CN206623987U - A kind of industrial unmanned plane of band landing auxiliary stand - Google Patents
A kind of industrial unmanned plane of band landing auxiliary stand Download PDFInfo
- Publication number
- CN206623987U CN206623987U CN201720397193.8U CN201720397193U CN206623987U CN 206623987 U CN206623987 U CN 206623987U CN 201720397193 U CN201720397193 U CN 201720397193U CN 206623987 U CN206623987 U CN 206623987U
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- rotor
- landing
- main body
- support
- 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
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Toys (AREA)
Abstract
A kind of industrial unmanned plane of band landing auxiliary stand, electric control gear is installed with unmanned plane main body rack, battery case and radar are installed with unmanned plane main body rack, radar is in front of battery case, it is respectively a pair of preceding rotor supports that rotor support, which has 3 pairs, one centering rotor support and a pair of rear rotor supports, rotor bracket end is passed through in unmanned plane main body rack by bracket holder, rotor motor is installed above rotor stent outer end, the rotating shaft of rotor motor is provided with propeller, the bracket at tail part both sides of the upper bracket of unmanned plane main body rack are connected by connector with rear rotor support, two bottoms of landing gear are outwardly, there is landing plate below two bottoms of a pair of landing gear sides, the bottom of landing gear is connected by flexible column with landing plate.The utility model supporting auxiliary landing support on the basis of industrial unmanned plane improves unmanned plane landing stability so as to reduce the vibrations that unmanned plane landing occurs.
Description
Technical field
The utility model is related to industrial unmanned plane field, more particularly to a kind of band land auxiliary stand industry nobody
Machine.
Background technology
With the further raising of social productive forces, industrial unmanned plane, as it is a kind of it is dynamic, controllable, can carry
Into the equipment of task, in recent years by the favor of every profession and trade.It does not have driving cabin, but is mounted with autopilot, shooting of taking photo by plane, flies
The equipment such as row gesture stability, moved to aid in unmanned plane to move horizontally, in a manner of VTOL etc., pass through hedgehopping and complete to appoint
Business and landing, are easy to more subjobs, and industrial unmanned plane is voluntarily to land mostly, and vibrations easily occur for descent causes to body
Larger damage.
Utility model content
In order to solve above-mentioned problem, the utility model provides a kind of industrial unmanned plane of band landing auxiliary stand,
Supporting auxiliary landing support improves unmanned plane drop so as to reduce the vibrations that unmanned plane landing occurs on the basis of industrial unmanned plane
Fall stability, for up to this purpose, the utility model provides a kind of industrial unmanned plane of band landing auxiliary stand, including unmanned owner
Body support frame, electric control gear, battery case, radar, propeller, rotor motor, rotor support, landing gear, flexible column, landing plate and branch
Frame fixed mount, electric control gear is installed with the unmanned plane main body rack, is fixedly mounted on the unmanned plane main body rack
There are battery case and radar, for the radar in front of battery case, it is respectively a pair preceding rotor supports, one that the rotor support, which there are 3 pairs,
Centering rotor support and a pair of rear rotor supports, the unmanned plane main body rack bottom are provided with landing gear, the rotor support
End is by bracket holder by unmanned plane main body rack, being provided with rotor electricity above the rotor stent outer end
Machine, the rotating shaft of the rotor motor are provided with propeller, and the bracket at tail part both sides of the upper bracket of the unmanned plane main body rack lead to
Cross connector with rear rotor support to be connected, the landing gear has a pair, and the landing gear is n-type, two bottoms of the landing gear
Outwardly, there is landing plate at end below two bottoms of a pair of landing gear sides, the bottom of the landing gear passes through flexible column and landing
Plate is connected.
Further improvement of the utility model, the upper bracket and lower carriage of the unmanned plane main body rack have hole, passed through
Opening can mitigate unmanned plane weight.
Further improvement of the utility model, angle is rotor branch after 76 °, two between two preceding rotor carriage center lines
Angle is 43 ° between frame center line, and angle is 67 ° between the preceding rotor support and middle rotor carriage center line of side, side
Angle is 53 ° between rotor support and middle rotor carriage center line afterwards, and the application unmanned plane has obtained accordingly in practice
With by test using above-mentioned angle with preferably test effect.
Further improvement of the utility model, there is spring in the flexible column, can be in order to improve landing gear support strength
Increase spring in flexible column.
A kind of industrial unmanned plane of band landing auxiliary stand of the utility model, increases in former industrial unmanned plane alighting carriage bottom
If landing plate, land flexible post between plate and alighting carriage bottom, and unmanned plane is reduced by flexible column in the auxiliary stand that lands
Shaken caused by descent, and then improve the service life and landing stability of unmanned plane, unmanned plane main body is using industry
Unmanned plane type, applicability can extensively be produced in enormous quantities.
Brief description of the drawings
Fig. 1 is the utility model schematic diagram;
Brief description of the drawings:
1st, unmanned plane main body rack;2nd, electric control gear;3rd, battery case;4th, radar;5th, propeller;6th, rotor motor;7th, it is preceding
Rotor support;8th, middle rotor support;9th, rear rotor support;10th, landing gear;11st, flexible column;12nd, land plate;13rd, support is fixed
Frame.
Embodiment
The utility model is described in further detail with embodiment below in conjunction with the accompanying drawings:
The utility model provides a kind of industrial unmanned plane of band landing auxiliary stand, supporting on the basis of industrial unmanned plane
Auxiliary landing support improves unmanned plane landing stability so as to reduce the vibrations that unmanned plane landing occurs.
As a kind of embodiment of the utility model, the utility model provide a kind of band landing auxiliary stand industry nobody
Machine, including unmanned plane main body rack 1, electric control gear 2, battery case 3, radar 4, propeller 5, rotor motor 6, rotor support, drop
Fall frame 10, flexible column 11, landing plate 12 and bracket holder 13, automatically controlled dress is installed with the unmanned plane main body rack 1
2 are put, battery case 3 and radar 4 are installed with the unmanned plane main body rack 1, the radar 4 is described in front of battery case 3
Rotor support has 3 pairs of respectively a pair of preceding rotor supports 7, a centering rotor support 8 and a pair of rear rotor supports 9, the rotor
Bracket end is by bracket holder 13 by unmanned plane main body rack 1, being installed above the rotor stent outer end
There is rotor motor 6, the rotating shaft of the rotor motor 6 is provided with propeller 5, the tail of the upper bracket of the unmanned plane main body rack 1
Portion support both sides are connected by connector with rear rotor support 9, and the bottom of unmanned plane main body rack 1 is provided with landing gear 10,
The landing gear 10 has a pair, and the landing gear 10 is n-type, two bottoms of the landing gear 10 outwardly, a pair of landing gears 10
There is landing plate 12 below two bottoms of side, the bottom of the landing gear 10 is connected by flexible column 11 with landing plate 12.
As a kind of specific embodiment of the utility model, the utility model provides a kind of band landing auxiliary as shown in Figure 1
The industrial unmanned plane of support, including unmanned plane main body rack 1, electric control gear 2, battery case 3, radar 4, propeller 5, rotor motor
6th, rotor support, landing gear 10, flexible column 11, landing plate 12 and bracket holder 13, it is fixed in the unmanned plane main body rack 1
Electric control gear 2 is installed, the upper bracket and lower carriage of the unmanned plane main body rack 1 have hole, can mitigate nothing by opening
Man-machine weight, battery case 3 and radar 4 is installed with the unmanned plane main body rack 1, the radar 4 is before battery case 3
Side, the rotor support have 3 pairs of respectively a pair of preceding rotor supports 7, a centering rotor support 8 and a pair of rear rotor supports 9, institute
Rotor bracket end is stated by bracket holder 13 by unmanned plane main body rack 1, two preceding center lines of rotor support 7 it
Between angle be 76 °, two after between the center line of rotor support 9 angle be 43 °, preceding rotor support 7 and the middle rotor support 8 of side
Angle is 67 ° between center line, and angle is 53 ° between the rear rotor support 9 of side and the middle center line of rotor support 8, the application
Unmanned plane has been used accordingly in practice, has preferably test effect using above-mentioned angle by test, described
Rotor motor 6 is installed above rotor stent outer end, the rotating shaft of the rotor motor 6 is provided with propeller 5, it is described nobody
The bracket at tail part both sides of the upper bracket of owner's body support frame 1 are connected by connector with rear rotor support 9, the unmanned plane main body branch
The bottom of frame 1 is provided with landing gear 10, and the landing gear 10 has a pair, and the landing gear 10 is n-type, two of the landing gear 10
Outwardly, there is landing plate 12 bottom, the bottom of the landing gear 10 passes through flexibility below two bottoms of a pair of sides of landing gear 10
Post 11 is connected with landing plate 12, has spring in the flexible column 11, can increase to improve landing gear support strength in flexible column
Add spring.
It is described above, only it is preferred embodiment of the present utility model, is not that any other is made to the utility model
The limitation of form, and any modification made according to the technical essence of the utility model or equivalent variations, it is new to still fall within this practicality
Type scope claimed.
Claims (4)
1. a kind of industrial unmanned plane of band landing auxiliary stand, including unmanned plane main body rack(1), electric control gear(2), battery case
(3), radar(4), propeller(5), rotor motor(6), rotor support, landing gear(10), flexible column(11), landing plate(12)With
Bracket holder(13), the unmanned plane main body rack(1)Inside it is installed with electric control gear(2), it is characterised in that:The nothing
Man-machine main body rack(1)On be installed with battery case(3)And radar(4), the radar(4)In battery case(3)Front, it is described
It is respectively a pair of preceding rotor supports that rotor support, which has 3 pairs,(7), a centering rotor support(8)With a pair of rear rotor supports(9), institute
State rotor bracket end and pass through bracket holder(13)By in unmanned plane main body rack(1)It is interior, the rotor stent outer end
Rotor motor is installed above portion(6), the rotor motor(6)Rotating shaft propeller is installed(5), the unmanned plane main body branch
Frame(1)The bracket at tail part both sides of upper bracket pass through connector and rear rotor support(9)It is connected, the unmanned plane main body rack
(1)Bottom is provided with landing gear(10), the landing gear(10)Have a pair, the landing gear(10)For n-type, the landing gear
(10)Two bottoms outwardly, a pair of landing gears(10)There is landing plate below two bottoms of side(12), the landing gear
(10)Bottom pass through flexible column(11)With the plate that lands(12)It is connected.
A kind of 2. industrial unmanned plane of band landing auxiliary stand according to claim 1, it is characterised in that:The unmanned plane
Main body rack(1)Upper bracket and lower carriage have hole.
A kind of 3. industrial unmanned plane of band landing auxiliary stand according to claim 1, it is characterised in that:Two preceding rotors
Support(7)Angle is rotor support after 76 °, two between center line(9)Angle is 43 ° between center line, the preceding rotor of side
Support(7)With middle rotor support(8)Angle is 67 ° between center line, the rear rotor support of side(9)With middle rotor support(8)
Angle is 53 ° between center line.
A kind of 4. industrial unmanned plane of band landing auxiliary stand according to claim 1, it is characterised in that:The flexible column
(11)Inside there is spring.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201720397193.8U CN206623987U (en) | 2017-04-17 | 2017-04-17 | A kind of industrial unmanned plane of band landing auxiliary stand |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201720397193.8U CN206623987U (en) | 2017-04-17 | 2017-04-17 | A kind of industrial unmanned plane of band landing auxiliary stand |
Publications (1)
Publication Number | Publication Date |
---|---|
CN206623987U true CN206623987U (en) | 2017-11-10 |
Family
ID=60205808
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201720397193.8U Expired - Fee Related CN206623987U (en) | 2017-04-17 | 2017-04-17 | A kind of industrial unmanned plane of band landing auxiliary stand |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN206623987U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108216515A (en) * | 2018-03-27 | 2018-06-29 | 金陵科技学院 | A kind of cellular unmanned plane seaborne supply platform and fishing water sky ship |
-
2017
- 2017-04-17 CN CN201720397193.8U patent/CN206623987U/en not_active Expired - Fee Related
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108216515A (en) * | 2018-03-27 | 2018-06-29 | 金陵科技学院 | A kind of cellular unmanned plane seaborne supply platform and fishing water sky ship |
CN108216515B (en) * | 2018-03-27 | 2023-10-27 | 金陵科技学院 | Honeycomb type unmanned aerial vehicle offshore supply platform and fishing water-air boat |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN104386238B (en) | A kind of agricultural depopulated helicopter | |
CN102285449A (en) | Coaxial double-rotor wing ducted aircraft | |
CN205293106U (en) | Novel unmanned aerial vehicle nacelle mounting structure | |
CN206623987U (en) | A kind of industrial unmanned plane of band landing auxiliary stand | |
CN201321159Y (en) | Unmanned aircraft with vertical ducts | |
CN202848024U (en) | Propeller hub assembly used for small and medium-sized unmanned helicopters | |
CN113184185A (en) | Streamlined coaxial many rotor unmanned aerial vehicle of adaptable adverse circumstances | |
CN104494817A (en) | Four-rotor unmanned aerial vehicle | |
CN208775012U (en) | A kind of VTOL flying platform high efficiency lift unit | |
CN106741933A (en) | A kind of amphibious unmanned plane | |
CN104229151A (en) | Precise trimming device for inner ring assembly of mast-type photoelectric stabilized tracking platform | |
CN202896879U (en) | Light concentric shaft helicopter | |
CN206856989U (en) | Adjustable-piston quadrotor | |
CN206125407U (en) | Miniature ducted fan aircraft | |
CN205931250U (en) | Four rotor crafts of variable pitch based on single driving system | |
CN106898187A (en) | A kind of rotor wing unmanned aerial vehicle landing training platform that takes off | |
CN206243461U (en) | A kind of miniature self-service drives helicopter | |
CN206437209U (en) | A kind of four rotor wing unmanned aerial vehicle demonstrators | |
CN208119424U (en) | A kind of multi-rotor unmanned aerial vehicle | |
CN205076042U (en) | Many rotor unmanned aerial vehicle box structure horn | |
CN204399472U (en) | A kind of four rotor wing unmanned aerial vehicles | |
CN203601562U (en) | Boomerang quadrotor aircraft | |
CN103803071B (en) | Engineering-type rotary wind type unmanned vehicle | |
CN206297730U (en) | Fixed-wing rotor mixed layout unmanned plane | |
CN206374983U (en) | Land and air double-used flying saucer |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
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: 20171110 Termination date: 20210417 |