CN205998108U - Helicopter under water - Google Patents
Helicopter under water Download PDFInfo
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- CN205998108U CN205998108U CN201620755535.4U CN201620755535U CN205998108U CN 205998108 U CN205998108 U CN 205998108U CN 201620755535 U CN201620755535 U CN 201620755535U CN 205998108 U CN205998108 U CN 205998108U
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- under water
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Abstract
This utility model provides one kind helicopter under water, main part by：Upper lid, lower cover, propeller, titanacycle, application cylinder, fixed mount, welding block, contiguous block, fixed block, screw mandrel composition, application cylinder is fixed on fixed mount, the pole end of fixed mount and welding block welding, welding block, contiguous block, titanacycle is made to fix by bolt and nut, Shang Gai, lower cover bolt pass through through hole and titanacycle to fix；If desired helicopter dive under water or floating, only need to control level propeller rotation upwards；To realize the forward-reverse of helicopter under water, then only need to control propeller rotating horizontally toward；To realize the hovering of helicopter under water, as long as controlling level propeller upwards with quality in certain rotating speed counteracting under water water of helicopter；This aircraft operations is easy, extremely flexibly.
Description
Technical field
This utility model is to be related to a kind of submersible, concretely relates to a kind of high using dish design, underwater wireless
3000 meter level submersibles of fast optical communication technique.
Background technology
It always is a difficult problem in the operation of water-bed environment especially abyssal environment and investigation work, enter with scientific and technological
Step, increasing underwater robot is continuously created, and carries mechanical hand, sonar, photographic head data collection sensor deeply
The water-bed exploration world under water.Due to the water-bed region difference explored, underwater robot be divided into have propeller and no propeller, have cable
Multiple with untethered, water-bed crawler travel and water-bed fixed point work (inaction ability) etc..And the profile of underwater robot is also many
For rectangle, cylindrical or streamlined, all robots with ability to act, mostly adopt these configuration designs to facilitate detection
The carrying of equipment or minimizing fluid resistance.Therefore, the most at present underwater robot with action performance capacity all exists
Following two deficiencies：1. flexibility ratio is poor；2. cannot realize arbitrarily hovering.
But the application of robot under water：The realization of seabed mobile observation network, the data between seabed operation point
Plug into energy, the cruise of sensitive sea-bed area and detection, submerged pipeline monitoring with safeguard, seabed rescue with salvage, seabed is examined
Gu etc., proposes higher requirement to the mobility of submersible, needs underwater robot to have good spot hover work energy
The motion flexibility ratio of power and superelevation.
Additionally, domestic at present main submarine navigation device is mostly using there being cable to communicate, therefore can be with longer cable, this meeting
The motion of impact underwater robot.
And this utility model then overcomes the deficiencies in the prior art, there is provided one kind is using dish design, it is possible to achieve appoint
Meaning turns to, arbitrarily bottom, any landing, arbitrarily hover, there is oversoul and live mobility, filled up submersible from sea to seabed work
Make the blank of mode so that submersible need not carry long cable, thus further increasing its motility.
Design work depth of water maximum of the present utility model, up to 3000 meters, belongs to deepwater work level submersible.
Content of the invention
The purpose of this utility model is to overcome the deficiencies in the prior art, there is provided a kind of using disk-shaped body design, can
To realize the underwater performance level aircraft of operation of hovering under water.
In order to solve above-mentioned technical problem, this utility model is to be achieved through the following technical solutions：
Helicopter under water of the present utility model, main part by：Upper lid 1, lower cover 2, propeller 3, titanacycle 4, application cylinder 5,
Fixed mount 6, welding block 7, contiguous block 8, fixed block 9, screw mandrel 10 form.
Described upper lid 1 is dish, four upper grooves 1.1 of edge uniform ring cloth, and bottom portion of groove has tapped through hole；
Described lower cover 2 is dish, four low grooves 2.1 of edge uniform ring cloth, and bottom portion of groove has tapped through hole；
Described titanacycle 4, located at upper lid 1,2 positions of lower cover, is made up of four sections of quarter circular arc, and material is titanium alloy,
There is end fit structure at circular arc two ends, and this end fit structure is by radial direction halfpace 4.1, screwed hole 4.2, chimb 4.3, axial halfpace
4.4 compositions, and the end fit structure at circular arc two ends is outside an inclined circular arc respectively, inside an inclined circular arc；
Described titanacycle 4 be fixed with application cylinder 5 centrally through fixed mount 6；Drive circuit and light is comprised in this application cylinder 5
The control module such as terminal and wireless telecommunications；
Described fixed mount 6 is made up of middle 6.2, four poles 6.1 of ring, and uniform welding exists respectively at the two ends of pole 6.1
On middle ring 6.2 and titanacycle 4 inwall；
Described pole 6.1 has some through holes with the weld of middle ring 6.2, and this through hole screw mandrel 10 passes through；Screw mandrel
10 two ends are fixed on application cylinder 5 by fixed block 9, and this fixed block 9 has screwed hole for Z-shaped, bottom surfaces, and this screwed hole supplies
Screw mandrel 10 passes through, and with nut screwing clamping screw mandrel 10 so that the fixed block up and down 9 of screw mandrel 10 is tightly stuck on application cylinder 5, is formed interior
Portion's fixed structure.
Described titanacycle 4 and the weld of pole 6.1 are provided with welding block 7；This welding block 7 is by boss 7.1, lateral threaded holes
7.2nd, longitudinal threaded bore 7.3 forms, and wherein lateral threaded holes 7.2 and longitudinal threaded bore 7.3 are through hole, and are mutually communicated,
Bar 6.1 passes through lateral threaded holes 7.2, and is weldingly fixed on boss 7.1；Longitudinal threaded bore 7.3 on welding block 7 is covered on 1 with upper
Upper groove 1.1 on screwed hole alignment, with bolt screw in longitudinal threaded bore 7.3 in, fixed cover 1；In the same manner, lower cover 2 adopts
Same mode is fixed.
Described titanacycle 4 lateral wall is uniformly arranged with four propellers 3, wherein relative to two symmetrical propeller level courts
Upper arrangement, other two is horizontally disposed；
Described titanacycle 4 is connected by contiguous block 8 between propeller 3, and this contiguous block 8 has stirrup hole 8.1, for wearing
Cross stirrup to fix propeller 3, centre has tapped through hole 8.2；The side of this contiguous block 8 is concave curved surface 8.3, opposite side
It is provided with two pieces of parallel up and down clamps 8.4；After the end fit structure of two sections of circular arcs is superimposed by this utility model, both axial directions
Halfpace 4.4 overlaps, and the screwed hole 4.2 on two end fit structures also overlaps；Again because the presence of chimb 4.3 thus being formed on
Groove on lower surface, the width of this groove is identical with the width of clamp 8.4 and thickness with depth；Clamp 8.4 snaps in this groove,
Pass through tapped through hole 8.2, screwed hole 4.2, lateral threaded holes 7.2 with stay bolt so that contiguous block 8, titanacycle 4, welding block 7 are fixing
Together.
Compared with prior art, the beneficial effects of the utility model are：The overall structure of this submarine navigation device is dish, profit
In realizing hovering action under the control of propeller, and the uniqueness in structure makes it move nimbly and freely, can be than other water
Lower robot is easier to realize the collection of underwater performance data.
Brief description
Fig. 1 is overall structure diagram of the present utility model；
Fig. 2 is fixing schematic diagram inside this utility model；
Fig. 3 is that schematic diagram fixed by this utility model application cylinder；
Fig. 4 is welding block 7, contiguous block 8 position view；
Fig. 5 is titanacycle 4 end fit structure schematic diagram；
Fig. 6 is welding block 7, the structural representation of contiguous block 8；
Reference：Upper lid 1, upper groove 1.1, lower cover 2, low groove 2.1, propeller 3, titanacycle 4, radial direction halfpace 4.1, spiral shell
Pit 4.2, chimb 4.3, axial halfpace 4.4, application cylinder 5, fixed mount 6, pole 6.1, middle ring 6.2, welding block 7, boss
7.1st, lateral threaded holes 7.2, longitudinal threaded bore 7.3, contiguous block 8, stirrup hole 8.1, tapped through hole 8.2, arcwall face 8.3, clamp
8.4th, fixed block 9, screw mandrel 10.
Specific embodiment
What time need below explanation before this：Because this utility model contains mechanical structure portion, electronic control unit
Point and wireless telecommunications and water surface control station part, structure is sufficiently complex, and this specification describes emphatically the machine of this helicopter under water
Tool structure division and its innovation, therefore in addition to mechanical structure portion, other parts are no longer discussed in detail.
With specific embodiment, this utility model is described in further detail below in conjunction with the accompanying drawings：
As shown in figures 1 to 6, helicopter under water of the present utility model, main part by：Upper lid 1, lower cover 2, propeller 3, titanium
Ring 4, application cylinder 5, fixed mount 6, welding block 7, contiguous block 8, fixed block 9, screw mandrel 10 form.
Wherein：
Upper lid 1 is dish, four upper grooves 1.1 of edge uniform ring cloth, and bottom portion of groove has tapped through hole；
Lower cover 2 is dish, four low grooves 2.1 of edge uniform ring cloth, and bottom portion of groove has tapped through hole；
Propeller 3 has four, is evenly distributed on integrally-built peripheral edge, wherein relative to two propeller levels
Upwardly disposed, other two is horizontally disposed；
Titanacycle 4 is made up of four sections of quarter circular arc, and material is titanium alloy, and there is end fit structure at circular arc two ends：By footpath
Form to halfpace 4.1, screwed hole 4.2, chimb 4.3, axial halfpace 4.4, and the end fit structure at circular arc two ends one is partially round
Outside arc, inside an inclined circular arc；
The control modules such as drive circuit and optical transmitter and receiver and wireless telecommunications are comprised in application cylinder 5；
Fixed mount 6 is made up of middle 6.2, four poles 6.1 of ring, and pole 6.1 uniform welding, on middle ring 6.2, welds
Place has through hole, and screw mandrel 10 passes through；
It is made up of boss 7.1, lateral threaded holes 7.2, longitudinal threaded bore 7.3 on welding block 7, wherein lateral threaded holes 7.2
It is through hole with longitudinal threaded bore 7.3；
Stirrup hole is had on contiguous block 8, for fix propeller 3, centre has tapped through hole 8.2, through stirrup
Face is arcwall face 8.3, is simultaneously provided with upper and lower two pieces of clamps 8.4；
Fixed block 9 has screwed hole for Z-shaped, bottom surfaces, and screw mandrel 10 passes through.
The annexation of each part is described below：
Internal fixing：Screwed hole is had on the middle ring 6.2 on fixed mount 6, screw mandrel 10 passes through；Screw mandrel 10 upper end is screwed into
Screwed hole in top fixed block 9 bottom surfaces, lower end is screwed into the bottom surfaces screwed hole of top fixed block 9, upper and lower fixed block upper
Portion face is stuck in the capping up and down of application cylinder, and with nut screwing clamping screw mandrel 10, then fixed block 9 is tightly stuck on application cylinder up and down,
Form internal fixing structure；
Pole 6.1 is pipe, is enclosed within boss 7.1, is welded and fixed；
Titanium alloy annulus section coordinates two-by-two：The chimb 4.3 on the fit structure of end in one annulus segmental arc is against another circle
On the radial direction halfpace 4.1 of ring segmental arc, and the radial direction halfpace 4.1 of itself is also propped up by the chimb 4.3 of other side, therefore, both sides'
Axial halfpace 4.4 overlaps, and the screwed hole 4.2 in two sections of titanacycle also overlaps；Formed on upper and lower end face because of the presence of chimb 4.3
Groove, the width of groove is identical with the width of clamp 8.4 and thickness with depth；Clamp 8.4 snaps in this groove, is worn with stay bolt
Cross tapped through hole 8.2, screwed hole 4.2, lateral threaded holes 7.2 so that contiguous block 8, titanacycle 4, welding block 7 are fixed together；
Propeller 3 is fixed on contiguous block 8 through stirrup hole 8.1 with stirrup；
So that the screwed hole covering on the upper groove 1.1 on 1 is alignd with the longitudinal threaded bore 7.3 on welding block 7, revolved with bolt
Enter in longitudinal threaded bore 7.3, fixed cover 1；In the same manner, lower cover 2 is fixed in the same way.
Work process：
Assembling finish and debug intact after will put in water by helicopter under water, water surface control station lever be controlled order
The input of order, if desired helicopter dive under water or floating, only level propeller 3 upwards need to be controlled to rotate；To realize water
The forward-reverse of lower helicopter, then only need to control propeller 3 rotating horizontally toward；To realize helicopter under water
Hovering, as long as control level propeller 3 upwards with quality in certain rotating speed counteracting under water water of helicopter.This navigation
Device is easy and simple to handle, extremely flexibly.
Above in association with accompanying drawing, embodiment of the present utility model is explained in detail, but this utility model is not limited to
State embodiment, in the ken that described technical field those of ordinary skill possesses, can also be without departing from this practicality
On the premise of new objective, various changes can be made.Additionally, be related in this utility model is undeclared partly same as the prior art,
Or realized using prior art.
Claims (4)
1. helicopter under water, by：Upper lid (1), lower cover (2), propeller (3), titanacycle (4), application cylinder (5), fixed mount (6), weldering
Connect block (7), contiguous block (8), fixed block (9), screw mandrel (10) composition it is characterised in that：
Described upper lid (1) and lower cover (2) are dish, four grooves of edge uniform ring cloth, and bottom portion of groove has tapped through hole；
Described titanacycle (4), located at position between Shang Gai (1), lower cover (2), is made up of four sections of quarter circular arc；Circular arc two ends are divided
It is not provided with end fit structure, this end fit structure is by radial direction halfpace (4.1), screwed hole (4.2), chimb (4.3), axially ladder
Platform (4.4) forms, and the end fit structure at circular arc two ends is outside an inclined circular arc respectively, inside an inclined circular arc；
Described titanacycle (4) be fixed with application cylinder (5) centrally through fixed mount (6)；This application cylinder is provided with drive circuit in (5)
With optical transmitter and receiver and wireless telecommunications；
Described fixed mount (6) is made up of middle ring (6.2), four poles (6.1), and the two ends of pole (6.1) are uniformly welded respectively
It is connected on middle ring (6.2) and titanacycle (4) inwall；
Described pole (6.1) has some through holes with the weld of middle ring (6.2), and this through hole screw mandrel (10) passes through；Silk
The two ends of bar (10) are fixed on application cylinder (5) by fixed block (9), and this fixed block (9) has screwed hole for Z-shaped, bottom surfaces,
This screwed hole screw mandrel (10) passes through, and with nut screwing clamping screw mandrel (10) so that the fixed block up and down (9) of screw mandrel (10) tightly blocks
On application cylinder (5), form internal fixing structure；
Described titanacycle (4) is provided with welding block (7) with the weld of pole (6.1)；This welding block (7) main by boss (7.1),
Lateral threaded holes (7.2), longitudinal threaded bore (7.3) composition, wherein lateral threaded holes (7.2) and longitudinal threaded bore (7.3) are
Through hole, pole (6.1) passes through lateral threaded holes (7.2), and is weldingly fixed on boss (7.1)；Longitudinal screw on welding block (7)
Being alignd with the screwed hole of upper lid (1) groove in hole (7.3), screws in longitudinal threaded bore (7.3) with bolt, fixed cover (1)；Welding
Longitudinal threaded bore (7.3) on block (7) is alignd with the screwed hole of lower cover (2) groove, screws in longitudinal threaded bore (7.3) with bolt
In, fixing lower cover (2)；
Described titanacycle (4) lateral wall is uniformly arranged with four propellers (3), wherein relative to two symmetrical propeller level courts
Upper arrangement, other two is horizontally disposed；
Described titanacycle (4) is connected by contiguous block (8) between propeller (3), and this contiguous block (8) has stirrup hole (8.1),
It is used for through stirrup to fix propeller (3), centre has tapped through hole (8.2)；The side of this contiguous block (8) is indent arc
Face (8.3), opposite side are provided with two pieces of parallel up and down clamps (8.4).
2. after helicopter under water as claimed in claim 1 is it is characterised in that be superimposed the end fit structure of two sections of circular arcs, two
The axial halfpace (4.4) of person overlaps, and the screwed hole (4.2) on two end fit structures also overlaps；Again because of chimb (4.3)
Exist thus forming the groove on upper and lower end face, the width of this groove is identical with the width of clamp (8.4) and thickness with depth；Card
Plate (8.4) snaps in this groove, with stay bolt pass through tapped through hole (8.2), screwed hole (4.2), lateral threaded holes (7.2) so that
Contiguous block (8), titanacycle (4), welding block (7) are fixed together.
3. helicopter under water as claimed in claim 1 is it is characterised in that the material of described titanacycle (4) is titanium alloy.
4. helicopter under water as claimed in claim 1, it is characterised in that if desired helicopter dive under water or floating, only needs to control
Controlling the water circulation puts down propeller (3) rotation upwards；To realize the forward-reverse of helicopter under water, then only need to control pushing away horizontally toward
Enter device (3) rotating；To realize the hovering of helicopter under water, as long as controlling level propeller (3) upwards with certain
Rotating speed offset quality in the water of helicopter under water.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620416102 | 2016-05-09 | ||
| CN2016204161026 | 2016-05-09 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205998108U true CN205998108U (en) | 2017-03-08 |
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ID=58201272
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620755535.4U Active CN205998108U (en) | 2016-05-09 | 2016-07-15 | Helicopter under water |
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| Country | Link |
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| CN (1) | CN205998108U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108045536A (en) * | 2017-11-15 | 2018-05-18 | 浙江大学 | A kind of small-sized VTOL underwater robot of untethered and its control method |
| CN108163165A (en) * | 2017-12-23 | 2018-06-15 | 左立亮 | A kind of revolution diving apparatus |
| CN109050838A (en) * | 2018-08-16 | 2018-12-21 | 浙江大学 | The underwater helicopter promoted based on vector |
| CN109649612A (en) * | 2018-12-20 | 2019-04-19 | 韩陈宇 | Underwater unmanned plane based on intelligent air bladder |
-
2016
- 2016-07-15 CN CN201620755535.4U patent/CN205998108U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108045536A (en) * | 2017-11-15 | 2018-05-18 | 浙江大学 | A kind of small-sized VTOL underwater robot of untethered and its control method |
| CN108163165A (en) * | 2017-12-23 | 2018-06-15 | 左立亮 | A kind of revolution diving apparatus |
| CN109050838A (en) * | 2018-08-16 | 2018-12-21 | 浙江大学 | The underwater helicopter promoted based on vector |
| CN109649612A (en) * | 2018-12-20 | 2019-04-19 | 韩陈宇 | Underwater unmanned plane based on intelligent air bladder |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20211202 Address after: 316000 room 101-9, No. 10, Baichuan Road, Lincheng street, Zhoushan Marine Science City, Dinghai District, Zhoushan City, Zhejiang Province Patentee after: Zhejiang oushentai Marine Technology Co.,Ltd. Address before: 310013 Yuhang Tang Road, Xihu District, Hangzhou, Zhejiang 866 Patentee before: ZHEJIANG University |