CN108341059A - A kind of battlefield is scouted and defence unmanned plane - Google Patents
A kind of battlefield is scouted and defence unmanned plane Download PDFInfo
- Publication number
- CN108341059A CN108341059A CN201810236870.7A CN201810236870A CN108341059A CN 108341059 A CN108341059 A CN 108341059A CN 201810236870 A CN201810236870 A CN 201810236870A CN 108341059 A CN108341059 A CN 108341059A
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- Prior art keywords
- fuselage
- unmanned plane
- connect
- mission payload
- battlefield
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- 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.)
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- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims abstract description 21
- 238000005183 dynamical system Methods 0.000 claims abstract description 13
- 238000012544 monitoring process Methods 0.000 claims abstract description 7
- 230000005611 electricity Effects 0.000 claims description 9
- 230000000007 visual effect Effects 0.000 claims description 4
- 235000006508 Nelumbo nucifera Nutrition 0.000 claims description 3
- 240000002853 Nelumbo nucifera Species 0.000 claims description 3
- 235000006510 Nelumbo pentapetala Nutrition 0.000 claims description 3
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 3
- 230000007613 environmental effect Effects 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000007774 longterm Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 1
- 231100000749 chronicity Toxicity 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/30—Aircraft characterised by electric power plants
- B64D27/35—Arrangements for on-board electric energy production, distribution, recovery or storage
- B64D27/353—Arrangements for on-board electric energy production, distribution, recovery or storage using solar cells
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT 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
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/20—Remote controls
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Catching Or Destruction (AREA)
Abstract
Unmanned plane is scouted and defendd the invention discloses a kind of battlefield, it include fuselage, it is set to navigation flight control system, electrical system and the Energy Management System of fuselage interior, the solar recharging system being set on fuselage roof end face, mission payload right over fuselage, the jacking system that outside fuselage and top is connect with mission payload, multiple uniform fixations and the rack on fuselage periphery are reached, it is multigroup to be connected to dynamical system and flexible folding undercarriage on corresponding rack outer end.Environmental suitability of the present invention is stronger, voyage is farther and can garrison battlefield for a long time and execute scouting and defensive missions, unmanned plane, which is hidden, to be scouted and is defendd in specified region, its own carries solar charging device and can power for a long time to mission payload, flexible folding undercarriage can ensure that it adapts to different landing places, control instruction is sent by earth station system remote monitoring unmanned plane and in real time, achievees the purpose that remotely to scout and defend.
Description
Technical field
The present invention relates to unmanned plane field, specifically a kind of battlefield is scouted and defence unmanned plane.
Background technology
Modern war majority belongs to local war, and duration of war is long, much belongs to the seasaw battle of long-term stalemate,
The one long-term continuous reconnaissance of battlefield surrounding area and defence are just particularly important in this way, traditional scouting and defence are set
Standby and means are all very high in expense and risk.With the extensive development of unmanned air vehicle technique, unmanned plane is widely applied to war
It is scouted and is defendd on, can play prodigious booster action, but existing unmanned plane in battle reconnaissance and defence really
It will be limited by battery, the flight time is short, cannot garrison execution task for a long time, and the conditions such as landing place limitation also constrain
It is applied.
Invention content
The technical problem to be solved in the present invention is to provide a kind of battlefield scout and defence unmanned plane, have fly it is farther,
Continuous working period is longer, and work is more stable, the advantages of can garrisoning for a long time.
The technical scheme is that：
A kind of battlefield is scouted and defence unmanned plane, includes fuselage, is set to the navigation flight control system of fuselage interior, electrical system
System and Energy Management System, the solar recharging system being set on fuselage roof end face are located at the task right over fuselage and carry
Lotus reaches the jacking system that outside fuselage and top is connect with mission payload, multiple uniform fixations and the rack on fuselage periphery,
It is multigroup to be connected to dynamical system and flexible folding undercarriage on corresponding rack outer end；It is the mission payload, electrical
System connect power supply with solar recharging system by Energy Management System, and the dynamical system includes motor and passes through
Electricity adjusts the propeller being connect with motor, and the motor and electricity of the dynamical system are adjusted, navigation flight control system connects with electrical system
Connect power supply；The dynamical system motor and the electric control terminal adjusted, the drive control end of jacking system, each flexible folding rises
The drive control end for falling frame is connect with navigation flight control system, and the navigation flight control system, mission payload pass through data-link
It is connect with earth station system, navigation flight control system is used for each flexible according to the automatic adjustment of the horizontal information of fuselage when fuselage lands
The length of folding undercarriage ensures unmanned plane stable landing, and after fuselage landing, controls jacking system by mission payload
It increases, obtains the broader monitoring visual field.
The flexible folding undercarriage include the connector sleeve being connected on the pedestal of the motor, top with
Connector sleeve is connected to the telescopic supporting rod in supporting rod positioning sleeve by the hinged supporting rod positioning sleeve of shaft and top；Institute
When the supporting rod positioning sleeve stated opens telescopic supporting rod along connector sleeve rotation, the top of the supporting rod positioning sleeve resists company
The bottom end of female connector.
The Energy Management System is connect with navigation flight control system, after navigation flight control system control unmanned plane landing,
Energy Management System is by the electrical energy transportation of solar recharging system to mission payload and electrical system.
Advantages of the present invention：
（1）, the present invention be provided with jacking system, unmanned plane reach specify landing place after, by Navigation of Pilotless Aircraft flight control system
Or earth station system remote control makes jacking system execute vertical motion, it is wider to obtain to drive mission payload to move up
The wealthy visual field, monitoring range is more extensive, and jacking system drives mission payload to return to original position after waiting for task.
（2）, the present invention by the solar panel mounted on fuselage centre to mission payload and aircraft electric power storage
Pond is powered, and not only ensure that the chronicity of aircraft work, but also resource is reasonably utilized；
（3）, the present invention be provided with Energy Management System, control solar panel converts solar energy into electrical energy, and a part is
Mission payload is powered, and a part is that electrical system is powered；After waiting for task, unmanned plane returns to finger by the power supply of electrical system
Positioning is set.
（4）, the present invention navigation flight control system, mission payload connect with earth station system by data-link, pass through ground
Face station system is monitored the working condition of unmanned plane, can carry out remote control by earth station system；Mission payload simultaneously
It works after aircraft reaches designated position, plays the role of monitoring to battlefield.
（5）, the present invention after reaching designated position can by earth station system before the program that sets landed automatically,
Flexible folding undercarriage can according to the device of landing place automatic controlled height, therefore no matter drop to where,
Can be levelling by the adjusting of undercarriage progress, make aircraft stable landing and reaches designated position；And flexible folding rises
It falls frame to can be folded in transportational process, reduces occupied space.
Environmental suitability of the present invention is stronger, voyage is farther and can garrison battlefield for a long time and execute scouting and defensive missions,
It is scouted and is defendd in specified region before war starts or during progress, unmanned plane is hidden, its own carries solar energy
Charging unit can give mission payload for a long time（Radar, loudspeaker, photoelectric nacelle and related weapon system etc.）Power supply, it is flexible to roll over
Stacked undercarriage can ensure that it adapts to different landing places, send by earth station system remote monitoring unmanned plane and in real time
Control instruction achievees the purpose that remotely to scout and defend.
Description of the drawings
Fig. 1 is the front view under landing state of the present invention.
Fig. 2 is the front view under undercarriage folded state of the present invention.
Fig. 3 is the vertical view of the present invention.
Fig. 4 is the structural schematic diagram that the flexible folding undercarriage connector sleeve of the present invention is connected with supporting rod positioning sleeve.
Fig. 5 is the principle of the present invention block diagram.
Specific implementation mode
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation describes, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
See Fig. 1-Fig. 3 and Fig. 5, a kind of battlefield is scouted and defence unmanned plane, includes fuselage 1, is set to inside fuselage 1
Navigation flight control system 2, electrical system 3 and Energy Management System 4, the solar recharging system being set in 1 top end surface of fuselage
System 5, the mission payload 6 being located at right over fuselage 1 reach the jacking system 7 that outside fuselage 1 and top is connect with mission payload 6,
Six uniform fixations and the rack 8 on 1 periphery of fuselage, six groups are connected to dynamical system 9 on corresponding rack outer end and stretch
Folding undercarriage 10；Mission payload 6, electrical system 3 are connect by Energy Management System 4 with solar recharging system 5
Power supply, dynamical system 9 include motor and adjust the propeller being connect with motor, the motor and electricity of dynamical system 9 to adjust, lead by electricity
Boat flight control system 2 connect power supply with electrical system 3；The driving for the control terminal, jacking system 7 that 9 motor of dynamical system and electricity are adjusted
Control terminal, the drive control end of each flexible folding undercarriage 10, Energy Management System 4 are connect with navigation flight control system 2,
Navigation flight control system 2, mission payload 6 are connect by data-link with earth station system 11, and navigation flight control system 2 is used in fuselage
The length for automatically adjusting each flexible folding undercarriage 10 when landing according to the horizontal information of fuselage ensures that unmanned plane steadily drops
It falls, and after fuselage landing, control jacking system 7 increases mission payload 6, obtains the broader monitoring visual field, while energy
Management system 4 is by the electrical energy transportation of solar recharging system 5 to mission payload 6 and electrical system 3.
Wherein, see Fig. 4, flexible folding undercarriage 10 includes the connector sleeve 101 being connected on the pedestal of motor, top
End is connected to by the hinged supporting rod positioning sleeve 102 of shaft and top in supporting rod positioning sleeve 102 with connector sleeve 101
Telescopic supporting rod 103（See Fig. 2）；When supporting rod positioning sleeve 102 opens telescopic supporting rod 103 along the rotation of connector sleeve 101, support
The top of bar positioning sleeve 102 resists the bottom end of connector sleeve 101.
UAV flight's mission payload lands after flying to designated position, and each flexible folding undercarriage 10 adjusts height and protects
Demonstrate,prove the horizontal smoothly landing of unmanned plane；After landing, make jacking system 7 that mission payload 6 be driven to reach according to battlefield actual conditions
Different height is monitored battlefield situation, and the solar panel of solar recharging system starts to absorb luminous energy, energy pipe
On the one hand reason system 4 provides the electric energy of conversion to electric energy to mission payload 6, remaining electric energy charges to electrical system 3, is carried in task
Lotus 6 executed task and electrical system 3 electricity be full of after, jacking system 7 drives mission payload 6 to return to initial position, nobody
Machine flies back appointed place.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
Understanding without departing from the principles and spirit of the present invention can carry out these embodiments a variety of variations, modification, replace
And modification, the scope of the present invention is defined by the appended.
Claims (3)
1. a kind of battlefield is scouted and defence unmanned plane, it is characterised in that：Include fuselage, the navigation for being set to fuselage interior flies
Control system, electrical system and Energy Management System, the solar recharging system being set on fuselage roof end face are being located at fuselage just
The mission payload of top reaches the jacking system that outside fuselage and top is connect with mission payload, multiple uniform fixations and fuselage
Rack on periphery, it is multigroup to be connected to dynamical system and flexible folding undercarriage on corresponding rack outer end；Described
Mission payload, electrical system connect power supply, the dynamical system packet with solar recharging system by Energy Management System
The propeller for including motor and being connect with motor by electricity tune, the motor and electricity tune, navigation flight control system of the dynamical system
Power supply is connect with electrical system；It is the drive control end of control terminal, jacking system that the dynamical system motor and electricity are adjusted, each
The drive control end of flexible folding undercarriage is connect with navigation flight control system, and the navigation flight control system, task carry
Lotus is connect by data-link with earth station system, and navigation flight control system is used for when fuselage lands according to the horizontal information of fuselage
The length for automatically adjusting each flexible folding undercarriage ensures unmanned plane stable landing, and after fuselage landing, control lifting
System increases mission payload, obtains the broader monitoring visual field.
2. a kind of battlefield according to claim 1 is scouted and defence unmanned plane, it is characterised in that：Described stretching can roll over
Stacked undercarriage includes that connector sleeve, top and the connector sleeve being connected on the pedestal of the motor pass through the hinged branch of shaft
Strut positioning sleeve and top are connected to the telescopic supporting rod in supporting rod positioning sleeve；The supporting rod positioning sleeve is along connection
When telescopic supporting rod is opened in set rotation, the top of the supporting rod positioning sleeve resists the bottom end of connector sleeve.
3. a kind of battlefield according to claim 1 is scouted and defence unmanned plane, it is characterised in that：The energy management
System is connect with navigation flight control system, and after navigation flight control system control unmanned plane landing, Energy Management System is by solar charging
The electrical energy transportation of electric system is to mission payload and electrical system.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810236870.7A CN108341059A (en) | 2018-03-21 | 2018-03-21 | A kind of battlefield is scouted and defence unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810236870.7A CN108341059A (en) | 2018-03-21 | 2018-03-21 | A kind of battlefield is scouted and defence unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108341059A true CN108341059A (en) | 2018-07-31 |
Family
ID=62957190
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810236870.7A Pending CN108341059A (en) | 2018-03-21 | 2018-03-21 | A kind of battlefield is scouted and defence unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108341059A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109334978A (en) * | 2018-09-30 | 2019-02-15 | 李元芳 | Scounting aeroplane damage separation information transfer device in maritime affairs intelligence cruise |
| CN112520021A (en) * | 2020-12-06 | 2021-03-19 | 山东省十里香芝麻制品股份有限公司 | Full-automatic sesame plant protection machine |
| CN112644725A (en) * | 2020-12-18 | 2021-04-13 | 深圳市爱华勘测工程有限公司 | Surveying and mapping aircraft and management control method thereof |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN112644725A (en) * | 2020-12-18 | 2021-04-13 | 深圳市爱华勘测工程有限公司 | Surveying and mapping aircraft and management control method thereof |
| CN112644725B (en) * | 2020-12-18 | 2022-03-11 | 深圳市爱华勘测工程有限公司 | Surveying and mapping aircraft and management control method thereof |
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