12 is ensured.
Claims (6)
1. Marine system pipeline with damping structure, including outer pneumatic flow pipeline (13) and interior pneumatic flow pipeline, its characterized in that: the outer pneumatic flow pipeline (13) is sleeved outside the inner pneumatic flow pipeline, the inner pneumatic flow pipeline is communicated between the first pipeline (11) and the second pipeline (12), a spring (141) is fixedly welded at the outer ring of the inner pneumatic flow pipeline, one end, far away from the outer ring of the inner pneumatic flow pipeline, of the spring (141) is movably attached to the inner wall of the outer pneumatic flow pipeline (13), the inner pneumatic flow pipeline comprises at least four inner pneumatic flow pipeline splice plates (14) and elastic connection structures, the inner pneumatic flow pipeline splice plates (14) are spliced to form a pipeline shape, the elastic connection structures are also provided with a plurality of inner pneumatic flow pipeline splice plates (14) in one-to-one correspondence, and the elastic connection structures are connected between two adjacent inner pneumatic flow pipeline splice plates (14);
an adhesive plate (17) is fixedly arranged on the inner wall of the outer pneumatic flow pipeline (13) through a screw, bristles (171) are arranged on the inner wall of the adhesive plate (17), dust entering between the inner ring of the outer pneumatic flow pipeline (13) and the outer ring of the inner pneumatic flow pipeline is adhered to the adhesive plate (17), and impurities are wound on the bristles (171);
the elastic connection structure comprises first rubber strips (143), wherein the first rubber strips (143) are arranged in pairs, a pair of first rubber strips (143) are respectively and fixedly arranged on two sides of each inner pneumatic flow pipeline splice plate (14) close to the inner pneumatic flow pipeline splice plates (14) on two sides of the inner pneumatic flow pipeline splice plates, the first rubber strips (143) on one side of each adjacent two inner pneumatic flow pipeline splice plates (14) close to each other are movably attached, and gaps for screening impurities in particles are generated when the two first rubber strips (143) are far away from each other;
the air current drives the particulate matter to flow from first pipeline (11), interior air force flow pipeline and second pipeline (12) in proper order, elastic connection structure has elasticity, when the air current drives the particulate matter and gets into in the air force flow pipeline, the air current drives particulate matter and can promote in air force flow pipeline splice plate (14) compression spring (141) and realize buffering, the maximum thrust that the air current drives the particulate matter flow and produces can only make the gap width that opens when keeping away from each other between two adjacent first rubber strips (143) be less than the diameter of particulate matter, avoid the particulate matter to get into between outer air force flow pipeline (13) inner circle and the interior air force flow pipeline outer lane from gap between two first rubber strips (143) to produce the leakage, based on can intermittent type between two first rubber strips (143) open and shut, impurity or dust in the particulate matter gets into between outer air force flow pipeline (13) inner circle and the interior air force flow pipeline outer lane through gap department, dust removal screening is carried out to the particulate matter in the flow process, dust adhesion between entering outer circle and the interior air force flow pipeline outer lane is on bonding board (17), wind on brush hair (171).
2. A marine pipeline with vibration damping structure according to claim 1, characterized in that: the outer ring of the inner pneumatic flow pipeline splice plate (14) is fixedly provided with a guide plate (142), the guide plate (142) is of an arc-shaped plate structure, and the guide plate (142) is shielded outside the two first rubber strips (143) which are mutually attached.
3. A marine pipeline with vibration damping structure according to claim 1, characterized in that: the outer pneumatic flow pipeline (13) comprises two pipeline shells with semi-annular radial sections, end fixing plates (132) are fixedly welded on one surfaces, close to each other, of the two pipeline shells, the two corresponding end fixing plates (132) are fixed through screws, end fixing rings (131) are fixedly welded on two ends, close to the first pipeline (11) and the second pipeline (12), of the two pipeline shells, and the end fixing rings (131) are fixedly connected to the outer ring of the corresponding first pipeline (11) and the outer ring of the corresponding second pipeline (12) through screws.
4. A marine pipeline with vibration damping structure according to claim 1, characterized in that: both ends of interior air flow pipeline splice plate (14) all are provided with locking mechanical system, and locking mechanical system includes locking ring (15) and locking plate (151), and two locking rings (15) are movably sleeved respectively in the outer lane department of first pipeline (11) and second pipeline (12), locking plate (151) are fixed to be set up in the one side that locking ring (15) is close to interior air flow pipeline splice plate (14), and locking plate (151) are equiangular along the axis of locking ring (15) and are provided with a plurality ofly.
5. A marine pipeline with vibration damping structure according to claim 4, wherein: the locking mechanism is matched with a power mechanism, the power mechanism comprises an electric push rod (16), connecting sleeves (161), first base plates (162) and second base plates (163), the power mechanism is provided with two groups, the two first base plates (162) are respectively fixedly connected to the outer ring of the first pipeline (11) and the outer ring of the second pipeline (12), the two second base plates (163) are respectively fixedly welded to the outer ring of the two locking rings (15), connecting sleeves (161) are fixedly arranged on the surfaces, close to each other, of the corresponding second base plates (163) and the first base plates (162), and the two ends of the electric push rod (16) are fixedly arranged between the two corresponding connecting sleeves (161) through screws.
6. A marine pipeline with vibration damping structure according to claim 1, characterized in that: rubber sections are fixedly arranged at two ends, close to the first pipeline (11) and the second pipeline (12), of the inner pneumatic flow pipeline splice plate (14).
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| CN202310868075.0A CN116608350B (en) | 2023-07-17 | 2023-07-17 | Marine system pipeline with vibration reduction structure |
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| CN202310868075.0A CN116608350B (en) | 2023-07-17 | 2023-07-17 | Marine system pipeline with vibration reduction structure |
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| CN116608350B true CN116608350B (en) | 2023-10-24 |
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|---|---|
| CN116608350A (en) | 2023-08-18 |
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