CN106043673A - Unmanned plane landing in random terrain - Google Patents
Unmanned plane landing in random terrain Download PDFInfo
- Publication number
- CN106043673A CN106043673A CN201610659277.4A CN201610659277A CN106043673A CN 106043673 A CN106043673 A CN 106043673A CN 201610659277 A CN201610659277 A CN 201610659277A CN 106043673 A CN106043673 A CN 106043673A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- shell
- connecting rod
- land
- support column
- 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.)
- Pending
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/06—Undercarriages fixed
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/10—UAVs characterised by their flight controls autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS]
- B64U2201/104—UAVs characterised by their flight controls autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS] using satellite radio beacon positioning systems, e.g. GPS
Abstract
The invention discloses an unmanned plane landing in random terrain. The unmanned plane comprises an unmanned plane body, the unmanned plane body comprises a shell, a connecting rod, supporting columns, supporting rods and a fixed ring, the supporting rods are arranged at the lower end of the shell, the shell is connected with the fixed ring through the supporting rods, the connecting rod is arranged at two sides of the shell, the supporting columns are arranged at one side of the connecting rod, the internal of every supporting column is hollow, a driving motor is arranged in every supporting column, the upper end and the lower end of every supporting column are provided with propellers, the driving motors are connected with the propellers through transmission shafts, the surface of the shell is provided with a display screen and a charging jack, the upper end of the connecting rod is provided with an emission antenna and a protection box, and a camera is arranged in the protection box. The shell is connected with the fixed ring through the supporting rods, so the unmanned plane can randomly land on ground, and inclination and falling to the ground of the landed unmanned plane, caused by ground unevenness, are effectively avoided.
Description
Technical field
The present invention relates to a kind of unmanned plane, particularly to a kind of unmanned plane that can land in any landform.
Background technology
Unmanned plane is the most manned aircraft of the presetting apparatus manipulation utilizing radio robot with providing for oneself.Nothing on machine
Driving cabin, but the equipment such as automatic pilot, presetting apparatus is installed.On ground, naval vessels or machine tool remote control station personnel pass through
The equipment such as radar, it be tracked, position, remote control, remote measurement and Digital Transmission.Can be as conventional airplane one under wireless remotecontrol
Sample takes off or launches with booster rocket, it is possible to is taken to by machine tool and throws in flight in the air.Unmanned plane enjoyed various countries in the last few years
Favor, it can be not only used for battlefield surveillance, the military field such as give warning in advance, and more has broad application prospects at civil area.
It can carry high-resolution visible ray or ir imaging system, can easily enter the area that the mankind cannot arrive at and detect in the air
Examining and take photo in the sky, can be used to carry out mapping, disaster surveillance etc., at present, present unmanned plane typically can only land
On smooth ground, it is impossible to arbitrarily land, but the general flight progress of unmanned plane is uncertain, and this significantly impacts nothing
Man-machine flight path, to this end, it is proposed that a kind of unmanned plane that can land in any landform.
Summary of the invention
Present invention is primarily targeted at a kind of unmanned plane that can land of offer in any landform, owing to shell is by supporting
Bar is connected with retainer ring, can arbitrarily land on the ground, effectively avoids because ground out-of-flatness causes nobody after landing
Machine run-off the straight also falls down to the ground, and can effectively solve the problem in background technology.
For achieving the above object, the technical scheme that the present invention takes is:
A kind of unmanned plane that can land in any landform, including unmanned plane body, described unmanned plane body includes shell, company
Extension bar, support column, support bar and retainer ring, described support bar is arranged on shell lower end, and described shell is by support bar and fixes
Ring connects, and described connecting rod is arranged on the both sides of shell, and described support column is arranged on the side of connecting rod, in described support column is
Hollow, is provided with driving motor in described support column, the upper and lower two ends of described support column are mounted on propeller, described driving motor
Being connected with propeller by power transmission shaft, described case surface is provided with display screen and charging socket, and described connecting rod upper end is installed
There are transmitting antenna and protecting box, in described protecting box, photographic head are installed.
Further, described shell upper end is provided with solar absorption thin film.
Further, being separated by dividing plate in described shell, described dividing plate both sides are separately installed with surface-mounted integrated circuit and work
Make power supply.
Further, described surface-mounted integrated circuit is provided with wireless communication apparatus, coulometric detector, GPS module, central authorities' process
Device, display module and energy conversion device, the signal output part of described coulometric detector passes through display module and display screen signal
Input connects, and the signal output part of described solar absorption thin film is exported by the signal of energy conversion device with working power
End connects, described photographic head, coulometric detector, GPS module data output end all with the data input pin of central processing unit company
Connecing, the data output end of described central processing unit is by the data input pin wireless connections of wireless communication apparatus with exterior terminal.
Compared with prior art, there is advantages that a kind of unmanned plane that can land in any landform, by
It is connected with retainer ring by support bar in shell, can arbitrarily land on the ground, effectively avoid because ground out-of-flatness is led
Cause the unmanned plane run-off the straight after landing and fall down to the ground, due to the photographic head in protecting box in connecting rod, unmanned plane can be recorded and fly
Market condition, avoids photographic head aloft to be damaged by bird strikes simultaneously, due to coulometric detector, can detect working power
Electricity, and be sent to exterior terminal by wireless communication apparatus, the beneficially reasonable adjusting unmanned plane during flying time, solar energy is inhaled
Receive thin film to absorb solar energy and be converted into electrical power storage in working power by energy conversion device；Due to GPS module,
The position of unmanned plane can be positioned the moment, when after unmanned plane lost contact, people are easy to find.
Accompanying drawing explanation
Fig. 1 is the overall structure schematic diagram of the unmanned plane that the present invention can be landed in any landform.
Fig. 2 is the enclosure structural representation of the unmanned plane that the present invention can be landed in any landform.
In figure: 1, unmanned plane body；2, solar absorption thin film；3, antenna is launched；4, photographic head；5, protecting box；6, outer
Shell；7, retainer ring；8, support bar；9, charging socket；10, display screen；11, connecting rod；12, power transmission shaft；13, propeller；14, prop up
Dagger；15, motor is driven；16, surface-mounted integrated circuit；17, wireless communication apparatus；18, coulometric detector；19, GPS module；20, in
Central processor；21, dividing plate；22, working power；23, energy conversion device；24, display module.
Detailed description of the invention
For the technological means making the present invention realize, creation characteristic, reach purpose and be easy to understand with effect, below in conjunction with
Detailed description of the invention, is expanded on further the present invention.
As shown in Figure 1-2, a kind of unmanned plane that can land in any landform, including unmanned plane body 1, described unmanned plane is originally
Body 1 includes that shell 6, connecting rod 11, support column 14, support bar 8 and retainer ring 7, described support bar 8 are arranged on shell 6 lower end, institute
Stating shell 6 to be connected with retainer ring 7 by support bar 8, described connecting rod 11 is arranged on the both sides of shell 6, and described support column 14 is pacified
It is contained in the side of connecting rod 11, is hollow in described support column 14, be provided with in described support column 14 and drive motor 15, described
Dagger about 14 two ends are mounted on propeller 13, and described driving motor 15 is electrically connected with propeller 13 by power transmission shaft 12,
Described shell 6 surface is provided with display screen 10 and charging socket 9, and described connecting rod 11 upper end is provided with transmitting antenna 3 and protection
Box 5, is provided with photographic head 4 in described protecting box 5.
The unmanned plane that the present invention can be landed in any landform, owing to shell 6 is connected with retainer ring 7 by support bar 8, permissible
Arbitrarily landing is on the ground, effectively avoids the unmanned plane run-off the straight after causing landing because of ground out-of-flatness and falls down to the ground, by
The photographic head 4 in protecting box 5 in connecting rod 11, can record unmanned plane during flying situation, avoids photographic head 4 to be aloft subject to simultaneously
Damage to bird strikes, due to coulometric detector 18, the electricity of working power 22 can be detected, and pass through wireless communication apparatus
17 are sent to exterior terminal, beneficially the reasonable adjusting unmanned plane during flying time, owing to solar absorption thin film 2 can absorb the sun
And electrical power storage can be converted in working power 22 by energy conversion device 23, due to GPS module 19, can position in the moment
The position of unmanned plane, when after unmanned plane lost contact, people are easy to find.
Wherein, described shell 6 upper end is provided with solar absorption thin film 2.
Wherein, being separated by dividing plate 21 in described shell 6, described dividing plate 21 both sides are separately installed with surface-mounted integrated circuit 16 He
Working power 22.
Wherein, described surface-mounted integrated circuit 16 is provided with wireless communication apparatus 17, coulometric detector 18, GPS module 19, centre
Reason device 20, display module 24 and energy conversion device 23, the signal output part of described coulometric detector 18 passes through display module 24
Be connected with display screen 10 signal input part, the signal output part of described solar absorption thin film 2 by energy conversion device 23 with
The signal output part of working power 22 connects, described photographic head 4, coulometric detector 18, GPS module 19 data output end all with
The data input pin of central processing unit 20 connects, the data output end of described central processing unit 20 by wireless communication apparatus 17 with
The data input pin wireless connections of exterior terminal.
The ultimate principle of the present invention and principal character and advantages of the present invention have more than been shown and described.The technology of the industry
Personnel, it should be appreciated that the present invention is not restricted to the described embodiments, simply illustrating this described in above-described embodiment and description
The principle of invention, without departing from the spirit and scope of the present invention, the present invention also has various changes and modifications, and these become
Change and improvement both falls within scope of the claimed invention.Claimed scope by appending claims and
Equivalent defines.
Claims (4)
1. the unmanned plane that can land in any landform, including unmanned plane body (1), it is characterised in that: described unmanned plane is originally
Body (1) includes shell (6), connecting rod (11), support column (14), support bar (8) and retainer ring (7), and described support bar (8) is installed
In shell (6) lower end, described shell (6) is connected with retainer ring (7), outside described connecting rod (11) is arranged on by support bar (8)
The both sides of shell (6), described support column (14) is arranged on the side of connecting rod (11), is hollow in described support column (14), described
Being provided with driving motor (15) in support column (14), described support column (14) is mounted on propeller (13) in two ends up and down, described
Drive motor (15) to be connected with propeller (13) by power transmission shaft (12), described shell (6) surface be provided with display screen (10) and
Charging socket (9), described connecting rod (11) upper end is provided with peace in transmitting antenna (3) and protecting box (5), described protecting box (5)
Equipped with photographic head (4).
The unmanned plane that can land in any landform the most according to claim 1, it is characterised in that: described shell (6) upper end
Solar absorption thin film (2) is installed.
The unmanned plane that can land in any landform the most according to claim 1, it is characterised in that: logical in described shell (6)
Crossing dividing plate (21) to separate, described dividing plate (21) both sides are separately installed with surface-mounted integrated circuit (16) and working power (22).
4. according to the unmanned plane that can land in any landform described in Claims 2 or 3, it is characterised in that: described integrated circuit
Plate (16) is provided with wireless communication apparatus (17), coulometric detector (18), GPS module (19), central processing unit (20), display module
(24) and energy conversion device (23), the signal output part of described coulometric detector (18) passes through display module (24) and display screen
(10) signal input part connects, and the signal output part of described solar absorption thin film (2) passes through energy conversion device (23) and work
The signal output part making power supply (22) connects, described photographic head (4), coulometric detector (18), the data output of GPS module (19)
End all data input pins with central processing unit (20) are connected, and the data output end of described central processing unit (20) passes through channel radio
News device (17) and the data input pin wireless connections of exterior terminal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610659277.4A CN106043673A (en) | 2016-08-12 | 2016-08-12 | Unmanned plane landing in random terrain |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610659277.4A CN106043673A (en) | 2016-08-12 | 2016-08-12 | Unmanned plane landing in random terrain |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106043673A true CN106043673A (en) | 2016-10-26 |
Family
ID=57481766
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610659277.4A Pending CN106043673A (en) | 2016-08-12 | 2016-08-12 | Unmanned plane landing in random terrain |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106043673A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106379548A (en) * | 2016-11-29 | 2017-02-08 | 朱耘彤 | Aerial photography unmanned aerial vehicle capable of illumination |
| CN106741882A (en) * | 2016-12-17 | 2017-05-31 | 北京小米移动软件有限公司 | Unmanned plane |
| CN107444628A (en) * | 2017-07-25 | 2017-12-08 | 芜湖超源力工业设计有限公司 | A kind of new unmanned plane with drop resistant abrasion-resistant blade |
| CN107914889A (en) * | 2017-11-15 | 2018-04-17 | 广东容祺智能科技有限公司 | A kind of unmanned plane is in the landing system of marine vessel |
| CN108557076A (en) * | 2018-01-17 | 2018-09-21 | 安徽中骄智能科技有限公司 | A kind of unmanned plane based on full protection skeleton |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203461088U (en) * | 2013-09-13 | 2014-03-05 | 重庆金泰航空工业有限公司 | Four-shaft farm-oriented unmanned aircraft fuselage positioning structure |
| CN204998757U (en) * | 2015-05-14 | 2016-01-27 | 苏州绿农航空植保科技有限公司 | Undercarriage that topples is prevented to many rotor crafts |
| CN105752329A (en) * | 2014-10-21 | 2016-07-13 | 蒋红娟 | Quad-rotor unmanned helicopter with remote control system |
| CN206125411U (en) * | 2016-08-12 | 2017-04-26 | 唐小波 | Can be at unmanned aerial vehicle of arbitrary topography descending |
-
2016
- 2016-08-12 CN CN201610659277.4A patent/CN106043673A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203461088U (en) * | 2013-09-13 | 2014-03-05 | 重庆金泰航空工业有限公司 | Four-shaft farm-oriented unmanned aircraft fuselage positioning structure |
| CN105752329A (en) * | 2014-10-21 | 2016-07-13 | 蒋红娟 | Quad-rotor unmanned helicopter with remote control system |
| CN204998757U (en) * | 2015-05-14 | 2016-01-27 | 苏州绿农航空植保科技有限公司 | Undercarriage that topples is prevented to many rotor crafts |
| CN206125411U (en) * | 2016-08-12 | 2017-04-26 | 唐小波 | Can be at unmanned aerial vehicle of arbitrary topography descending |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106379548A (en) * | 2016-11-29 | 2017-02-08 | 朱耘彤 | Aerial photography unmanned aerial vehicle capable of illumination |
| CN106741882A (en) * | 2016-12-17 | 2017-05-31 | 北京小米移动软件有限公司 | Unmanned plane |
| CN107444628A (en) * | 2017-07-25 | 2017-12-08 | 芜湖超源力工业设计有限公司 | A kind of new unmanned plane with drop resistant abrasion-resistant blade |
| CN107914889A (en) * | 2017-11-15 | 2018-04-17 | 广东容祺智能科技有限公司 | A kind of unmanned plane is in the landing system of marine vessel |
| CN108557076A (en) * | 2018-01-17 | 2018-09-21 | 安徽中骄智能科技有限公司 | A kind of unmanned plane based on full protection skeleton |
| CN108557076B (en) * | 2018-01-17 | 2021-10-29 | 安徽赛安安全设备有限责任公司 | Unmanned aerial vehicle based on full protection skeleton |
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Legal Events
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20161026 |