CN112748481B - Sounding device based on deep water submerged buoy - Google Patents
Sounding device based on deep water submerged buoy Download PDFInfo
- Publication number
- CN112748481B CN112748481B CN202011524749.8A CN202011524749A CN112748481B CN 112748481 B CN112748481 B CN 112748481B CN 202011524749 A CN202011524749 A CN 202011524749A CN 112748481 B CN112748481 B CN 112748481B
- Authority
- CN
- China
- Prior art keywords
- sounding
- fuse
- fusing
- valve group
- release
- 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.)
- Active
Links
Images
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01W—METEOROLOGY
- G01W1/00—Meteorology
- G01W1/02—Instruments for indicating weather conditions by measuring two or more variables, e.g. humidity, pressure, temperature, cloud cover or wind speed
- G01W1/04—Instruments for indicating weather conditions by measuring two or more variables, e.g. humidity, pressure, temperature, cloud cover or wind speed giving only separate indications of the variables measured
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01W—METEOROLOGY
- G01W1/00—Meteorology
- G01W1/08—Adaptations of balloons, missiles, or aircraft for meteorological purposes; Radiosondes
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
- Y02A90/00—Technologies having an indirect contribution to adaptation to climate change
- Y02A90/30—Assessment of water resources
Landscapes
- Environmental & Geological Engineering (AREA)
- Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Atmospheric Sciences (AREA)
- Biodiversity & Conservation Biology (AREA)
- Ecology (AREA)
- Environmental Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Testing Or Calibration Of Command Recording Devices (AREA)
Abstract
The invention provides a sounding device based on a deepwater submerged buoy, which relates to the technical field of special equipment for ocean surveying and comprises a sounding releasing mechanism and a sounding mechanism; the sounding mechanism comprises a sounding measuring mechanism, a fusing mechanism and an air source mechanism; the sounding measurement mechanism is connected with the air source mechanism through the fusing mechanism and is communicated with the air source mechanism; when the airspace at the position of the deepwater submerged buoy needs to be measured, the air source mechanism is utilized to inflate the sounding measuring mechanism, the fusing mechanism separates the inflated sounding measuring mechanism from the air source mechanism, and the sounding releasing mechanism releases the inflated sounding measuring mechanism so that the inflated sounding measuring mechanism extends out of the water surface and rises to the air; the parameters such as the wind speed, the wind direction, the air temperature and the like of the airspace at the position of the submerged buoy can be measured; the technical problem that the meteorological information of the airspace at the position of the deepwater submerged buoy cannot be synchronously measured on the basis of the deepwater submerged buoy in the prior art is solved.
Description
Technical Field
The invention relates to the technical field of special equipment for ocean surveying, in particular to a sounding device based on a deep water submerged buoy.
Background
The high-altitude meteorological detection is to acquire high-altitude meteorological data through a sonde carried by a sounding balloon; the deep water submerged buoy is a system for observing marine environmental elements below the sea surface for a long time.
The deepwater submerged buoy in the prior art can only obtain underwater data, and when the high altitude weather of the deepwater submerged buoy needs to be known, a ship needs to go out of the sea to discharge sounding balloons, so that the defect of high cost exists; therefore, on the basis of the deepwater submerged buoy, how to synchronously measure the meteorological information of the airspace at the position of the deepwater submerged buoy is an urgent technical problem to be solved.
Disclosure of Invention
The invention aims to provide a sounding device based on a deep water submerged buoy, which aims to solve the technical problem that meteorological information of an airspace at the position of the deep water submerged buoy cannot be synchronously measured on the basis of the deep water submerged buoy in the prior art.
The invention provides a sounding device based on a deepwater submerged buoy, which comprises: a sounding release mechanism and a sounding mechanism;
the sounding mechanism comprises a sounding measuring mechanism, a fusing mechanism and an air source mechanism; the sounding measurement mechanism is arranged inside the sounding release mechanism, the sounding measurement mechanism is connected with the air source mechanism through the fusing mechanism, the sounding measurement mechanism is communicated with the air source mechanism, the air source mechanism is used for inflating the sounding measurement mechanism, the fusing mechanism is used for separating the inflated sounding measurement mechanism from the air source mechanism, and the sounding release mechanism is used for releasing the inflated sounding measurement mechanism so that the inflated sounding measurement mechanism stretches out of the water surface and rises to the air.
In a preferred embodiment of the invention, the sounding measurement mechanism comprises a flight balloon, an inflation tube and a sounding measurement assembly;
the inflation inlet of the flying balloon is connected with the inflation tube, the inflation tube is connected with the air source mechanism through the fusing mechanism, the inflation tube is communicated with the air source mechanism, and the air source mechanism inflates the flying balloon through the inflation tube;
the sounding measurement assembly is connected with the fusing mechanism and ascends to the air along with the flight balloon through the fusing mechanism so as to measure the environmental information of the deep water subsurface buoy position airspace.
In a preferred embodiment of the invention, the sounding measurement assembly comprises a sonde controller, a measurement sensor and a satellite antenna;
the sonde controller is respectively in electrical signal connection with the measuring sensor wire and the fusing mechanism, and is used for controlling the fusing mechanism and the air source mechanism to fall off and separate;
the sonde controller is in electric signal connection with the ground base station through the satellite antenna, the measuring sensor is used for detecting the wind speed, the wind direction and the temperature information of the deep-water submerged buoy position airspace and transmitting the environmental information to the sonde controller, and the sonde controller is used for transmitting the environmental information to the ground base station through the satellite antenna.
In a preferred embodiment of the present invention, the fusing mechanism includes a fusing control mechanism, a fuse assembly, a female plug valve set, a male plug valve set, and an elastic mechanism;
the plug valve group male head is connected with the plug valve group female head, the plug valve group male head is used for opening an inflation channel of the plug valve group female head, the plug valve group female head is communicated with the inflation pipe, and the plug valve group male head is communicated with the air source mechanism;
the fuse assembly is respectively connected with the plug valve group female head and the elastic mechanism, the other end of the elastic mechanism is connected with the plug valve group male head, and the fuse assembly is used for tensioning the elastic mechanism so that the elastic mechanism has an elastic trend of enabling the plug valve group male head to be far away from the plug valve group female head;
the fusing control mechanism is electrically connected with the fuse wire assembly and is used for controlling fusing separation of the fuse wire assembly.
In a preferred embodiment of the present invention, the fuse assembly includes a fuse and a fuse holder;
the both ends of fuse respectively with fusing control mechanism with the elastic mechanism connects, fuse fixer cover is located the outside of the female head of plug valves, just the fuse fixer with the fuse is connected, the fuse fixer is used for fixing the fuse, and is right with tensioning effort is applyed to the elastic mechanism.
In a preferred embodiment of the present invention, the elastic mechanism includes a first fixing ring, a second fixing ring, and a spring;
the male head of plug valves includes first valve train section and second valve train section, first valve train section with second valve train section swing joint, first valve train section with the female first connection of plug valves, first solid fixed ring with first valve train section is connected, the solid fixed ring of second with the second valve train section is connected, the spring is located first solid fixed ring with between the solid fixed ring of second, the fusible link with first solid fixed ring is connected, the spring has the order first valve train section to the elasticity trend that the second valve train section is close to, in order to control first valve train section with the female first separation of plug valves.
In a preferred embodiment of the present invention, a plurality of connecting bolts are disposed on the first fixing ring, the plurality of connecting bolts are uniformly arranged along a circumferential direction of the first valve train section, a plurality of spring fixing bolts are disposed on the second fixing ring, the plurality of spring fixing bolts are uniformly arranged along a circumferential direction of the second valve train section, and the number of the connecting bolts corresponds to the number of the spring fixing bolts one to one;
the springs are arranged in a corresponding manner to the spring fixing bolts, and two ends of each spring are respectively connected with the corresponding connecting bolt and the corresponding spring fixing bolt; the number of the fuse wires is corresponding to the number of the connecting bolts, and each fuse wire is connected with the corresponding connecting bolt.
In a preferred embodiment of the invention, the fuse control mechanism comprises a fuse controller and a fuse battery compartment;
the fuse controller respectively with fuse battery compartment with fuse electrical signal connection, the fuse with fuse battery compartment electricity core is connected, the fuse controller is used for controlling the fuse battery compartment to the fuse provides fusing current, so that fuse fusing separation.
In a preferred embodiment of the present invention, the fusing mechanism further includes a valve block female connector end and a valve block male connector end;
the valve group female head interface end is connected with one end of the plug valve group female head, which is far away from the plug valve group male head, and the plug valve group female head is connected with the inflation tube through the valve group female head interface end;
the valve group male head interface end is connected with one end, far away from the plug valve group female head, of the plug valve group male head, and the plug valve group male head is connected with the air source mechanism through the valve group male head interface end.
In a preferred embodiment of the invention, the air source mechanism comprises an air inflation cylinder, a fixed magnetic block and a floating body;
the floating body is sleeved outside the inflatable gas cylinder, the inflatable gas cylinder is connected with the fusing mechanism through the fixed magnetic block, the fixed magnetic block is connected with the sounding releasing mechanism, and the sounding releasing mechanism is used for adjusting the communication or closing of the inflatable gas cylinder and the fusing mechanism through the fixed magnetic block.
In a preferred embodiment of the present invention, the sounding release mechanism includes a mounting frame, a release controller, a release solenoid valve, and a release battery compartment;
the release controller with release battery compartment install respectively in on the installation frame, be provided with a plurality of mounting bases on the installation frame, the quantity of release solenoid valve with mounting base's quantity one-to-one, every mounting base corresponds and has arranged one sounding mechanism and one release solenoid valve, shown release battery compartment respectively with release controller with release solenoid valve electric connection, release controller with release solenoid valve electric signal connection, release solenoid valve with fixed magnetic path is connected, release controller is used for through release solenoid valve adjusts the position of fixed magnetic path, in order to control gas filled gas cylinder with fuse mechanism's intercommunication or close.
The invention provides a sounding device based on a deepwater submerged buoy, which comprises: a sounding release mechanism and a sounding mechanism; the sounding mechanism comprises a sounding measuring mechanism, a fusing mechanism and an air source mechanism; the sounding measurement mechanism is arranged inside the sounding release mechanism and is connected with the air source mechanism through the fusing mechanism, and the sounding measurement mechanism is communicated with the air source mechanism; when the airspace at the position of the deep-water submerged buoy needs to be measured, the air source mechanism is utilized to inflate the sounding measuring mechanism, at the moment, the fusing mechanism can separate the inflated sounding measuring mechanism from the air source mechanism, and the sounding releasing mechanism releases the inflated sounding measuring mechanism so that the inflated sounding measuring mechanism extends out of the water surface and rises into the air; the method can realize long-time measurement of parameters such as wind speed, wind direction and air temperature of the airspace at the position of the submerged buoy, so that researchers can obtain more complete scientific research data; the technical problem that the meteorological information of the airspace at the position of the deepwater submerged buoy can not be synchronously measured on the basis of the deepwater submerged buoy in the prior art is solved.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the embodiments or the prior art descriptions will be briefly described below, and it is obvious that the drawings in the following description are some embodiments of the present invention, and other drawings can be obtained by those skilled in the art without creative efforts.
Fig. 1 is a schematic overall structure diagram of a sounding device based on a deep water submerged buoy provided by an embodiment of the invention;
fig. 2 is a schematic structural diagram of a sounding mechanism of a sounding device based on a deep water submerged buoy located in a sounding release mechanism according to an embodiment of the present invention;
fig. 3 is a schematic structural diagram of a sounding mechanism of a sounding device based on a deep water submerged buoy provided by an embodiment of the invention;
fig. 4 is a schematic structural diagram of a fusing mechanism and a sounding measuring mechanism of a sounding device based on a deep water submerged buoy provided by an embodiment of the invention;
fig. 5 is a schematic structural diagram of a fusing mechanism of a sounding device based on a deep water submerged buoy provided by an embodiment of the invention;
fig. 6 is a schematic structural diagram of a sounding release mechanism of a sounding device based on a deep water submerged buoy provided by an embodiment of the invention;
fig. 7 is a schematic structural diagram of a inflated flight balloon of a sounding measurement mechanism of a sounding device based on a deep water submerged buoy provided by an embodiment of the invention;
fig. 8 is a schematic structural diagram of a fusing mechanism of the sounding device based on the deep water submerged buoy after fusing, according to the embodiment of the present invention;
fig. 9 is a schematic structural diagram of a flying balloon of the sounding device based on the deep water submerged buoy provided by the embodiment of the invention after rising.
Icon: 100-a sounding release mechanism; 101-a mounting frame; 111-a mounting base; 102-a release controller; 103-release electromagnetic valve; 104-releasing the battery compartment; 200-a sounding mechanism; 300-a sounding measurement mechanism; 301-a flying balloon; 302-a gas-filled tube; 303-sounding measurement assembly; 313-sonde controller; 323-a measurement sensor; 333-satellite antenna; 400-a fusing mechanism; 401-a fusing control mechanism; 411-a fuse controller; 421-fuse battery compartment; 402-a fuse assembly; 412-fuse; 422-fuse holder; 403-plugging a valve group female head; 404-plugging a valve group male head; 414 — first valve train section; 424-second valve train section; 405-a resilient mechanism; 415-a first retaining ring; 425-a second retaining ring; 435-a spring; 445-connecting bolts; 455-spring set bolt; 406-a valve block female interface end; 407-valve bank male interface end; 500-an air supply mechanism; 501-an inflatable gas cylinder; 502-fixed magnetic block; 503-floating body.
Detailed Description
The technical solutions of the present invention will be described clearly and completely with reference to the following embodiments, and it should be understood that the described embodiments are some, but not all, embodiments of the present invention. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
As shown in fig. 1 to 9, the present embodiment provides a sounding device based on a deep water submerged buoy, including: a sounding release mechanism 100 and a sounding mechanism 200; the sounding mechanism 200 comprises a sounding measurement mechanism 300, a fusing mechanism 400 and a gas source mechanism 500; sounding measurement mechanism 300 sets up inside sounding release mechanism 100, sounding measurement mechanism 300 is connected with air supply mechanism 500 through fusing mechanism 400, and sounding measurement mechanism 300 and air supply mechanism 500 intercommunication, air supply mechanism 500 is used for aerifing sounding measurement mechanism 300, fusing mechanism 400 is used for separating the sounding measurement mechanism 300 after aerifing from air supply mechanism 500, sounding release mechanism 100 is used for releasing the sounding measurement mechanism 300 after aerifing to make the sounding measurement mechanism 300 after aerifing stretch out the surface of water and rise to aloft.
It should be noted that, the sounding device based on the deep water submersible buoy provided in this embodiment can be located under deep water, when a space domain where the deep water submersible buoy is located needs to be subjected to meteorological detection, the sounding measuring mechanism 300 may be inflated by using the air source mechanism 500, after the sounding measuring mechanism 300 is inflated, the air source mechanism 500 and the sounding measuring mechanism 300 are separated by using the fusing mechanism 400, and the sounding measuring mechanism 300 has a normally closed valve, so that it is ensured that gas in the sounding measuring mechanism 300 does not leak, at this time, the inflated sounding measuring mechanism 300 is released by using the sounding releasing mechanism 100, and the sounding measuring mechanism 300 floats out of the water surface under the action of the gas until the sounding measuring mechanism rises to the air.
The sounding device based on the deepwater submerged buoy provided by the embodiment comprises: a sounding release mechanism 100 and a sounding mechanism 200; the sounding mechanism 200 comprises a sounding measurement mechanism 300, a fusing mechanism 400 and a gas source mechanism 500; the sounding measurement mechanism 300 is arranged inside the sounding release mechanism 100, the sounding measurement mechanism 300 is connected with the air source mechanism 500 through the fusing mechanism 400, and the sounding measurement mechanism 300 is communicated with the air source mechanism 500; when the airspace at the position of the deepwater submerged buoy needs to be measured, the air source mechanism 500 is used for inflating the sounding measuring mechanism 300, at the moment, the fusing mechanism 400 can separate the inflated sounding measuring mechanism 300 from the air source mechanism 500, and the sounding releasing mechanism 100 releases the inflated sounding measuring mechanism 300, so that the inflated sounding measuring mechanism 300 extends out of the water surface and rises into the air; the method can realize long-time measurement of parameters such as wind speed, wind direction and air temperature of the airspace at the position of the submerged buoy, so that researchers can obtain more complete scientific research data; the technical problem that the meteorological information of the airspace at the position of the deepwater submerged buoy cannot be synchronously measured on the basis of the deepwater submerged buoy in the prior art is solved.
On the basis of the above embodiment, further, in the preferred embodiment of the present invention, the sounding measurement mechanism 300 includes a flight balloon 301, an inflation tube 302 and a sounding measurement assembly 303; an inflation port of the flying balloon 301 is connected with an inflation tube 302, the inflation tube 302 is connected with an air source mechanism 500 through a fusing mechanism 400, the inflation tube 302 is communicated with the air source mechanism 500, and the air source mechanism 500 inflates the flying balloon 301 through the inflation tube 302; the sounding measurement assembly 303 is connected with the fusing mechanism 400, and the sounding measurement assembly 303 ascends to the air along with the flying balloon 301 through the fusing mechanism 400 so as to measure the environmental information of the deep water subsurface buoy position airspace.
In this embodiment, the inflation tube 302 is an inflation hose, and when the inflation hose is not used for inflating the flying balloon 301, the inflation hose can be coiled inside the sounding release mechanism 100, the inflation tube 302 is connected with the flying balloon 301 through an armor, the sounding measurement assembly 303 is connected with the inflation tube 302 through the fuse mechanism 400, and when the fuse mechanism 400 is fused and separated, the sounding measurement assembly 303 is connected with the inflation tube 302 along with the fused part of the fuse mechanism 400 and ascends into the air along with the flying balloon 301.
In the preferred embodiment of the present invention, the sounding measurement assembly 303 includes a sonde controller 313, a measurement sensor 323, and a satellite antenna 333; the sonde controller 313 is respectively in electrical signal connection with the measuring sensor 323 line and the fusing mechanism 400, and the sonde controller 313 is used for controlling the fusing mechanism 400 and the air source mechanism 500 to fall off and separate; the sonde controller 313 is in electrical signal connection with a ground base station through a satellite antenna 333, the measuring sensor 323 is used for detecting wind speed, wind direction and temperature information of an airspace at the deep-water submerged buoy position and transmitting the environment information to the sonde controller 313, and the sonde controller 313 is used for transmitting the environment information to the ground base station through the satellite antenna 333.
In this embodiment, the measurement sensor 323 may include a wind speed sensor, a wind direction sensor, and a temperature sensor, and the different types of measurement sensors 323 are respectively used to detect the environment of the air space, and transmit the detected environment information to the sonde controller 313, and the sonde controller 313 transmits the detected environment information in the air space to the ground base by using the signal transmission of the satellite antenna 333.
In addition, since the satellite antenna 333 has a signal transmission function, the sonde controller 313 can receive a control signal of the ground base by using the satellite antenna 333, when the sonde controller 313 receives a ground base release instruction, the sonde controller 313 transmits the control signal to the fuse mechanism 400, and after the air supply mechanism 500 completes inflation of the flying balloon 301, the fuse mechanism 400 separates the sounding measurement component 303 from the air supply mechanism 500 by using a self-fusing manner.
In the preferred embodiment of the present invention, the fuse mechanism 400 includes a fuse control mechanism 401, a fuse assembly 402, a female valve block connector 403, a male valve block connector 404, and an elastic mechanism 405; the plug valve group male head 404 is connected with the plug valve group female head 403, the plug valve group male head 404 is used for opening an inflation channel of the plug valve group female head 403, the plug valve group female head 403 is communicated with the inflation tube 302, and the plug valve group male head 404 is communicated with the air source mechanism 500; the fuse component 402 is respectively connected with the plug valve group female head 403 and the elastic mechanism 405, the other end of the elastic mechanism 405 is connected with the plug valve group male head 404, and the fuse component 402 is used for tensioning the elastic mechanism 405, so that the elastic mechanism 405 has an elastic tendency of enabling the plug valve group male head 404 to be far away from the plug valve group female head 403; the fuse control mechanism 401 is electrically connected to the fuse element 402, and the fuse control mechanism 401 is used for controlling the fuse element 402 to fuse and separate.
In this embodiment, the male plug valve group head 404 and the female plug valve group head 403 are connected to form a quick release joint, wherein when the male plug valve group head 404 and the female plug valve group head 403 are combined, the female plug valve group head 403 is in a normally open state, so that the whole inflation process can be completed; when the male plug valve block head 404 is separated from the female plug valve block head 403, the female plug valve block head 403 is in a normally closed state, so that the gas leakage in the flying balloon 301 is prevented by the female plug valve block head 403.
In the preferred embodiment of the present invention, the fuse assembly 402 includes a fuse 412 and a fuse holder 422; both ends of the fuse 412 are respectively connected with the fusing control mechanism 401 and the elastic mechanism 405, the fuse holder 422 is sleeved outside the plug-in valve set female head 403, the fuse holder 422 is connected with the fuse 412, and the fuse holder 422 is used for fixing the fuse 412 so as to apply a tensioning action force to the elastic mechanism 405.
In the preferred embodiment of the present invention, the fusing control mechanism 401 includes a fusing controller 411 and a fuse battery compartment 421; fusing controller 411 is connected with fuse battery compartment 421 and fuse 412 electrical signal respectively, and fuse 412 is connected with fuse battery compartment 421 electricity core, and fusing controller 411 is used for controlling fuse battery compartment 421 to provide fusing current for fuse 412 to make fuse 412 fuse separation.
In this embodiment, the fuse 412 can pass through the fuse controller 411, the fuse controller 411 is welded and fixed at the center of the fuse 412, the connection between the fuse 412 and the fuse controller 411 is realized, the lengths of the fuses 412 on both sides of the fuse controller 411 are substantially the same, the fuse controller 411 is installed on the fuse battery compartment 421, and the fuses 412 are symmetrically distributed on both sides of the fuse battery compartment 421 after installation; the fuse battery compartment 421 can provide the fusing current of the fuse 412, and the fuse battery compartment 421 can also provide the electric quantity for the sounding measurement assembly 303; when the fuse 412 is fused and separated, the fusing controller 411, the fuse battery compartment 421 and the plug valve group female head 403 rise together with the flying balloon 301 to the air.
In the preferred embodiment of the present invention, the resilient mechanism 405 includes a first stationary ring 415, a second stationary ring 425, and a spring 435; plug valves public head 404 includes first valve train section 414 and second valve train section 424, first valve train section 414 and second valve train section 424 swing joint, first valve train section 414 is connected with plug valves female head 403, first fixed ring 415 is connected with first valve train section 414, second fixed ring 425 is connected with second valve train section 424, spring 435 is located between first fixed ring 415 and the second fixed ring 425, fuse 412 is connected with first fixed ring 415, spring 435 has the elasticity trend that makes first valve train section 414 be close to second valve train section 424 to control first valve train section 414 and plug valves female head 403 separation.
In a preferred embodiment of the present invention, the first fixing ring 415 is provided with a plurality of connecting bolts 445, the plurality of connecting bolts 445 are uniformly arranged along the circumferential direction of the first valve group section 414, the second fixing ring 425 is provided with a plurality of spring fixing bolts 455, the plurality of spring fixing bolts 455 are uniformly arranged along the circumferential direction of the second valve group section 424, and the number of the connecting bolts 445 corresponds to the number of the spring fixing bolts 455 one by one; the number of the springs 435 and the number of the spring fixing bolts 455 are correspondingly set, and two ends of each spring 435 are respectively connected with the corresponding connecting bolt 445 and the spring fixing bolt 455; the number of the fusible links 412 is set corresponding to the number of the connecting bolts 445, and each fusible link 412 is connected to the corresponding connecting bolt 445.
In this embodiment, the first fixing ring 415 can fasten and fix the first valve group section 414 of the male plug valve group head 404, and when the first valve group section 414 is connected to the female plug valve group head 403, the first fixing ring 415 can separate the first valve group section 414 and the second valve group section 424 by a certain distance, and a sealed inflation channel exists between the first valve group section 414 and the second valve group end; the first fixing ring 415 and the second fixing ring 425 are connected through a spring 435, the fuse wire 412 is connected with a connecting bolt 445 on the first fixing ring 415, the spring 435 is in a tensioning state at the moment, and the relative position of the second fixing ring 425 and the second valve group section 424 is fixed, so that after the fuse wire 412 is fused, the plug valve group female head 403 is separated from the first valve group section 414 at the moment, the first valve group section 414 is close to the second valve group section 424 under the resilience acting force of the spring 435, and the plug valve group male head 404 and the plug valve group female head 403 are fused and separated.
Alternatively, four connecting bolts 445 may be provided along the circumferential direction of the first valve train section 414, and the four connecting bolts 445 are respectively located at four corners of the first fixing ring 415, that is, the number of the fusible links 412, the springs 435, and the spring fixing bolts 455 is also four.
In the preferred embodiment of the present invention, the fusing mechanism 400 further includes a valve block female interface end 406 and a valve block male interface end 407; the valve group female connector end 406 is connected with one end of the plug valve group female connector 403 far away from the plug valve group male connector 404, and the plug valve group female connector 403 is connected with the inflation tube 302 through the valve group female connector end 406; the valve block male connector port 407 is connected to an end of the plug valve block male connector 404 away from the plug valve block female connector 403, and the plug valve block male connector 404 is connected to the air source mechanism 500 through the valve block male connector port 407.
In this embodiment, the valve block female connector end 406 can be in an armored connection with the air charging pipe 302, and the valve block male connector end 407 can be in an armored connection with a channel formed by the fixed magnetic block 502 of the air supply mechanism 500.
In the preferred embodiment of the present invention, the air source mechanism 500 comprises an air cylinder 501, a fixed magnetic block 502 and a floating body 503; the floating body 503 is sleeved outside the gas-filled cylinder 501, the gas-filled cylinder 501 is connected with the fusing mechanism 400 through the fixed magnetic block 502, the fixed magnetic block 502 is connected with the air detection releasing mechanism 100, and the air detection releasing mechanism 100 is used for adjusting the communication or closing of the gas-filled cylinder 501 and the fusing mechanism 400 through the fixed magnetic block 502.
In this embodiment, gas is filled in the gas cylinder 501, the fixed magnetic block 502 is used as a channel switch of the gas cylinder 501, the fixed magnetic block 502 is in a normally closed state in a normal state, and when the sounding release mechanism 100 opens the release solenoid valve 103, the release solenoid valve 103 is used to control the fixed magnetic block 502 to open the gas channel between the gas cylinder 501 and the valve set male connector port 407, so that the gas in the gas cylinder 501 enters the flying balloon 301 through the fusing mechanism 400 and the gas tube 302.
Optionally, the floating body 503 is sleeved at the middle position of the gas-filled cylinder 501, and the floating body 503 can ensure the buoyancy of the gas-filled cylinder 501 and the sounding release mechanism 100 under water; specifically, when the sounding release mechanism 100 and the sounding mechanism 200 are located underwater, the sounding release mechanism 100 is located below the gas cylinder 501, and the gas cylinder 501 provides buoyancy under water for the whole structure by using the buoyancy of the floating body 503.
In the preferred embodiment of the present invention, the sounding release mechanism 100 includes a mounting frame 101, a release controller 102, a release solenoid valve 103, and a release battery compartment 104; the release controller 102 and the release battery compartment 104 are respectively mounted on the mounting frame 101, a plurality of mounting bases 111 are arranged on the mounting frame 101, the number of the release electromagnetic valves 103 corresponds to the number of the mounting bases 111 one by one, each mounting base 111 is correspondingly provided with one sounding mechanism 200 and one release electromagnetic valve 103, the release battery compartment 104 is respectively electrically connected with the release controller 102 and the release electromagnetic valves 103, the release controller 102 is in electrical signal connection with the release electromagnetic valves 103, the release electromagnetic valves 103 are connected with the fixed magnetic blocks 502, and the release controller 102 is used for adjusting the positions of the fixed magnetic blocks 502 through the release electromagnetic valves 103 to control the communication or the closing of the gas-filled gas cylinder 501 and the fusing mechanism 400.
In this embodiment, the release controller 102 may be installed at a side of the installation frame 101, and the installation base 111 and the release solenoid valve 103 constitute a release actuator, wherein the installation frame 101 may have a square structure or a rectangular structure, the bottom of the installation base 111 may be provided with a water drainage through hole, and the release battery compartment 104 may be installed on the installation frame 101 in a sealing connection manner.
Alternatively, the sonde controller 313, the fuse controller 411 and the release controller 102 may be respectively of various types, such as: an MCU, a computer, a PLC controller, etc., preferably, the sonde controller 313, the fusing controller 411 and the release controller 102 may be an MCU. A Micro Control Unit (MCU), also called a single-chip microcomputer or a single-chip microcomputer, is a computer that properly reduces the frequency and specification of a central processing Unit, and integrates peripheral interfaces such as a memory, a counter, a USB, an a/D conversion, a UART, a PLC, a DMA, and the like, even an LCD driving circuit, on a single chip to form a chip-level computer, which is used for different combined control in different application occasions.
Preferably, the sonde controller 313, the fusing controller 411 and the release controller 102 can all adopt STM32F103C8T6 single-chip microcomputers which are high in processing capacity, rich in internal resources and stable in operation.
The assembly use method in the embodiment comprises the following steps: assembling the fusing mechanism 400, firstly, enabling a fuse wire 412 to penetrate through the fusing controller 411, fixedly welding the fusing controller 411 at the center of the fuse wire 412, enabling the lengths of the fuse wires 412 on two sides of the fusing controller 411 to be approximately the same, then, installing the fusing controller 411 on a fuse battery compartment 421, and after installation, symmetrically distributing the fuse wires 412 on two sides of the fuse battery compartment 421; the fuse 412 penetrates through an inner hole of the fuse holder 422, and the fuse 412 is fixed, so that the fuse battery compartment 421 is mounted on the plug valve bank female head 403; butting the male plug valve group head 404 with the female plug valve group head 403 to form a quick-release connector, and pushing and pulling the first fixing ring 415 upwards to lock the quick-release connector; the fuse holder 422 fixes the fuse 412, and then connects the female plug valve block head 403 with the male plug valve block head 404, the first fixing ring 415 is in the locking position, and then the fuse 412 is fixed on the connecting bolt 445 on the first fixing ring 415, and the fuse assembly is completed. Further, the sonde controller 313, the measurement sensor 323 and the satellite antenna 333 are installed on the fusing mechanism 400, and the installation of the sonde measurement component 303 is completed; then, connecting the interface end 407 of the valve group male head with a fixed magnetic block 502, connecting the fixed magnetic block 502 with an inflatable gas cylinder 501, and then installing a floating body 503 outside the inflatable gas cylinder 501; one end of an air inflation tube 302 is connected with a valve bank female connector end 406, and the other end of the air inflation tube is connected with a flying balloon 301; after the assembly of a single sonde is completed, a plurality of sets of sonde mechanisms 200 are repeatedly assembled.
For the assembly of the sounding release mechanism 100, the release controller 102 is first mounted on the mounting frame 101, and then the release battery compartment 104 is mounted on the mounting frame 101; the release solenoid valves 103 are mounted on the mounting bases 111 of the mounting frame 101, and the mounting of the plurality of release solenoid valves 103 on the plurality of mounting bases 111 is completed in sequence, and the sounding release mechanism 100 is completed.
And (3) integral assembly test: firstly, the flying balloon 301 of one sounding mechanism 200 is placed into the mounting base 111 of the sounding release mechanism 100, then the gas filled tube 302 is placed into the mounting base 111 of the sounding release mechanism 100, then the fusing mechanism 400 is placed into the mounting base 111 of the sounding release mechanism 100, after the placement is completed, the fixed magnetic block 502 of the sounding mechanism 200 is aligned with the release electromagnetic valve 103 of the mounting base 111, the installation of a plurality of sounding mechanisms 200 is completed in sequence, and the whole system assembly is completed.
Finally, it should be noted that: the above embodiments are only used to illustrate the technical solution of the present invention, and not to limit the same; while the invention has been described in detail and with reference to the foregoing embodiments, it will be understood by those skilled in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some or all of the technical features may be equivalently replaced; and the modifications or the substitutions do not make the essence of the corresponding technical solutions depart from the scope of the technical solutions of the embodiments of the present invention.
Claims (9)
1. A sounding device based on a deepwater submerged buoy is characterized by comprising: a sounding release mechanism and a sounding mechanism;
the sounding mechanism comprises a sounding measuring mechanism, a fusing mechanism and an air source mechanism; the sounding measurement mechanism is arranged inside the sounding release mechanism, the sounding measurement mechanism is connected with the air source mechanism through the fusing mechanism, the sounding measurement mechanism is communicated with the air source mechanism, the air source mechanism is used for inflating the sounding measurement mechanism, the fusing mechanism is used for separating the inflated sounding measurement mechanism from the air source mechanism, and the sounding release mechanism is used for releasing the inflated sounding measurement mechanism so that the inflated sounding measurement mechanism extends out of the water surface and rises into the air;
the sounding measurement mechanism comprises an inflation tube; the inflation tube is connected with the air source mechanism through the fusing mechanism, and is communicated with the air source mechanism;
the fusing mechanism comprises a fusing control mechanism, a fusing wire assembly, a plug valve group female head, a plug valve group male head and an elastic mechanism; the plug valve group male head is connected with the plug valve group female head, the plug valve group male head is used for opening an inflation channel of the plug valve group female head, the plug valve group female head is communicated with the inflation pipe, and the plug valve group male head is communicated with the air source mechanism; the fuse assembly is respectively connected with the plug valve group female head and the elastic mechanism, the other end of the elastic mechanism is connected with the plug valve group male head, and the fuse assembly is used for tensioning the elastic mechanism so that the elastic mechanism has an elastic trend of enabling the plug valve group male head to be far away from the plug valve group female head; the fusing control mechanism is electrically connected with the fuse wire assembly and is used for controlling fusing separation of the fuse wire assembly;
the fuse wire assembly comprises a fuse wire, and two ends of the fuse wire are respectively connected with the fusing control mechanism and the elastic mechanism;
the elastic mechanism comprises a first fixing ring, a second fixing ring and a spring; the male head of plug valves includes first valve train section and second valve train section, first valve train section with second valve train section swing joint, first valve train section with the female first connection of plug valves, first solid fixed ring with first valve train section connection, the solid fixed ring of second with the second valve train section connection, the spring is located first solid fixed ring with between the solid fixed ring of second, the fuse with first solid fixed ring is connected, the spring has the order first valve train section to the elasticity trend that the second valve train section is close to, in order to control first valve train section with the female first separation of plug valves.
2. The deep water submersible buoy-based sounding device of claim 1, wherein the sounding measurement mechanism further comprises a flight balloon and a sounding measurement assembly;
the inflation port of the flying balloon is connected with the inflation tube, and the air source mechanism inflates the flying balloon through the inflation tube;
the sounding measurement assembly is connected with the fusing mechanism and ascends to the air along with the flight balloon through the fusing mechanism so as to measure the environmental information of the deep water subsurface buoy position airspace.
3. The deep water submersible buoy-based sounding device of claim 2, wherein the sounding measurement assembly comprises a sonde controller, a measurement sensor and a satellite antenna;
the sonde controller is respectively in electrical signal connection with the measuring sensor wire and the fusing mechanism and is used for controlling the fusing mechanism and the air source mechanism to fall off and separate;
the sonde controller is in electric signal connection with the ground base station through the satellite antenna, the measuring sensor is used for detecting the wind speed, the wind direction and the temperature information of the deep-water submerged buoy position airspace and transmitting the environmental information to the sonde controller, and the sonde controller is used for transmitting the environmental information to the ground base station through the satellite antenna.
4. The deepwater-based buoy sounding device as recited in claim 3, wherein the fusible link assembly further comprises a fusible link holder;
the fuse wire fixer is sleeved outside the plug valve group female head, the fuse wire fixer is connected with the fuse wire, and the fuse wire fixer is used for fixing the fuse wire so as to apply tensioning acting force to the elastic mechanism.
5. The deepwater-based underwater buoy detection device as claimed in claim 4, wherein a plurality of connection bolts are arranged on the first fixing ring, the plurality of connection bolts are uniformly arranged along the circumferential direction of the first valve train section, a plurality of spring fixing bolts are arranged on the second fixing ring, the plurality of spring fixing bolts are uniformly arranged along the circumferential direction of the second valve train section, and the number of the connection bolts corresponds to the number of the spring fixing bolts one to one;
the springs are arranged in a corresponding number with the spring fixing bolts, and two ends of each spring are respectively connected with the corresponding connecting bolt and the corresponding spring fixing bolt; the number of the fuses corresponds to the number of the connecting bolts, and each fuse is connected with the corresponding connecting bolt.
6. The deepwater-based buoy sounding device as recited in claim 5, wherein the fuse control mechanism comprises a fuse controller and a fuse battery compartment;
the fuse controller is respectively connected with the fuse battery bin and the fuse wire through electric signals, the fuse wire is connected with the fuse battery bin electric core, and the fuse controller is used for controlling the fuse battery bin to provide fusing current for the fuse wire so as to fuse and separate the fuse wire.
7. The deepwater-based buoy sounding device as recited in claim 3, wherein the fusing mechanism further comprises a valve block female interface end and a valve block male interface end;
the valve group female head interface end is connected with one end of the plug valve group female head, which is far away from the plug valve group male head, and the plug valve group female head is connected with the inflation tube through the valve group female head interface end;
the valve group male head interface end is connected with one end, far away from the plug valve group female head, of the plug valve group male head, and the plug valve group male head is connected with the air source mechanism through the valve group male head interface end.
8. The sounding device based on deep water submerged buoy of any one of claims 1 to 7, characterized in that the gas source mechanism comprises a gas-filled cylinder, a fixed magnetic block and a floating body;
the floating body is sleeved outside the inflatable gas cylinder, the inflatable gas cylinder is connected with the fusing mechanism through the fixed magnetic block, the fixed magnetic block is connected with the sounding releasing mechanism, and the sounding releasing mechanism is used for adjusting the communication or closing of the inflatable gas cylinder and the fusing mechanism through the fixed magnetic block.
9. The deepwater-based underwater buoy detection device of claim 8, wherein the sounding release mechanism comprises a mounting frame, a release controller, a release solenoid valve and a release battery compartment;
the release controller and the release battery compartment are respectively installed on the installation frame, a plurality of installation bases are arranged on the installation frame, the number of the release electromagnetic valves corresponds to the number of the installation bases one by one, each installation base is correspondingly provided with one sounding mechanism and one release electromagnetic valve, the release battery compartment is respectively electrically connected with the release controller and the release electromagnetic valves, the release controller is in electrical signal connection with the release electromagnetic valves, the release electromagnetic valves are connected with the fixed magnetic blocks, and the release controller is used for adjusting the positions of the fixed magnetic blocks through the release electromagnetic valves so as to control the communication or closing of the gas charging cylinder and the fusing mechanism.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011524749.8A CN112748481B (en) | 2020-12-22 | 2020-12-22 | Sounding device based on deep water submerged buoy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011524749.8A CN112748481B (en) | 2020-12-22 | 2020-12-22 | Sounding device based on deep water submerged buoy |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN112748481A CN112748481A (en) | 2021-05-04 |
| CN112748481B true CN112748481B (en) | 2022-10-25 |
Family
ID=75648202
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011524749.8A Active CN112748481B (en) | 2020-12-22 | 2020-12-22 | Sounding device based on deep water submerged buoy |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112748481B (en) |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2015196098A1 (en) * | 2014-06-20 | 2015-12-23 | Lockheed Martin Corporation | Inflatable radar signal device |
| CN108919383A (en) * | 2018-06-08 | 2018-11-30 | 中国气象局气象探测中心 | The small-sized automatic sounder of one kind and its control system, method |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2000111658A (en) * | 1998-10-06 | 2000-04-21 | Churyo Eng Kk | Ejector of meterologtical sonde |
| CN108337052B (en) * | 2017-12-29 | 2021-09-24 | 中国船舶重工集团公司第七一0研究所 | Communication transmission device using optical communication and having fusing release function |
| CN108845377A (en) * | 2018-06-19 | 2018-11-20 | 北京无线电测量研究所 | A kind of miniaturization is automatic to put ball system |
| CN109297803B (en) * | 2018-10-24 | 2019-12-10 | 中国海洋大学 | Submarine sediment mechanical property measuring system suitable for full sea depth |
| CN110308499B (en) * | 2019-06-26 | 2023-12-12 | 中国科学院大气物理研究所 | Recoverable multiplexing lifting double-pass effective measurement weather sounding device |
| CN210666072U (en) * | 2019-09-02 | 2020-06-02 | 山东省科学院海洋仪器仪表研究所 | Automatic sounding balloon releasing system for buoy |
| CN211791511U (en) * | 2020-04-17 | 2020-10-27 | 青岛海洋地质研究所 | Timing communication device suitable for deep sea in-situ measurement system |
-
2020
- 2020-12-22 CN CN202011524749.8A patent/CN112748481B/en active Active
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2015196098A1 (en) * | 2014-06-20 | 2015-12-23 | Lockheed Martin Corporation | Inflatable radar signal device |
| CN108919383A (en) * | 2018-06-08 | 2018-11-30 | 中国气象局气象探测中心 | The small-sized automatic sounder of one kind and its control system, method |
Also Published As
| Publication number | Publication date |
|---|---|
| CN112748481A (en) | 2021-05-04 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US9254892B2 (en) | Fixation releasing device | |
| CA2845265C (en) | Communication buoy and method of deployment | |
| CN102981185B (en) | three-component magnetic field and three-component electric field marine electromagnetic data acquisition station | |
| CN103342153B (en) | A kind of sounding buoy of spilled-oil tracking under water system of tracking and early warning semi-submersible oil | |
| CN112748481B (en) | Sounding device based on deep water submerged buoy | |
| CN106125144A (en) | A kind of small-sized seabed controllable source electromagnetism acquisition station | |
| US9511506B2 (en) | Fusion cutting device | |
| CN103454682A (en) | Control device for positioning an instrumented cable provided with buoyancy means for retrieving the control device and instrumented cable from submerged positioning | |
| CN105334408B (en) | A kind of device of autonomous detection deep-sea watertight performance of connector | |
| CN104764444A (en) | Real-time monitoring instrument of submersible type profile ocean-current meter and use method thereof | |
| CN206954454U (en) | A kind of buoy for being easy to positioning to find | |
| RU2645427C2 (en) | Depth-activated sensor switch and method of switching it off | |
| CN209776742U (en) | A strong anchor system flotation pontoon of stability for measuring marine hydrological meteorological | |
| CN114889827A (en) | Throwing type black box emergency device | |
| CN220894555U (en) | Underwater mounting type dam piping detection and acquisition device | |
| TWM530407U (en) | Buoy structure improvement of marine meteorological observation operation | |
| CN218198827U (en) | Prevent sinking survey unmanned aerial vehicle device | |
| CN216035161U (en) | Many rotor unmanned aerial vehicle weight aircraft flotation device | |
| US20230323993A1 (en) | Marine breakaway couplings | |
| CN218647153U (en) | Underwater Beidou optical beacon machine | |
| CN216668708U (en) | High-reliability ocean turbulence sensor packaging module | |
| CN219737456U (en) | Oily thing detection device and waters monitoring system | |
| CN113277043B (en) | Positioning device and underwater equipment | |
| WO2024067991A1 (en) | Submarine power cable arrangement for an offshore structure | |
| CA2234285A1 (en) | Drifting datum marker buoy |
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 |