CN111190026A - A five-beam ADCP with replaceable transducer array - Google Patents

A five-beam ADCP with replaceable transducer array Download PDF

Info

Publication number
CN111190026A
CN111190026A CN202010140308.1A CN202010140308A CN111190026A CN 111190026 A CN111190026 A CN 111190026A CN 202010140308 A CN202010140308 A CN 202010140308A CN 111190026 A CN111190026 A CN 111190026A
Authority
CN
China
Prior art keywords
electronic cabin
measurement probe
adcp
transducer
holes
Prior art date
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.)
Granted
Application number
CN202010140308.1A
Other languages
Chinese (zh)
Other versions
CN111190026B (en
Inventor
周志新
王媛媛
徐利军
冯宏
赵俊俊
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hangzhou Ruili Marine Equipment Co Ltd
Original Assignee
Hangzhou Ruili Marine Equipment Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Hangzhou Ruili Marine Equipment Co Ltd filed Critical Hangzhou Ruili Marine Equipment Co Ltd
Priority to CN202010140308.1A priority Critical patent/CN111190026B/en
Publication of CN111190026A publication Critical patent/CN111190026A/en
Application granted granted Critical
Publication of CN111190026B publication Critical patent/CN111190026B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P5/00Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
    • G01P5/24Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring the direct influence of the streaming fluid on the properties of a detecting acoustical wave
    • G01P5/241Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring the direct influence of the streaming fluid on the properties of a detecting acoustical wave by using reflection of acoustical waves, i.e. Doppler-effect
    • G01P5/244Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring the direct influence of the streaming fluid on the properties of a detecting acoustical wave by using reflection of acoustical waves, i.e. Doppler-effect involving pulsed waves
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C13/00Surveying specially adapted to open water, e.g. sea, lake, river or canal
    • G01C13/008Surveying specially adapted to open water, e.g. sea, lake, river or canal measuring depth of open water
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S15/00Systems using the reflection or reradiation of acoustic waves, e.g. sonar systems
    • G01S15/02Systems using the reflection or reradiation of acoustic waves, e.g. sonar systems using reflection of acoustic waves
    • G01S15/06Systems determining the position data of a target
    • G01S15/08Systems for measuring distance only
    • G01S15/32Systems for measuring distance only using transmission of continuous waves, whether amplitude-, frequency-, or phase-modulated, or unmodulated
    • G01S15/34Systems for measuring distance only using transmission of continuous waves, whether amplitude-, frequency-, or phase-modulated, or unmodulated using transmission of continuous, frequency-modulated waves while heterodyning the received signal, or a signal derived therefrom, with a locally-generated signal related to the contemporaneously transmitted signal
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02ATECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
    • Y02A90/00Technologies having an indirect contribution to adaptation to climate change
    • Y02A90/30Assessment of water resources

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Acoustics & Sound (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Hydrology & Water Resources (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Multimedia (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Measuring Volume Flow (AREA)

Abstract

本发明公开了一种换能器阵可替换的五波束ADCP。包括:电子舱、电子舱端盖、换能器底座、流速测量探头、深度测量探头、温压传感器、温压传感器封盖、姿态传感器组件、水密接插件和水密接插件堵头。相比传统的硫化的ADCP基阵探头,本发明打破了传统非相控ADCP在4个流速测量探头一致性较差时不可替换的局限性。通过筛选和替换探头,本发明可实现各流速测量探头较好的阻抗一致性。并且通过更换探头可提高不同性能、不同频率探头的适装性,大大降低传统ADCP整体硫化的换能器探头设计制造成本和维修成本。第五波束——深度测量探头的应用可为ADCP提供第五垂直波束信息,可为船载走航式测量提供更精准的水深数据,并为系统拓展测湍流和测波浪提供了技术途径。

Figure 202010140308

The invention discloses a five-beam ADCP with replaceable transducer array. Including: electronic cabin, electronic cabin end cover, transducer base, flow rate measurement probe, depth measurement probe, temperature and pressure sensor, temperature and pressure sensor cover, attitude sensor assembly, watertight connector and watertight connector plug. Compared with the traditional vulcanized ADCP matrix probe, the invention breaks the limitation that the traditional non-phased ADCP cannot be replaced when the consistency of the four flow rate measurement probes is poor. By screening and replacing the probes, the present invention can achieve better impedance consistency of each flow velocity measuring probe. And by replacing the probe, the adaptability of probes with different performance and different frequencies can be improved, and the design, manufacture and maintenance costs of the traditional ADCP integrally vulcanized transducer probe can be greatly reduced. The fifth beam - the application of the depth measurement probe can provide ADCP with fifth vertical beam information, provide more accurate water depth data for ship-borne navigation measurement, and provide a technical way for the system to expand turbulence and wave measurement.

Figure 202010140308

Description

Transducer array replaceable five-beam ADCP
Technical Field
The invention relates to a transducer array replaceable five-beam ADCP, and belongs to the field of applied acoustics.
Background
An Acoustic Doppler Current Profiler (ADCP) is an advanced real-time measuring device for Current flow rate and flow rate in the world. By using the acoustic Doppler principle, the ADCP emits acoustic pulses to the water body, the acoustic pulses generate reflected waves after encountering particles which are suspended in the water body and move along with the water body, the ADCP receives the reflected waves and records the frequency change between the reflected waves and the emitted waves, and the frequency change is Doppler frequency shift, so that the water flow velocity is calculated. The working modes of the ADCP mainly include: ship-borne sailing type, ship-borne towing type, underwater self-contained type and shore-based direct reading type. The shipborne sailing type ADCP is widely applied to the fields of oceans, lakes, rivers and the like, and is generally divided into a phased array ADCP and a non-phased array ADCP. Phased arrays ADCP are more applied to the low-frequency field, and the array is generally integrally vulcanized and poured. Common home and abroad non-phased array ADCP generally independently pours and vulcanizes 4 transducer arrays onto a base, the planes of the 4 transducer arrays form an included angle of about 20 degrees with the horizontal plane, and a wave beam obliquely faces downwards in four directions. In the process of pouring and vulcanizing 4 independent transducer arrays, 4 array performances are easy to be inconsistent in the traditional non-phased array ADCP, and the impedance difference is large, so that the performance index of the complete ADCP is reduced. In the production process, as the filling vulcanization process basically has no maintainability, the performance indexes of 1 transducer array are unqualified in the filling vulcanization process, and the rest 3 transducer arrays can not be used, so that the production and manufacturing cost is increased, the yield is reduced, and the resource waste is also caused. The manufacturing method of integrally pouring and vulcanizing the transducer array to the base also results in poor versatility and adaptability of the transducer array with different frequencies, and if a non-phased array ADCP with different frequencies is used, the transducer array and the vulcanized base need to be redesigned and manufactured. When the traditional non-phased array ADCP needs to measure the depth information of the paired bases, the ADCP is generally set to be a speed measurement mode of the paired bases, the speed measurement mode is obtained through conversion of four oblique downward wave beam measurement information, and the precision of the measured depth information is low.
Disclosure of Invention
The technical problem to be solved by the invention is as follows: a five beam ADCP with an alternative transducer array is provided. The four flow velocity measurement probes are used for measuring water body flow velocity information, the depth measurement probe can provide fifth vertical beam information for ADCP (acoustic Doppler current profiler), more accurate water depth data are provided for shipborne navigation type measurement, and a technical approach is provided for system expansion turbulence measurement and wave measurement. The replaceable flow velocity measuring probe with better consistency is detected and screened in advance, and the flow measuring performance of the ADCP complete machine is improved. The replaceable design of the measuring probe can also effectively reduce the design and manufacturing cost and the maintenance cost of the ADCP complete machine, and can improve the universality and the replaceability of the measuring probes with different frequencies.
The invention adopts the following technical scheme for solving the technical problems:
a transducer array replaceable five-beam ADCP comprises an electronic cabin, an electronic cabin end cover, a transducer base, a flow velocity measuring probe, a depth measuring probe, a temperature and pressure sensor sealing cover, an attitude sensor assembly, a watertight connector and a watertight connector plug;
the electronic cabin is a hollow cylinder, and the top flange ring and the bottom flange ring are both provided with screw mounting holes; the electronic cabin end cover is arranged at the top of the electronic cabin, the transducer base is arranged at the bottom of the electronic cabin, and first waterproof sealing pieces used for ensuring the watertightness of the interior of the electronic cabin are arranged between the electronic cabin and the electronic cabin end cover and between the electronic cabin and the transducer base;
a watertight connector and a watertight connector plug are fixed on the outer side of the electronic cabin end cover, an internal terminal of the watertight connector is communicated with an inner cavity of the electronic cabin, and an external terminal is sealed by the watertight connector plug; an attitude sensor assembly is fixedly mounted on the inner side of the electronic cabin end cover;
the attitude sensor assembly includes: the attitude sensor, the attitude sensor shielding box and the attitude sensor shielding cover; the attitude sensor is fixed in the attitude sensor shielding box, and the attitude sensor shielding cover is fixed at the top of the attitude sensor shielding box and is used for shielding the interference of electromagnetic signals to the attitude sensor;
the outer bottom of the transducer base is provided with 4 flow velocity measurement probe mounting holes which are uniformly distributed in the circumferential direction and used for fixedly mounting 4 flow velocity measurement probes; the central axis of the flow velocity measurement probe mounting hole and the central axis of the ADCP are arranged at the same included angle, the bottom of the flow velocity measurement probe mounting hole close to the inner cavity of the electronic cabin is provided with a plurality of screw mounting holes and wire outlet holes of the flow velocity measurement probe, and the tops of the 4 flow velocity measurement probe mounting holes and the horizontal plane form the same slope angle; the center of the bottom of the transducer base is provided with a single depth measuring probe mounting hole for fixing a depth measuring probe; the depth measuring probe mounting hole is positioned on a central axis of the electronic cabin, and a plurality of screw mounting holes and depth measuring probe wire outlet holes are formed in the bottom of the depth measuring probe mounting hole, which is close to an inner cavity of the electronic cabin; second waterproof sealing parts are arranged between the transducer base and the 4 flow velocity measuring probes and between the transducer base and the depth measuring probe; the inner wall of the transducer base is a concave spherical surface, and 1 circular screw mounting plane is arranged on the concave spherical surface at the position corresponding to the 4 flow velocity measuring probe mounting holes and the depth measuring probe mounting holes and is used for mounting fastening screws of the flow velocity measuring probe and the depth measuring probe;
the temperature and pressure sensor is embedded in a temperature and pressure sensor mounting hole in the inner wall of the transducer base; the temperature and pressure sensor mounting hole is vertically arranged on a concave spherical surface on the inner wall of the transducer base, and the bottom of the temperature and pressure sensor mounting hole is at least provided with one vent hole communicated with the outer side of the transducer base, so that the sensing end of the temperature and pressure sensor can be contacted with external fluid; the periphery of the temperature and pressure sensor mounting hole is provided with 1 temperature and pressure sensor seal cover mounting plane and a plurality of screw holes for sealing and mounting the temperature and pressure sensor seal cover; the shape of the temperature and pressure sensor sealing cover is matched with the mounting plane of the temperature and pressure sensor sealing cover, and a round temperature and pressure sensor wire outlet hole is formed in the middle of the temperature and pressure sensor sealing cover.
Preferably, the first waterproof sealing element comprises a third O-shaped sealing ring for sealing a right-angle groove, and the third O-shaped sealing ring is used for sealing the electronic cabin and the electronic cabin end cover and sealing the electronic cabin and the transducer base.
Preferably, the second waterproof sealing element comprises a first O-shaped sealing ring and a second O-shaped sealing ring which are used for sealing the rectangular groove; the first O-shaped sealing ring is used for sealing between the depth measuring probe and the transducer base; and the second O-shaped sealing ring is used for sealing between the 4 flow velocity measurement probes and the transducer base.
Preferably, the top of the transducer base is provided with an annular boss, and the annular boss is provided with a plurality of screw mounting holes for mounting the internal circuit board; the bottom of the transducer base is provided with a transducer base mounting plane at the gap position of the 4 flow velocity measurement probe mounting holes; the vent hole at the bottom of the temperature and pressure sensor mounting hole is connected with the outside fluid environment through the transducer base mounting plane; transition fillets are arranged at the connecting edges of the transducer base mounting plane and the 4 flow velocity measurement probe mounting holes; the energy converter base mounting plane is provided with 4 first U-shaped counter bores which are uniformly distributed in the circumferential direction, and screw mounting through holes are formed in the bottoms of the first U-shaped counter bores and correspond to the screw mounting holes in the flange ring at the bottom of the electronic cabin.
Preferably, the top of the electronic cabin end cover is provided with a boss enclosure for preventing the watertight connector from loosening at the periphery of the fixed watertight connector; the boss enclosure is in inverted 'V' -shaped bilateral symmetry, and two ends of the boss enclosure are connected with bosses on the periphery of the top of the end cover of the electronic cabin into a whole; a plurality of second U-shaped counter bores, a switching installation through hole and a cover opening screw hole which are uniformly distributed are arranged on a boss on the periphery of the top of the electronic cabin end cover; the bottom of the second U-shaped counter bore is provided with a screw mounting through hole corresponding to a screw mounting hole on a flange ring at the top of the electronic cabin; the through-connection mounting through hole is used for carrying and mounting ADCP equipment on different platforms; the cover-opening screw hole is used for ejecting the cover-opening screw hole out of the electronic cabin by using a screw when the end cover of the electronic cabin is disassembled; an attitude sensor assembly mounting boss is arranged on the inner side of the electronic cabin end cover, and a plurality of screw holes are formed in the boss and correspond to the screw mounting holes in the attitude sensor shielding box.
Preferably, the flow velocity measurement probe employs a non-phased transducer array, and the depth measurement probe also employs a non-phased transducer array.
Preferably, a first heading arrow mark is etched on the installation plane of the transducer base, and a second heading arrow mark is etched at the front end of the boss enclosure; the first heading arrow mark and the vent hole are positioned on the same side of the same transducer base mounting plane; the first heading arrow mark and the second heading arrow mark face towards the same direction.
Preferably, the installation direction of the plug pin of the watertight connector faces to the opposite direction of the second heading arrow mark.
Preferably, the temperature and pressure sensor and the watertight connector are both watertight structures and are provided with waterproof sealing elements for sealing the inside of the electronic cabin.
Preferably, the diameter of the flow velocity measurement probe is slightly smaller than that of the flow velocity measurement probe mounting hole, and the flow velocity measurement probe are mounted in a clearance fit manner; the diameter of the depth measuring probe is slightly smaller than that of the depth measuring probe mounting hole, and the depth measuring probe are mounted in a clearance fit mode.
The invention provides a five-beam ADCP with an exchangeable transducer array, wherein a fifth vertical beam is added on the basis of the traditional four-beam ADCP, more accurate water depth data can be provided for shipborne sailing type measurement, and a technical approach is provided for system development turbulence measurement and wave measurement. The replaceable design of the transducer array can effectively reduce the design and manufacturing cost and the maintenance cost of the ADCP complete machine, and can improve the universality and the replaceability of the transducer arrays with different frequencies. By screening the transducer array with better performance impedance consistency in advance, the current measuring performance of the ADCP complete machine can be effectively improved.
Drawings
FIG. 1 is a schematic diagram of a five-beam ADCP structure with an alternative transducer array;
figure 2 is a five beam ADCP composition 3 view of an alternative transducer array;
FIG. 3 is a cross-sectional view of a five-beam ADCP replaceable with a transducer array through the central axis of a flow measurement probe;
FIG. 4 is an isometric view of an electronics compartment end cap;
FIG. 5 is an isometric view of a transducer base;
FIG. 6 is an isometric view of a temperature and pressure sensor cover;
FIG. 7 is an enlarged schematic view of a part I of a temperature and pressure sensor and a temperature and pressure sensor cover mounting structure;
FIG. 8 is an enlarged schematic view of a portion II of the attitude sensor assembly mounting structure;
the reference numbers in the figures are as follows:
1. an electronic compartment; 2. an electronic compartment end cap; 3. a transducer base; 4. a flow rate measuring probe; 5. a depth measurement probe; 6. a temperature and pressure sensor; 7. sealing the temperature and pressure sensor; 8. an attitude sensor assembly; 9. a watertight connector; 10. a watertight connector plug; 11. an attitude sensor; 12. an attitude sensor shield case; 13. an attitude sensor shield cover; 14. a flow velocity measurement probe mounting hole; 15. a depth measurement probe mounting hole; 16. a circular screw mounting plane; 17. a temperature and pressure sensor mounting hole; 18. a vent aperture; 19. a temperature and pressure sensor sealing cover mounting plane; 20. a first O-ring seal; 21. a second O-ring seal; 22. a third O-shaped sealing ring; 23. a transducer base mounting plane; 24. a first U-shaped counter bore; 25. a first heading arrow indicator; 26. the boss is surrounded and blocked; 27. a second heading arrow indicator; 28. a second U-shaped counter bore; 29. through holes are installed in a switching way; 30. a cap-opening screw hole; 31. the attitude sensor assembly is provided with a boss.
Detailed Description
The invention will be further elucidated and described with reference to the drawings and the detailed description. The technical features of the embodiments of the present invention can be combined correspondingly without mutual conflict.
As shown in fig. 1, fig. 2 and fig. 7, the transducer array replaceable five-beam ADCP in an embodiment of the present invention mainly includes an electronic cabin 1, an electronic cabin end cover 2, a transducer base 3, four flow velocity measurement probes 4, a depth measurement probe 5, a temperature and pressure sensor 6, a temperature and pressure sensor cover 7, an attitude sensor assembly 8, a watertight connector 9, and a watertight connector plug 10. The invention adds a depth measuring probe 5 on the basis of the traditional four flow velocity measuring probes 4. The four flow velocity measurement probes can measure water flow velocity information by using an acoustic Doppler principle, the depth measurement probe can provide fifth vertical beam information for ADCP measurement by using the acoustic Doppler principle, and more accurate water depth data is provided for shipborne sailing measurement. The specific form of the flow rate measuring probe 4 and the depth measuring probe 5 is not limited, and any device capable of achieving this function may be used. In the present embodiment, the flow velocity measurement probe 4 and the depth measurement probe 5 are preferably measured using a non-phased transducer array. Certainly, the non-phased transducer array needs to be matched with necessary circuit boards for signal transceiving, processing and the like, and these electronic devices such as the PCB board and the like can be placed in the inner cavity of the electronic cabin 1. According to the invention, the flow velocity measuring probe 4 and the depth measuring probe 5 can be detached and replaced through screws on the back of the probes, and the flow measuring performance of the ADCP complete machine is improved by detecting and screening the measuring probes with better consistency in advance. The replaceable design of the measuring probe can also effectively reduce the design and manufacturing cost and the maintenance cost of the ADCP complete machine, and can improve the universality and the replaceability of the measuring probes with different frequencies. The specific structure of each part and its operation principle are described in detail below.
As shown in fig. 2, the electronic cabin 1 is a hollow cylinder, and the top flange ring and the bottom flange ring are provided with screw mounting holes, and various electronic devices and cables can be accommodated inside the screw mounting holes. In order to ensure the airtightness of the inner cavity of the electronic cabin 1, the electronic cabin end cover 2 is mounted at the top of the electronic cabin 1 through screws, the transducer base 3 is mounted at the bottom of the electronic cabin 1 through screws, and first waterproof sealing parts are arranged between the electronic cabin 1 and the electronic cabin end cover 2 and between the electronic cabin 1 and the transducer base 3, so that water vapor is prevented from entering the inner cavity of the electronic cabin 1, and the form of the waterproof sealing parts is not limited. In this embodiment, the electronic capsule 1 and the electronic capsule end cover 2, and the electronic capsule 1 and the transducer base 3 are sealed by the third O-ring 22 through right-angle grooves. In addition, in consideration of the transmission requirements of power supply and signals, the transmission between the inside and the outside of the cabin body needs to be realized through watertight connectors. Thus, a watertight connector 9 is fixed to the top of the electronics compartment end cap 2. The internal terminal of the watertight connector 9 is communicated with the inner cavity of the electronic cabin 1, and the external terminal is sealed by a watertight connector plug 10. A matched watertight connector plug 10 can be installed under the condition that an external watertight cable is not connected, so that water is prevented from entering or being blocked, and the plug can be pulled out when in use.
As shown in fig. 2 and 5, in order to prevent the watertight connector 9 from loosening and leaking water during high-speed sailing, a boss enclosure 26 is disposed on the top of the electronic cabin end cap 2 and symmetrically arranged in an inverted "u" shape, so as to limit and fix the installation direction of the watertight connector 9. A second heading arrow 27 is etched into the front of the raised perimeter 26 to help the user of the apparatus discern the heading of the ADCP. An attitude sensor assembly mounting boss 31 is arranged on the inner side of the electronic cabin end cover 2, and a screw hole is formed in the boss. The attitude sensor assembly 8 is mounted on the attitude sensor assembly mounting boss 31 by screws. In addition, in this embodiment, six second U-shaped counter bores 28, four through-connection mounting through holes 29 and three cover-opening screw holes 30 are circumferentially and uniformly arranged on a boss on the periphery of the top of the electronic cabin end cover 2. And the bottom of the second U-shaped counter bore 28 is provided with a screw mounting through hole respectively for mounting a fastening screw between the electronic cabin 1 and the electronic cabin end cover 2. The same number of screw holes are provided at the top end of the electronic compartment 1 corresponding to the positions of the through holes 29 for docking the ADCP with the external mounting structure in this embodiment. The cover-opening screw hole 30 is used for ejecting the electronic cabin end cover 2 tightly matched with the electronic cabin 1 out of the matching surface without damaging the appearance and the structure by screwing in the screw when the electronic cabin end cover 2 of the ADCP is detached. The number and arrangement of the second U-shaped counter bore 28, the connecting and mounting through holes 29 and the cap-opening screw holes 30 are not limited.
As shown in fig. 3 and 4, the outer bottom of the transducer base 3 is provided with 4 flow velocity measurement probe mounting holes 14 which are uniformly arranged in the circumferential direction, the four flow velocity measurement probes 4 are arranged in the flow velocity measurement probe mounting holes 14 of the transducer base 3 in the circumferential direction, the central axis of the measurement beam and the central axis of the hollow cylinder of the ADCP electronic cabin 1 are all in the same slope angle, and the slope surface of the measurement beam is gradually reduced towards the side edge by taking the central axis of the ADCP electronic cabin 1 as the vertex. The depth measuring probe 5 is vertically installed in a depth measuring probe installation hole 15 at the bottom of the transducer base 3. Screw holes and second waterproof sealing pieces which are annularly arranged are arranged on back mounting surfaces of the flow velocity measuring probe 4 and the depth measuring probe 5, and the waterproof sealing pieces are not limited in form but need to be larger than the center distance of the screw holes in size. In the present embodiment, the back of the flow rate measurement probe 4 is sealed with a rectangular groove by the second O-ring, and the depth measurement probe 5 is sealed with a rectangular groove by the first O-ring 20. The number and the arrangement mode of the screw holes are all corresponding to the through holes on the circular screw mounting plane 16 on the inner wall of the transducer base 3. The fixing screws of the flow velocity measuring probe 4 and the depth measuring probe 5 are fixedly arranged outwards from the inner wall of the transducer base 3. The round screw mounting plane 16 is arranged to provide a screw mounting plane on the concave spherical surface of the inner wall of the transducer base 3, so that the screw mounting and screwing are facilitated. And wire outlet holes for the routing of the flow velocity measuring probe 4 and the depth measuring probe 5 are formed in the inner sides of the circular screw mounting planes 16.
As shown in fig. 4, 6 and 7, since the ADCP also needs to measure the current water temperature and water pressure, a temperature and pressure sensor mounting hole 17 perpendicular to the inner wall is formed on the concave spherical surface of the inner wall of the transducer base 3 for mounting the temperature and pressure sensor 6. At least one vent hole 18 is arranged at the bottom of the temperature and pressure sensor mounting hole 17 and communicated with the outer side of the transducer base 3, so that the sensing energy of the temperature and pressure sensor can contact external fluid. The periphery of the temperature and pressure sensor mounting hole 17 is provided with 1 temperature and pressure sensor sealing cover mounting plane 19 and is provided with a plurality of screw holes. The shape and the arrangement of the screw holes are matched with the shape of the temperature and pressure sensor cover 7 shown in figure 6. The temperature and pressure sensor sealing cover 7 is used for limiting and fixing the temperature and pressure sensor 6, a round temperature and pressure sensor 6 wire outlet hole is formed in the middle of the temperature and pressure sensor sealing cover, and the temperature and pressure sensor sealing cover is installed on the inner wall of the energy converter base 3 through screws. Wherein, the temperature and pressure sensor 6 is of a watertight structure and is provided with a waterproof sealing element. An annular boss is arranged at the top of the transducer base 3, a plurality of screw holes are arranged on the boss and used for mounting electronic devices such as an internal PCB, and the form of the boss is not limited, so that the details are not repeated. A transducer base mounting plane 23 is provided at the bottom of the transducer base 3 at a position of the gap of the flow rate measurement probe mounting hole 14. The edge shape of the sensor is similar to the projection shape of the 4 flow rate measurement probe mounting holes on the transducer base mounting plane 23 and is slightly larger than the projection shape. Transition fillets are arranged at the connecting edges of the transducer base mounting plane 23 and the 4 flow rate measurement probe mounting holes 14, so that the fluid resistance of the ADCP in the process of use during sailing is reduced, and cavitation bubbles are prevented. In the present embodiment, the vent hole 18 of the warm-pressure sensor 6 is vertically arranged on the transducer base mounting plane 23, i.e., communicates internally to the warm-pressure sensor mounting hole 17. The transducer base mounting plane 23 is etched with a first heading arrow mark 25, and is located on the same side of the vent hole 18, so that water flow on the upstream side can enter the vent hole 18 in the process of heading navigation of the ADCP. The transducer base mounting plane 23 is provided with first U-shaped counter bores 24 arranged in a circumferential direction, and the bottom of the transducer base mounting plane is provided with screw mounting through holes for mounting fastening screws between the transducer base 3 and the electronic cabin 1, wherein the number of the first U-shaped counter bores 24 is not limited, and 4 groups of the first U-shaped counter bores are arranged in the circumferential direction in the embodiment.
As shown in fig. 8, since the ADCP also needs attitude and heading angle information of the ADCP in the cruising operation state, an attitude sensor assembly 8 including an attitude sensor 11, an attitude sensor shield case 12, and an attitude sensor shield cover 13 is mounted on the inner side of the electronic cabin end cover 2. The attitude sensor shielding box 12 is a hollow box structure, and is mounted on the attitude sensor assembly mounting boss 31 as a mounting base of the attitude sensor 11 by screws. The attitude sensor 11 is mounted in the inner cavity of the attitude sensor shield case 12, and the top is enclosed by an attitude sensor shield cover 13. In this embodiment, the attitude sensor shielding box 12 and the attitude sensor shielding cover 13 are both made of aluminum alloy, and play a role in protecting and shielding the attitude sensor 11 from electromagnetic signal interference.
In the five-beam ADCP of the invention, 4 flow velocity measurement probes are used for measuring the flow velocity profile, and the depth measurement probe is used for measuring the vertical depth of the water bottom. Compared with the depth information of the ground pair obtained in the four-beam ground speed measurement mode, the vertical beam depth measurement has higher precision and better performance. Compared with the traditional vulcanized ADCP array probe, the invention breaks through the irreplaceable limitation of the traditional non-phased ADCP when the consistency of the 4 flow rate measurement probes is poor, and the 5 probes can be detached and replaced under the condition of ensuring the sealing performance through structural optimization. Therefore, the invention can realize better impedance consistency of each flow velocity measuring probe by screening and replacing the probe, and can improve the adaptability of probes with different performances and different frequencies by replacing the probe, thereby greatly reducing the design and manufacturing cost and the maintenance cost of the transducer probe integrally vulcanized by the traditional ADCP. The depth measurement probe carried by the invention can provide fifth vertical beam information for ADCP, provide more accurate water depth data for shipborne sailing type measurement, and provide a technical approach for system development turbulence measurement and wave measurement.
The above-described embodiments are merely preferred embodiments of the present invention, which should not be construed as limiting the invention. Various changes and modifications may be made by one of ordinary skill in the pertinent art without departing from the spirit and scope of the present invention. Therefore, the technical scheme obtained by adopting the mode of equivalent replacement or equivalent transformation is within the protection scope of the invention.

Claims (10)

1.一种换能器阵可替换的五波束ADCP,其特征在于:包括电子舱(1)、电子舱端盖(2)、换能器底座(3)、流速测量探头(4)、深度测量探头(5)、温压传感器(6)、温压传感器封盖(7)、姿态传感器组件(8)、水密接插件(9)和水密接插件堵头(10);1. A five-beam ADCP with a replaceable transducer array, it is characterized in that: comprise electronic cabin (1), electronic cabin end cover (2), transducer base (3), flow velocity measurement probe (4), depth Measuring probe (5), temperature and pressure sensor (6), temperature and pressure sensor cover (7), attitude sensor assembly (8), watertight connector (9) and watertight connector plug (10); 所述的电子舱(1)呈中空柱体,顶部法兰环及底部法兰环上均设有螺钉安装孔;所述的电子舱端盖(2)安装于电子舱(1)的顶部,所述的换能器底座(3)安装于电子舱(1)的底部,且电子舱(1)与电子舱端盖(2)以及电子舱(1)与换能器底座(3)之间均设有用于保证电子舱(1)内部不透水的第一防水密封件;所述的电子舱端盖(2)外侧固定有水密接插件(9)以及水密接插件堵头(10),水密接插件(9)内部接线端连通电子舱(1)内腔,外部接线端通过水密接插件堵头(10)密封;电子舱端盖(2)内侧固定安装有姿态传感器组件(8);The electronic cabin (1) is in the form of a hollow cylinder, and the top flange ring and the bottom flange ring are provided with screw mounting holes; the electronic cabin end cover (2) is installed on the top of the electronic cabin (1), The transducer base (3) is installed at the bottom of the electronic cabin (1), and between the electronic cabin (1) and the end cover (2) of the electronic cabin and between the electronic cabin (1) and the transducer base (3) Both are provided with a first waterproof seal for ensuring that the inside of the electronic cabin (1) is impermeable to water; the outer side of the electronic cabin end cover (2) is fixed with a watertight connector (9) and a watertight connector plug (10). The inner terminal of the tight connector (9) is connected to the inner cavity of the electronic cabin (1), and the external terminal is sealed by the watertight connector plug (10); the inner side of the electronic cabin end cover (2) is fixedly installed with an attitude sensor assembly (8); 所述的姿态传感器组件(8)包括:姿态传感器(11)、姿态传感器屏蔽盒(12)和姿态传感器屏蔽盖(13);所述姿态传感器(11)固定于姿态传感器屏蔽盒(12)内部,所述姿态传感器屏蔽盖(13)固定于姿态传感器屏蔽盒(12)顶部,用于屏蔽电磁信号对姿态传感器(11)的干扰;The attitude sensor assembly (8) comprises: an attitude sensor (11), an attitude sensor shielding box (12) and an attitude sensor shielding cover (13); the attitude sensor (11) is fixed inside the attitude sensor shielding box (12) , the posture sensor shielding cover (13) is fixed on the top of the posture sensor shielding box (12) for shielding the interference of electromagnetic signals to the posture sensor (11); 所述的换能器底座(3)外底部开有4个周向均匀排布的流速测量探头安装孔(14),用于固定安装4个流速测量探头(4);所述的流速测量探头安装孔(14)中轴线与ADCP中轴线呈相同夹角排布,流速测量探头安装孔(14)靠近电子舱(1)内腔的底部设有若干螺钉安装孔以及流速测量探头(4)的出线孔,4个流速测量探头安装孔(14)的顶部与水平面呈相同坡角;换能器底座(3)的底部中心位置开有单个深度测量探头安装孔(15),用于固定深度测量探头(5);所述的深度测量探头安装孔(15)处于电子舱(1)中轴线上,深度测量探头安装孔(15)靠近电子舱(1)内腔的底部设有若干螺钉安装孔以及深度测量探头(5)出线孔;换能器底座(3)与4个流速测量探头(4)以及换能器底座(3)与深度测量探头(5)之间均设有第二防水密封件;所述的换能器底座(3)内壁呈下凹球形面,该下凹球形面上与4个流速测量探头安装孔(14)以及深度测量探头安装孔(15)的对应位置均设有1个圆形螺钉安装平面(16),用于流速测量探头(4)和深度测量探头(5)的紧固螺钉安装;The outer bottom of the transducer base (3) is provided with 4 flow velocity measurement probe mounting holes (14) evenly arranged in the circumferential direction, which are used for the fixed installation of the 4 flow velocity measurement probes (4); the flow velocity measurement probe The central axis of the installation hole (14) and the central axis of the ADCP are arranged at the same angle, and the flow velocity measurement probe installation hole (14) is provided with a number of screw installation holes at the bottom of the inner cavity of the electronic cabin (1) close to the bottom of the flow velocity measurement probe (4). Outlet holes, the tops of the four flow velocity measurement probe installation holes (14) are at the same slope angle as the horizontal plane; a single depth measurement probe installation hole (15) is opened at the bottom center of the transducer base (3) for fixing the depth measurement Probe (5); the depth measurement probe installation hole (15) is located on the central axis of the electronic cabin (1), and the depth measurement probe installation hole (15) is provided with a number of screw installation holes at the bottom of the inner cavity of the electronic cabin (1). and the outlet hole of the depth measurement probe (5); a second waterproof seal is provided between the transducer base (3) and the four flow rate measurement probes (4) and the transducer base (3) and the depth measurement probe (5). The inner wall of the transducer base (3) is a concave spherical surface, and the concave spherical surface and the corresponding positions of the four flow velocity measurement probe installation holes (14) and the depth measurement probe installation holes (15) are set There is a round screw mounting plane (16) for the fastening screw mounting of the flow rate measuring probe (4) and the depth measuring probe (5); 所述的温压传感器(6)嵌入式安装于换能器底座(3)内壁的温压传感器安装孔(17)内;所述的温压传感器安装孔(17)垂直布置于换能器底座(3)内壁下凹球形面上,底部至少开设一个与换能器底座(3)外侧连通的通气孔(18),使温压传感器(6)的感应端能接触外部流体;所述的温压传感器安装孔(17)周边设有1个温压传感器封盖安装平面(19)和若干螺钉孔,用于温压传感器封盖(7)的密封安装;所述的温压传感器封盖(7)形状与温压传感器封盖安装平面(19)相匹配,中间开有圆形温压传感器出线孔。The temperature and pressure sensor (6) is embedded in the temperature and pressure sensor installation hole (17) on the inner wall of the transducer base (3); the temperature and pressure sensor installation hole (17) is vertically arranged on the transducer base (3) On the concave spherical surface of the inner wall, at least one ventilation hole (18) connected to the outside of the transducer base (3) is provided at the bottom, so that the sensing end of the temperature and pressure sensor (6) can contact the external fluid; A temperature and pressure sensor cover installation plane (19) and several screw holes are arranged around the pressure sensor installation hole (17) for sealing installation of the temperature and pressure sensor cover (7); the temperature and pressure sensor cover ( 7) The shape matches the temperature and pressure sensor cover installation plane (19), and a circular temperature and pressure sensor outlet hole is opened in the middle. 2.如权利要求1所述的一种换能器阵可替换的五波束ADCP,其特征在于:所述的第一防水密封件包括用于直角型沟槽密封的第三O型密封圈(22),用于电子舱(1)与电子舱端盖(2)以及电子舱(1)与换能器底座(3)之间的密封。2. The five-beam ADCP with a replaceable transducer array according to claim 1, wherein the first waterproof seal comprises a third O-ring ( 22), used for sealing between the electronic cabin (1) and the end cover (2) of the electronic cabin and between the electronic cabin (1) and the transducer base (3). 3.如权利要求1所述的一种换能器阵可替换的五波束ADCP,其特征在于:所述的第二防水密封件包括用于矩形沟槽密封的第一O型密封圈(20)和第二O型密封圈(21);所述的第一O型密封圈(20)用于深度测量探头(5)与换能器底座(3)之间的密封;所述的第二O型密封圈(21)用于4个流速测量探头(4)与换能器底座(3)之间的密封。3. The five-beam ADCP with a replaceable transducer array according to claim 1, wherein the second waterproof seal comprises a first O-ring (20) for sealing a rectangular groove ) and the second O-ring (21); the first O-ring (20) is used for sealing between the depth measurement probe (5) and the transducer base (3); the second The O-ring (21) is used for sealing between the four flow rate measuring probes (4) and the transducer base (3). 4.如权利要求1所述的一种换能器阵可替换的五波束ADCP,其特征在于:所述的换能器底座(3)顶部设有一环形凸台,环形凸台上设有若干用于内部电路板的安装的螺钉安装孔;换能器底座(3)底部位于4个流速测量探头安装孔(14)的间隙位置设有换能器底座安装平面(23);所述的温压传感器安装孔(17)底部的通气孔(18)通过换能器底座安装平面(23)连接外侧流体环境;所述的换能器底座安装平面(23)与4个流速测量探头安装孔(14)的连接边缘处设有过渡圆角;换能器底座安装平面(23)上设有4个周向均匀分布的第一U形沉孔(24),所述的第一U形沉孔(24)底部设有螺钉安装通孔,与电子舱(1)底部法兰环上的螺钉安装孔相对应。4. The five-beam ADCP with replaceable transducer array as claimed in claim 1, characterized in that: the top of the transducer base (3) is provided with an annular boss, and the annular boss is provided with several Screw mounting holes for the installation of the internal circuit board; a transducer base mounting plane (23) is provided at the bottom of the transducer base (3) at the clearance position of the four flow rate measurement probe mounting holes (14); the temperature The vent hole (18) at the bottom of the pressure sensor installation hole (17) is connected to the outside fluid environment through the transducer base installation plane (23); the transducer base installation plane (23) is connected to the four flow rate measurement probe installation holes ( 14) The connecting edge is provided with a transition fillet; the transducer base mounting plane (23) is provided with four first U-shaped counterbores (24) evenly distributed in the circumferential direction, and the first U-shaped counterbores (24) There are screw mounting through holes at the bottom, which correspond to the screw mounting holes on the flange ring at the bottom of the electronic compartment (1). 5.如权利要求4所述的一种换能器阵可替换的五波束ADCP,其特征在于:所述的电子舱端盖(2)顶部在固定水密接插件(9)的四周设有防止水密接插接(9)松动的凸台围挡(26);所述的凸台围挡(26)呈倒“几”字形左右对称,且两端与电子舱端盖(2)顶部周边的凸台连成一体;电子舱端盖(2)顶部周边凸台设有均匀排布的若干第二U形沉孔(28)、转接安装通孔(29)以及起盖螺钉孔(30);所述的第二U形沉孔(28)的底部设有螺钉安装通孔与电子舱(1)顶部法兰环上的螺钉安装孔相对应;所述的转接安装通孔(29)用于ADCP设备在不同平台的搭载安装;所述的起盖螺钉孔(30)用于在拆卸电子舱端盖(2)时用螺钉将其顶出电子舱(1);电子舱端盖(2)内侧设有姿态传感器组件安装凸台(31),且在凸台上设有若干螺钉孔与姿态传感器屏蔽盒(12)上的螺钉安装孔相对应。5. The five-beam ADCP that a transducer array can replace as claimed in claim 4, characterized in that: the top of the end cover of the electronic cabin (2) is provided with a preventer around the fixed watertight connector (9). The boss enclosure (26) that is loosely connected to the watertight plug (9); the boss enclosure (26) is symmetrical in the shape of an inverted "ji", and the two ends are connected to the top periphery of the end cover (2) of the electronic cabin. The bosses are integrated into one body; the peripheral bosses on the top of the electronic cabin end cover (2) are provided with a plurality of second U-shaped countersunk holes (28), adapter mounting through holes (29) and cover screw holes (30) that are evenly arranged The bottom of the second U-shaped counterbore (28) is provided with screw mounting holes corresponding to the screw mounting holes on the top flange ring of the electronic cabin (1); the adapter mounting holes (29) It is used for the loading and installation of ADCP equipment on different platforms; the screw holes (30) for lifting the cover are used to push the electronic cabin end cover (2) out of the electronic cabin (1) with screws when disassembling it; the electronic cabin end cover ( 2) An attitude sensor assembly mounting boss (31) is provided on the inner side, and several screw holes are arranged on the boss corresponding to the screw mounting holes on the attitude sensor shielding box (12). 6.如权利要求1所述的一种换能器阵可替换的五波束ADCP,其特征在于:所述的流速测量探头(4)采用非相控换能器阵,所述的深度测量探头(5)也采用非相控换能器阵。6. The five-beam ADCP that a transducer array can replace as claimed in claim 1, it is characterized in that: described flow velocity measurement probe (4) adopts non-phased transducer array, described depth measurement probe (5) A non-phased transducer array is also used. 7.如权利要求5所述的一种换能器阵可替换的五波束ADCP,其特征在于:所述的换能器底座安装平面(23)蚀刻有第一艏向箭头标志(25),在凸台围挡(26)的前端蚀刻有第二艏向箭头标志(27);所述的第一艏向箭头标志(25)与通气孔(18)位于同一个换能器底座安装平面(23)的同一侧;所述第一艏向箭头标志(25)和第二艏向箭头标志(27)均朝向同一方向。7. The five-beam ADCP with replaceable transducer array as claimed in claim 5, characterized in that: the transducer base mounting plane (23) is etched with a first heading arrow mark (25), A second heading arrow mark (27) is etched on the front end of the boss enclosure (26); the first heading arrow mark (25) and the vent hole (18) are located on the same transducer base installation plane ( 23); the first heading arrow mark (25) and the second heading arrow mark (27) both face the same direction. 8.如权利要求1所述的一种换能器阵可替换的五波束ADCP,其特征在于:所述的水密接插件(9)的插针安装方向朝向第二艏向箭头标志(27)的反方向。8. A five-beam ADCP with replaceable transducer array as claimed in claim 1, characterized in that: the pin installation direction of the watertight connector (9) is toward the second heading arrow mark (27) the opposite direction. 9.如权利要求1所述的一种换能器阵可替换的五波束ADCP,其特征在于:所述的温压传感器(6)和水密接插件(9)均为水密结构,自带用于实现电子舱(1)内部的密封的防水密封件。9. The five-beam ADCP replaceable by a transducer array as claimed in claim 1, characterized in that: the temperature and pressure sensor (6) and the watertight connector (9) are both watertight structures, and are self-contained for use with A waterproof seal for sealing the interior of the electronic compartment (1). 10.如权利要求1所述的一种换能器阵可替换的五波束ADCP,其特征在于:所述的流速测量探头(4)的直径略小于流速测量探头安装孔(14)的直径,两者为间隙配合安装;所述的深度测量探头(5)的直径略小于深度测量探头安装孔(15)的直径,两者也为间隙配合安装。10. A five-beam ADCP with a transducer array replaceable as claimed in claim 1, characterized in that: the diameter of the flow velocity measurement probe (4) is slightly smaller than the diameter of the flow velocity measurement probe mounting hole (14), The two are installed with clearance fit; the diameter of the depth measurement probe (5) is slightly smaller than the diameter of the installation hole (15) of the depth measurement probe, and the two are also installed with clearance fit.
CN202010140308.1A 2020-03-03 2020-03-03 A five-beam ADCP with replaceable transducer array Active CN111190026B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202010140308.1A CN111190026B (en) 2020-03-03 2020-03-03 A five-beam ADCP with replaceable transducer array

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010140308.1A CN111190026B (en) 2020-03-03 2020-03-03 A five-beam ADCP with replaceable transducer array

Publications (2)

Publication Number Publication Date
CN111190026A true CN111190026A (en) 2020-05-22
CN111190026B CN111190026B (en) 2025-05-09

Family

ID=70708514

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202010140308.1A Active CN111190026B (en) 2020-03-03 2020-03-03 A five-beam ADCP with replaceable transducer array

Country Status (1)

Country Link
CN (1) CN111190026B (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112162111A (en) * 2020-09-25 2021-01-01 杭州瑞利海洋装备有限公司 Self-contained ADCP (advanced digital control Panel) suitable for deepwater distribution
CN113029110A (en) * 2021-02-26 2021-06-25 滨州职业学院 Detachable shipborne sailing ocean current measuring device
CN115119438A (en) * 2022-05-19 2022-09-27 南京欣网通信科技股份有限公司 An easy-to-install high-performance radio frequency microwave device
CN116930938A (en) * 2023-09-12 2023-10-24 海底鹰深海科技股份有限公司 Doppler measuring instrument and assembling method thereof

Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6098466A (en) * 1998-06-09 2000-08-08 Transonic Systems, Inc. Ultrasonic flow sensor incorporating full flow illumination
US20030076742A1 (en) * 2001-08-28 2003-04-24 Rowe Francis D. Acoustic doppler channel flow measurement device
US20100154561A1 (en) * 2008-12-19 2010-06-24 Ramon Cabrera Integrated Multi-Beam Acoustic Doppler Discharge Measurement System
US20110075518A1 (en) * 2008-12-19 2011-03-31 Craig Huhta Multi-frequency, multi-beam acoustic doppler system
CN105842477A (en) * 2016-03-23 2016-08-10 中国海洋大学 Current surveying method by means of acoustic Doppler current meter
CN107783137A (en) * 2016-08-31 2018-03-09 北京自动化控制设备研究所 A kind of sound Doppler's harmony correlation speed measurement method based on five beam configurations
CN207570541U (en) * 2017-12-05 2018-07-03 山东省科学院海洋仪器仪表研究所 A kind of acoustic wave tide measuring instrument
US20190257930A1 (en) * 2018-02-21 2019-08-22 Rowe Technologies, Inc. Multi frequency piston transducer
CN209296759U (en) * 2018-12-26 2019-08-23 江苏中海达海洋信息技术有限公司 A kind of low-power consumption ADCP flow rate measuring device of built-in GNSS
CN209640370U (en) * 2019-03-20 2019-11-15 杭州瑞利海洋装备有限公司 It is a kind of suitable for underwater self-containing formula and the multipurpose type ADCP of boat-carrying boating type
CN110632347A (en) * 2018-06-22 2019-12-31 中国计量大学 A New Four-beam ADCP Small Calibration Device
CN211426538U (en) * 2020-03-03 2020-09-04 杭州瑞利海洋装备有限公司 Transducer array replaceable five-beam ADCP

Patent Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6098466A (en) * 1998-06-09 2000-08-08 Transonic Systems, Inc. Ultrasonic flow sensor incorporating full flow illumination
US20030076742A1 (en) * 2001-08-28 2003-04-24 Rowe Francis D. Acoustic doppler channel flow measurement device
US20100154561A1 (en) * 2008-12-19 2010-06-24 Ramon Cabrera Integrated Multi-Beam Acoustic Doppler Discharge Measurement System
US20110075518A1 (en) * 2008-12-19 2011-03-31 Craig Huhta Multi-frequency, multi-beam acoustic doppler system
CN105842477A (en) * 2016-03-23 2016-08-10 中国海洋大学 Current surveying method by means of acoustic Doppler current meter
CN107783137A (en) * 2016-08-31 2018-03-09 北京自动化控制设备研究所 A kind of sound Doppler's harmony correlation speed measurement method based on five beam configurations
CN207570541U (en) * 2017-12-05 2018-07-03 山东省科学院海洋仪器仪表研究所 A kind of acoustic wave tide measuring instrument
US20190257930A1 (en) * 2018-02-21 2019-08-22 Rowe Technologies, Inc. Multi frequency piston transducer
CN110632347A (en) * 2018-06-22 2019-12-31 中国计量大学 A New Four-beam ADCP Small Calibration Device
CN209296759U (en) * 2018-12-26 2019-08-23 江苏中海达海洋信息技术有限公司 A kind of low-power consumption ADCP flow rate measuring device of built-in GNSS
CN209640370U (en) * 2019-03-20 2019-11-15 杭州瑞利海洋装备有限公司 It is a kind of suitable for underwater self-containing formula and the multipurpose type ADCP of boat-carrying boating type
CN211426538U (en) * 2020-03-03 2020-09-04 杭州瑞利海洋装备有限公司 Transducer array replaceable five-beam ADCP

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
胡国栋 等: "水利系统首台进口ADCP在长江口成功开发应用对国产ADCP推广应用的启示", 《海洋信息技术与应用》, no. 4, 15 November 2019 (2019-11-15), pages 53 - 59 *

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112162111A (en) * 2020-09-25 2021-01-01 杭州瑞利海洋装备有限公司 Self-contained ADCP (advanced digital control Panel) suitable for deepwater distribution
CN113029110A (en) * 2021-02-26 2021-06-25 滨州职业学院 Detachable shipborne sailing ocean current measuring device
CN115119438A (en) * 2022-05-19 2022-09-27 南京欣网通信科技股份有限公司 An easy-to-install high-performance radio frequency microwave device
CN116930938A (en) * 2023-09-12 2023-10-24 海底鹰深海科技股份有限公司 Doppler measuring instrument and assembling method thereof
CN116930938B (en) * 2023-09-12 2023-11-28 海底鹰深海科技股份有限公司 Doppler measuring instrument and assembling method thereof

Also Published As

Publication number Publication date
CN111190026B (en) 2025-05-09

Similar Documents

Publication Publication Date Title
CN111190026A (en) A five-beam ADCP with replaceable transducer array
CN211426538U (en) Transducer array replaceable five-beam ADCP
CN112964897B (en) Doppler transducer array with asymmetric structure
CN210375302U (en) Differential pressure type accumulator liquid level meter
CN112162111A (en) Self-contained ADCP (advanced digital control Panel) suitable for deepwater distribution
CN209946383U (en) Large depth small doppler log
CN211373815U (en) Vector hydrophone device
CN208043147U (en) A kind of ultrasonic flowmeter of two sound channels
CN220040641U (en) GIS partial discharge detection device
CN220691098U (en) Underwater large-detection-angle ultrasonic ranging sensor
CN210533453U (en) Wireless remote water meter
CN113135276A (en) Depth finder transducer mounting structure and mounting method thereof
CN216283915U (en) Sound velocity measuring device
CN216118019U (en) Medium parameter calibration structure of sonar detection instrument
CN109341660A (en) Universal level-metre
CN215909914U (en) Radar flowmeter of reverse lens mounting structure
CN205221002U (en) Underwater buoy and deep sea are with big dipper satellite communication device
CN212904972U (en) Two-channel acoustic Doppler current profiler transducer sealing structure
CN102006535A (en) Packaging structure for vector hydrophone
CN214930487U (en) Depth finder transducer mounting structure
CN209166415U (en) Universal level-metre
CN210664665U (en) Radar level meter dual-channel structure and radar level meter comprising same
CN207881774U (en) A kind of quadrophonic ultrasonic flowmeter
CN215117271U (en) Five-wave-speed underwater obstacle avoidance sensor
CN210279751U (en) Acoustic positioning main control transducer of submarine detector

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant