CN106413351A - Water-cooled heat dissipation type pressure-resistant electronic cabin - Google Patents
Water-cooled heat dissipation type pressure-resistant electronic cabin Download PDFInfo
- Publication number
- CN106413351A CN106413351A CN201611047528.XA CN201611047528A CN106413351A CN 106413351 A CN106413351 A CN 106413351A CN 201611047528 A CN201611047528 A CN 201611047528A CN 106413351 A CN106413351 A CN 106413351A
- Authority
- CN
- China
- Prior art keywords
- cabin
- heat dissipation
- fin
- pressure
- cavity
- 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
Links
- 230000017525 heat dissipation Effects 0.000 title abstract description 11
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 21
- 238000001816 cooling Methods 0.000 claims description 28
- 238000007789 sealing Methods 0.000 claims description 8
- 230000000694 effects Effects 0.000 abstract description 4
- 208000031481 Pathologic Constriction Diseases 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 210000001215 vagina Anatomy 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 239000003292 glue Substances 0.000 description 2
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000005489 elastic deformation Effects 0.000 description 1
- 239000008393 encapsulating agent Substances 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000003032 molecular docking Methods 0.000 description 1
- 230000004899 motility Effects 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K7/00—Constructional details common to different types of electric apparatus
- H05K7/20—Modifications to facilitate cooling, ventilating, or heating
- H05K7/2039—Modifications to facilitate cooling, ventilating, or heating characterised by the heat transfer by conduction from the heat generating element to a dissipating body
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63G—OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
- B63G8/00—Underwater vessels, e.g. submarines; Equipment specially adapted therefor
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Wind Motors (AREA)
Abstract
The invention discloses a water-cooled heat dissipation type pressure-resistant electronic cabin which comprises a main cabin body. A front end cover and a rear end cover are respectively arranged on both ends of the main cabin body. The main cabin body is sealed into a cavity by the front end cover and the rear end cover. A heat dissipation device is arranged in the cavity. The heat dissipation device comprises four heat sinks which are supported by cross-shaped telescopic brackets on both ends and are arranged on the inner wall of the cavity through the cross-shaped telescopic brackets. The heat sinks are arranged on electrical components. According to the water-cooled heat dissipation type pressure-resistant electronic cabin, the pressure-resistant cabin casing and the internal electrical device are respectively two separate systems, and can be completely separated; the convenience of assembling and debugging is improved; the electrical device is arranged on a separate heat dissipation bracket; the heat dissipation bracket can transfer heat of the electrical components to the wall of the pressure-resistant cabin and water outside the cabin; heat dissipation of the electrical device in the cabin body is realized; and in addition, the support effect of the heat dissipation bracket on the cabin wall enhances the pressure-resistant ability of the pressure-resistant cabin casing and improves the reliability of the whole system.
Description
Technical field
The present invention relates to a kind of pressure electronic compartment of water cooling radiating type, belong to Underwater Engineering field.
Background technology
The electrical equipment that deep water is dived in device typically requires and works in anhydrous conditions it is therefore necessary to be positioned over the airtight of water proof
In nacelle, and nacelle need to have enough anti-pressure abilities, can keep indeformable, thus protecting inside under the effect of extraneous hydraulic pressure
Equipment.For ensureing comprcssive strength, pressure Tibetan shell typically adopts cylindrical or spherical designs under water, but compared to square nacelle,
Its curved inner surface shape leads to electric original paper inconvenience to install and debug, and space availability ratio can be greatly reduced.In addition, part
Electrically caloric value during original paper work is very high, and it is tired that airtight pressure Tibetan shell and irregular curved inner surface also bring to radiating
Difficult.
Under water in pressure electronic compartment patent and product, electrical equipment all directly adopts non-removable side to existing major part
Formula is fixed on inside nacelle, is that later maintenance brings very big trouble.A few patents have devised dismountable electronic equipment
Support, but its version is excessively complicated, and cargo handling process is also relatively cumbersome.Send out in China Patent No. ZL200610134453.9
There is in bright electronics pressure-resistant cabin movable electronics docking frame, but effective erection space is less, the number of devices that can carry
Limited, and do not consider the radiating of electrical equipment.The problems referred to above do not obtain effectively solving always.
Content of the invention
Goal of the invention：In order to overcome the deficiencies in the prior art, the present invention provides a kind of resistance to piezoelectricity of water cooling radiating type
Sub- cabin, pressure-resistant cabin shell is respectively two independent systems with internal electric equipment, can be kept completely separate between the two, improve dress
The convenience joined and debug, electrical equipment is installed on independent cooling stand, and cooling stand can be by the heat of electrical equipment
Conduct to pressure bulkhead and water out of my cabin, solve heat dissipation problem in nacelle for the electrical equipment.In addition cooling stand is to cabin
The supporting role of wall enhances the anti-pressure ability of pressure-resistant cabin shell, improves the reliability of whole system.
Technical scheme：For achieving the above object, the pressure electronic compartment of the water cooling radiating type of the present invention, including main nacelle, main cabin
Body be respectively arranged at two ends with drive end bearing bracket and rear end cap, main nacelle is sealed to a cavity by drive end bearing bracket and rear end cap, in cavity
Inside heat abstractor is installed, described heat abstractor comprises four fin, four fin pass through the cross telescope support at two ends
Support, be arranged on the inwall of cavity by cross telescope support, electrical equipment is installed on fin.
Preferably, described cross telescope support comprises four connectors, long nut and threaded rod, described four connectors
It is connected to four connecting rods, the angle of adjacent connecting rod is 90 °, and described connecting rod is provided with screw thread, the spiral shell in connecting rod
Stricture of vagina is contrary with the hand of spiral on threaded rod, the spiral shell being respectively arranged at two ends with connecting rod and shaft of described long nut
Stricture of vagina, is cased with locking the locking spring of long nut in connecting rod.
Preferably, the inwall of described cavity is provided with several limiting cards, it is provided with stopper slot at the two ends of fin, limit
Position groove snaps in limiting card.
Preferably, some circle annular seal grooves are equipped with described drive end bearing bracket and rear end cap, pacify in annular seal groove
Equipped with O sealing ring, by O-ring seal by the inner wall sealing of drive end bearing bracket and rear end cap and main nacelle.
Preferably, described fin one side is plane, for installing electrical equipment, another side is arc surface, arc surface
Radius identical with the radius of cavity inner wall.
Preferably, the two ends of described main nacelle are equipped with dismounting groove.
Beneficial effect：Compared with prior art, the present invention's has advantages below：
1. it is easily installed electrical equipment, electrical equipment in pressure-resistant cabin is integrated on independent support, support and pressure-resistant cabin
Shell can be kept completely separate, and substantially increases handling and the later maintenance convenience of equipment.
2. solve the heat dissipation problem of closed cabin indoor electric equipment, electrical equipment is installed on and can fit tightly pressure-resistant cabin
On the fin of shell inwall, the heat that produces when electrical equipment is worked be introduced directly into out of my cabin in cold water it is achieved that unconfined
Water-cooling, solves the problems, such as that on-plane surface closed cabin indoor electric equipment is difficult to radiate, extends the sustainable of below deck equipment
Working time, improve the reliability of system.
3. improve radiating efficiency further, the Telescopic of cooling stand can adjust between fin within the specific limits
Distance, change the integral diameter of cooling stand, enhance between electrical equipment and compressive cabin motility during handling, and can
So that fin is fitted tightly in bulkhead by pretightning force, improve radiating efficiency, and achieve the radial positioning of mounting system.
4. the limiting card of nacelle internal reservation coordinates the Telescopic of cooling stand can easily realize independent rack system
Axially and tangentially positioning in nacelle within for the system, it is to avoid use the loaded down with trivial details fixed forms such as bolt.
5. improve space availability ratio, be filled with fin in the arc space that script is difficult by, be greatly improved resistance to
Space availability ratio in ballasting.
6. enhance compressive cabin structural strength, internal heat dissipating support provides certain supporting role to pressure-resistant cabin shell,
Reduce deformation rate under deepwater high-pressure for the cabin shell, enhance the anti-pressure ability of pressure-resistant cabin shell, improve the safety of whole system.
7. anti-loosening property is good, and the four pieces of locking springs often installed in set cross telescope support can strengthen screw thread self-locking energy
Power, prevents threaded loosening that compressive cabin causes in motor process under water from leading to electrical equipment impaired, carries further
High reliability.
8. sealing property is reliable, adopts twice O-ring as encapsulant, be further ensured that between main nacelle and every piece of end cap
Its underwater sealing property.
9. it is easy to load and unload, main nacelle both ends of the surface are respectively kept with twice dismounting groove, convenient insertion ripping bar, improve radial seal
Structural member is difficult to the problem dismantled.
Brief description
Fig. 1 is the exterior three dimensional view of pressure electronic compartment in the present invention.
Fig. 2 is the 3-D view of drive end bearing bracket in the present invention.
Fig. 3 is the internal view of pressure electronic compartment.
Fig. 4 is the partial enlarged drawing of I part in Fig. 3.
Fig. 5 is the 3-D view of fin.
Fig. 6 is the 3-D view of cooling stand system.
Specific embodiment
Below in conjunction with the accompanying drawings the present invention is further described.
As shown in Figures 1 to 6, the pressure-resistant cabin shell in the present invention includes the main nacelle 1 of a cylinder type, before one piece of cylinder
End cap 5 and one piece of cylindrical rearward end lid 9.Flange is left at described main nacelle 1 two ends, end face of flange has eight with regard in axis
The symmetrical screwed hole of the heart 3, in addition end face of flange has twice with regard to the symmetrical dismounting groove 4 of axis centre.
As shown in Fig. 2 described drive end bearing bracket 5 is second order column structure, outside cylinder end face has corresponding in eight and main nacelle 1
Circular locating openings 8, interior cylindrical end face has some jointing holes 7 for installing watertight cable connector, and interior cylindrical side is opened
There is twice annular seal groove 6, for mounting O-shaped sealing ring 10.
The assembling mode of explanation main nacelle 1 and drive end bearing bracket 5 and rear end cap 9 below.Respectively by four pieces of O-ring seals 10 in the past
The interior cylindrical side of end cap 5 and rear end cap 9 loads seal groove 6；The inner cylinder face of drive end bearing bracket 5 and rear end cap 9 is directed at main nacelle 1
Inside it is ensured that eight screw thread hole sites at two ends correspond, you can drive end bearing bracket 5 and rear end cap 9 are pushed home into；Reference picture
4 it is ensured that after all O-ring seals 10 are pushed into main nacelle 1 inside, eight pieces of screws are screwed into often along the axis direction of main nacelle 1
In the location hole 8 and screwed hole 3 at end, you can main nacelle 1 is installed together with drive end bearing bracket 5 and rear end cap 9.This mounting means can
To guarantee axially or tangentially not slide between main nacelle 1 and end cap.Install rear O-ring seal in main nacelle 1 internal face
Squeezing action under produce elastic deformation, you can prevent outside liquid enter, realize water-tight function.The advantage of this design is in water
The lower main nacelle 1 of pressure effect is tightr with the combination meeting of drive end bearing bracket 5 and rear end cap 9, and theoretical headwater depth is bigger, the sealing of O-ring
Can be better.
As shown in Figure 3, Figure 5 and Figure 6, the cooling stand system within pressure-resistant cabin comprises what two sets of cross telescope supports connected
Four pieces of fin 11, the one side of described fin 11 is plane, can be used for holding electrical element 19, described plane two ends are opened respectively
There is left handed threaded hole 12, the another side of fin 11 is arc surface, the inwall radius surface of the radius of this cambered surface and described main nacelle 1
Identical it is ensured that the two fits tightly；Fin 11 two ends have stopper slot 13, for coordinating the spacing of main nacelle 1 inwall
Card 2, tangential and axial restraint in nacelle for the achievable cooling stand system.Described cross telescope support includes one piece four and leads to
Connect 14, four pieces of device, 16, four pieces of connecting rods of locking spring, four pieces of positive/negative thread long nuts 17 and four pieces of left hand thread bars 18, connect
Bar is right-handed thread bar 15.Four passages of four connectors 14 all have dextrorotation female thread, for connecting four pieces of right-handed threads
Bar 15；In positive/negative thread long nut 17, half is levogyrate inner thread, and second half is dextrorotation female thread, and above-mentioned screw thread can be with dextrorotation
Threaded rod 15 and left-hand thread bar 17 cooperate.
The assembling mode of described cooling stand system is described below.Revolve after injection screw thread glue in described four connectors 14
Enter described right-handed thread bar 15, be completely fixed.And right-handed thread bar 15 is put locking spring 16.In described left hand thread
Screw in left hand thread bar 18 after injection screw thread glue in hole 12, the two is completely fixed.Will be all electric on described fin 11
After element 19 installs, described positive/negative thread long nut 17 is placed in right-handed thread bar 15 and the free end of left hand thread bar 18
Between, rotate counterclockwise two ends positive/negative thread long nut 17 simultaneously, you can make right-handed thread bar 15 and left hand thread bar 18 simultaneously
Enter；If turn clockwise two ends positive/negative thread long nut 17 simultaneously, you can make right-handed thread bar 15 and left hand thread bar 18 same
When exit the radial expansion function it is achieved that four pieces of fin 11.
The assembling mode of described cooling stand system and main nacelle 1 is described below.Described cooling stand system and electrically unit
After part 19 assembling finishes, rotate counterclockwise all positive/negative threads long nut 17, make four pieces of fin 11 shrink, to cooling stand system
The diameter of system reaches minimum；Heat dissipating package mounting system is inserted in described main nacelle 1 it is ensured that the stopper slot at fin 11 two ends
13 are in cooperation position with the limiting card 2 on main nacelle 1 internal face, and turn clockwise all positive/negative thread long nuts 17, makes four
Block fin 11 is upheld, and the arc surface to all fin 11 is fitted tightly with the internal face of main nacelle 1, all limiting cards simultaneously
2 all in stopper slot 13, realizes axially and tangentially fixing to heat dissipating package system.Locking spring 16 can make positive and negative spiral shell simultaneously
Condition of self-locking is consistently achieved, it is to avoid because of the play of compressive cabin between stricture of vagina long nut 17 and right-handed thread bar 15 and left hand thread bar 18
Strong motion leads to threaded loosening it is ensured that radially fixed effect.Because locking spring 16 withstands long nut 17, can be by length
Nut 17 self-locking.Cooling stand system and main nacelle 1 are assembled after finishing, the watertight needing to electrical equipment and being installed on end cap
Connector carries out wiring, subsequently can as described above main nacelle 1 be assembled with drive end bearing bracket 5 and rear end cap 9.
The dismounting mode of the pressure electronic compartment of the present invention is described below.By 16 pieces on described drive end bearing bracket 5 and rear end cap 9 end face
Fixed screw unloads, and so that compressive cabin is disposed vertically in plane, inserts in the dismounting groove 4 of main nacelle 1 end face with two pieces of skid plates,
Outwards prize, you can end cap is taken out from main nacelle 1, another piece of end cap is in the same manner simultaneously.By electrical equipment and underwater electrical connector
Between lug disconnect, rotate counterclockwise all positive/negative threads long nut 17, make four pieces of fin 11 shrink, to cooling stand
The diameter of system reaches minimum, and limiting card 2 can be automatically separated with stopper slot 13, and cooling stand system is taken out from main nacelle 1
Go out.
Heretofore described electrical equipment 19 can fit tightly with the plane of fin 11, the cambered surface of fin 11 and master
The internal face of nacelle 1 also can fit tightly it is achieved that heat is from the outside cold water of electrical equipment 19- fin 11- main nacelle 1-
Conductive process.This water cooling method ultrahigh in efficiency, can be prevented effectively from electric original paper because of high temperature failure, enable pressure electronic compartment
Enough long-time stable work in deepwater environment.Particularly in main nacelle, under conditions of main nacelle limited space, can be very
Facilitate your dismounting electrical equipment 17, and the area of dissipation of fin 11 is big.
The above be only the preferred embodiment of the present invention it should be pointed out that：Ordinary skill people for the art
For member, under the premise without departing from the principles of the invention, some improvements and modifications can also be made, these improvements and modifications also should
It is considered as protection scope of the present invention.
Claims (6)
1. a kind of pressure electronic compartment of water cooling radiating type it is characterised in that：Including main nacelle, main nacelle be respectively arranged at two ends with front end
Lid and rear end cap, main nacelle is sealed to a cavity by drive end bearing bracket and rear end cap, is provided with heat abstractor in cavity, described
Heat abstractor comprises four fin, and four fin are supported by the cross telescope support at two ends, by cross telescope support
Fin is arranged on the inwall of cavity, electric original paper is installed on a heat sink.
2. the pressure electronic compartment of water cooling radiating type according to claim 1 it is characterised in that：Described cross telescope support comprises
Four connectors, long nut and threaded rod, described four connectors are connected to four connecting rods, the angle of adjacent connecting rod
For 90 °, described connecting rod is provided with screw thread, and the screw thread in connecting rod is contrary with the hand of spiral on threaded rod, described long nut
The screw thread being respectively arranged at two ends with connecting rod and shaft, connecting rod is cased with lock long nut locking spring.
3. the pressure electronic compartment of water cooling radiating type according to claim 1 it is characterised in that：The inwall of described cavity is provided with
Several limiting cards, are provided with stopper slot at the two ends of fin, and stopper slot snaps in limiting card.
4. the pressure electronic compartment of water cooling radiating type according to claim 1 it is characterised in that：On described drive end bearing bracket and rear end cap
Be equipped with some circle annular seal grooves, annular seal groove be provided with O sealing ring, by O-ring seal by drive end bearing bracket and
Rear end cap and the inner wall sealing of main nacelle.
5. the pressure electronic compartment of water cooling radiating type according to claim 1 it is characterised in that：Described fin one side is flat
Face, for installing electrical equipment, another side is arc surface, and the radius of arc surface is identical with the radius of cavity inner wall.
6. the pressure electronic compartment of water cooling radiating type according to claim 1 it is characterised in that：The two ends of described main nacelle are all provided with
There is dismounting groove.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611047528.XA CN106413351B (en) | 2016-11-22 | 2016-11-22 | A kind of water cooling radiating type pressure resistance electronic compartment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611047528.XA CN106413351B (en) | 2016-11-22 | 2016-11-22 | A kind of water cooling radiating type pressure resistance electronic compartment |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106413351A true CN106413351A (en) | 2017-02-15 |
| CN106413351B CN106413351B (en) | 2019-02-15 |
Family
ID=58081513
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611047528.XA Expired - Fee Related CN106413351B (en) | 2016-11-22 | 2016-11-22 | A kind of water cooling radiating type pressure resistance electronic compartment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106413351B (en) |
Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107380383A (en) * | 2017-08-11 | 2017-11-24 | 江苏科技大学 | A kind of observation type unmanned remotely controlled submersible vehicle |
| CN108674576A (en) * | 2018-05-04 | 2018-10-19 | 江苏科技大学 | A kind of the segmented circle cylindricality pressure-resistant cabin and assembly method of deep water unmanned vehicles |
| CN108801053A (en) * | 2018-01-16 | 2018-11-13 | 西安电子工程研究所 | A kind of Seeker-eCabin structure based on skeleton radiating principle |
| CN109110090A (en) * | 2018-07-24 | 2019-01-01 | 大连理工大学 | A kind of underwater robot electronic compartment |
| CN109152303A (en) * | 2018-10-11 | 2019-01-04 | 无锡市海鹰加科海洋技术有限责任公司 | A kind of radiator structure of underwater electronic compartment |
| CN109413955A (en) * | 2018-11-27 | 2019-03-01 | 中国船舶重工集团公司第七〇九研究所 | A kind of underwater instrument passive radiating device |
| CN109552589A (en) * | 2019-01-10 | 2019-04-02 | 中国海洋大学 | A kind of underwater sealing cabin piston heat-exchanger rig |
| CN112793750A (en) * | 2020-12-21 | 2021-05-14 | 浙江大学 | Heat dissipation device for necking cabin sections at two ends of underwater sealed cavity |
| CN112996312A (en) * | 2021-02-07 | 2021-06-18 | 中船海洋探测技术研究院有限公司 | Sealing cabin with quick assembly and disassembly structure for seabed connection box and assembly and disassembly method |
| CN114062340A (en) * | 2020-07-30 | 2022-02-18 | 中国科学院大连化学物理研究所 | Ultraviolet optical system pressure bearing device for deep sea environment |
| CN114630548A (en) * | 2020-12-10 | 2022-06-14 | 中国科学院沈阳自动化研究所 | Internal locking heat conduction frame body of small cabin and installation method |
| CN115103560A (en) * | 2022-05-13 | 2022-09-23 | 中国船舶科学研究中心 | Flexible wall-attached heat dissipation system for deep sea submersible vehicle |
| CN115113343A (en) * | 2022-07-04 | 2022-09-27 | 中国科学院沈阳自动化研究所 | Large-depth quick-insertion type optical communication cabin structure of underwater robot |
| CN117320416A (en) * | 2023-11-27 | 2023-12-29 | 西安中核核仪器股份有限公司 | Heat radiation structure for nuclear radiation detector |
| CN117622450A (en) * | 2024-01-24 | 2024-03-01 | 天津瀚海蓝帆海洋科技有限公司 | Modularized high-power underwater propulsion system |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101841996A (en) * | 2010-05-07 | 2010-09-22 | 浙江大学 | Elastic heat dissipating bracket for deep-sea seal cavity |
| CN204956890U (en) * | 2015-09-23 | 2016-01-13 | 中国科学院沈阳自动化研究所 | Cabin body inner structure under water dispels heat |
| WO2016092043A1 (en) * | 2014-12-12 | 2016-06-16 | Ge Oil & Gas Uk Limited | Locking mechanism |
| CN206260194U (en) * | 2016-11-22 | 2017-06-16 | 江苏科技大学 | A kind of pressure-resistant electronic compartment of water cooling radiating type |
-
2016
- 2016-11-22 CN CN201611047528.XA patent/CN106413351B/en not_active Expired - Fee Related
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101841996A (en) * | 2010-05-07 | 2010-09-22 | 浙江大学 | Elastic heat dissipating bracket for deep-sea seal cavity |
| WO2016092043A1 (en) * | 2014-12-12 | 2016-06-16 | Ge Oil & Gas Uk Limited | Locking mechanism |
| CN204956890U (en) * | 2015-09-23 | 2016-01-13 | 中国科学院沈阳自动化研究所 | Cabin body inner structure under water dispels heat |
| CN206260194U (en) * | 2016-11-22 | 2017-06-16 | 江苏科技大学 | A kind of pressure-resistant electronic compartment of water cooling radiating type |
Cited By (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107380383B (en) * | 2017-08-11 | 2023-03-28 | 江苏科技大学 | Observation type unmanned remote control submersible |
| CN107380383A (en) * | 2017-08-11 | 2017-11-24 | 江苏科技大学 | A kind of observation type unmanned remotely controlled submersible vehicle |
| CN108801053A (en) * | 2018-01-16 | 2018-11-13 | 西安电子工程研究所 | A kind of Seeker-eCabin structure based on skeleton radiating principle |
| CN108674576A (en) * | 2018-05-04 | 2018-10-19 | 江苏科技大学 | A kind of the segmented circle cylindricality pressure-resistant cabin and assembly method of deep water unmanned vehicles |
| CN109110090A (en) * | 2018-07-24 | 2019-01-01 | 大连理工大学 | A kind of underwater robot electronic compartment |
| CN109152303A (en) * | 2018-10-11 | 2019-01-04 | 无锡市海鹰加科海洋技术有限责任公司 | A kind of radiator structure of underwater electronic compartment |
| CN109413955A (en) * | 2018-11-27 | 2019-03-01 | 中国船舶重工集团公司第七〇九研究所 | A kind of underwater instrument passive radiating device |
| CN109552589A (en) * | 2019-01-10 | 2019-04-02 | 中国海洋大学 | A kind of underwater sealing cabin piston heat-exchanger rig |
| CN114062340A (en) * | 2020-07-30 | 2022-02-18 | 中国科学院大连化学物理研究所 | Ultraviolet optical system pressure bearing device for deep sea environment |
| CN114630548A (en) * | 2020-12-10 | 2022-06-14 | 中国科学院沈阳自动化研究所 | Internal locking heat conduction frame body of small cabin and installation method |
| CN112793750A (en) * | 2020-12-21 | 2021-05-14 | 浙江大学 | Heat dissipation device for necking cabin sections at two ends of underwater sealed cavity |
| CN112996312A (en) * | 2021-02-07 | 2021-06-18 | 中船海洋探测技术研究院有限公司 | Sealing cabin with quick assembly and disassembly structure for seabed connection box and assembly and disassembly method |
| CN115103560A (en) * | 2022-05-13 | 2022-09-23 | 中国船舶科学研究中心 | Flexible wall-attached heat dissipation system for deep sea submersible vehicle |
| CN115113343A (en) * | 2022-07-04 | 2022-09-27 | 中国科学院沈阳自动化研究所 | Large-depth quick-insertion type optical communication cabin structure of underwater robot |
| CN117320416A (en) * | 2023-11-27 | 2023-12-29 | 西安中核核仪器股份有限公司 | Heat radiation structure for nuclear radiation detector |
| CN117622450A (en) * | 2024-01-24 | 2024-03-01 | 天津瀚海蓝帆海洋科技有限公司 | Modularized high-power underwater propulsion system |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106413351B (en) | 2019-02-15 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106413351A (en) | Water-cooled heat dissipation type pressure-resistant electronic cabin | |
| CN206260194U (en) | A kind of pressure-resistant electronic compartment of water cooling radiating type | |
| CN103904263B (en) | A kind of microminiature underwater robot battery flat | |
| CN109110090B (en) | A kind of underwater robot electronic compartment | |
| CN110212133A (en) | A kind of sealing fixed structure of automobile batteries lodge body and cooling water pipe pipe fitting | |
| CN207131926U (en) | A kind of charge valve | |
| CN202523905U (en) | Single-core large-current electric connector | |
| CN110854584B (en) | High-voltage cable connector | |
| CN209909326U (en) | MCT sealing structure for marine pod type propeller | |
| CN202720436U (en) | Stainless steel underwater camera device | |
| CN203851394U (en) | Sealing shell of underwater power supply | |
| CN214625540U (en) | Waterproof photovoltaic connector | |
| CN207915344U (en) | Cable fixing head spanner | |
| CN206092648U (en) | A leak protection magnetism clamping unit for distribution equipment | |
| CN103192964B (en) | The mechanical device of seabed observation network scientific instrument jack module | |
| CN112118690A (en) | Circuit control assembly device for new energy logistics vehicle | |
| CN203237394U (en) | Mechanical device of scientific instrument socket module of seabed observation network | |
| CN102107416A (en) | Detaching device for thyristor of converter valve | |
| CN207919863U (en) | Adjustable skeletal connector | |
| CN206388921U (en) | Connector and electric automobile | |
| CN218958002U (en) | Waterproof device for portable coupler | |
| CN112904322B (en) | High-efficient self-cooling sonar processor device | |
| CN204034401U (en) | Large discharge foldable filter element guide support ring | |
| CN219892581U (en) | Conducting ring with heat dissipation effect | |
| CN220797297U (en) | Connector for interconnecting and installing portable photovoltaic modules |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| EE01 | Entry into force of recordation of patent licensing contract | ||
| EE01 | Entry into force of recordation of patent licensing contract |
Application publication date: 20170215 Assignee: Center for technology transfer Jiangsu University of Science and Technology Assignor: JIANGSU University OF SCIENCE AND TECHNOLOGY Contract record no.: X2021980006173 Denomination of invention: A water cooling and heat dissipation pressure electronic cabin Granted publication date: 20190215 License type: Common License Record date: 20210714 |
|
| EC01 | Cancellation of recordation of patent licensing contract | ||
| EC01 | Cancellation of recordation of patent licensing contract |
Assignee: Center for technology transfer Jiangsu University of Science and Technology Assignor: JIANGSU University OF SCIENCE AND TECHNOLOGY Contract record no.: X2021980006173 Date of cancellation: 20210826 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190215 |