CN206766346U - A kind of unmanned plane for lifting endurance - Google Patents
A kind of unmanned plane for lifting endurance Download PDFInfo
- Publication number
- CN206766346U CN206766346U CN201720501650.3U CN201720501650U CN206766346U CN 206766346 U CN206766346 U CN 206766346U CN 201720501650 U CN201720501650 U CN 201720501650U CN 206766346 U CN206766346 U CN 206766346U
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- unmanned plane
- composite cable
- fixed
- reduction box
- gear reduction
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Abstract
The utility model discloses a kind of unmanned plane for lifting endurance,Including unmanned plane body and cop plug,The unmanned plane body upper end is provided with thermal infrared sensor,The unmanned plane body lower end is connected with composite cable,Composite cable wrapping head is installed on the right side of the composite cable,Gear reduction box servomotor is fixed with the right side of the composite cable wrapping head,Linear screw driving lock is installed on the right side of the gear reduction box servomotor,Conical overcoat is fixed with the upside of the linear screw driving lock,Flight controller is fixed with the right side of the linear screw driving lock,The cop plug upper end is connected with infrared external reflection position sensor,The infrared external reflection position sensor is provided with shell,Built-in thrust bearing is fixed with the left of the shell,Driving gear component is fixed with the downside of the gear reduction box servomotor.The unmanned plane of the lifting endurance has reasonable in design, simple, and endurance is strong.
Description
Technical field
The utility model belongs to unmanned air vehicle technique field, and in particular to a kind of unmanned plane for lifting endurance.
Background technology
Unmanned plane is the not manned aircraft manipulated using radio robot and the presetting apparatus provided for oneself.Nothing on machine
Driving cabin, but the equipment such as automatic pilot, presetting apparatus are installed.On ground, naval vessels or machine tool remote control station personnel pass through
The equipment such as radar, it is tracked, positioned, is remotely controlled, remote measurement and Digital Transmission.Can be under wireless remotecontrol as conventional airplane one
Sample takes off or launched with booster rocket, can also take aerial launch to by machine tool and fly.During recovery, it can with conventional airplane
The same mode automatic Landing of land process, it can also be reclaimed by remote control parachute or block.It can be reused several times.Use extensively
In aerial reconnaissance, monitoring, communication, antisubmarine, electronic interferences etc..
Unmanned plane in the market, it is maximum the problem of be endurance, either occupation rate highest in the world at present
Big boundary unmanned plane, or the unmanned plane of some sector applications, general civilian unmanned plane endurance is not strong, and in the market has
A little unmanned plane during flyings are also unstable, and structure is not compact enough, and position is not accurate enough, and service life is not grown, and are not suitable for very much extensively should
Used in every profession and trade, therefore the unmanned plane with lifting endurance is found as mainly solving the problems, such as at present.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane for lifting endurance, to solve in above-mentioned background technology
The problem of proposition.
To achieve the above object, the utility model provides following technical scheme：A kind of unmanned plane for lifting endurance, bag
Unmanned plane body and cop plug are included, the unmanned plane body upper end is provided with thermal infrared sensor, the unmanned plane body
Lower end is connected with composite cable, and composite cable wrapping head is provided with the right side of the composite cable, and the composite cable wrapping head is right
Side is fixed with gear reduction box servomotor, and linear screw driving locking is provided with the right side of the gear reduction box servomotor
Device, the linear screw driving lock upside are fixed with conical overcoat, fixed on the right side of the linear screw driving lock
There is flight controller, the cop plug upper end is connected with infrared external reflection position sensor, the infrared external reflection position sensing
Device is provided with shell, and built-in thrust bearing is fixed with the left of the shell, is fixed with the downside of the gear reduction box servomotor
Driving gear component.
Preferably, the cop plug inside left is provided with vertical direction lock hole, the vertical direction lock hole
Right side is fixed with direction alignment mark layer.
Preferably, it is fixed with lock pin on the inside of the conical overcoat.
Preferably, the clutch end of the gear reduction box servomotor passes through outside driving gear component and outer set upper side
The gear engagement in portion.
Preferably, the composite cable wrapping head is wrapped in composite cable surface and controls composite cable by folding and unfolding
Length.
Preferably, the flight controller controls unmanned plane body by composite cable.
Technique effect of the present utility model and advantage：The unmanned plane of the lifting endurance passes through inside cop plug
Left side is provided with vertical direction lock hole, is fixed with direction alignment mark layer on the right side of vertical direction lock hole, unmanned plane passes through circle
The grafting of cone-shaped plug can ensure the stabilization of unmanned plane structure, it is improved work capacity, and service life is grown, in conical overcoat
Side is fixed with lock pin, its advantage be lock pin be fix conical overcoat with this come protect cop plug by the external world extruding and
Destroying, the clutch end of gear reduction box servomotor is engaged by driving gear component with the gear outside outer set upper side,
Its advantage is that the gear reduction box servomotor drives unmanned plane during flying by pinion rotation, and composite cable wrapping head is wrapped in
Composite cable surface and the length that composite cable is controlled by folding and unfolding, its advantage are that the unmanned plane can for a long time hover and be detected
Operation, there is higher detection range, flight controller controls unmanned plane body by composite cable, and its advantage is unmanned plane
Thermal infrared sensor on body effectively can be accurately positioned to the position on ground.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model；
Fig. 2 is the structural representation inside the utility model cop plug.
In figure：1 unmanned plane body, 2 thermal infrared sensors, 3 composite cables, 4 composite cable wrapping heads, 5 gear reduction boxs
Servomotor, 6 driving gear components, 7 lock pins, 8 conical overcoats, 9 linear screws driving lock, 10 flight controllers, 11
Shell, 12 infrared external reflection position sensors, 13 cop plugs, 131 vertical direction lock holes, 132 direction alignment mark layers, 14
Built-in thrust bearing.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belong to the scope of the utility model protection.
Referring to Fig. 1, Fig. 1 is structural representation of the present utility model；A kind of unmanned plane for lifting endurance, including nothing
Man-machine body 1 and cop plug 13, the upper end of unmanned plane body 1 are provided with thermal infrared sensor 2, its thermal infrared sensor
2 function is effectively the position on ground to be accurately positioned, and the lower end of unmanned plane body 1 is connected with composite cable 3,
The function of its composite cable 3 is mainly connected to unmanned plane body 1, unmanned plane is hovered for a long time with this and carries out detection operation,
The right side of composite cable 3 is provided with composite cable wrapping head 4, and the function of its composite cable wrapping head 4 is that composite cable 3 is entered
Row winding, the right side of composite cable wrapping head 4 are fixed with gear reduction box servomotor 5, its gear reduction box servomotor 5
Function be that unmanned plane during flying is driven by pinion rotation, the right side of gear reduction box servomotor 5 is provided with straight line spiral shell
Bar drives lock 9, and the function of its linear screw driving lock 9 is that unmanned plane propeller is driven and locked, described
The upside of linear screw driving lock 9 is fixed with conical overcoat 8, and the function of its conical overcoat 8 is to cop plug 13
Protection, fix, the right side of linear screw driving lock 9 is fixed with flight controller 10, the function of its flight controller 10
It is that unmanned plane is controlled, the upper end of cop plug 13 is connected with infrared external reflection position sensor 12, its infrared external reflection
The function of position sensor 12 is that ground location is positioned, and improves the accurate positioning function of unmanned plane, described infrared anti-
Penetrate position sensor 12 and shell 11 is installed, the left side of shell 11 is fixed with built-in thrust bearing 14, its built-in thrust bearing
14 function is to support the rotation of unmanned plane propeller, and it is excessive to reduce its motion, under the gear reduction box servomotor 5
Side is fixed with driving gear component 6, and the function of its driving gear component 6 is to allow gear reduction box servomotor 5 and outer set upper side
Outside gear engages drives unmanned plane during flying with this by pinion rotation.
Referring to Fig. 2, Fig. 2 is the structural representation inside the utility model cop plug；One kind lifting endurance
Unmanned plane, including cop plug 13, the inside left of cop plug 13 be provided with vertical direction lock hole 131, institute
State the right side of vertical direction lock hole 131 and be fixed with direction alignment mark layer 132, unmanned plane can by the grafting of cop plug 13
Ensure the stabilization of unmanned plane structure, it is improved work capacity, service life length.
Finally it should be noted that：Preferred embodiment of the present utility model is the foregoing is only, is not limited to this
Utility model, although the utility model is described in detail with reference to the foregoing embodiments, for those skilled in the art
For, it can still modify to the technical scheme described in foregoing embodiments, or to which part technical characteristic
Progress equivalent substitution, all within the spirit and principles of the utility model, any modification, equivalent substitution and improvements made etc.,
It should be included within the scope of protection of the utility model.
Claims (6)
1. a kind of unmanned plane for lifting endurance, including unmanned plane body (1) and cop plug (13), it is characterised in that：
Unmanned plane body (1) upper end is provided with thermal infrared sensor (2), and unmanned plane body (1) lower end is connected with compound electric
Cable (3), composite cable (3) right side are provided with composite cable wrapping head (4), and composite cable wrapping head (4) right side is solid
Surely there is gear reduction box servomotor (5), linear screw driving locking is installed on the right side of the gear reduction box servomotor (5)
Device (9), linear screw driving lock (9) upside are fixed with conical overcoat (8), and the linear screw drives lock
(9) right side is fixed with flight controller (10), and cop plug (13) upper end is connected with infrared external reflection position sensor
(12), the infrared external reflection position sensor (12) is provided with shell (11), and built-in thrust is fixed with the left of the shell (11)
Bearing (14), gear reduction box servomotor (5) downside are fixed with driving gear component (6).
A kind of 2. unmanned plane for lifting endurance according to claim 1, it is characterised in that：The cop plug
(13) inside left is provided with vertical direction lock hole (131), and direction pair is fixed with the right side of the vertical direction lock hole (131)
Neat mark layer (132).
A kind of 3. unmanned plane for lifting endurance according to claim 1, it is characterised in that：The conical overcoat
(8) inner side is fixed with lock pin (7).
A kind of 4. unmanned plane for lifting endurance according to claim 1, it is characterised in that：The gear reduction box is watched
The clutch end for taking motor (5) is engaged by driving gear component (6) with the gear outside outer set upper side.
A kind of 5. unmanned plane for lifting endurance according to claim 1, it is characterised in that：The composite cable winding
Device (4) is wrapped in composite cable (3) surface and the length of composite cable (3) is controlled by folding and unfolding.
A kind of 6. unmanned plane for lifting endurance according to claim 1, it is characterised in that：The flight controller
(10) unmanned plane body (1) is controlled by composite cable (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720501650.3U CN206766346U (en) | 2017-05-08 | 2017-05-08 | A kind of unmanned plane for lifting endurance |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720501650.3U CN206766346U (en) | 2017-05-08 | 2017-05-08 | A kind of unmanned plane for lifting endurance |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206766346U true CN206766346U (en) | 2017-12-19 |
Family
ID=60650499
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720501650.3U Active CN206766346U (en) | 2017-05-08 | 2017-05-08 | A kind of unmanned plane for lifting endurance |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206766346U (en) |
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2017
- 2017-05-08 CN CN201720501650.3U patent/CN206766346U/en active Active
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