CN209467306U - Nobody is from steady aircraft under water - Google Patents
Nobody is from steady aircraft under water Download PDFInfo
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- CN209467306U CN209467306U CN201822001671.6U CN201822001671U CN209467306U CN 209467306 U CN209467306 U CN 209467306U CN 201822001671 U CN201822001671 U CN 201822001671U CN 209467306 U CN209467306 U CN 209467306U
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- propeller
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- power distribution
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Abstract
The utility model provide it is a kind of it is underwater nobody from steady aircraft, including aircraft ontology, the aircraft ontology includes cabin shell, propulsion device is fixedly connected on the outer wall of the cabin shell, the propulsion device includes balance empennage and the first propeller, the balance empennage is installed on cabin shell one end, and the other end of the relatively described balance empennage of the cabin shell is fixedly connected with cabin front shroud, and first propeller is movably connected in cabin shell two sides；It is equipped with a power distribution equipment and one in the cabin shell and carries platform, the utility model structure is simple, mechanical space is compact, its first propeller being equipped with, the second propeller and balance empennage, aircraft athletic performance is controlled by driving the first propeller and the second propeller simultaneously to realize maximum power output, the mobility of underwater experiment platform is enhanced, while stability of equilibrium of the balance empennage holding aircraft therein in progress action process guarantees the stabilization of underwater experiment platform with this.
Description
Technical field
The utility model relates to a kind of underwater navigation apparatus fields, and in particular to it is a kind of it is underwater nobody from steady aircraft.
Background technique
In civil field, the intelligent behaviors such as task and path planning, motion control, status monitoring are that nobody navigates from steady under water
The important research content of row device, and the underwater unmanned vehicle as test carrier is increasingly concerned, traditional builds formula
Underwater experiment platform needs to build platform under water in advance when carrying out underwater experiment and builds complexity and the experiment built is flat
Platform mobility is poor, now using nobody a kind of underwater use from steady aircraft as underwater experiment platform, can effectively solve traditional
Build the problem of formula underwater experiment platform mobility difference.
Summary of the invention
The main purpose of the utility model is to provide it is a kind of it is underwater nobody from steady aircraft, to solve traditional build
The technical problem of formula underwater experiment platform mobility difference.
To achieve the goals above, the utility model provide it is a kind of it is underwater nobody from steady aircraft, including aircraft ontology,
The aircraft ontology includes cabin shell, and propulsion device, the propulsion device are fixedly connected on the outer wall of the cabin shell
Including balance empennage and the first propeller, the balance empennage is installed on cabin shell one end, the outer shell phase of the cabin
Cabin front shroud is fixedly connected with to the other end of balance empennage, first propeller is movably connected in cabin shell two sides；
It is equipped with a power distribution equipment and one in the cabin shell and carries platform, the carrying platform side is fixedly connected with the power distribution equipment,
The other side is electrically connected by connector and the cabin front shroud detachable connection, the power distribution equipment with first propeller
It connects.
Further, the propeller total at least four of cabin shell two sides and the propeller are set symmetrically
It is distributed in the left and right sides of the cabin shell.
Further, the power distribution equipment include an at least power distribution and one electricity adjust, it is described electricity adjust input terminal with it is described
The electrical connection of power distribution enable end, output end are electrically connected with the propeller.
Further, the carrying platform is in cylindrical body.
Further, the second propeller is also equipped in the bottom of the cabin shell and setting angle is in that 45 degree of angles are arranged,
Second propeller at least adds up to be mutually perpendicular to be uniformly distributed between four and adjacent second propeller.The utility model is beneficial
Effect:
1, the utility model provide it is a kind of it is underwater nobody from steady aircraft, the first propeller, the second propeller that are equipped with
And balance empennage, aircraft athletic performance is controlled by driving the first propeller and the second propeller simultaneously to realize most
High-power output enhances the mobility of underwater experiment platform, while balance empennage therein keeps aircraft acted
Stability of equilibrium in journey guarantees the stabilization of underwater experiment platform with this.
2, the utility model provide it is a kind of it is underwater nobody from steady aircraft, the carrying platform being equipped with can provide for underwater experiment
One stable support platform enables underwater experiment more steadily effectively efficiently to carry out.
3, the utility model provide it is a kind of it is underwater nobody from steady aircraft, structure is simple, and mechanical space is compact and can
Strong operability.
Detailed description of the invention
The utility model is described in further detail with reference to the accompanying drawings and examples:
Fig. 1 is the overall structure diagram of the utility model.
Fig. 2 is Fig. 1 bottom view.
In figure: 1. aircraft ontologies, 2. propulsion devices, 3. cabin front shrouds, 4. power distribution equipments, 5. carry platform, and 6. second push away
Into device, 10. cabin shells, 20. balance empennages, 21. first propellers, 40. power distributions, 41. electricity tune.
Specific embodiment
Further to illustrate technical means and efficacy that the utility model is taken to reach above-mentioned purpose, below in conjunction with
Attached drawing and preferred embodiment, specific embodiment of the present utility model, structure, feature and its effect describe in detail it is bright, should
Understand, specific embodiment described in the utility model only to explain the utility model, is not used to limit the utility model.
As described in Fig. 1~2, it is a kind of it is underwater nobody from steady aircraft, including aircraft ontology 1, aircraft ontology 1 includes cabin
Body case 10, propulsion device 2 is fixedly connected on the outer wall of cabin shell 10, and propulsion device 2 includes balance empennage 20 and first
Propeller 21, balance empennage 20 are installed on 10 one end of cabin shell, and the other end of 10 relative equilibrium empennage 20 of cabin shell is fixed
Cabin front shroud 3 is connected, the first propeller 21 is movably connected in 10 two sides of cabin shell；A power distribution equipment is equipped in cabin shell 10
4 and one carry platform 5, connect wherein carrying platform 5 using the carrying platform of cylindrical shape and carrying 5 side of platform and power distribution equipment 4 are fixed
It connects, the other side is electrically connected by connector and 3 detachable connection of cabin front shroud, power distribution equipment 4 with the first propeller 21, and boat is worked as
When row device ontology 1 is used for the carrying to underwater experiment platform, the carrying platform 5 being equipped with effectively can make its holding by carried experiment platform
One stabilised platform passes through the cabin shell 10 for including to aircraft ontology 1 when needing experiment porch to decline or rising
On the first propeller 21 for being equipped with of two sides and meanwhile carry out rotating forward running so that aircraft starts to float so that carrying on platform 5
The experiment porch of reprinting is begun to ramp up, while when the first propeller 21 of the two sides of cabin shell 10 setting while being inverted,
So that aircraft starts to float downward, so that the experiment porch carried on platform 5 starts to float downward.
Shown referring to Fig.1 in the utility model preferred embodiment, first that 10 two sides of cabin shell are arranged in promotes
Device 21 total at least four and the first propeller 21 are uniformly and symmetrically distributed in the left and right sides of cabin shell 10, and power distribution equipment 4 wraps
It includes at least a power distribution 40 and an electricity and adjusts 41, electricity adjusts 41 input terminal to be electrically connected with the enable end of power distribution 40, output end
It is electrically connected with the first propeller 21, when aircraft ontology 1 needs to move, power distribution 40 adjusts 41 to carry out speed regulating control by electricity
First propeller 21 is operated simultaneously, so that the experiment porch quick acting carried in aircraft, it is flat to improve experiment
The mobility of platform.
In the utility model preferred embodiment, referring to shown in Fig. 2, second is also equipped in the bottom of cabin shell 10
Propeller 6 and setting angle are in 45 degree of angles arrangements, and the second propeller 6 at least adds up to phase between four and adjacent second propeller 6
Mutual vertical uniform distribution may make that aircraft ontology 1 is controlled when adjacent two propeller of the second propeller 6 starts running
Or be moved forward and backward so that carrying the experiment porch reprinted on platform 5 and aircraft is also followed to carry out multidirectional movement, improve experiment
The mobility of platform；Simultaneously because when the second propeller 6 is installed using 45 degree of angles during installation, it can be by wherein
One propeller, which is powered, to be operated, so that aircraft ontology 1 generates certain turning moment, and then realizes returning for aircraft ontology 1
Transhipment is dynamic, to improve the mobility of experiment porch.
The above embodiments are only the optimal technical scheme of the utility model, and are not construed as the limit for the utility model
System, the technical solution that the protection scope of the utility model should be recorded with claim, the technical solution recorded including claim
The equivalents of middle technical characteristic are protection scope.Equivalent replacement i.e. within this range is improved, also in the utility model
Protection scope within.
Claims (5)
1. it is a kind of it is underwater nobody from steady aircraft, including aircraft ontology (1), it is characterised in that: aircraft ontology (1) packet
It includes cabin shell (10), is fixedly connected propulsion device (2) on the outer wall of the cabin shell (10), propulsion device (2) packet
It includes balance empennage (20) and the first propeller (21), the balance empennage (20) is installed on described cabin shell (10) one end,
The other end of relatively described balance empennage (20) of the cabin shell (10) is fixedly connected cabin front shroud (3), and described first promotes
Device (21) is movably connected in cabin shell (10) two sides；A power distribution equipment (4) and one are equipped in the cabin shell (10)
It carries platform (5), the carrying platform (5) side is fixedly connected with the power distribution equipment (4), and the other side passes through connector and the cabin
Body front shroud (3) detachable connection, the power distribution equipment (4) are electrically connected with first propeller (21).
2. it is according to claim 1 it is a kind of it is underwater nobody from steady aircraft, it is characterised in that: be arranged in the cabin shell
(10) the first propeller (21) of two sides adds up at least four and first propeller (21) is uniformly and symmetrically distributed in the cabin
The left and right sides of body case (10).
3. it is according to claim 1 it is a kind of it is underwater nobody from steady aircraft, it is characterised in that: power distribution equipment (4) packet
It includes an at least power distribution (40) and an electricity adjusts (41), the electric input terminal for adjusting (41) is enabled with the power distribution (40)
End electrical connection, output end are electrically connected with first propeller (21).
4. it is according to claim 1 it is a kind of it is underwater nobody from steady aircraft, it is characterised in that: the carryings platform (5) is in justifying
Cylinder.
5. it is according to claim 1 it is a kind of it is underwater nobody from steady aircraft, it is characterised in that: in the cabin shell (10)
Bottom be also equipped with the second propeller (6) and setting angle in 45 degree angles arrangements, second propeller (6) at least adds up to four
It is mutually perpendicular to be uniformly distributed between a and adjacent second propeller (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822001671.6U CN209467306U (en) | 2018-11-30 | 2018-11-30 | Nobody is from steady aircraft under water |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822001671.6U CN209467306U (en) | 2018-11-30 | 2018-11-30 | Nobody is from steady aircraft under water |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209467306U true CN209467306U (en) | 2019-10-08 |
Family
ID=68088633
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822001671.6U Active CN209467306U (en) | 2018-11-30 | 2018-11-30 | Nobody is from steady aircraft under water |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209467306U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111591421A (en) * | 2020-05-26 | 2020-08-28 | 博雅工道（北京）机器人科技有限公司 | Compact egg-shaped propeller |
| CN112298505A (en) * | 2020-11-09 | 2021-02-02 | 广东石油化工学院 | Wingless hydraulic and chemical reaction comprehensive spiral propulsion type intelligent underwater unmanned aircraft |
| CN112339954A (en) * | 2020-11-10 | 2021-02-09 | 广东石油化工学院 | Wingless electric forward and reverse bidirectional extrusion spiral propulsion type intelligent underwater unmanned aircraft |
| CN116513421A (en) * | 2023-04-14 | 2023-08-01 | 威海多鱼海洋科技有限公司 | Unmanned autonomous underwater vehicle |
-
2018
- 2018-11-30 CN CN201822001671.6U patent/CN209467306U/en active Active
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111591421A (en) * | 2020-05-26 | 2020-08-28 | 博雅工道（北京）机器人科技有限公司 | Compact egg-shaped propeller |
| CN112298505A (en) * | 2020-11-09 | 2021-02-02 | 广东石油化工学院 | Wingless hydraulic and chemical reaction comprehensive spiral propulsion type intelligent underwater unmanned aircraft |
| CN112339954A (en) * | 2020-11-10 | 2021-02-09 | 广东石油化工学院 | Wingless electric forward and reverse bidirectional extrusion spiral propulsion type intelligent underwater unmanned aircraft |
| CN112339954B (en) * | 2020-11-10 | 2022-04-29 | 广东石油化工学院 | Wingless electric forward and reverse bidirectional extrusion spiral propulsion type intelligent underwater unmanned aircraft |
| CN116513421A (en) * | 2023-04-14 | 2023-08-01 | 威海多鱼海洋科技有限公司 | Unmanned autonomous underwater vehicle |
| CN116513421B (en) * | 2023-04-14 | 2023-09-19 | 威海多鱼海洋科技有限公司 | Unmanned autonomous underwater vehicle |
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