CN205844896U - A kind of unmanned boat of band self-righting feature - Google Patents
A kind of unmanned boat of band self-righting feature Download PDFInfo
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- CN205844896U CN205844896U CN201620765143.6U CN201620765143U CN205844896U CN 205844896 U CN205844896 U CN 205844896U CN 201620765143 U CN201620765143 U CN 201620765143U CN 205844896 U CN205844896 U CN 205844896U
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Abstract
The utility model discloses the unmanned boat of a kind of band self-righting feature, it is desirable to provide a kind of behaviour at sea is strong, the unmanned boat of the band self-righting feature of self control ability and good stability.This utility model includes hull, described hull left surface is provided with left from holding up air bag, described hull right flank is provided with right from holding up air bag, control device systems cabin it is provided with in described hull, described control device systems cabin is provided with MCU controller, attitude transducer, inflator pump and certainly holds up with a described left side air bag and the described right side from holding up the inflation inductive switch that airbags is logical, and described attitude transducer, described inflator pump and described inflation inductive switch are all electrically connected with described MCU controller.This utility model is applied to the technical field of unmanned boat.
Description
Technical field
This utility model relates to a kind of unmanned boat, particularly to the unmanned boat of a kind of band self-righting feature.
Background technology
Along with the development of society, unmanned boat development and application is the most more and more significant.At present, unmanned boat has telecommunication, spy
Survey the functions such as investigation, underwater surface operation and Based Intelligent Control, and be widely used in communication, security, water analysis, scientific exploration
Etc. technical field, this application prospect situation the most sufficiently embodying unmanned boat is the best, also promotes research staff to nothing simultaneously
The research and development further of people's ship and production.But it is bad that existing unmanned boat also exists balance, anti-wave scarce capacity, self control ability has
Limit, operation is easily to be overturned by wave the most across the sea, its this function having that just loses it when unmanned boat is overturned,
At this moment also need to manually remove unmanned boat of suing and labouring, the most not only waste manpower, also waste the Innovation Input to unmanned boat.If energy
Design the unmanned boat of a kind of band auto-strengthening function, thus just can solve unmanned boat and overturned and ineffective awkward
The appearance of a word used for translation situation.
Utility model content
Technical problem to be solved in the utility model is to overcome the deficiencies in the prior art, it is provided that a kind of behaviour at sea is strong,
The unmanned boat of the band self-righting feature of self control ability and good stability.
The technical scheme is that this utility model of this utility model includes that hull, described hull left surface are provided with a left side
From holding up air bag, described hull right flank is provided with right from holding up air bag, is provided with control device systems cabin in described hull, and described control sets
Standby system cabin is provided with MCU controller, attitude transducer, inflator pump and certainly holds up with a described left side air bag and the described right side from holding up air bag
The inflation inductive switch being connected, described attitude transducer, described inflator pump and described inflation inductive switch all with described MC
U controller is electrically connected with.
Further, described inflation inductive switch include with a described left side from hold up left inductive switch valve that airbags is logical and with
The described right side is from holding up the right inductive switch valve that airbags is logical.
Further, described inflator pump by described left inductive switch valve and described right inductive switch valve respectively with a described left side
From holding up air bag and with the described right side from holding up airbags to lead to.
Further, described control device systems cabin also includes the battery being electrically connected with described MCU controller.
Further, described Attitude sensor uses horizontal gyro sensor or geomagnetic sensor.
Further, left and right, the bottom end face symmetrically arc-shaped of described hull, the left side, bottom of the most described hull is first
Outward expansion, then draw in the bottom centre of described hull, the bottom, right end face of described hull and the bottom left end of described hull
Face symmetrically profile.
Further, left and right, the bottom end face of described hull is provided with high-speed thruster.
The beneficial effects of the utility model are: owing to this utility model includes that the described left side being wrapped on described hull is from holding up
Air bag and right air bag of certainly holding up, and the horizontal deflection of described hull is sensed by described attitude induction apparatus, thus controlled by described MCU
Corresponding described inflation inductive switch opened by device processed, makes described inflator pump certainly hold up air bag to be inflated described in corresponding, thus
It is that described hull keeps stable, is not overturned by water wave.
Accompanying drawing explanation
Fig. 1 is that three-dimensional schematic representation of the present utility model is intended to;
Fig. 2 is right view of the present utility model;
Fig. 3 is the schematic diagram in described control device systems cabin 4.
Detailed description of the invention
As shown in Figure 1 to Figure 3, in the present embodiment, this utility model includes the unmanned boat of a kind of band self-righting feature, it
Including hull 1, described hull 1 left surface is provided with left right from holding up air bag 3 from holding up air bag 2, described hull 1 right flank to be provided with, described
A left side is two independent disconnected air bags from holding up air bag 2 and the described right side from holding up air bag, and a described left side is from holding up air bag 2 and the described right side certainly
Hold up the air bag one layer of air bag protective layer that made described hull many, and the stability of described hull can be increased;It is provided with in described hull 1
Control device systems cabin 4, described control device systems cabin 4 include MCU controller 5, attitude transducer 6, inflator pump 7 and with
A described left side can be rocker switch from the inflation inductive switch 8(holding up air bag 2 certainly to hold up air bag 3 to be connected with the described right side), described attitude
Sensor 6, described inflator pump 7 and described inflation inductive switch 8 are all electrically connected with described MCU controller 5.
In the present embodiment, described inflation inductive switch 8 includes with a described left side from the left inductive switch holding up air bag 2 to be connected
Valve 9 and with the described right side from holding up the right inductive switch valve 10 that air bag 3 is connected, described left inductive switch valve 9 and described right sensing are opened
Close whether valve 10 all opens switch valve to a described left side from holding up air bag 2 or the described right side from holding up air bag 3 to be inflated for sensing.
In the present embodiment, described inflator pump 7 is by described left inductive switch valve 9 and described right inductive switch valve 10 difference
With a described left side from holding up air bag 2 and with the described right side from holding up air bag 3 to be connected.When described attitude transducer 6 senses described hull side
When turning over, described MCU controller 5 controls to open described inflator pump 7 and inflation inductive switch 8, makes described inflator pump 7 to described
Air bag is inflated, and makes hull automatically carry out righting recovery.
In the present embodiment, described control device systems cabin 4 also includes the electricity being electrically connected with described MCU controller 5
Pond 11, described battery 11 is detachable battery, provides required power supply for described hull 1.
In the present embodiment, described hull 1 attitude transducer 6 uses horizontal gyro sensor or geomagnetic sensor.
In the present embodiment, left and right, the bottom end face symmetrically arc-shaped of described hull 1, the bottom of the most described hull 1 is left
End face elder generation outward expansion, then draw in the bottom centre of described hull 1, the bottom, right end face of described hull 1 and described hull 1
Left side, bottom symmetrically profile, thus overall in inverted m type shape bottom described hull 1, left and right, the bottom end of described hull 1
Face is provided with high-speed thruster 12, and described propeller 12 is for advancing the kinestate of described hull.
Its operation principle is: obtains power by described high-speed thruster 12, the most automatically navigates by water, when running into wave
Bringing it about to during while turning on one's side, during as turned on one's side to the right, described attitude transducer 6 senses the level condition of described hull 1, and
By sensed situation about rolling to the right be sent to described MCU controller 5 in time, then controlled by described MCU
Device 5 controls to open rollover right inductive switch valve 10 on one side, makes described inflator pump 7 to the described right side from holding up air bag 3 to be inflated, makes
Described hull 1 lifts to the right, and when described hull 1 arrives horizontal plane, described left inductive switch valve 9 also can be opened, and makes institute
Stating inflator pump 7 holds up air bag 2 to be inflated on a described left side more certainly, prevents described hull 1 avris to the left from turning over;Occur in the ban to the left
During rollover, its general principles is consistent, the most first to a described left side from holding up air bag 2 to be inflated with rollover situation to the right so that it is recover
Certainly hold up air bag 3 to be inflated on the described right side again after level, it is ensured that its both sides level, do not overturned.
This utility model is applied to the technical field of unmanned boat.
Although embodiment of the present utility model describes with practical solution, but is not intended that and contains this utility model
The restriction of justice, for those skilled in the art, according to this specification to the amendment of its embodiment and with the group of other schemes
Conjunction will be apparent from.
Claims (7)
1. the unmanned boat of a band self-righting feature, it is characterised in that: it includes that hull (1), the left surface of described hull (1) set
Have left right from holding up air bag (3) from holding up air bag (2), the right flank of described hull (1) to be provided with, be provided with control in described hull (1) and set
Standby system cabin (4), described control device systems cabin (4) be provided with MCU controller (5), attitude transducer (6), inflator pump (7) and with
A described left side is from holding up air bag (2) with the described right side from the inflation inductive switch (8) holding up air bag (3) to be connected, described attitude transducer
(6), described inflator pump (7) and described inflation inductive switch (8) are all electrically connected with described MCU controller (5).
The unmanned boat of a kind of band self-righting feature the most according to claim 1, it is characterised in that: described inflation inductive switch
(8) include that from the left inductive switch valve (9) holding up air bag (2) to be connected and oneself holds up air bag (3) to be connected with the described right side with a described left side
Right inductive switch valve (10).
The unmanned boat of a kind of band self-righting feature the most according to claim 2, it is characterised in that: described inflator pump (7) leads to
Cross described left inductive switch valve (9) and described right inductive switch valve (10) respectively with a described left side from hold up air bag (2) and with the described right side
It is connected from holding up air bag (3).
The unmanned boat of a kind of band self-righting feature the most according to claim 1, it is characterised in that: described control device systems
Cabin (4) also includes the battery (11) being electrically connected with described MCU controller (5).
The unmanned boat of a kind of band self-righting feature the most according to claim 1, it is characterised in that: described hull (1) attitude
Sensor (6) uses horizontal gyro sensor or geomagnetic sensor.
The unmanned boat of a kind of band self-righting feature the most according to claim 1, it is characterised in that: the end of described hull (1)
Left and right, portion end face symmetrically arc-shaped, left side, the bottom elder generation outward expansion of the most described hull (1), then to described hull (1)
Bottom centre draws in, the bottom, right end face of described hull (1) and left side, the bottom symmetrically profile of described hull (1).
The unmanned boat of a kind of band self-righting feature the most according to claim 6, it is characterised in that: the end of described hull (1)
Left and right, portion end face is provided with high-speed thruster (12).
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CN201620765143.6U CN205844896U (en) | 2016-07-20 | 2016-07-20 | A kind of unmanned boat of band self-righting feature |
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CN201620765143.6U CN205844896U (en) | 2016-07-20 | 2016-07-20 | A kind of unmanned boat of band self-righting feature |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
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CN105974926A (en) * | 2016-07-20 | 2016-09-28 | 珠海科微智能科技有限公司 | Unmanned ship with self-righting function |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
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CN105974926A (en) * | 2016-07-20 | 2016-09-28 | 珠海科微智能科技有限公司 | Unmanned ship with self-righting function |
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