CN206494124U - A kind of detachable unmanned plane - Google Patents
A kind of detachable unmanned plane Download PDFInfo
- Publication number
- CN206494124U CN206494124U CN201720089757.1U CN201720089757U CN206494124U CN 206494124 U CN206494124 U CN 206494124U CN 201720089757 U CN201720089757 U CN 201720089757U CN 206494124 U CN206494124 U CN 206494124U
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- main body
- plugboard
- horn
- connector
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Landscapes
- Toys (AREA)
Abstract
The utility model discloses a kind of detachable unmanned plane, with the unmanned plane main body being detachably connected（100）, undercarriage（300）And horn（200）, the unmanned plane main body（100）Lateral wall be provided with several symmetrical horn connecting seats（101）；The horn（200）One end be provided with rotor assemblies（201）, the other end passes through the first plugboard（103）With the second plugboard（203）It is detachable to coordinate electric connection, also pass through the first connector（102）With the second connector（202）Detachable cooperative mechanical connection.The utility model is simple in construction, convenient disassembly, with higher efficiency of assembling and structural stability, moreover it is possible to shake is produced because of the vibrations of rotor assemblies, ensures during flight stability and reliability effectively between reduction horn and fuselage main body.
Description
Technical field
The utility model is related to unmanned plane field, especially a kind of detachable unmanned plane.
Background technology
Unmanned air vehicle technique was developed rapidly in recent years, and multi-rotor unmanned aerial vehicle is widely used to public safety, power-line patrolling, friendship
A variety of application fields such as logical monitoring, fire-fighting, ocean and hydrological monitoring, military surveillance.Due to the requirement of Field Operational, many rotors without
Man-machine need to possess the functions such as detachable, portable, easy assembling, working stability, but existing multi-rotor unmanned aerial vehicle appoint exist it is following
Problem：
1st, although collapsible multi-rotor unmanned aerial vehicle is easy to store, and can assemble quick, but collapsible multi-rotor unmanned aerial vehicle is more suitable
For small-sized unmanned plane, for medium-and-large-sized unmanned plane, the volume after it is folded is excessively huge, between all parts easily
There is mutually collision, rub and damage.
2nd, part multi-rotor unmanned aerial vehicle connects each dismounting part, its disassembling part of unmanned plane by additional locking device
Part and locking device separated state after removal, locking device easily go out the situation of active.
3rd, in existing detachable multi-rotor unmanned aerial vehicle, if locking device is excessively complicated, its manufacturing cost is larger, and also needs
Consider its weight issue, if locking device is overweight, mechanical balance of the unmanned plane in state of flight can be influenceed.
4th, in existing detachable multi-rotor unmanned aerial vehicle, some locking devices, which exist, connects unsteady defect, in flight
During state, if locking device connection is built on the sand between horn and unmanned plane main body, easily because of rotation between horn and unmanned plane main body
Wing component and produce and rock, influence unmanned plane normal flight.
5th, in existing detachable multi-rotor unmanned aerial vehicle, horn, in assembling, is not supported blindmate to connect, wasted with fuselage body
Time in the operation of alignment, influences efficiency of assembling.
The content of the invention
Utility model purpose of the present utility model is：For above-mentioned problem there is provided one kind it is detachable nobody
Machine, it is simple in construction, it is easy to assemble, it is practical.
The technical solution adopted in the utility model is as follows：A kind of detachable unmanned plane, including unmanned plane main body, undercarriage
With several horns, the unmanned plane main body is removably mounted on undercarriage, and several described horns are arranged on unmanned plane
On the lateral wall of main body.
The unmanned plane also includes several horn connecting seats being symmetrically distributed on the lateral wall of the unmanned plane main body；
The fixing end of the horn connecting seat is fixedly connected with unmanned plane main body, and its free end is provided with the first connector and the first grafting
Plate, the rotor end end of the horn is provided with rotor assemblies, and its connection end is provided with the second connector and the second plugboard；Described first
Detachable cooperation is docked between plugboard and the second plugboard, and first connector and the second connector detachably coordinate company
Connect, first plugboard and the second plugboard include electrical interface and blind connecting-disconnecting interface.
Using said structure, the horn of unmanned plane is detachably separated with fuselage, first plugboard and the second plugboard
Including electrical interface and blind connecting-disconnecting interface, it is aligned to can be achieved to coordinate between horn and unmanned plane main body without naked eyes and is docked,
And complete to be electrically connected with；First connector and the second connector are mechanical splice, and machine is realized after its detachable mating connection
It is fixedly connected between arm and unmanned plane main body.
Based on above-described embodiment, further, first connector and the second connector at least have following two match somebody with somebody
Conjunction mode.
One：First connector includes external thread structure, is arranged on the outer wall of the free end of the horn connecting seat
On；Second connector includes being socketed in the first company with female thread structure and for being connected with external thread structure matching
Connection cover on fitting, the connection cover is also actively socketed on the connection end of the horn, and on the connection end of the horn
The cooperation connection cover is additionally provided with to limit the locating part of the scope of activities of the second connector.
Second, second connector is included on external thread structure, the outer wall for being arranged on the connection end of the horn；It is described
First connector includes being socketed on the second connector with female thread structure and for being connected with external thread structure matching
Connection cover, the connection cover is also actively socketed on the free end of the horn connecting seat, and the freedom of the horn connecting seat
The cooperation connection cover is additionally provided with end to limit the locating part of the scope of activities of the first connector.
Based on any of the above-described embodiment, further, the plugboard of first plugboard/second is provided with female electrical plug
Mouthful, several positioning holes and some locating pieces, the locating piece is outwardly to be arranged on the plugboard of first plugboard/second
On panel on.
It is corresponding, if the plugboard of second plugboard/first provided with male electric mortiser interface, several locating dowels and
A dry locating slot, the locating dowel is outwardly to be arranged on the panel of the plugboard of second plugboard/first.
The female electric mortiser interface is engaged with the male electric mortiser interface, and the positioning hole matches with the locating dowel
Close, the locating piece is engaged with the locating slot, the positioning hole, locating piece, locating dowel and locating slot are blind connecting-disconnecting interface.
Based on above-described embodiment, further, the undercarriage is main by landing pipe, support tube, bending connecting tube, inclination
Pipe, main body installing pipe and three-way pipe composition demountable structure；Wherein, several described landing pipes are connected by some three-way pipes
Connect the grounded parts of composition undercarriage, each three-way pipe is also associated with support tube, the support tube also successively with tipping tube and master
The bracket component of body installing pipe connection composition undercarriage, between the support tube and tipping tube, tipping tube and main body installing pipe it
Between connected by bending connecting tube, the connecting hole for connecting unmanned plane main body is further opened with the main body installing pipe.
Based on above-described embodiment, further, the undercarriage includes two groups of bracket components and two groups of phases being parallel to each other
Mutual parallel grounded parts, bracket component described in two groups is set in parallel between two groups of grounded parts.
Based on any of the above-described embodiment, further, the bottom of the unmanned plane main body, which is provided with, to be used to install described rise and fall
First inverted L shape dividing plate of frame and the 3rd inverted L shape dividing plate, and for carrying the second partition of battery component, first inverted L shape
The epipleural of dividing plate and the 3rd inverted L shape dividing plate is connected with the side wall of unmanned plane main body, the first inverted L shape dividing plate and the 3rd inverted L shape
The lower side panel of dividing plate is connected to the both sides of second partition；The first inverted L shape dividing plate, second partition and the 3rd inverted L shape
Some thermal vias are offered on dividing plate.
Based on above-described embodiment, further, being equipped with the first inverted L shape dividing plate and the 3rd inverted L shape dividing plate is used for
The undercarriage mounting seat being connected is matched with connecting hole.
Based on any of the above-described embodiment, further, the top of the unmanned plane main body is provided with cabin cover, the cabin cover
Be connected in hinged way with the hinge seat in the unmanned plane main body wall, the cabin cover in a snap-fit manner with the unmanned plane
Locking switch connection in main body wall, the hinge seat is oppositely arranged with locking switch.
Based on above-described embodiment, further, the cabin cover, which is protruded above, is provided with antenna cover, the inwall of the antenna cover
For the mounting groove for installing Anneta module.
In summary, by adopting the above-described technical solution, the beneficial effects of the utility model are：
1）The unmanned plane that the utility model is proposed possesses horn and the detachable separation function of fuselage, its first plugboard and
Second plugboard is aligned to can be achieved to coordinate between horn and unmanned plane main body without naked eyes and docked, and completes electrically to connect
Connect；Realize and be fixedly connected between horn and unmanned plane main body after being connected again by the first connector with the second connector.
2）Mode is detachably connected between its horn of the unmanned plane that the utility model is proposed and fuselage, it is simple and reliable,
There is larger connection contact area each other, strengthen the steadiness of its connection, and can cut down what rotor assemblies were produced on horn
The shaking force of all directions, ensures stability of the unmanned plane in state of flight.
3）The unmanned plane that the utility model is proposed, simple in construction, convenient disassembly, with higher efficiency of assembling and structure
Stability, moreover it is possible to shake is produced because of the vibrations of rotor assemblies effectively between reduction horn and fuselage main body, when ensureing flight
Stability and reliability；The undercarriage of the unmanned plane is also demountable structure, structural strong, can carry bigger weight；This
Utility model also has higher heat dispersion and wireless communication ability.
Brief description of the drawings
The utility model will illustrate by example and with reference to the appended drawing, wherein：
Fig. 1 is the complete machine structure schematic diagram of unmanned plane in the utility model.
Fig. 2 is the structural representation of horn connecting seat in the utility model.
Fig. 3 is the structural representation of horn in the utility model.
Fig. 4 is the structural representation of unmanned plane main body in the utility model.
In figure：
100- unmanned plane main bodys, 101- horn connecting seats, the connectors of 102- first, the plugboards of 103- first, 104- females
Electric mortiser interface, 105- positioning holes, 106- locating pieces, 107- the first inverted L shape dividing plates, 108- second partitions, the inverted L shapes of 109- the 3rd every
Plate, 110- cabin covers, 111- hinge seats, 112- locking switch, 113- antenna covers；
200- horns, 201- rotor assemblies, the connectors of 202- second, the plugboards of 203- second, 204- male electric mortiser interfaces,
205- locating dowels, 206- locating slots；
300- undercarriages, 301- landing pipes, 302- support tubes, 303- bending connecting tubes, 304- tipping tubes, 305- main bodys peace
Tubulature, 306- three-way pipes, 307- connecting holes.
Embodiment
All features disclosed in this specification, or disclosed all methods or during the step of, except mutually exclusive
Feature and/or step beyond, can combine in any way.
This specification（Including any accessory claim, summary）Disclosed in any feature, unless specifically stated otherwise,
Replaced by other equivalent or with similar purpose alternative features.I.e., unless specifically stated otherwise, each feature is a series of
An example in equivalent or similar characteristics.
As shown in Fig. 1, Fig. 1 describes a kind of detachable unmanned plane, including unmanned plane main body 100, the and of undercarriage 300
Several horns 200, the unmanned plane main body 100 is removably mounted on undercarriage 300, and several described horns 200 are set
Put on the lateral wall of unmanned plane main body 100.
Embodiment 1
In the utility model, the unmanned plane also includes several outsides for being symmetrically distributed in the unmanned plane main body 100
Horn connecting seat 101 on wall；The fixing end of the horn connecting seat 101 is fixedly connected with unmanned plane main body 100, its free end
Provided with the first connector 102 and the first plugboard 103, the rotor end end of the horn 200 is provided with rotor assemblies 201, and it is connected
End is provided with the second connector 202 and the second plugboard 203；It is detachable between the plugboard 203 of first plugboard 103 and second
Coordinate docking, the detachable mating connection of first connector, 102 and second connector 202, first plugboard 103 and the
Two plugboards 203 include electrical interface and blind connecting-disconnecting interface.
Using said structure, the horn of unmanned plane is detachably separated with fuselage, the grafting of the first plugboard 103 and second
Plate 203 includes electrical interface and blind connecting-disconnecting interface, be aligned without naked eyes can be achieved horn 200 and unmanned plane main body 100 it
Between coordinate docking, and complete be electrically connected with；The connector 202 of first connector 102 and second is mechanical splice, and its is detachable
Realize and be fixedly connected between horn 200 and unmanned plane main body 100 after mating connection.
Embodiment 2
As shown in Fig. 2 on the basis of embodiment 1, further, first connector 102 includes external thread structure,
On the outer wall for being arranged on the free end of the horn connecting seat 101；As shown in figure 3, second connector 202 is included with interior
Helicitic texture and the connection cover for being connected and being socketed on the first connector 102 with external thread structure matching, the connection cover
The cooperation connection cover is additionally provided with the connection end for being also actively socketed on the horn 200, and on the connection end of the horn 200
With the locating part for the scope of activities for limiting the second connector 202.
Embodiment 3
On the basis of embodiment 1, further, second connector 202 includes external thread structure, is arranged on described
On the outer wall of the connection end of horn 200；First connector 102 includes with female thread structure and is used for and external screw thread knot
Structure matching connects and is socketed in the connection cover on the second connector 202, and the connection cover is also actively socketed on the horn connection
The cooperation connection cover is additionally provided with the free end of seat 101, and on the free end of the horn connecting seat 101 to limit the first company
The locating part of the scope of activities of fitting 102.
In embodiment 2 and embodiment 3, the first connector 102 and the second connector 202 are realized removable using helicitic texture
Connection is unloaded, wherein, the female connection cover activity of tool is spacing to be socketed on the horn connecting seat 101 of horn 200/, and screw thread is solid
Surely it is socketed on the horn 200 of horn connecting seat 101/；When horn is assembled in unmanned plane main body, horn and machine only need to be docked
Arm connecting seat, after the first plugboard 103 and the second plugboard 203 coordinate and docked, rotatable connection lid the first connector 102 of connection
With the second connector 202, connection cover is hugged on the outer wall of the horn 200 of horn connecting seat 101/, increase locking device and horn
Contact area between 200 and horn connecting seat 101, strengthens the steadiness of connection, can cut down rotor assemblies and be produced on horn
All directions shaking force.
In the utility model, the locating part, which can protrude, to be arranged on the outer wall of the end of 200/ horn connecting seat of horn 101,
Its peak is connected to the distance at the center of 200/ horn connecting seat of horn 101 more than connection cover minimum point to the horn of horn 200/
The distance at 101 centers of seat.Connection cover is limited setting, and unloading part can be avoided to lose,
Embodiment 4
On the basis of embodiment 1 or 2 or 3, further, set on the plugboard 203 of the first plugboard 103/ second
There are female electric mortiser interface 104, several positioning holes 105 and some locating pieces 106, the locating piece 106 is outwardly to be arranged on
On panel on the plugboard 203 of first plugboard 103/ second.
It is corresponding, the plugboard 103 of the second plugboard 203/ first provided with male electric mortiser interface 204, several
Locating dowel 205 and several locating slots 206, the locating dowel 205 is outwardly to be arranged on second plugboard 203/ first
On the panel of plugboard 103.
The female electric mortiser interface 104 is engaged with the male electric mortiser interface 204, the positioning hole 105 with it is described fixed
Position post 205 is engaged, and the locating piece 106 is engaged with the locating slot 206, the positioning hole 105, locating piece 106, positioning
Post 205 and locating slot 206 are blind connecting-disconnecting interface.
Positioning hole 105 and locating dowel 205 of the utility model based on mutual cooperation, and the locating piece 106 cooperated
With locating slot 206, realize that blindmate can be carried out between horn and horn connecting seat pulls out connection.In assembling horn and unmanned plane main body
When, by horn close to horn connecting seat, the first plugboard 103 is oppositely arranged with the second plugboard 203, now, without naked eyes
The connecting interface between horn and horn connecting seat is aimed at, directly locating dowel and/or locating piece can be contacted on plugboard, made
Locating dowel insertion positioning hole, locating piece insertion locating slot, you can complete horn and docked with the matching of unmanned plane main body, operation letter
Single, assembling is quick.And in the presence of two kinds of location structures of locating dowel and locating piece, further enhance horn and unmanned owner
Connective stability between body, eliminates the vibrations of horn.
Embodiment 5
On the basis of any one of embodiment 1 ~ 4, further, the undercarriage 300 is main by landing pipe 301, support
Pipe 302, bending connecting tube 303, tipping tube 304, main body installing pipe 305 and the composition demountable structure of three-way pipe 306；Wherein, if
The dry landing pipe 301 is made up of the grounded parts of undercarriage 300, each three-way pipe some connections of three-way pipe 306
306 are also associated with support tube 302, and the support tube 302 is also connected and constituted with tipping tube 304 and main body installing pipe 305 successively
Fall the bracket component of frame 300, lead between the support tube 302 and tipping tube 304, between tipping tube 304 and main body installing pipe 305
Cross bending connecting tube 303 to connect, the connecting hole for connecting unmanned plane main body 100 is further opened with the main body installing pipe 305
307。
In the utility model, the undercarriage of multi-rotor unmanned aerial vehicle is also Demountable, and its undercarriage is detachably many
Between individual connection member, each connection member by three-way pipe or bending connecting tube be fixedly connected, using bending connecting tube,
Tipping tube, can strengthen the bearing capacity of undercarriage.Further, spring interface arrangment also can be set in the three-way pipe 306, increase
The convenience of strong ties, improves efficiency of assembling.
Further, the undercarriage 300 includes two groups of bracket components and two groups of ground connection being parallel to each other being parallel to each other
Part, bracket component described in two groups is set in parallel between two groups of grounded parts.
Embodiment 6
As shown in figure 4, based on any of the above-described embodiment, further, the bottom of the unmanned plane main body 100, which is provided with, to be used for
The the first inverted L shape dividing plate 107 and the 3rd inverted L shape dividing plate 109 of the undercarriage 300 are installed, and for carrying battery component
Second partition 108, the epipleural of the first inverted L shape dividing plate 107 and the 3rd inverted L shape dividing plate 109 with unmanned plane main body 100
The lower side panel of side wall connection, the first inverted L shape dividing plate 107 and the 3rd inverted L shape dividing plate 109 is connected to the two of second partition 108
Sidepiece；Some radiatings are offered on the first inverted L shape dividing plate 107, the inverted L shape dividing plate 109 of second partition 108 and the 3rd logical
Hole.
Using said structure, the unmanned plane main body 100 in the utility model has higher heat dispersion, for carrying electricity
The second partition 108 of pond component is arranged between the first inverted L shape dividing plate 107 and the 3rd inverted L shape dividing plate 109 so that in cross section
On, the bottom of unmanned plane main body is in integrally the structure of falling convex character shape, and battery component is arranged in second partition 108, it is possible to decrease nobody
The overall center of gravity of machine, improves stability during unmanned plane during flying.In addition, offering some thermal vias on each dividing plate, have
Effect improves the heat dispersion of unmanned plane main body inner wall, in flight, and cold air can be effectively from the first inverted L shape dividing plate 107 and the
The thermal vias of three inverted L shape dividing plates 109 enters unmanned plane body interior, and hot-air is exported from the thermal vias of second partition 108,
Complete heat discharging operation.
Further, being equipped with the first inverted L shape dividing plate 107 and the 3rd inverted L shape dividing plate 109 is used for and connecting hole
The undercarriage mounting seat of 307 matching connections.In the utility model, it can be connected between undercarriage and unmanned plane main body by wing nut
Connect, convenient and swift, stable connection is reliable.
Embodiment 7
Based on any of the above-described embodiment, further, the top of the unmanned plane main body 100 is provided with cabin cover 110, described
Cabin cover 110 is connected with the hinge seat 111 on the side wall of unmanned plane main body 100 in hinged way, and the cabin cover 110 is with card
Button mode is connected with the locking switch 112 on the side wall of unmanned plane main body 100, the hinge seat 111 and the phase of locking switch 112
To setting.Using snap, can effective guarantee in flight course, cabin cover 110 is closed all the time, it is not easy to because
Fuselage rocks, shakes and open.
Embodiment 8
Based on above-described embodiment, further, the cabin cover 110, which is protruded above, is provided with antenna cover 113, the antenna cover
113 inwall is the mounting groove for installing Anneta module.The protrusion of antenna cover 113 is arranged on cabin cover 110, nothing can be strengthened
Man-machine communication capacity.
The utility model is not limited to foregoing embodiment.The utility model expands to any in this specification
The new feature of middle disclosure or any new combination, and disclose any new method or process the step of or any new group
Close.
Claims (10)
1. a kind of detachable unmanned plane, including unmanned plane main body（100）, undercarriage（300）With several horns（200）, institute
State unmanned plane main body（100）It is removably mounted to undercarriage（300）On, several described horns（200）It is arranged on unmanned plane
Main body（100）Lateral wall on, it is characterised in that：
The unmanned plane is also symmetrically distributed in the unmanned plane main body including several（100）Lateral wall on horn connecting seat
（101）；The horn connecting seat（101）Fixing end and unmanned plane main body（100）It is fixedly connected, its free end connects provided with first
Fitting（102）With the first plugboard（103）；The horn（200）Rotor end be provided with rotor assemblies（201）, its connection end is set
There is the second connector（202）With the second plugboard（203）；First plugboard（103）With the second plugboard（203）Between can
Dismounting coordinates docking, first connector（102）With the second connector（202）It is detachable to be connected, first grafting
Plate（103）With the second plugboard（203）Including electrical interface and blind connecting-disconnecting interface.
2. based on a kind of detachable unmanned plane described in claim 1, it is characterised in that：First connector（102）Bag
External thread structure is included, the horn connecting seat is arranged on（101）Free end outer wall on；
Second connector（202）Including being socketed in female thread structure and for being connected with external thread structure matching
First connector（102）On connection cover, the connection cover is also actively socketed on the horn（200）Connection end on, and institute
State horn（200）Connection end on the cooperation connection cover is additionally provided with to limit the second connector（202）Scope of activities limit
Position part.
3. based on a kind of detachable unmanned plane described in claim 1, it is characterised in that：Second connector（202）Bag
External thread structure is included, the horn is arranged on（200）Connection end outer wall on；
First connector（102）Including being socketed in female thread structure and for being connected with external thread structure matching
Second connector（202）On connection cover, the connection cover is also actively socketed on the horn connecting seat（101）Free end
On, and the horn connecting seat（101）Free end on the cooperation connection cover is additionally provided with to limit the first connector（102）'s
The locating part of scope of activities.
4. based on a kind of detachable unmanned plane described in any one of claim 1 ~ 3, it is characterised in that：First plugboard
（103）/ the second plugboard（203）It is provided with female electric mortiser interface（104）, several positioning holes（105）And some locating pieces
（106）, the locating piece（106）It is outwardly to be arranged on first plugboard（103）/ the second plugboard（203）On face
On plate；
Corresponding, second plugboard（203）/ the first plugboard（103）It is provided with male electric mortiser interface（204）, it is some
Individual locating dowel（205）And several locating slots（206）, the locating dowel（205）It is outwardly to be arranged on second plugboard
（203）/ the first plugboard（103）Panel on；
The female electric mortiser interface（104）With the male electric mortiser interface（204）It is engaged, the positioning hole（105）With it is described
Locating dowel（205）It is engaged, the locating piece（106）With the locating slot（206）It is engaged, the positioning hole（105）, positioning
Block（106）, locating dowel（205）And locating slot（206）For blind connecting-disconnecting interface.
5. based on a kind of detachable unmanned plane described in claim 1, it is characterised in that：The undercarriage（300）It is main by
Landing pipe（301）, support tube（302）, bending connecting tube（303）, tipping tube（304）, main body installing pipe（305）And three-way pipe
（306）Constitute demountable structure；
Wherein, several described landing pipes（301）Pass through some three-way pipes（306）Connection composition undercarriage（300）Connect
Ground part, each three-way pipe（306）It is also associated with support tube（302）, the support tube（302）Also successively with tipping tube（304）
With main body installing pipe（305）Connection composition undercarriage（300）Bracket component, the support tube（302）With tipping tube（304）It
Between, tipping tube（304）With main body installing pipe（305）Between by bending connecting tube（303）Connection, the main body installing pipe
（305）On be further opened be used for connect unmanned plane main body（100）Connecting hole（307）.
6. based on a kind of detachable unmanned plane described in claim 5, it is characterised in that：The undercarriage（300）Including two
Bracket component and two groups of grounded parts being parallel to each other that group is parallel to each other, bracket component described in two groups are set in parallel in two groups and connect
Between ground part.
7. based on a kind of detachable unmanned plane described in any one of claim 1 ~ 3,5 and 6, it is characterised in that：It is described nobody
Owner's body（100）Bottom be provided be used for the undercarriage is installed（300）The first inverted L shape dividing plate（107）With the 3rd inverted L shape every
Plate（109）, and for carrying the second partition of battery component（108）, the first inverted L shape dividing plate（107）With the 3rd inverted L shape
Dividing plate（109）Epipleural with unmanned plane main body（100）The connection of side wall, the first inverted L shape dividing plate（107）With the 3rd inverted L shape
Dividing plate（109）Lower side panel be connected to second partition（108）Both sides；The first inverted L shape dividing plate（107）, second
Dividing plate（108）With the 3rd inverted L shape dividing plate（109）On offer some thermal vias.
8. based on a kind of detachable unmanned plane described in claim 7, it is characterised in that：The first inverted L shape dividing plate（107）
With the 3rd inverted L shape dividing plate（109）On be equipped with and be used for and connecting hole（307）Match the undercarriage mounting seat of connection.
9. based on a kind of detachable unmanned plane described in any one of claim 1 ~ 3,5,6 and 8, it is characterised in that：The nothing
Man-machine main body（100）Top be provided with cabin cover（110）, the cabin cover（110）In hinged way with the unmanned plane main body
（100）Hinge seat on the wall of side（111）Connection, the cabin cover（110）In a snap-fit manner with the unmanned plane main body（100）Side
Locking switch on wall（112）Connection, the hinge seat（111）With locking switch（112）It is oppositely arranged.
10. based on a kind of detachable unmanned plane described in claim 9, it is characterised in that：The cabin cover（110）Protrude above
It is provided with antenna cover（113）, the antenna cover（113）Inwall be mounting groove for installing Anneta module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720089757.1U CN206494124U (en) | 2017-01-24 | 2017-01-24 | A kind of detachable unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720089757.1U CN206494124U (en) | 2017-01-24 | 2017-01-24 | A kind of detachable unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206494124U true CN206494124U (en) | 2017-09-15 |
Family
ID=59803890
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720089757.1U Active CN206494124U (en) | 2017-01-24 | 2017-01-24 | A kind of detachable unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206494124U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108177767A (en) * | 2017-12-04 | 2018-06-19 | 陈威巍 | A kind of multi-rotor unmanned aerial vehicle |
| CN110341949A (en) * | 2019-08-16 | 2019-10-18 | 厦门大学嘉庚学院 | A kind of unmanned dispensing device and its application method |
| CN112644683A (en) * | 2021-01-18 | 2021-04-13 | 傅荣 | Unmanned aerial vehicle frame construction that can freely assemble |
| CN114194383A (en) * | 2021-12-07 | 2022-03-18 | 中电科芜湖通用航空产业技术研究院有限公司 | Unmanned aerial vehicle undercarriage and unmanned aerial vehicle |
-
2017
- 2017-01-24 CN CN201720089757.1U patent/CN206494124U/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108177767A (en) * | 2017-12-04 | 2018-06-19 | 陈威巍 | A kind of multi-rotor unmanned aerial vehicle |
| CN110341949A (en) * | 2019-08-16 | 2019-10-18 | 厦门大学嘉庚学院 | A kind of unmanned dispensing device and its application method |
| CN110341949B (en) * | 2019-08-16 | 2024-04-12 | 厦门大学嘉庚学院 | Unmanned distribution equipment and use method thereof |
| CN112644683A (en) * | 2021-01-18 | 2021-04-13 | 傅荣 | Unmanned aerial vehicle frame construction that can freely assemble |
| CN114194383A (en) * | 2021-12-07 | 2022-03-18 | 中电科芜湖通用航空产业技术研究院有限公司 | Unmanned aerial vehicle undercarriage and unmanned aerial vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206494124U (en) | A kind of detachable unmanned plane | |
| CN105691589B (en) | Unmanned vehicle | |
| CN105000163B (en) | A kind of more rotor unmanned aircrafts of fold-down formula | |
| CN104580606B (en) | A kind of mobile phone shell that can be changed into unmanned plane | |
| CN106184729A (en) | A kind of many rotor wing unmanned aerial vehicles | |
| CN106892128A (en) | The multi-functional landing platform of rotor wing unmanned aerial vehicle | |
| CN109515706A (en) | A kind of Modularized unmanned machine | |
| CN109050898A (en) | Non-homogeneous ten rotor wing unmanned aerial vehicle of power arrangement formula | |
| CN106892086A (en) | A kind of multi-rotor unmanned aerial vehicle | |
| US20220001980A1 (en) | Group configurations for a modular drone system | |
| CN205574258U (en) | Unmanned aerial vehicle | |
| US20210217318A1 (en) | Autonomous aerial vehicle system | |
| CN107933902A (en) | A kind of more rotor unmanned aircrafts | |
| CN107031828A (en) | A kind of unmanned plane | |
| CN105947210B (en) | A kind of four axis folding unmanned planes | |
| CN107235139A (en) | Portable many rotor unmanned aircrafts | |
| CN205010466U (en) | A casing for folding rotor unmanned aerial vehicle | |
| CN106005362A (en) | Multifunctional unmanned aerial vehicle frame set | |
| CN110539889A (en) | Plant protection unmanned aerial vehicle of two medical-kit double cell overall arrangement of big load | |
| CN208360493U (en) | A kind of portable aerial survey quadrotor drone | |
| CN106184745A (en) | flapping wing aircraft | |
| CN207311823U (en) | Unmanned plane and its frame assembly | |
| CN105109679B (en) | A kind of latch assembly and many rotor unmanned aircrafts | |
| CN208198805U (en) | Unmanned plane | |
| CN209454991U (en) | A kind of Modularized unmanned machine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |