CN104554716B - A kind of split type unmanned vehicle - Google Patents
A kind of split type unmanned vehicle Download PDFInfo
- Publication number
- CN104554716B CN104554716B CN201510041217.1A CN201510041217A CN104554716B CN 104554716 B CN104554716 B CN 104554716B CN 201510041217 A CN201510041217 A CN 201510041217A CN 104554716 B CN104554716 B CN 104554716B
- Authority
- CN
- China
- Prior art keywords
- driving lever
- unmanned vehicle
- shell
- split type
- box
- 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.)
- Expired - Fee Related
Links
Landscapes
- Toys (AREA)
Abstract
The present invention relates to the unmanned vehicle of a kind of low maintenance cost.This aircraft includes the shell of unmanned vehicle, and shell is provided with propeller and drives the motor of propeller rotational, also includes being embedded at the control box in the middle of shell, is provided with the main control board of unmanned vehicle in controlling box.The vitals of unmanned vehicle is fixed on by the present invention in control box; controlling box to be then independently mounted on the shell of aircraft, parts subregion is placed, convenient maintenance; and when aircraft bumps against big tree or building and damages; the vitals controlling box obtains duplicate protection, and damaged probability reduces, and the parts on aircraft skin are the most relatively cheap; maintenance cost is relatively low; even if cannot repair, it is also possible to retaining and control box and directly change shell, spent cost is the highest.
Description
Technical field
The present invention relates to unmanned vehicle, particularly relate to a kind of split type unmanned vehicle.
Background technology
At present small-sized unmanned aircraft widely apply taking photo by plane, agricultural, fire, natural disaster early warning etc.
Field, along with maturation and the reduction of cost of technology, it will there is increasing field to use.
The small-sized unmanned aircraft of commercial type, commonly used upper and lower covers designs, required for aircraft
Motor, flight display lamp, flight control system, GPS system, magnetic system etc. be all put into
In aircraft upper and lower covers, production and assembly are extremely difficult, are not easy to maintenance.Aircraft when high-speed flight,
Manipulator is easy to misoperation, and whole aircraft knocks building or sets greatly in high-altitude, even directly from
Falling from high altitude, thus cause aircraft to be damaged, it is impossible to maintenance.Manipulator can only buy new product,
But the current price of aircraft is the most costly, it is a no small loss for consumers.
Summary of the invention
It is an object of the invention to the defect for overcoming prior art, and provide a kind of split type nobody fly
Row device.
For achieving the above object, the present invention is by the following technical solutions:
A kind of split type unmanned vehicle, including the shell of unmanned vehicle, shell is provided with propeller
With the motor of driving propeller rotational, also include being embedded at the control box in the middle of shell, set in controlling box
There is the main control board of unmanned vehicle.
Further, shell is provided with the installation position for fixing control box, and installation position is provided with upper shed
And under shed, control box and load in installation position under shed, control insertion installation position, top upper of box
Opening.
Further, upper casing and the lower casing that box includes interfixing is controlled.
Further, upper casing is equipped with louvre with the outer wall of lower casing.
Further, main control board is fixed on lower casing, and main control board is provided with RF module, control
Being additionally provided with GPS circuitry plate in box processed, GPS circuitry plate is fixed on above main control board and both it
Between be provided with shielding cotton.
Further, upper casing is provided with the driving lever being rotatably connected with upper casing, and main control board is provided with electricity
Source switch, on and off switch is provided with the elastic pressuring plate for controlling on and off switch break-make, and driving lever includes main
Body and for extruding the afterbody of elastic pressuring plate, driving lever and housing are in the junction of main part Yu afterbody
It is rotatably connected.
Further, when driving lever is positioned at de-energized, within the main part of driving lever is placed in housing, dial
The afterbody of bar is away from elastic pressuring plate, on and off switch power-off；When driving lever is allocated to on-position, driving lever
Main part expose to outside housing, the afterbody of driving lever is pressed under elastic pressuring plate, on and off switch be energized.
Further, when driving lever is positioned at de-energized, driving lever horizontal positioned.
Further, when driving lever is allocated to on-position, driving lever is vertically placed.
Further, it is provided with earth magnetism circuit board in the main part of driving lever.
The present invention compared with prior art provides the benefit that:
The vitals of unmanned vehicle is fixed on by the present invention in control box, controls box then independent
Being arranged on the shell of aircraft, parts subregion is placed, convenient maintenance, and when aircraft bumps against greatly
Tree or building and when damaging, the vitals controlling box obtains duplicate protection, and damaged probability reduces,
And parts on aircraft skin are the most relatively cheap, maintenance cost is relatively low, even if cannot repair, it is possible to
Directly changing shell to retain control box, spent cost is the highest.
Accompanying drawing explanation
Fig. 1 is the shell of unmanned vehicle and the explosive view controlling box；
Fig. 2 is the explosive view controlling box；
Fig. 3 is main control board axonometric chart；
Fig. 4 is the sectional view (driving lever is in de-energized) controlling box；
Fig. 5 is the sectional view (driving lever is between on-position and de-energized) controlling box；
Fig. 6 is the sectional view (driving lever is in on-position) controlling box；
Fig. 7 is the partial enlarged drawing of Fig. 6.
Detailed description of the invention
In order to more fully understand the technology contents of the present invention, below in conjunction with specific embodiment to the present invention's
Technical scheme is described further and illustrates.
The concrete structure of the embodiment of the present invention is as shown in Figures 1 to 7.
The unmanned vehicle of the present embodiment includes the shell 90 of unmanned vehicle and for protecting nobody to fly
The control box 10 of row device expensive components.Shell 90 is provided with propeller 71 and drives propeller 71 to rotate
Motor 72.Control box 10 and be embedded at the centre of shell 90.The main control board 31 of unmanned vehicle, GPS
Circuit board 35, RF module and earth magnetism circuit board 23 are fixed in control box 10.
Control box 10 to be fixed in shell 90.Specifically, shell 90 is provided with for fixing control box 10
Installation position 91, installation position 91 is provided with upper shed and under shed, controls box 10 and loads under shed and install
In position 91, control the upper shed of the insertion installation position, top 91 of box 10.In the present embodiment, control box 10
Loading installation position 91 from the bottom up, and in other embodiments, it can be provided control box from top to bottom
Load installation position.
Control upper casing 12 and lower casing 13 that box 10 includes interfixing.In the present embodiment, installation position 91
Upper shed is that corner is starlike, and the upper casing 12 controlling box 10 is also starlike in corresponding corner.Upper casing 12 with
The outer wall of lower casing 13 is equipped with louvre.Main control board 31 is fixed on lower casing 13, and RF module is located at
On main control board 31, GPS circuitry plate 35 is fixed on above main control board 31 and sets between the two
There is shielding cotton 36.
Upper casing 12 is provided with the driving lever 20 being rotatably connected with upper casing 12.Main control board 31 is provided with power supply
Switch 32.On and off switch 32 is provided with the elastic pressuring plate 33 for controlling on and off switch 32 break-make.Elastic
Tabletting 33 is fixed on above on and off switch 32 and forms acute angle with the end face of on and off switch 32.On and off switch
The end face of 32 is provided with shift knob 34, and shift knob 34 is positioned at below elastic pressuring plate 33.
Driving lever 20 includes main part 21 and for extruding the afterbody 22 of elastic pressuring plate 33.Driving lever 20 is with upper
Shell 12 is rotatably connected with the junction bearing pin of afterbody 22 at main part 21.Upper casing 12 is provided with receiving driving lever
The groove 11 of 20 main parts 21.
During driving lever 20 horizontal positioned, driving lever 20 is positioned at de-energized, and the main part 21 of driving lever 20 is placed in
Within shell 12 (i.e. the main part 21 of driving lever 20 is placed in groove 11), the afterbody 22 of driving lever 20 is away from elasticity
Tabletting 33, elastic pressuring plate 33 does not contacts with shift knob 34, on and off switch 32 power-off.
Driving lever 20 is when horizontal positioned becomes vertically placing, and driving lever 20 is allocated to on-position, driving lever 20
Main part 21 expose to outside upper casing 12, elastic pressuring plate is pressed for 33 times by the afterbody 22 of driving lever 20, and bullet
Shift knob is pressed for 34 times by property tabletting 33, and on and off switch 32 is energized.
Earth magnetism circuit board 23 is located in the main part 21 of driving lever 20, and it is for when being in vertical position pair
Earth magnetism is corrected.Therefore, when driving lever 20 horizontal positioned, earth magnetism circuit board 23 also is located on horizontal plane,
Earth magnetism circuit board 23 does not carry out earth magnetism correction；And when driving lever 20 is vertically placed, at earth magnetism circuit board 23
On vertical plane, on and off switch 32 is also energized simultaneously, and now earth magnetism circuit board 23 just can carry out ground
Magnetic corrects to ensure unmanned vehicle normal flight.
The technology contents only further illustrating the present invention with embodiment set forth above, in order to Du Zhegeng
Easy to understand, but do not represent embodiments of the present invention and be only limitted to this, any skill done according to the present invention
Art extends or recreation, is all protected by the present invention.
Claims (8)
1. a split type unmanned vehicle, including the shell of unmanned vehicle, shell be provided with propeller and
Drive the motor of propeller rotational, it is characterised in that also include being embedded at the control box in the middle of shell, described
The main control board of unmanned vehicle it is provided with in controlling box；Described control box include the upper casing that interfixes with under
Shell；Described upper casing is provided with the driving lever being rotatably connected with upper casing, and described main control board is provided with on and off switch,
Described on and off switch is provided with the elastic pressuring plate for controlling on and off switch break-make, driving lever include main part and
For extruding the afterbody of elastic pressuring plate, driving lever is rotatably connected with the junction of afterbody at main part with housing.
Split type unmanned vehicle the most as claimed in claim 1, it is characterised in that described shell is provided with
For the installation position of fixing control box, installation position is provided with upper shed and under shed, controls box and loads under shed
In installation position, control the upper shed of the insertion installation position, top of box.
Split type unmanned vehicle the most as claimed in claim 1, it is characterised in that described upper casing and lower casing
Outer wall be equipped with louvre.
Split type unmanned vehicle the most as claimed in claim 1, it is characterised in that described main control board
Being fixed on lower casing, main control board is provided with RF module, is additionally provided with GPS circuitry plate, GPS in controlling box
Circuit board is fixed on above main control board and is provided with shielding cotton between the two.
Split type unmanned vehicle the most as claimed in claim 1, it is characterised in that when driving lever is positioned at power-off
During position, within the main part of driving lever is placed in housing, the afterbody of driving lever breaks away from elastic pressuring plate, on and off switch
Electricity；When driving lever is allocated to on-position, the main part of driving lever exposes to outside housing, and the afterbody of driving lever will
Pressing under elastic pressuring plate, on and off switch is energized.
Split type unmanned vehicle the most as claimed in claim 5, it is characterised in that when driving lever is positioned at power-off
During position, driving lever horizontal positioned.
Split type unmanned vehicle the most as claimed in claim 5, it is characterised in that when driving lever is allocated to lead to
During electric position, driving lever is vertically placed.
Split type unmanned vehicle the most as claimed in claim 1, it is characterised in that the main body of described driving lever
Earth magnetism circuit board it is provided with in portion.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510041217.1A CN104554716B (en) | 2015-01-27 | 2015-01-27 | A kind of split type unmanned vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510041217.1A CN104554716B (en) | 2015-01-27 | 2015-01-27 | A kind of split type unmanned vehicle |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104554716A CN104554716A (en) | 2015-04-29 |
| CN104554716B true CN104554716B (en) | 2016-10-05 |
Family
ID=53071994
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510041217.1A Expired - Fee Related CN104554716B (en) | 2015-01-27 | 2015-01-27 | A kind of split type unmanned vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104554716B (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203090471U (en) * | 2013-01-11 | 2013-07-31 | 河南科技大学 | Airframe of four-rotor aircraft |
| GB2511754A (en) * | 2013-03-11 | 2014-09-17 | Univ Bristol | Radiation Detection Device and Method |
| CN104085529A (en) * | 2014-07-31 | 2014-10-08 | 山东创惠电子科技股份有限公司 | Eight-rotor-wing unmanned plane system |
| CN203996882U (en) * | 2014-06-07 | 2014-12-10 | 珠海羽人飞行器有限公司 | The agricultural aircraft of four rotors |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20130105635A1 (en) * | 2011-10-31 | 2013-05-02 | King Abdullah II Design and Development Bureau | Quad tilt rotor vertical take off and landing (vtol) unmanned aerial vehicle (uav) with 45 degree rotors |
-
2015
- 2015-01-27 CN CN201510041217.1A patent/CN104554716B/en not_active Expired - Fee Related
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203090471U (en) * | 2013-01-11 | 2013-07-31 | 河南科技大学 | Airframe of four-rotor aircraft |
| GB2511754A (en) * | 2013-03-11 | 2014-09-17 | Univ Bristol | Radiation Detection Device and Method |
| CN203996882U (en) * | 2014-06-07 | 2014-12-10 | 珠海羽人飞行器有限公司 | The agricultural aircraft of four rotors |
| CN104085529A (en) * | 2014-07-31 | 2014-10-08 | 山东创惠电子科技股份有限公司 | Eight-rotor-wing unmanned plane system |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104554716A (en) | 2015-04-29 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN204568055U (en) | A kind of Modularized unmanned aircraft | |
| CN104627361A (en) | Modularized unmanned aerial vehicle | |
| CN104554716B (en) | A kind of split type unmanned vehicle | |
| CN106325340A (en) | Computer network safety control device for teaching | |
| CN209471376U (en) | A kind of UAV Flight Control device and unmanned plane | |
| CN206163845U (en) | Plug on -off control box | |
| CN105539844A (en) | Unmanned aerial vehicle with accident record inquiring function | |
| CN204046979U (en) | The shell mechanism of LED drive power | |
| CN203270254U (en) | Industrial sewing machine | |
| CN207481667U (en) | A kind of car high voltage connector protection system of anti-stop-band load action | |
| CN205354978U (en) | Pilot lamp protection architecture of undervoltage protection ware is crossed from double entry | |
| CN207346087U (en) | A kind of unmanned plane | |
| CN210416975U (en) | Multi-rotor unmanned aerial vehicle and motor device thereof | |
| CN209517342U (en) | A kind of video matrix switcher with audio separation | |
| CN108923881A (en) | A kind of movable unmanned helicopter jamming equipment | |
| CN205092385U (en) | Power saving controller | |
| CN220897015U (en) | Controller of power distribution cabinet | |
| CN205354912U (en) | Self -reset overvoltage and undervoltage protector | |
| CN209385036U (en) | A kind of automatic switching controller of rolling screen door | |
| CN214566194U (en) | Make things convenient for unmanned aerial vehicle driving system buffer stop of dismouting | |
| CN108173145A (en) | A kind of low pressure rain-proof heat-dissipation switch cabinet | |
| CN103809478B (en) | The modular power supply insurance of a kind of loading machine controls box | |
| CN220164190U (en) | Oil pipeline detects unmanned aerial vehicle | |
| CN213958245U (en) | Remote controller chip circuit and remote controller that accessible interface that charges resets | |
| CN213517301U (en) | Power-off alarm |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20161005 Termination date: 20210127 |