CN207890009U - A kind of combined modular unmanned plane during flying device - Google Patents
A kind of combined modular unmanned plane during flying device Download PDFInfo
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- CN207890009U CN207890009U CN201721839283.4U CN201721839283U CN207890009U CN 207890009 U CN207890009 U CN 207890009U CN 201721839283 U CN201721839283 U CN 201721839283U CN 207890009 U CN207890009 U CN 207890009U
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Abstract
The utility model provides a kind of combined modular unmanned plane during flying device, wherein control module is that the side wall quantity of regular prism structure and regular prism is even number, and cross pin end is provided on each of which side wall；Power plant module is multiple, and each power plant module is the regular prism structure equal with control module side wall quantity, and is provided with the cross female connector for capableing of grafting with pin end on each side wall；Corresponding positive contact, negative contact terminal and signal wire contact are both provided in cross pin end and cross female connector；Control module provides power resources for the power plant module；It is provided in control module and flies control computing unit, the winged control computing unit transmission flight control parameter gives each power plant module.The utility model can be realized by control module and power plant module modularized design and fast assemble, be convenient for changing trouble unit and be easy to the purpose of harvesting, and the unmanned plane during flying device by assembling different scales, can improve adaptive capacity to environment.
Description
Technical field
The utility model is related to unmanned plane fields, more particularly, to a kind of combined modular unmanned plane during flying device.
Background technology
UAV abbreviation unmanned plane (Unmanned Aerial Vehicle, abbreviation UAV), be it is a kind of utilize nothing
The not manned aircraft that line electrical remote control equipment and the presetting apparatus provided for oneself manipulate.With the fast development of unmanned air vehicle technique, nothing
It is man-machine to be widely used in the industries such as city management, agricultural, geology, meteorology, electric power, rescue and relief work, video capture.
Currently, China's small drone is usually an overall structure, using being fixedly connected between main functional modules
Mode.
There are larger deficiencies in transport, making and repair etc. for this unmanned plane, such as in a certain part damage of unmanned plane
Bad when, can only whole unmanned plane sent for maintenance, cannot in time, quickly cope with problem；And used in some special screnes
Unmanned plane is required to reach and be convenient for carrying, the requirement of rapid deployment, for example, anti-terrorism special duty, rescue and relief work individual soldier carry nothing
Man-machine, but the volume and weight of existing unmanned plane is big, the problem of not readily portable harvesting, protrudes.
Utility model content
The purpose of this utility model be for presently, there are the problem of, a kind of combined modular unmanned plane during flying is provided
Device, the unmanned plane during flying device can be answered by modularized design, not only convenience in transport and assembling according to different loads etc.
With needing to be combined into corresponding pattern, so as to improve the scene adaptive capacity of unmanned plane, and convenient for harvesting and repair.
The purpose of this utility model is achieved through the following technical solutions：
The purpose of this utility model is to provide a kind of combined modular unmanned plane during flying device comprising：
Control module and power plant module；
The control module is that the side wall quantity of regular prism structure and regular prism is even number, and ten are provided on each of which side wall
Font pin end；The power plant module is multiple, and each power plant module is the regular prism knot equal with control module side wall quantity
Structure, and it is provided with the cross female connector for capableing of grafting with the pin end on each side wall；The cross pin end and ten
Corresponding positive contact, negative contact terminal and signal wire contact are both provided in font female connector；
It is provided with battery in the control module, passes through the positive contact and negative contact terminal pair of the pin end and female connector
It connects, power resources is provided for the power plant module；
It is provided in the control module and flies control computing unit, the winged control computing unit is connect by the pin end and mother
The signal wire contact of head is connected, and transmission flight control parameter gives each power plant module.
It is highly preferred that the positive contact, negative contact terminal and signal wire contact, are opened from the center of cross pin end
Beginning sets gradually outward along the branch line direction of cross pin end.
It is highly preferred that the positive contact, negative contact terminal and signal wire contact, are opened from the center of cross female connector
Beginning sets gradually outward along the branch line direction of cross pin end.
It is highly preferred that the also embedded suction block that is magnetic on each side wall of the control module；Each of described power plant module
Multiple iron blocks corresponding with the magnetism suction block are additionally provided on side wall.
It is highly preferred that the power plant module of stating includes：
Shell, inner casing, supporting beam, blade, fixing sleeve and rotary shaft；
The shell is the regular prism structure with cavity, and the inner casing is accommodated in the cavity；
The inner casing is the cylindrical structure with cavity, and the supporting beam is connected on the inner casing inner wall and to cavity
Central part extends, and is connect with the fixing sleeve positioned at inner casing center；Rotary shaft is provided in the fixing sleeve, and rotary shaft is another
End is fixed with blade by sleeve.
It is highly preferred that being additionally provided with clump weight in the control module.
The utility model compared with prior art, has as follows it can be seen from above-mentioned the technical solution of the utility model
Technique effect：
Airflight can be realized by splicing modules in the utility model, convenient and efficient, and in harvesting,
Harvesting can be stacked, occupied space is minimum.
The utility model can reach the needs suitable for various use environments by the quantity of change module.
The utility model assembles modules by Modularized splice formula and only passes through replacement when unmanned plane breaks down
Module can quickly normally come into operation again, and only need to be substituted into out of order module with spare part, convenient and efficient,
It improves work efficiency.
Description of the drawings
Fig. 1 is the structural schematic diagram of the utility model embodiment one；
Fig. 2-1 is the front view of each side of control module in the utility model embodiment two；
Fig. 2-2 is the vertical view of control module in the utility model embodiment one；
Fig. 3-1 is the front view of each side of power plant module in the utility model embodiment one；
Fig. 3-2 is the vertical view of power plant module in the utility model embodiment one；
Fig. 3-3 is the A-A sectional views of power plant module in the utility model embodiment one；
Fig. 4 is the structural schematic diagram of the utility model embodiment two.
In attached drawing：
Control module l, power plant module 2；Pin end 11, magnetic suction block 12, clump weight 13, power supply unit 14；Pin end is just
Pole contact 111, pin end negative contact terminal 112, pin end signal wire contact 113；Shell 21, inner casing 22, supporting beam 23, blade
24, fixing sleeve 25, rotary shaft 26, female connector 27, iron block 28；Female connector positive contact 271, female connector negative contact terminal 272 and mother
Joint signal line contact 273.
Specific implementation mode
In order to make those skilled in the art more fully understand the technical solution of the application, below with reference to attached drawing to this reality
It is described in further details with novel.
The orientation such as upper, lower, left, right, front and rear in present specification term be position relationship based on ... shown in the drawings and
It establishes.Attached drawing is different, then corresponding position relationship is also possible to change therewith, therefore cannot be interpreted as with this to protecting model
The restriction enclosed.
In the utility model, belong to " installation ", " connected ", " connecting ", " connection ", " fixation " etc. shall be understood in a broad sense, example
Such as, it may be a fixed connection, may be a detachable connection, can also be to be integrally connected, can also be mechanical connection, also may be used
To be electrical connection or can be in communication with each other, it can also be to be directly connected to, can also be to be indirectly connected with by intermediary, Ke Yishi
Unicom inside two components can also be the interaction relationship of two components.For the ordinary skill people of this field
For member, the concrete meaning of above-mentioned term in the present invention can be understood as the case may be.
Embodiment one
The utility model embodiment one provides a kind of combined modular unmanned plane during flying device, structure as shown in Figure 1, Figure 2-1
Shown in~Fig. 2-2 and Fig. 3-1~Fig. 3-3, including：
A kind of combined modular unmanned plane during flying device provided by the utility model, including control module l and power plant module
2.Power plant module 2 is uniformly arranged on the side wall of control module 1, be both provided on the side wall of the two it is corresponding anode, cathode with
And signal wire；Control module 1 is that power plant module 2 provides power resources by connecting anode and cathode；It is sent and is flown by signal wire
Row parameter is to power plant module 2.
The structure and function of modules are specific as follows：
For the structure of control module l therein as shown in Fig. 2-1 and Fig. 2-2, which is positive six rib with cavity
Circuit board is arranged inside in rod structure, and IMU measurement and control units are welded on the circuit board and fly control computing unit.
It is provided with pin end 11 on each side wall of control module l, which is cross pin end, and from cross
The center of type pin end starts outside along the branch line direction of cross pin end, is disposed with pin end positive contact
111, pin end negative contact terminal 112 and pin end signal wire contact 113.
Above-mentioned IMU measurement and control units are used to measure the raw measurement data of unmanned plane, such as acceleration, angular speed measurement letter
Breath, and by the raw measurement data to winged control computing unit；Fly control computing unit and carries out operation using these raw measurement datas
Obtain flight control parameter.Fly control computing unit to communicate with above-mentioned pin end 11 by circuit, be flown with being transmitted by signal wire
Control parameter.The IMU measurement and control units and winged control computing unit may be used the IMU measurement and control units of the prior art and fly control calculating
Unit.
The also embedded suction block 12 that is magnetic on each side wall of above-mentioned control module 1, to be attracted above-mentioned power plant module 2.
Power supply unit 14 is also equipped in above-mentioned control module 1, which is on entire unmanned plane during flying device
All modules provide power.
In order to better ensure that the balance during unmanned plane during flying, clump weight 13 is additionally provided in the control module 1.It should
One or more lightening hole is also provided in configuration block 13.
The structure of above-mentioned power plant module 2 such as Fig. 3-1 to Fig. 3-3, above-mentioned power plant module 2 are also regular hexagonal prism structure, and should
The side wall length of side of power plant module 2 is consistent with the side wall length of side of above-mentioned control module 1, so as to can be perfect with above-mentioned control module 1
It docks on ground.
Above-mentioned power plant module 2 includes：Shell 21, inner casing 22, supporting beam 23, blade 24, fixing sleeve 25, rotary shaft 26, mother
Connector 27 and iron block 28.
Shell 21 is the hexagonal prisms structure that middle part has cavity, and each side wall is connect with control module 1；Central cavity is used for
Accommodate inner casing 22.
Inner casing 22 is the cylindrical structure with cavity, and supporting beam 23 is connected on 22 inner wall of inner casing and to cavity center
Portion extends, and is connect with the fixing sleeve 25 positioned at 22 center of inner casing.Rotary shaft 26 is provided in fixing sleeve 25, and rotary shaft 26 is another
One end is fixed with blade 24 by sleeve.
Female connector 27 is fixed on the lateral wall of shell 21, and shape is corresponding with the pin end 11 on control module l side walls,
It is still cross-shaped configuration so that power plant module 2 can be quickly plugged in together with control module l.27 upper edge cross of female connector
The branch line of type is extended outward from cross center is disposed with female connector positive contact 271, female connector negative contact terminal 272
With female connector signal wire contact 273, and the contact in position and control module 1 corresponds.
In order to make the connection that can be more consolidated between power plant module 2 and control module l, also set on the side wall of the power plant module 2
Multiple iron blocks 28 are equipped with, the iron block 28 is corresponding with the multiple magnetic suction blocks 12 being arranged on control module l side walls.
Above-described embodiment is illustrated so that control module 1 and power plant module 2 are hexagonal prisms structure as an example, but this reality
It is not limited thereto with novel, above-mentioned control module 1 and power plant module 2 can also be other regular prism structures, and ensure positive rib
The side wall quantity of column is even number.
The operation principle of the utility model is as follows：
First, the quantity of control module 1 and power plant module 2 is determined according to the scale of required unmanned plane；Then, it will move
The progress grafting corresponding with the pin end of control module 1 of the female connector of power module 2, completes the quick assembling of aircraft.
During aircraft flight, control module l acquires the original measurement number of aircraft by IMU inertial navigation units etc. in real time
According to, including such as acceleration, angular speed metrical information, and operation is carried out according to these raw measurement datas, and according to operation knot
Fruit obtains flight parameter, including：Flight attitude, position of aircraft, speed, height etc., and controlled each according to the flight parameter
The operation of power plant module 2.
Compared with prior art, the Modularized splice formula aircraft of the utility model has superior harvesting property and maintenance
Property.It can be the application for being suitable for different occasions by splicing modules, be suitable for various use environments；When unmanned plane occurs
When failure, can quickly normally can again be come into operation by replacing module, and only need to the module of failure into
Row repair, saves maintenance cost, greatly improves work efficiency.
Embodiment two：
Two structure of embodiment as shown in figure 4, which show there are four control module 1 and multiple power plant modules 2 combination
Example shows to be suitable for various application demands at aircraft of different shapes by connection type Optional assembling according to this.
Certainly, the utility model do not limit to the connection type of above-described embodiment one and embodiment two, can also be
The combination of more control modules and power plant module.
In use, when needing unmanned plane during flying, control module and power plant module are spliced, the electricity of control module after assembling
Pond can be that power plant module powers to realize flight.
Although the utility model has been described by way of example and in terms of the preferred embodiments, embodiment does not limit the utility model.Not
It is detached from the spirit and scope of the utility model, any equivalent change or retouch done also belongs to the guarantor of the utility model
Protect range.Therefore the scope of protection of the utility model should be using the content that claims hereof is defined as standard.
Claims (6)
1. a kind of combined modular unmanned plane during flying device, which is characterized in that the combined modular unmanned plane during flying device packet
It includes：
Control module (1) and power plant module (2)；
The control module (1) is that the side wall quantity of regular prism structure and regular prism is even number, and ten are provided on each of which side wall
Font pin end；The power plant module (2) is multiple, and each power plant module (2) is equal with control module (1) side wall quantity
Regular prism structure, and it is provided with the cross female connector for capableing of grafting with the pin end (11) on each side wall；The cross
Corresponding positive contact, negative contact terminal and signal wire contact are both provided in type pin end and cross female connector；
It is provided with battery in the control module (1), passes through the positive contact and negative contact terminal pair of the pin end and female connector
It connects, power resources is provided for the power plant module；
It is provided in the control module (1) and flies control computing unit, the winged control computing unit is connect by the pin end and mother
The signal wire contact of head is connected, and transmission flight control parameter gives each power plant module (2).
2. a kind of combined modular unmanned plane during flying device according to claim 1, which is characterized in that
The positive contact, negative contact terminal and signal wire contact, along cross public affairs since the center of cross pin end
The branch line direction of connector is set gradually outward.
3. a kind of combined modular unmanned plane during flying device according to claim 1, which is characterized in that
The positive contact, negative contact terminal and signal wire contact, along cross public affairs since the center of cross female connector
The branch line direction of connector is set gradually outward.
4. a kind of combined modular unmanned plane during flying device according to claim 1, which is characterized in that
The also embedded suction block (12) that is magnetic on each side wall of the control module (1)；
Multiple iron blocks (28) corresponding with magnetic suction block (12) are additionally provided on each side wall of the power plant module (2).
5. a kind of combined modular unmanned plane during flying device according to claim 1, which is characterized in that the power plant module
(2) include：
Shell (21), inner casing (22), supporting beam (23), blade (24), fixing sleeve (25) and rotary shaft (26)；
The shell (21) is the regular prism structure with cavity, and the inner casing (22) is accommodated in the cavity；
The inner casing (22) is the cylindrical structure with cavity, and the supporting beam (23) is connected on the inner casing (22) inner wall
And extend to cavity center portion, it is connect with the fixing sleeve (25) positioned at inner casing (22) center；It is provided in the fixing sleeve (25)
Rotary shaft (26), and the other end of rotary shaft (26) is fixed with blade (24) by sleeve.
6. a kind of combined modular unmanned plane during flying device according to claim 1, which is characterized in that the control module
(1) clump weight (13) is additionally provided on.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721839283.4U CN207890009U (en) | 2017-12-25 | 2017-12-25 | A kind of combined modular unmanned plane during flying device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721839283.4U CN207890009U (en) | 2017-12-25 | 2017-12-25 | A kind of combined modular unmanned plane during flying device |
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| Publication Number | Publication Date |
|---|---|
| CN207890009U true CN207890009U (en) | 2018-09-21 |
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ID=63550067
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| CN201721839283.4U Active CN207890009U (en) | 2017-12-25 | 2017-12-25 | A kind of combined modular unmanned plane during flying device |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110861772A (en) * | 2019-12-03 | 2020-03-06 | 向杰 | Multifunctional device for aircraft |
| CN113165728A (en) * | 2019-12-03 | 2021-07-23 | 向杰 | Honeycomb array multi-rotor composite part, rack and aircraft |
| CN114787032A (en) * | 2020-12-11 | 2022-07-22 | 深圳市大疆创新科技有限公司 | Modular unmanned aerial vehicle and method of operating the same |
-
2017
- 2017-12-25 CN CN201721839283.4U patent/CN207890009U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110861772A (en) * | 2019-12-03 | 2020-03-06 | 向杰 | Multifunctional device for aircraft |
| CN113165728A (en) * | 2019-12-03 | 2021-07-23 | 向杰 | Honeycomb array multi-rotor composite part, rack and aircraft |
| CN114787032A (en) * | 2020-12-11 | 2022-07-22 | 深圳市大疆创新科技有限公司 | Modular unmanned aerial vehicle and method of operating the same |
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