CN106828896A - Modularization concatenation formula unmanned aerial vehicle - Google Patents
Modularization concatenation formula unmanned aerial vehicle Download PDFInfo
- Publication number
- CN106828896A CN106828896A CN201611249816.3A CN201611249816A CN106828896A CN 106828896 A CN106828896 A CN 106828896A CN 201611249816 A CN201611249816 A CN 201611249816A CN 106828896 A CN106828896 A CN 106828896A
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- China
- Prior art keywords
- module
- main body
- navigation
- unmanned plane
- rotor
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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 8
- 238000012423 maintenance Methods 0.000 abstract description 4
- 241001544487 Macromiidae Species 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000012938 design process Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000012827 research and development Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H5/00—Arrangements on vessels of propulsion elements directly acting on water
- B63H5/07—Arrangements on vessels of propulsion elements directly acting on water of propellers
- B63H5/08—Arrangements on vessels of propulsion elements directly acting on water of propellers of more than one propeller
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C37/00—Convertible aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/13—Propulsion using external fans or propellers
- B64U50/14—Propulsion using external fans or propellers ducted or shrouded
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Ocean & Marine Engineering (AREA)
- Remote Sensing (AREA)
- Manufacture Of Motors, Generators (AREA)
Abstract
The modularized spliced unmanned aerial vehicle comprises a main body module and a power module, wherein the power module comprises a rotor wing module capable of providing longitudinal thrust to fly and a navigation module capable of providing transverse thrust to navigate, the main body module is detachably connected with the rotor wing module or the navigation module, and the power module is electrically connected with the main body module. Compared with the prior art, the modularized spliced unmanned aerial vehicle has excellent maneuvering performance, can realize the function of air flight or marine navigation by splicing each module, and is suitable for various use environments; when unmanned aerial vehicle broke down, can normally drop into use once more fast through changing the module, in addition only need to break down the module maintain can, need not to inspect the complete machine, saved cost of maintenance, improved work efficiency greatly.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, and in particular to Modularized splice formula unmanned plane.
Background technology
In recent years, unmanned vehicle/unmanned plane has been widely used for various fields, for example Aerial photography, investigation,
Scientific research, geologic survey and remote sensing.China's SUAV industry is started late, in profile, specification chi in design process
One is to refer to external active service unmanned aerial vehicle design to very little and carrying equipment aspect, and unmanned plane is usually an overall structure, mainly
Between functional module by the way of being fixedly connected, there is larger deficiency at aspects such as transport, making, such as it is a certain in unmanned plane
During damage parts, can only whole unmanned plane sent for maintenance, it is impossible in time, quickly cope with problem.And existing unmanned plane is special
Strong with property, the adaptability to disaster relief environment is poor, needs to use different types of unmanned plane for different disaster environments, for example
Aerial reconnaissance needs to use the unmanned plane of aviation formula, and the unmanned plane of navigation formula is needed to use when at sea scouting rescue, there is machine
Dynamic performance is looked into, and utilization rate is low, R＆D costs problem high.
The content of the invention
There is above-mentioned technical problem for prior art, the present invention provides a kind of suitable various environment, saves manufacture maintenance
Cost, improves the Modularized splice formula unmanned plane of operating efficiency.
Invention thinking：.
To achieve the above object, the present invention provides following technical scheme：
Modularized splice formula unmanned plane, including main body module and power plant module are provided, the power plant module includes to provide vertical
It is described to thrust is so as to the rotor module flown and/or can provide lateral thrust so as to the navigation module navigated by water
Main body module is detachably connected the rotor module and/or navigation module, is when the power plant module is connected to main body module
Electrical connection.
Wherein, the rotor module includes multiple, and multiple rotor modules are evenly arranged around the main body module.
Wherein, the cross section of the cross section of the main body module and the rotor module is regular hexagon, the rotor
Module is six, and the side of six sides of rotor module respectively with the main body module is connected.
Wherein, it is detachably connected between two neighboring rotor module.
Wherein, the cross section of the cross section of the main body module and the navigation module is regular hexagon, the navigation
Module is provided with two, the both sides connection adjacent with main body module or relative respectively of two navigation modules.
Wherein, it is detachably connected between two navigation modules.
Beneficial effects of the present invention：
Modularized splice formula unmanned plane of the invention, including main body module and power plant module, power plant module include to provide vertical
To thrust is so as to the rotor module flown and can provide lateral thrust so as to the navigation module navigated by water, main body module
Rotor module or navigation module are detachably connected, are electrical connection when power plant module is connected to main body module.When using, work as needs
During unmanned plane during flying, main body module and rotor module are spliced, main body module can power so as to export for rotor module after assembling
The power of longitudinal direction and then flight；When needing unmanned plane to navigate by water on the water, main body module and navigation module are spliced, after assembling
Main body module is navigated by water for navigation module for power supply so as to export lateral dynamics.Compared with prior art, modularization of the invention
Spliced unmanned aerial vehicle has superior mobility, can be capable of achieving airflight or marine boat by splicing modules
Capable function, it is adaptable to various use environments；When unmanned plane breaks down, can by changing module by quickly it is normal again
It is secondary to come into operation, and only need to repair the module for breaking down, without checking whole machine, save dimension
Accomplish this, substantially increase operating efficiency.
Brief description of the drawings
Fig. 1 is the rotor module structural representation of Modularized splice formula unmanned plane of the invention.
Fig. 2 is the navigation modular structure schematic diagram of Modularized splice formula unmanned plane of the invention.
Structural representation when Fig. 3 is the offline mode of Modularized splice formula unmanned plane of the invention.
Structural representation when Fig. 4 is the sail mode of Modularized splice formula unmanned plane of the invention.
Reference：
Main body module 1；
Rotor module 2；
Navigation module 3.
Specific embodiment
Below in conjunction with specific embodiment and accompanying drawing, the present invention is described in detail.
The Modularized splice formula unmanned plane of the present embodiment, as shown in Figures 1 to 4, including main body module 1 and power plant module,
Power plant module includes that longitudinal thrust can be provided so as to the rotor module 2 flown and can provide lateral thrust so as to carry out
The navigation module 3 of navigation, main body module 1 is detachably connected rotor module 2 or navigation module 3, when power plant module is connected to main body
It is electrical connection during module 1, and junction is waterproof.When using, when unmanned plane during flying is needed, unmanned plane is carried by cruiser
Modules, when receiving alarm it is rapid assemble and release unmanned plane go to live scouting, cruiser before scene is arrived at just
Field condition is grasped, rescue work can faster launch, main body module 1 and rotor module 2 is spliced to form as shown in Figure 3
Structure, main body module 1 can power so as to export longitudinal power and then flight for rotor module 2 after assembling；When needing unmanned plane
When navigating by water on the water, recyclable unmanned plane converts its mode of operation after cruiser arrives at scene, main body module 1 and navigation module
3 splicings, form structure as shown in Figure 4, and the main body module 1 after assembling powers to enter so as to export lateral dynamics for navigation module 3
Row navigation, live support is changed into from scene scouting, is acted on unmanned plane and is maximized.Compared with prior art, module of the invention
Changing spliced unmanned aerial vehicle has superior mobility, can be capable of achieving airflight or sea by splicing modules
The function of navigation, it is adaptable to various use environments；When unmanned plane breaks down, can by changing module by it is quickly normal
Come into operation again, and only need to repair the module for breaking down, without checking whole machine, save
Maintenance cost, substantially increases operating efficiency.
In the present embodiment, the cross section of main body module 1 and the cross section of rotor module 2 are regular hexagon and both length of sides
Equal, rotor module 2 is six, and the side of six sides of rotor module 2 respectively with main body module 1 is connected, two neighboring rotation
It is detachably connected between wing module 2, after splicing, overall structure is compact.
In the present embodiment, the cross section of main body module 1 and the cross section of navigation module 3 are regular hexagon, navigation module 3
It is provided with two, the adjacent both sides connection respectively with main body module 1 of two navigation modules 3 is detachable between two navigation modules 3
Connection.After splicing, overall structure is compact.
Finally it should be noted that the above embodiments are merely illustrative of the technical solutions of the present invention, rather than the present invention is protected
The limitation of scope is protected, although being explained to the present invention with reference to preferred embodiment, one of ordinary skill in the art should
Work as understanding, technical scheme can be modified or equivalent, without deviating from the reality of technical solution of the present invention
Matter and scope.
Claims (6)
1. Modularized splice formula unmanned plane, it is characterized in that：Including main body module and power plant module, the power plant module includes can
Longitudinal thrust is provided so as to the rotor module flown or/and lateral thrust can be provided so as to the navigation mould for being navigated by water
Block, the main body module is detachably connected the rotor module or/and navigation module, when the power plant module is connected to main body mould
Connection is conducted during block simultaneously with one another.
2. Modularized splice formula unmanned plane according to claim 1, it is characterized in that：The rotor module includes multiple, many
Individual rotor module is evenly arranged around the main body module.
3. Modularized splice formula unmanned plane according to claim 2, it is characterized in that：The cross section of the main body module and institute
The cross section for stating rotor module is regular hexagon, and the rotor module is six, six sides of rotor module respectively with institute
State the side connection of main body module.
4. Modularized splice formula unmanned plane according to claim 3, it is characterized in that：It is removable between two neighboring rotor module
Unload connection.
5. Modularized splice formula unmanned plane according to claim 1, it is characterized in that：The cross section of the main body module and institute
The cross section for stating navigation module is regular hexagon, and the navigation module is provided with two, two navigation modules respectively with main body mould
The adjacent or relative both sides connection of block.
6. Modularized splice formula unmanned plane according to claim 5, it is characterized in that：Detachably connect between two navigation modules
Connect.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611249816.3A CN106828896A (en) | 2016-12-29 | 2016-12-29 | Modularization concatenation formula unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611249816.3A CN106828896A (en) | 2016-12-29 | 2016-12-29 | Modularization concatenation formula unmanned aerial vehicle |
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| Publication Number | Publication Date |
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| CN106828896A true CN106828896A (en) | 2017-06-13 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611249816.3A Pending CN106828896A (en) | 2016-12-29 | 2016-12-29 | Modularization concatenation formula unmanned aerial vehicle |
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Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107264769A (en) * | 2017-06-22 | 2017-10-20 | 北京信息科技大学 | A kind of rigid multi-rotor aerocraft combination system |
| CN108674677A (en) * | 2018-05-28 | 2018-10-19 | 河南农贝得农业科技有限公司 | A kind of dismountable unmanned plane anticollision damping device |
| CN108791878A (en) * | 2018-07-12 | 2018-11-13 | 首航国翼（武汉）科技有限公司 | A kind of Modularized unmanned machine |
| CN108883836A (en) * | 2017-12-13 | 2018-11-23 | 深圳市大疆创新科技有限公司 | Unmanned plane and UAV system |
| CN109398704A (en) * | 2018-12-19 | 2019-03-01 | 向杰 | A kind of urgent transport flight equipment |
| CN109515702A (en) * | 2019-01-15 | 2019-03-26 | 张轶南 | A kind of portable, modularization, expansible 3D printing multi-rotor unmanned aerial vehicle |
| CN111123968A (en) * | 2020-02-03 | 2020-05-08 | 向杰 | Honeycomb array aircraft control system |
| CN113220012A (en) * | 2021-04-06 | 2021-08-06 | 中国电子科技集团公司电子科学研究院 | Integrated cabin section for swarm unmanned aerial vehicle and swarm unmanned aerial vehicle |
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| CN102556341A (en) * | 2011-12-05 | 2012-07-11 | 北京航空航天大学 | Group flying robot with distribution and self-assembly characteristics |
| CN104608923A (en) * | 2015-01-31 | 2015-05-13 | 中南大学 | Honeycomb-type six-rotor transport aircraft |
| CN105539823A (en) * | 2015-12-25 | 2016-05-04 | 深圳市哆啦智能科技有限公司 | Assembling multi-rotor air vehicle |
| KR20160094052A (en) * | 2015-01-30 | 2016-08-09 | 순천향대학교 산학협력단 | Improved drone |
| CN205661655U (en) * | 2016-06-03 | 2016-10-26 | 南京奇蛙智能科技有限公司 | Many rotor unmanned aerial vehicle of modularization combination formula |
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2016
- 2016-12-29 CN CN201611249816.3A patent/CN106828896A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN102556341A (en) * | 2011-12-05 | 2012-07-11 | 北京航空航天大学 | Group flying robot with distribution and self-assembly characteristics |
| KR20160094052A (en) * | 2015-01-30 | 2016-08-09 | 순천향대학교 산학협력단 | Improved drone |
| CN104608923A (en) * | 2015-01-31 | 2015-05-13 | 中南大学 | Honeycomb-type six-rotor transport aircraft |
| CN105539823A (en) * | 2015-12-25 | 2016-05-04 | 深圳市哆啦智能科技有限公司 | Assembling multi-rotor air vehicle |
| CN205661655U (en) * | 2016-06-03 | 2016-10-26 | 南京奇蛙智能科技有限公司 | Many rotor unmanned aerial vehicle of modularization combination formula |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107264769A (en) * | 2017-06-22 | 2017-10-20 | 北京信息科技大学 | A kind of rigid multi-rotor aerocraft combination system |
| CN107264769B (en) * | 2017-06-22 | 2020-05-08 | 北京信息科技大学 | Rigid multi-rotor aircraft merging system |
| CN108883836A (en) * | 2017-12-13 | 2018-11-23 | 深圳市大疆创新科技有限公司 | Unmanned plane and UAV system |
| WO2019113845A1 (en) * | 2017-12-13 | 2019-06-20 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and unmanned aerial vehicle system |
| CN108674677A (en) * | 2018-05-28 | 2018-10-19 | 河南农贝得农业科技有限公司 | A kind of dismountable unmanned plane anticollision damping device |
| CN108791878A (en) * | 2018-07-12 | 2018-11-13 | 首航国翼（武汉）科技有限公司 | A kind of Modularized unmanned machine |
| CN109398704A (en) * | 2018-12-19 | 2019-03-01 | 向杰 | A kind of urgent transport flight equipment |
| CN109515702A (en) * | 2019-01-15 | 2019-03-26 | 张轶南 | A kind of portable, modularization, expansible 3D printing multi-rotor unmanned aerial vehicle |
| CN111123968A (en) * | 2020-02-03 | 2020-05-08 | 向杰 | Honeycomb array aircraft control system |
| CN113220012A (en) * | 2021-04-06 | 2021-08-06 | 中国电子科技集团公司电子科学研究院 | Integrated cabin section for swarm unmanned aerial vehicle and swarm unmanned aerial vehicle |
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Application publication date: 20170613 |