CN113309493A - Deep sea pressure balancer - Google Patents

Deep sea pressure balancer Download PDF

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Publication number
CN113309493A
CN113309493A CN202110484016.4A CN202110484016A CN113309493A CN 113309493 A CN113309493 A CN 113309493A CN 202110484016 A CN202110484016 A CN 202110484016A CN 113309493 A CN113309493 A CN 113309493A
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CN
China
Prior art keywords
lotus
deep sea
fixedly connected
pressure balancer
reversing
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Granted
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CN202110484016.4A
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Chinese (zh)
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CN113309493B (en
Inventor
夏博昌
鲁郑
严梁柱
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Yangtze University
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Yangtze University
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Priority to CN202110484016.4A priority Critical patent/CN113309493B/en
Publication of CN113309493A publication Critical patent/CN113309493A/en
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Publication of CN113309493B publication Critical patent/CN113309493B/en
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    • EFIXED CONSTRUCTIONS
    • E21EARTH OR ROCK DRILLING; MINING
    • E21BEARTH OR ROCK DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
    • E21B43/00Methods or apparatus for obtaining oil, gas, water, soluble or meltable materials or a slurry of minerals from wells
    • E21B43/01Methods or apparatus for obtaining oil, gas, water, soluble or meltable materials or a slurry of minerals from wells specially adapted for obtaining from underwater installations
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03BMACHINES OR ENGINES FOR LIQUIDS
    • F03B13/00Adaptations of machines or engines for special use; Combinations of machines or engines with driving or driven apparatus; Power stations or aggregates
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D1/00Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D1/06Multi-stage pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D13/00Pumping installations or systems
    • F04D13/02Units comprising pumps and their driving means
    • F04D13/06Units comprising pumps and their driving means the pump being electrically driven
    • F04D13/08Units comprising pumps and their driving means the pump being electrically driven for submerged use
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/44Fluid-guiding means, e.g. diffusers
    • F04D29/445Fluid-guiding means, e.g. diffusers especially adapted for liquid pumps
    • F04D29/448Fluid-guiding means, e.g. diffusers especially adapted for liquid pumps bladed diffusers
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K5/00Casings; Enclosures; Supports
    • H02K5/04Casings or enclosures characterised by the shape, form or construction thereof
    • H02K5/10Casings or enclosures characterised by the shape, form or construction thereof with arrangements for protection from ingress, e.g. water or fingers
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K7/00Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
    • H02K7/18Structural association of electric generators with mechanical driving motors, e.g. with turbines
    • H02K7/1807Rotary generators
    • H02K7/1823Rotary generators structurally associated with turbines or similar engines

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Power Engineering (AREA)
  • Geology (AREA)
  • Mining & Mineral Resources (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Physics & Mathematics (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Fluid Mechanics (AREA)
  • Environmental & Geological Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Drilling And Exploitation, And Mining Machines And Methods (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The invention relates to a deep sea pressure balancer, comprising: the device comprises a multistage turbofan, a lotus barrel, reversing blades and balancing weights; the output end of the multistage turbofan is fixedly connected with the lotus barrel and is used for enabling seawater to uniformly flow out of the reversing blades through the lotus barrel; the output end of the lotus flower cylinder is fixedly connected with the reversing blade, and the reversing blade is used for enabling seawater to flow out at an angle with the axial direction; the bottom end of the reversing blade is fixedly connected with the balancing weight, and a gap exists between the bottom end of the reversing blade and the balancing weight. The deep sea pressure balancer can form negative pressure below the combustible ice pressure balancer, and the effect of reducing the pressure of a mining area is achieved, so that the combustible ice can be mined smoothly, and the energy development problem of China is solved.

Description

Deep sea pressure balancer
Technical Field
The invention relates to the technical field of mining tools for unconventional oil and gas resources such as combustible ice, in particular to a deep sea pressure balancer.
Background
Energy and environment in the 21 st century are two major problems which people pay more and more attention to, and with the increasingly serious environmental problems and the gradual exhaustion of the energy problems in China, the reduction of energy consumption and the reduction of pollutant emission are important, and the environment-friendly dream of 'blue sky and white cloud' is realized by strictly following the sustainable development concept. The combustible ice is abundant in storage, wide in distribution, efficient and clean, and wide in commercial development prospect, and researchers use the combustible ice as the first choice of strategic backup energy. Geological survey experts show that the storage capacity of combustible ice in China is high and higher than that of conventional natural gas resources, and the combustible ice has the condition of becoming clean energy in the future. Therefore, the research on combustible ice, particularly the exploitation of combustible ice, has important strategic significance on future energy and is also an important future scientific research direction.
Due to the unique advantages of combustible ice, the characteristics of abundant reserves, wide distribution and the like, a heat wave has been raised about the exploitation work of combustible ice, and investigation shows that at least 30 countries and regions research combustible ice. Generally speaking, the mining of foreign combustible ice is in the experimental simulation trial mining stage, the detection and identification technology is relatively mature, and the problem to be solved in the aspect of safety is still urgent. In recent years, countries such as japan, the united states, germany, india, and the like have successively made detailed development routes of combustible ice, and incorporated it into the national energy source long-term development program. Significant progress has been made in japan and the united states in the field of combustible ice, and in particular japan, which is internationally recognized as the first country in the world to achieve offshore production of combustible ice. Compared with foreign countries, the development of domestic combustible ice is relatively delayed, and currently, the combustible ice is mainly in the investigation stage due to the limitation of technology and technology. In 2004, the natural gas hydrate research center was established at the Guangzhou energy institute of Chinese academy of sciences. Meanwhile, the Zhongde scientists detected a "Jiulong methane reef" of about 430 km 2. In 2005, a combustible ice simulation system was successfully developed. In 2006, a combustible ice fidelity sampler is developed and a relevant simulation experiment is performed, and the geological characteristics of a natural gas hydrate development area are examined in the south-east-sand-west-south sea area in the north of the south sea. In 2007, the combustible ice is successfully drilled for the first time in 2008 of the Shenhu sea area in the north of south China sea, and the combustible ice substance is successfully extracted in the north of south China sea by using the self-researched ocean number six. Meanwhile, the drilling work of 'combustible ice' in the Qilian mountain frozen soil area of Qinghai province in China is also progressed, and the fact that China has 'combustible ice' in the land is proved. In 6 months in 2009, the 'combustible ice' (natural gas hydrate) samples were successfully drilled on south foot of keelian mountain in Qinghai-Tibet plateau, so that China became the country where natural gas hydrate samples were drilled in alpine frozen soil areas for the first time and also became the country where natural gas hydrate samples were drilled in land frozen soil areas after Canada, USA and Russia.
Generally speaking, the exploitation of combustible ice in China mainly needs to solve the problem of difficult exploitation, and the key of the difficult exploitation lies in the huge seawater pressure in the deep sea water, and whether the pressure of the deep sea water can be reduced is the most important aspect of whether the combustible ice can be successfully exploited.
Disclosure of Invention
In view of the above, there is a need to provide a deep sea pressure balancer to solve the problem of drilling difficulty caused by excessive seawater pressure during deep sea drilling.
The invention provides a deep sea pressure balancer, comprising:
the device comprises a multistage turbofan, a lotus barrel, reversing blades and balancing weights;
the output end of the multistage turbofan is fixedly connected with the lotus barrel and is used for enabling seawater to uniformly flow out of the reversing blades through the lotus barrel;
the output end of the lotus flower cylinder is fixedly connected with the reversing blade, and the reversing blade is used for enabling seawater to flow out at an angle with the axial direction;
the bottom end of the reversing blade is fixedly connected with the balancing weight, and a gap exists between the bottom end of the reversing blade and the balancing weight.
Further, the multistage turbofan jet engine further comprises a driving motor, wherein an output shaft of the driving motor is connected with an input end of the multistage turbofan and is used for driving the multistage turbofan to rotate in an accelerating mode.
Further, still include the battery, the battery is used for driving motor power supply.
Further, multistage turbofan includes that connecting axle, spacer sleeve establish a plurality of turbofan on the connecting axle, the one end of connecting axle with driving motor's output shaft fixed connection, the other end with lotus flower section of thick bamboo fixed connection, a plurality of the diameter of turbofan reduces step by step along the flow direction of sea water.
Further, the lotus flower section of thick bamboo is an eight-petal lotus flower section of thick bamboo, eight lotus flower section of thick bamboo is including being equipped with eight passageways along the circumferential direction array, eight the passageway is arranged along radial direction, eight the entry of passageway with multistage turbofan bottom intercommunication, the export with the switching-over blade intercommunication, the bottom downwardly extending of an eight-petal lotus flower section of thick bamboo forms the sleeve, the sleeve with switching-over blade interference fit connects.
Further, the reversing blade comprises a plurality of blades arranged in an array along the axial direction, each blade comprises a first part and a second part, the first part extends along the axial direction, the second part is fixedly connected to the bottom of the first part, and the second part and the first part form a right angle or an obtuse angle.
Further, the second portion is inclined downward from inside to outside in the radial direction.
Furthermore, a motor isolation cover is fixedly sleeved outside the driving motor and used for isolating seawater.
Further, still include a shell, driving motor and multistage turbofan all overlap and establish in the shell, the top opening of shell, the sea water is followed get into in the opening, the bottom with the sealed fixed connection of the lateral wall of lotus flower section of thick bamboo.
Further, the motor isolation cover comprises an isolation sleeve and a plurality of partition plates which are arranged along the circumferential direction of the outer side wall of the isolation sleeve at equal intervals, the partition plates are fixedly connected with the inner side wall of the shell, a channel is formed between every two adjacent partition plates, and the top of the isolation sleeve is sealed.
Compared with the prior art, the invention has the advantages of
According to the invention, seawater is introduced into the lotus barrel through the multistage turbofan, and is introduced into the reversing blades through the lotus barrel to be reversed, so that local vacuum is generated, namely, negative pressure is formed below the combustible ice pressure balancer, the effect of reducing the pressure intensity of a mining area is achieved, and therefore, the combustible ice can be mined smoothly, and the energy development problem of China is solved.
Drawings
Fig. 1 is a schematic structural diagram of a deep sea pressure balancer according to a first embodiment of the present invention;
FIG. 2 is a schematic view of the internal structure of FIG. 1 with the outer shell removed;
FIG. 3 is a schematic structural view of FIG. 2 with the lotus barrel sleeved outside the commutation blade removed;
FIG. 4 is a schematic structural view of an embodiment of a reversing blade;
FIG. 5 is a schematic structural view of an embodiment of an octapetal cartridge;
FIG. 6 is a top view of FIG. 6;
FIG. 7 is a schematic structural view of a weight member;
description of reference numerals:
1-driving motor, 2-multistage turbofan, 3-lotus barrel, 4-reversing blade, 5-counterweight, 6-gap, 7-shell, 8-opening, 9-motor isolation cover, 901-clapboard, 902-sleeve, 401-first part, 402-second part, 301-sleeve and 302-channel.
Detailed Description
The accompanying drawings, which are incorporated in and constitute a part of this application, illustrate preferred embodiments of the invention and together with the description, serve to explain the principles of the invention and not to limit the scope of the invention.
Embodiments of the present invention provide a deep sea pressure balancer for reducing the pressure of seawater to create a vacuum low pressure environment before a drill bit drills, thereby reducing the pressure of seawater and improving the drilling efficiency of combustible ice in the bottom layer of deep sea.
Referring to fig. 1 to 3, the deep sea pressure balancer includes a driving motor 1, a multi-stage turbofan 2, a lotus barrel 3, a reversing blade 4, and a weight block 5. An output shaft of the driving motor 1 is fixedly connected with the multistage turbofan 2 and is used for driving the multistage turbofan 2 to rotate, the multistage turbofan 2 rotates to introduce seawater into the lotus flower cylinder 3, and meanwhile, the pressure of the seawater above the multistage turbofan is reduced, so that the effect of lower pressure is achieved; the output end of the multistage turbofan 2 is fixedly connected with the lotus flower cylinder 3, and the lotus flower cylinder 3 is used for enabling seawater to uniformly pass through and flow out to the reversing blades 4; the output end of the lotus flower cylinder 3 is fixedly connected with the reversing blades 4, and the reversing blades 4 are used for enabling seawater to flow out at an angle with the axial direction; the output end of the reversing blade 4 is fixedly connected with the balancing weight 5.
As shown in fig. 4, the multistage turbofan 2 is driven to rotate at an accelerated speed by the rotation of the driving motor 1, so that the effect of reducing seawater pressure is achieved, seawater is introduced into the lotus barrel 3, the seawater uniformly passes through the lotus barrel 3 to the reversing blades 4, the reversing blades 4 enable the seawater to flow out at an angle with the axial direction, vertical water flow can be converted into horizontal water flow to be sprayed out, the seawater sprayed out from the middle of the reversing blades 4 and the balancing weight 5 can be horizontally thrown around under the action of the pressure of the surrounding seawater to form a bowl-shaped protective umbrella, namely negative pressure can be formed below the combustible ice pressure balancer, the effect of reducing the pressure of a mining area is achieved, and the combustible ice can be mined smoothly to solve the problem of energy development in China. According to the invention, by means of reducing the local pressure, the regional negative pressure is formed, the pressure of the region for exploiting combustible ice in seawater can be reduced, a particularly good effect is provided for smooth exploitation of combustible ice, and the exploitation efficiency is improved.
As another embodiment of the present invention, the deep sea pressure balancer according to the present invention may be provided without including the driving motor 1, and may be configured to rotate the multi-stage turbofan 2 by the action of seawater. But preferably includes the above-mentioned driving motor 1, by which the multistage turbofan 2 can be driven to rotate at an accelerated speed by the driving motor 1. When the driving motor 1 is included, a battery (not shown in the figure) can be further arranged, the driving motor 1 and the multistage turbofan 2 are connected by fastening screws, and when the power of the battery is sufficient, the battery discharges to drive the turbofan 2 to rotate, so that the flow of seawater is accelerated, and the pressure reduction speed is higher; if the electric quantity of the battery is low, the lower turbofan 2 rotates to drive the motor to rotate 1 so as to charge the battery, and the circulation is carried out so that the combustible ice pressure balancer has sufficient electric power.
Further, multistage turbofan 2 includes that connecting axle 201, interval cover establish a plurality of turbofan 202 on the connecting axle 201, the one end of connecting axle 201 with driving motor 1's output shaft fixed connection, the other end with 3 fixed connection of lotus flower section of thick bamboo, a plurality of the fixed cover of turbofan 202 is established on the connecting axle 201.
According to the invention, by arranging the plurality of turbofan 202, seawater can be sucked into the lotus flower cylinder 3 and the reversing blades 4 step by step, so that the effect of reducing the seawater pressure is further improved.
Further, in order to ensure that the seawater is gradually sucked to the reversing blades 4, thereby further improving the effect of reducing the pressure of the seawater above the reversing blades, the diameters of the plurality of turbofan 202 are gradually reduced along the flow direction of the seawater.
As shown in fig. 5 and 6, the lotus barrel 3 is an eight-petal lotus barrel, the eight-petal lotus barrel 3 is provided with eight passages 302 along the circumferential direction array, the eight passages 302 are arranged along the radial direction, the inlets of the eight passages 302 are communicated with the bottom of the multistage turbofan 2, and the outlets are communicated with the reversing vanes 4. Eight passages 302 are arranged on the device, seawater flows through the eight passages 302, the flow velocity is more uniform, and the pressure of the combustible ice pressure balancer is more stable.
In order to facilitate installation and connection, the bottom of the eight-petal lotus barrel 3 extends downwards to form a sleeve 301, and the sleeve 301 is connected with the reversing blade 4 in an interference fit manner.
The turning vane 4 comprises a plurality of vanes arranged in a circumferential direction array, each vane 4 comprises a first part 401 and a second part 401, the first part 401 extends along the axial direction, the second part 402 is fixedly connected to the bottom of the first part 401, and the second part 402 forms a right angle or an obtuse angle with the first part 401. The second portion 402 is inclined downwardly from the inside to the outside in the radial direction. The reversing blade 4 can convert vertical water flow into horizontal water flow to be sprayed out, seawater sprayed out from the middle of the reversing blade 4 and the balancing weight 5 can horizontally throw around under the action of surrounding seawater pressure to form a bowl-shaped protective umbrella, and negative pressure can be formed below the combustible ice pressure balancer to achieve the effect of reducing the pressure of a mining area, so that the combustible ice can be mined smoothly to solve the problem of energy development in China.
In order to prevent seawater from entering the interior of the driving motor 1 and damaging the driving motor 1, a motor isolation cover 9 is fixedly sleeved outside the driving motor 1 and used for isolating seawater.
The deep sea pressure balancer further comprises a shell 7, the driving motor 1 and the multistage turbofan 2 are sleeved in the shell 7, the top end of the shell 7 is provided with an opening, seawater enters the opening, and the bottom of the deep sea pressure balancer is fixedly connected with the outer side wall of the lotus flower cylinder 3 in a sealing mode. When the multi-stage turbofan jet engine is used, the multi-stage turbofan 2 is driven by the driving motor 1 to rotate in an accelerated mode, so that external seawater is sucked into the shell 7 and enters the reversing blades 4 through the lotus flower cylinder 3 to be reversed, local vacuum is formed, seawater pressure is reduced, and a drill bit can conveniently drill.
The motor isolation cover 9 comprises an isolation sleeve 902 and a plurality of partition plates 901 which are arranged at equal intervals along the circumferential direction of the outer side wall of the isolation sleeve 902, the partition plates 901 are fixedly connected with the inner side wall of the shell 7, a channel is formed between every two adjacent partition plates 901, and the top of the isolation sleeve 02 is sealed.
As shown in fig. 7, since the pressure in the sea water is higher and higher as the water depth increases, the 5-weight block in the present invention is made of a metal material with a higher density. The middle parts of the reversing blades 4 and the balancing weights 5 are welded, and sufficient gaps 6 are formed around the reversing blades and the balancing weights.
When the deep sea pressure balancer provided by the invention is used, the drive motor 1 drives the multistage turbofan 2 to rotate in an accelerating way, the multistage turbofan 2 introduces seawater into the lotus barrel 3, and introduces the seawater into the reversing blades 4 through the lotus barrel 3 for reversing, so that local vacuum is caused, negative pressure can be formed below the combustible ice pressure balancer, the effect of reducing the pressure intensity of a mining area is achieved, and the combustible ice can be mined smoothly to solve the problem of energy development in China.
The above description is only for the preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any changes or substitutions that can be easily conceived by those skilled in the art within the technical scope of the present invention are included in the scope of the present invention.

Claims (10)

1. A deep sea pressure balancer, comprising:
the device comprises a multistage turbofan, a lotus barrel, reversing blades and balancing weights;
the output end of the multistage turbofan is fixedly connected with the lotus barrel and is used for enabling seawater to uniformly flow out of the reversing blades through the lotus barrel;
the output end of the lotus flower cylinder is fixedly connected with the reversing blade, and the reversing blade is used for enabling seawater to flow out at an angle with the axial direction;
the bottom end of the reversing blade is fixedly connected with the balancing weight, and a gap exists between the bottom end of the reversing blade and the balancing weight.
2. The deep sea pressure balancer of claim 1, further comprising a driving motor, wherein an output shaft of the driving motor is connected to an input end of the multi-stage turbofan for driving the multi-stage turbofan to rotate at an accelerated speed.
3. The deep sea pressure balancer of claim 2, further comprising a battery for powering the drive motor.
4. The deep sea pressure balancer as claimed in claim 1, wherein the multi-stage turbofan includes a connecting shaft, a plurality of volutes sleeved on the connecting shaft at intervals, one end of the connecting shaft is fixedly connected with the output shaft of the driving motor, the other end of the connecting shaft is fixedly connected with the lotus cylinder, and the diameters of the plurality of volutes are gradually reduced along the flow direction of the seawater.
5. The deep sea pressure balancer of claim 1, wherein the lotus cylinder is a eight-petal lotus cylinderIncludedEight passageways along the setting of circumference direction array, eight the passageway is arranged along radial direction, eight the entry of passageway with multistage turbofan bottom intercommunication, the export with the switching-over blade intercommunication, the bottom downwardly extending of eight lamella lotus flower section of thick bamboo forms the sleeve, the sleeve with switching-over blade interference fit connects.
6. The deep sea pressure balancer of claim 1, wherein the commutating blades comprise a plurality of blades arranged in an array along an axial direction, each of the blades comprises a first portion and a second portion, the first portion extends along the axial direction, the second portion is fixedly connected to the bottom of the first portion, and the second portion forms a right angle or an obtuse angle with the first portion.
7. The deep sea pressure balancer of claim 1, wherein the second section is sloped downwardly from inside to outside along a radial direction.
8. The deep sea pressure balancer of claim 1, wherein the drive motor is further covered with a motor isolation cover for isolating sea water.
9. The deep sea pressure balancer of claim 6, further comprising a housing, wherein the driving motor and the multi-stage turbofan are both sleeved in the housing, the top end of the housing is open, seawater enters from the opening, and the bottom of the housing is fixedly connected with the outer side wall of the lotus barrel in a sealing manner.
10. The deep sea pressure balancer of claim 7, wherein the motor isolation cover comprises an isolation sleeve and a plurality of partition plates arranged at equal intervals along the circumferential direction of the outer side wall of the isolation sleeve, the partition plates are fixedly connected with the inner side wall of the housing, a channel is formed between every two adjacent partition plates, and the top of the isolation sleeve is sealed.
CN202110484016.4A 2021-04-30 2021-04-30 Deep sea pressure balancer Active CN113309493B (en)

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CN113309493A true CN113309493A (en) 2021-08-27
CN113309493B CN113309493B (en) 2023-01-24

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Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201218066Y (en) * 2008-03-31 2009-04-08 中国石油天然气集团公司 Down-hole decompression tool
CN104234786A (en) * 2014-06-28 2014-12-24 山东省科学院海洋仪器仪表研究所 Underwater multi-phase jet flow noise elimination and reduction device with flower-fold flow guide pipe
WO2016022123A1 (en) * 2014-08-07 2016-02-11 Schlumberger Canada Limited Electric submersible pump components
CN206246119U (en) * 2016-11-22 2017-06-13 长江大学 Continuous wave slurry pulse generator pressure equalization module
EP3379083A1 (en) * 2017-03-21 2018-09-26 OneSubsea IP UK Limited Short impeller for a turbomachine
CN212272029U (en) * 2019-11-21 2021-01-01 北京探矿工程研究所 Seabed pump-free reverse circulation drilling tool

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201218066Y (en) * 2008-03-31 2009-04-08 中国石油天然气集团公司 Down-hole decompression tool
CN104234786A (en) * 2014-06-28 2014-12-24 山东省科学院海洋仪器仪表研究所 Underwater multi-phase jet flow noise elimination and reduction device with flower-fold flow guide pipe
WO2016022123A1 (en) * 2014-08-07 2016-02-11 Schlumberger Canada Limited Electric submersible pump components
CN206246119U (en) * 2016-11-22 2017-06-13 长江大学 Continuous wave slurry pulse generator pressure equalization module
EP3379083A1 (en) * 2017-03-21 2018-09-26 OneSubsea IP UK Limited Short impeller for a turbomachine
CN212272029U (en) * 2019-11-21 2021-01-01 北京探矿工程研究所 Seabed pump-free reverse circulation drilling tool

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