CN113686315A - A sealed cabin for wave glider communication system - Google Patents
A sealed cabin for wave glider communication system Download PDFInfo
- Publication number
- CN113686315A CN113686315A CN202110840519.0A CN202110840519A CN113686315A CN 113686315 A CN113686315 A CN 113686315A CN 202110840519 A CN202110840519 A CN 202110840519A CN 113686315 A CN113686315 A CN 113686315A
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- sealing
- sealed cabin
- ais
- antenna
- vacuum
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- 238000004891 communication Methods 0.000 title claims abstract description 48
- 238000007789 sealing Methods 0.000 claims abstract description 123
- 238000001514 detection method Methods 0.000 claims abstract description 18
- 229910052741 iridium Inorganic materials 0.000 claims abstract description 15
- GKOZUEZYRPOHIO-UHFFFAOYSA-N iridium atom Chemical compound [Ir] GKOZUEZYRPOHIO-UHFFFAOYSA-N 0.000 claims abstract description 15
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 5
- 238000012360 testing method Methods 0.000 claims description 6
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 2
- 239000004917 carbon fiber Substances 0.000 claims description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 2
- 239000002775 capsule Substances 0.000 claims 2
- 238000009434 installation Methods 0.000 abstract description 8
- 238000012544 monitoring process Methods 0.000 abstract description 2
- 230000006870 function Effects 0.000 description 16
- 230000007774 longterm Effects 0.000 description 4
- 238000001125 extrusion Methods 0.000 description 3
- 238000013480 data collection Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 210000004556 brain Anatomy 0.000 description 1
- 108010066057 cabin-1 Proteins 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008092 positive effect Effects 0.000 description 1
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Classifications
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C13/00—Surveying specially adapted to open water, e.g. sea, lake, river or canal
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B22/00—Buoys
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B35/00—Vessels or similar floating structures specially adapted for specific purposes and not otherwise provided for
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M3/00—Investigating fluid-tightness of structures
- G01M3/02—Investigating fluid-tightness of structures by using fluid or vacuum
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO 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
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/13—Receivers
- G01S19/14—Receivers specially adapted for specific applications
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/27—Adaptation for use in or on movable bodies
- H01Q1/34—Adaptation for use in or on ships, submarines, buoys or torpedoes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B35/00—Vessels or similar floating structures specially adapted for specific purposes and not otherwise provided for
- B63B2035/006—Unmanned surface vessels, e.g. remotely controlled
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Remote Sensing (AREA)
- Radar, Positioning & Navigation (AREA)
- General Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Computer Networks & Wireless Communication (AREA)
- Life Sciences & Earth Sciences (AREA)
- Hydrology & Water Resources (AREA)
- Details Of Aerials (AREA)
Abstract
The invention provides a sealed cabin for a wave glider communication system, which comprises an electric sealed cabin, a vacuum seal detection device, an external contactless switch device, an antenna sealing device and an AIS device, wherein a control system, a GPS (global positioning system) positioning module, a satellite communication module and an AIS module are arranged in the electric sealed cabin, the control system receives data of the AIS, the Iridium and the GPS positioning module and communicates with a shore base through the satellite communication module, the external contactless switch device controls the on-off of a power supply in the electric sealed cabin, and the vacuum seal detection device detects the water tightness of the sealed cabin. The device is used for sealing installation of a wave glider communication system, can also be used for equipment such as unmanned ships, sea surface drifting buoys and the like, and collected marine environment parameters and the positions of the equipment can be remotely returned in real time through satellite communication, so that reference is provided for monitoring personnel to perform next task planning on the equipment.
Description
Technical Field
The invention relates to the field of ocean sealing, in particular to a sealed cabin of a wave glider communication system.
Background
The wave glider is a novel ocean mobile observation platform, and can simultaneously utilize wave energy and solar energy to realize long-range and large-scale sea-air interface observation. The communication system sealed cabin is the brain of the wave glider, the main function is to ensure the normal communication between the wave glider platform and the shore-based monitoring center, and the feasible performance of the communication system sealed cabin has important significance for the ocean observation and application of the wave glider. However, the conventional communication system sealed cabin has the problems of poor long-term reliability, simple function, complex opening/closing operation, harsh sealing test conditions and limitation of an external interface, and is difficult to provide an effective solution for the communication system of the wave glider, so that a communication system sealed cabin which is reliable for a long time, convenient and practical is needed, and an effective guarantee is provided for the wave glider to carry out various ocean observations.
Disclosure of Invention
The invention provides a sealed cabin for a wave glider communication system for solving the technical problems in the prior art, the sealed cabin of the communication system has the advantages of strong long-term reliability, complete functions, simple opening/closing operation, convenient and fast sealing test, and capability of providing a comprehensive external interface and ensuring the performance of the sealed cabin of the communication system in a feasible way.
The technical scheme adopted by the invention for solving the technical problems in the prior art is as follows: a sealed cabin for a wave glider communication system comprises an electric sealed cabin, an external non-contact switch device, a vacuum sealing detection device, an antenna sealing device and an AIS device.
The electric sealed cabin comprises a sealed cabin body and a cover plate, wherein the bottom surface of the cabin body is provided with an installation hole site for an electric system and a watertight connector, a flange surface of the cabin body is provided with a sealing groove for accommodating an O-shaped rubber ring, a groove-shaped hole site for fastening the cover plate with a threaded hole and an external connection, the cover plate is provided with a hole site for fastening the cabin body, and the cover plate is provided with an installation interface for a vacuum sealing detection device, an external non-contact switch device, an antenna sealing device and an AIS device.
Outside contactless switching device includes limit switch seat, limit switch axle, rotary switch seat, sealing washer III and sealing washer IV, the limit switch seat be equipped with be used for with the rotary switch seat with the fixed screw hole of limit switch, the flange face of rotary switch seat is equipped with holds sealing washer III's seal groove, rotary switch seat lower extreme is equipped with the external screw thread with the limit switch seat fastening, limit switch is equipped with a set of screw thread with the limit switch seat fastening, the rotary switch axle is equipped with holds sealing washer IV's seal groove, rotary switch epaxial end is equipped with the word groove that is used for revolving the twist switch.
The vacuum seal detection device comprises a vacuum valve seat, a vacuum seal head, a seal ring V, a seal ring VI, a gasket II, a vacuum seal head fixing nut, a seal ring VII, a check valve and a vacuum seal cap, wherein the lower end of the vacuum valve seat is provided with an external thread used for being connected with the cover plate, the vacuum valve seat is fixed on the cover plate through the cooperation of the gasket II and the vacuum seal head fixing nut, the flange seal surface of the vacuum valve seat is provided with a seal groove, the seal ring VI is arranged on the seal groove of the vacuum valve seat to be extruded to achieve sealing, the upper end of the vacuum valve seat is provided with a threaded hole, the lower end of the vacuum seal head is provided with a seal groove for installing the seal ring V, the lower end of the vacuum seal head is provided with the external thread to be screwed on the upper end of the vacuum valve seat, when the vacuum seal is detected, the vacuum seal head is unloaded, and the check valve is screwed on the upper end of the vacuum valve seat, and inflating the electric sealing cabin through the one-way valve to perform sealing test.
The antenna sealing device comprises a communication mounting cover, a communication mounting base, a communication head fixing nut, a sealing ring VIII, a GPS circuit board, an iridium satellite, a sealing ring IX and an iridium cover plate, wherein sealing grooves for containing the sealing ring IX and the sealing ring VIII are respectively arranged at the upper end and the lower end of the communication mounting base, a thread which is fastened with the communication mounting cover in a screwing mode is arranged at the upper end of the communication mounting base, an external thread which is fastened with the communication head fixing nut is arranged at the lower end of the communication mounting base, and the iridium cover plate encapsulates the iridium satellite, the GPS circuit board and is fastened at a mounting position in the communication mounting base.
The AIS device includes POM sleeve, AIS flange, sealing washer X, sealing washer XI, AIS antenna, gasket III and AIS mounting nut, the AIS flange is equipped with the seal groove that holds sealing washer XI, the AIS flange be equipped with the circumference distribution screw hole that the apron was fastened, POM sleeve lower extreme is equipped with the seal groove that holds sealing washer X, POM sleeve lower extreme be equipped with the screw thread that the AIS flange was fastened, POM sleeve inside is equipped with hold the cavity of AIS antenna.
The invention has the advantages and positive effects that: the sealed cabin adopts the welded and integrated sealed cabin body and the cover plate made of the carbon fiber material, so that the strength, the electromagnetic shielding performance and the corrosion resistance of the sealed cabin are improved, and the long-term reliability of the sealed cabin is improved; by adding the external non-contact switch device, the vacuum seal detection device, the antenna sealing device and the AIS device, the functions of communication, test and switch of the sealed cabin are met, and the functionality of the sealed cabin is improved; by adding an external non-contact device, the problem of an electric power switch in a sealed cabin is solved, and meanwhile, the excellent waterproof performance is still kept; by adding the vacuum sealing detection device, the water tightness and air tightness of the assembled sealed cabin can be simply and clearly tested; the design and installation of the external electrical interface of the sealed cabin are reliable and simple, and the setting of the water tight-sealing plug-in can be properly increased and reduced according to the requirement; the sealing of each part in the sealed cabin is carried out by adopting an O-shaped sealing element, the installation is simple and convenient, and the long-term sealing reliability is realized; the top ends of the AIS device and the antenna sealing device are made of POM materials, and interference of iridium and GPS signals can be reduced while sealing and protecting the sealed cabin. Therefore, the sealed cabin of the wave glider communication system meets the use performance, functional requirements and test requirements, and the wave glider communication system can also be used in the process of collecting marine environment parameters of equipment such as unmanned ships, sea surface drifting buoys and the like, remotely transmits information back to a shore base in real time through a satellite, and provides reference for monitoring personnel to perform next task planning on the equipment.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic structural view of the sealed cabin of the present invention;
FIG. 3 is a schematic diagram of an external contactless switch device according to the present invention;
FIG. 4-1 is a schematic view of the vacuum seal detection apparatus according to the present invention in a normal state;
FIG. 4-2 is a schematic structural view of the vacuum seal detection apparatus of the present invention in a working detection state;
FIG. 5 is a schematic structural diagram of an iridium and GPS antenna multiplexing antenna sealing device according to the present invention;
fig. 6 is a schematic structural view of an AIS device of the present invention.
In the figure: 1. sealing the cabin body; 1-1, fixing a cylinder on a circuit board; 1-2, a watertight connector locking cover; 1-3, a watertight plug; 1-4, watertight connector; 2. a cover plate; 3. an external contactless switching device; 3-1, rotating a switch seat; 3-2, a limit switch seat; 3-3, a limit switch; 3-4, rotating a switch shaft; 3-5, sealing ring III; 3-6, and a sealing ring IV; 4. a vacuum seal detection device; 4-1, a vacuum valve seat; 4-2, vacuum sealing head; 4-3, a sealing ring V; 4-4 sealing ring VI; 4-5 of a gasket II; 4-6, fixing a nut by using a vacuum sealing head; 4-7, a sealing ring VII; 4-8, a one-way valve; 4-9, vacuum sealing cap; 5. an antenna sealing device; 5-1, a communication mounting cover; 5-2, a communication installation base; 5-3, fixing a nut on the communication head; 5-4, a sealing ring VIII; 5-5, a GPS circuit board; 5-6 iridium; 5-7 of a sealing ring IX; 5-8 parts of iridium cover plate; 6. an AIS device; 6-1, POM sleeve; 6-2, AIS flange; 6-3, sealing ring X; 6-4 of a sealing ring XI; 6-5, AIS antenna; 6-6, a gasket III; 6-7, AIS antenna mounting nuts.
Detailed Description
For further understanding of the contents, features and effects of the present invention, the following examples are given in conjunction with the accompanying drawings to illustrate and describe the following:
the electric sealed cabin is composed of a sealed cabin body 1 and a cover plate 2, a circuit board fixing cylinder 1-1 for installing an electric system is welded on the inner bottom surface of the sealed cabin body 1, a through hole for installing the watertight connector 1-4 is formed in the side surface of the sealed cabin body 1, a sealing groove is formed in the flange sealing surface of the watertight connector 1-4, threads are arranged on the lower portion of the flange sealing surface of the watertight connector 1-4 and are screwed and fixed with a threaded hole of the sealed cabin body 1, so that a sealing ring I in the sealing groove is extruded to achieve a waterproof sealing function, the watertight connector 1-3 is plugged with the watertight connector 1-4 according to the number of cores, the watertight connector locking cover 1-2 is locked with the threads on the upper portion of the flange sealing surface of the watertight connector 1-4, and the flange sealing surface of the sealed cabin body 1 is provided with the sealing groove, threaded holes are formed in the periphery of the upper end face of the sealed cabin body 1 and are fastened with the cover plate 2 through screws, 4 straight-mouth grooves are formed in the periphery of the upper end face of the sealed cabin body 1, the whole sealed cabin is fixed on a ship body through screws, a sealing groove is formed in the upper end face of the sealed cabin body 1, and a sealing ring II in the sealing groove is extruded through the cover plate 2 to achieve the waterproof sealing function of the sealing groove; the cover plate 2 is provided with a threaded hole fastened with the sealed cabin 1 and mounting holes for mounting an external contactless switch device 3, a vacuum seal detection device 4, an antenna sealing device 5 and an AIS device 6.
The external contactless switch device 3 comprises a rotary switch seat 3-1, a limit switch seat 3-2, a limit switch 3-3, a rotary switch shaft 3-4, a sealing ring III 3-5 and a sealing ring IV 3-6, wherein the limit switch seat 3-2 is provided with 1M 12 threaded hole and 2M 3 threaded holes which are distributed diagonally, a sealing groove is arranged on the sealing end surface of the rotary switch seat 3-1, the sealing groove uses the sealing ring III, the waterproof sealing function is achieved by extrusion deformation between the sealing end surface of the rotary switch seat 3-1 and the cover plate 2, M12 threads are arranged at the lower end of the rotary switch seat 3-1 and matched with the M12 threaded holes in the limit switch seat 3-2, so that the limit switch seat 3-2 is tightly attached to the cover plate 2, and 2M 3 threaded holes in the limit switch seat 3-2 are matched through screws so that the limit switch 3-3, 4, 3, and 2M 12 threaded holes in the limit switch seat 3-2 are matched through screws The sealing ring IV is used in the sealing groove, the waterproof sealing function is achieved by matching and extruding the rotary switch shaft 3-4 and a stepped hole of the rotary switch base 3-1, the switch at the lower end of the rotary switch shaft 3-4 is in contact fit with the limit switch 3-3, and the function of switching on and off a power supply is achieved through a straight groove at the upper end of the rotary switch shaft 3-4.
The vacuum seal detection device 4 consists of a vacuum valve seat 4-1, a vacuum seal head 4-2, a seal ring V4-3, a seal ring VI 4-4, a gasket II 4-5, a vacuum seal head fixing nut 4-6, a seal ring VII 4-7, a check valve 4-8 and a vacuum seal cap 4-9, wherein the lower end of the vacuum valve seat 4-1 is provided with threads, the vacuum valve seat 4-1 is fixed on the cover plate 2 by matching with the vacuum seal head fixing nut 4-6 and the gasket II 4-5, the sealing end face of the vacuum valve seat 4-1 is provided with a sealing groove, the sealing groove uses the seal ring V4-3, the waterproof sealing function is achieved by extrusion deformation between the sealing end face of the vacuum valve seat 4-1 and the cover plate 2, the upper end face of the vacuum valve seat 4-1 is provided with a step threaded hole, the vacuum sealing head 4-2 is provided with threads at the lower end and is screwed on a step hole of a vacuum valve seat 4-1, a sealing groove is formed in the sealing end face of the vacuum sealing head 4-2, a sealing ring VI 4-4 is used in the sealing groove, the waterproof sealing function is achieved through extrusion deformation between the sealing end face of the vacuum sealing head 4-2 and the step hole of the vacuum valve seat 4-1, the vacuum sealing head 4-2 is unloaded in a working detection state, a check valve 4-8 is screwed on the vacuum valve seat 4-1 through threads at the lower end, the vacuum sealing cap 4-9 is covered, sealing grooves are formed in two sides of a cap opening of the vacuum sealing cap 4-9, and the sealing ring VII 4-7 is used and is extruded by the side wall of a counter bore of the vacuum valve seat 4-1, so that the waterproof sealing function is achieved.
The antenna sealing device 5 comprises a communication mounting cover 5-1, a communication mounting base 5-2, a communication head fixing nut 5-3, a GPS circuit board 5-5, an iridium satellite 5-6, a sealing ring IX 5-7, an iridium satellite cover plate 5-8 and a GPS, wherein a sealing groove is formed in the lower end of the communication mounting base 5-2, a sealing ring VIII 5-4 is used, the communication mounting base 5-2 is screwed and fixed on the cover plate 2 through the communication head fixing nut 5-3, the sealing ring VIII 5-4 is extruded to achieve a waterproof sealing function, the communication mounting base 5-2 is provided with a conical counter bore, the iridium satellite cover plate 5-8 and the GPS circuit board 5-5 are fixed on the step of the conical counter bore through 4 screws, the iridium satellite 5-6 and the GPS are mounted on the GPS circuit board 5-5, the upper end of the communication installation base 5-2 is provided with a sealing groove, a sealing ring IX 5-7 is arranged in the sealing groove, and a waterproof sealing function is achieved by installing and extruding the sealing groove and the communication installation cover 5-1.
The AIS device 6 is composed of a POM sleeve 6-1, AIS flanges 6-2, sealing rings X6-3, sealing rings XI 6-4, AIS antennas 6-5, gaskets III 6-6 and AIS antenna mounting nuts 6-7. The flange sealing surface of the AIS flange 6-2 is provided with a sealing groove and 6 fixed threaded holes, the sealing groove is internally provided with the sealing ring X6-3, the threaded holes are matched through screwing screws to fix the AIS flange 6-2 on the cover plate 2, so that the sealing ring XI 6-4 is extruded to achieve a waterproof sealing function, the sealing groove is arranged on the outer ring of the fixed threaded holes and can prevent water leakage caused by the threaded holes, the lower end of the POM sleeve 6-1 is provided with the sealing groove, the POM sleeve 6-1 is matched with the AIS flange 6-2 through screwing threads, the sealing ring X6-3 is extruded with the inner hole surface of the AIS flange 6-2 to achieve the waterproof sealing function, and the AIS antenna 6-5 penetrates through the gasket III 6-6 and the mounting hole of the cover plate 2, and then is tightly screwed and matched with the AIS antenna mounting nuts 6-7 and fixed on the cover plate 2.
When the ship-mounted watertight cable-armored cable-type ship glider is used, the communication system sealed cabin is mounted at the corresponding position of the ship body, the watertight connector and the watertight cable are connected with the battery cabin, and the compass and the steering engine on the glider are connected through the armored cable. The marine environment data to be collected are transmitted to the data collection module and the control module, the data collection module and the control module store information into a memory, and meanwhile, the data are periodically transmitted to the shore base through the satellite communication module according to a fixed time interval.
Although the preferred embodiments of the present invention have been described above with reference to the accompanying drawings, the present invention is not limited to the above-described embodiments, which are merely illustrative and not restrictive, and those skilled in the art can make many modifications without departing from the spirit and scope of the present invention as defined in the appended claims.
Claims (4)
1. A sealed cabin for a wave glider communication system is characterized by comprising an electric sealed cabin, an external non-contact switch device, a vacuum seal detection device, an antenna sealing device and an AIS device,
the electric sealed cabin comprises a cabin body and a cover plate, the cover plate is provided with the external non-contact switch device, a vacuum seal detection device, an antenna sealing device and an AIS device, the outer side of the cabin body is fixedly provided with a watertight plug for electrically connecting with the outside,
the external non-contact switch device is used for opening and closing an electric power switch in the sealed cabin,
the vacuum sealing detection device tests the air tightness and the water tightness of the sealed cabin through the one-way valve,
the antenna sealing device is internally provided with an iridium satellite and a GPS, the interference of an iridium satellite signal and a GPS signal is reduced through the communication mounting cover,
an AIS antenna is installed in the AIS device, and interference of AIS signals is reduced through the POM sleeve.
2. The capsule according to claim 1, wherein the cover plate is made of carbon fiber.
3. The capsule of claim 1, wherein the communication mounting cap and the POM sleeve are both POM.
4. The pod for wave glider communication system of claim 1, wherein the electrical pod, the external contactless switch device, the vacuum seal detection device, the antenna seal device and the AIS device are sealed by means of O-rings.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110840519.0A CN113686315A (en) | 2021-07-24 | 2021-07-24 | A sealed cabin for wave glider communication system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110840519.0A CN113686315A (en) | 2021-07-24 | 2021-07-24 | A sealed cabin for wave glider communication system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN113686315A true CN113686315A (en) | 2021-11-23 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110840519.0A Pending CN113686315A (en) | 2021-07-24 | 2021-07-24 | A sealed cabin for wave glider communication system |
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| Country | Link |
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| CN (1) | CN113686315A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114291221A (en) * | 2021-12-09 | 2022-04-08 | 天津大学青岛海洋技术研究院 | Hidden floating body platform for underwater real-time observation system |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR19990046475A (en) * | 1999-03-18 | 1999-07-05 | 임건 | Satellite-directional case for emergency position indicating radio beacons |
| CN1800800A (en) * | 2004-12-30 | 2006-07-12 | 中国科学院沈阳自动化研究所 | Underwater control cabin capable of detecting sealing condition |
| CN205543237U (en) * | 2016-02-29 | 2016-08-31 | 中海蓝水自动化装备有限公司 | Wireless satellite communication combined antenna of underwater vehicle |
| CN111846169A (en) * | 2020-08-18 | 2020-10-30 | 中船海洋探测技术研究院有限公司 | Be used for withstand voltage sealed cabin of long distance wireless communication under water |
-
2021
- 2021-07-24 CN CN202110840519.0A patent/CN113686315A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR19990046475A (en) * | 1999-03-18 | 1999-07-05 | 임건 | Satellite-directional case for emergency position indicating radio beacons |
| CN1800800A (en) * | 2004-12-30 | 2006-07-12 | 中国科学院沈阳自动化研究所 | Underwater control cabin capable of detecting sealing condition |
| CN205543237U (en) * | 2016-02-29 | 2016-08-31 | 中海蓝水自动化装备有限公司 | Wireless satellite communication combined antenna of underwater vehicle |
| CN111846169A (en) * | 2020-08-18 | 2020-10-30 | 中船海洋探测技术研究院有限公司 | Be used for withstand voltage sealed cabin of long distance wireless communication under water |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114291221A (en) * | 2021-12-09 | 2022-04-08 | 天津大学青岛海洋技术研究院 | Hidden floating body platform for underwater real-time observation system |
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