CN108639330A - A kind of air traffic air route prospecting unmanned plane - Google Patents
A kind of air traffic air route prospecting unmanned plane Download PDFInfo
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- CN108639330A CN108639330A CN201810632738.8A CN201810632738A CN108639330A CN 108639330 A CN108639330 A CN 108639330A CN 201810632738 A CN201810632738 A CN 201810632738A CN 108639330 A CN108639330 A CN 108639330A
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- unmanned plane
- fuselage
- pair
- motor
- screw
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/10—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles characterised by the energy transfer between the charging station and the vehicle
- B60L53/12—Inductive energy transfer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
- B64C27/10—Helicopters with two or more rotors arranged coaxially
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/10—Stabilising surfaces adjustable
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L2200/00—Type of vehicles
- B60L2200/10—Air crafts
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/14—Plug-in electric vehicles
Abstract
The invention discloses a kind of air traffic air routes to reconnoitre unmanned plane, including head, fuselage, a pair of of flank, first balance wing, second balance wing and balance tailstock, head is internally provided with radar altitude sensor, Big Dipper alignment sensor, ultrasonic detector and infrared detector, fuselage interior, which is equipped with, stores accumulator and signal tube, coulometric detector is set below accumulator, setting information processor beside coulometric detector, setting command lock beside message handler, the following setting signal receiver of order lock, the wireless charging receiver is arranged in signal receiver below, positioning shooting head is set beside wireless charging receiver, fuselage lower end setting positioning support leg.The present invention can keep good stability and balance quality when undergoing the particular surroundings such as barrier and bad weather, and it can realize self-service charging, with locking mechanism, unmanned plane can not be avoided to be generated due to having consumed electricity when the external world instructs and fallen from the external world's input instruction when locking.
Description
Technical field
The present invention relates to air vehicle technique field, unmanned plane is reconnoitred in specially a kind of air traffic air route.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned unmanned plane, have the characteristics that portability is high, easy to operate, using flexible.Existing unmanned plane mainly utilizes navigation
The course line planned in advance carries out flight automatically or is flown by operating personnel's remote control real-time control, however flight course
In be possible to encounter various complicated or uncertain environment, such as barrier needs to temporarily change course line with avoiding barrier, no
Installation or air crash accident may then be caused.Therefore, air traffic air route reconnaissance UAV surveys air route meteorology, air route environment, draws
Manned navigation aircraft or guiding heavy duty work unmanned plane during flying are led, is necessary.This requires unmanned planes in experience obstacle
There can be preferable stability when the particular surroundings such as object and bad weather, it is effective by maintaining the stability of itself to carry out
Evade and avoiding collision, this is the technical barrier that current unmanned plane faces.
Invention content
The purpose of the present invention is to provide a kind of air traffic air routes to reconnoitre unmanned plane, to solve to carry in above-mentioned background technology
The problem of going out.
In order to solve the above technical problem, the present invention provides following technical solutions：Nobody is reconnoitred in a kind of air traffic air route
Machine, including head, fuselage, a pair of of flank, the first balance wing, the second balance wing and balance tailstock, the head are internally provided with
Radar altitude sensor, Big Dipper alignment sensor, ultrasonic detector and infrared detector, the fuselage interior, which is equipped with, to be stored
Battery and signal tube, the storage accumulator lower section setting coulometric detector, coulometric detector side setting information processor,
Setting command lock beside described information processor, the following setting signal receiver of order lock, the signal connect
It receives device and the wireless charging receiver is set below, positioning shooting head, the fuselage are set beside the wireless charging receiver
Lower end setting positioning support leg, support frame as described above top are arranged the landing gear, the wireless charging are arranged among the landing gear
Electric transmitter, the landing gear top setting landing identify, the landing mark surrounding setting locator, below the locator
Pressure inductor is set, and power module, support frame as described above side setting signal transmitter, the letter is arranged in support frame as described above lower end
Drawing fumicants is accommodated in horn, the pair of flank is symmetricly set on the both sides of the head, and the free end of the flank is equipped with
First motor, first balance wing, including the first propeller and the second motor, second motor are fixed on by mounting base
The top of the head, second motor drive the first propeller rotation, and second balance wing is mounted on described the
The top of one balance wing, second balance wing include the second propeller and third motor, and the third motor is mounted on described
The top of mounting base, it includes a pair of of extension frame, one that the third motor, which drives the second propeller rotation, the balance tailstock,
To empennage and connecting plate, a pair extends frame and is horizontally disposed with, along the length direction distribution of the fuselage, and a pair extends one end of frame
Be separately fixed on a pair of of flank, the other end is fixedly connected by the connecting plate, the extension frame passes through a feed tube and institute
Signal tube connection is stated, the frame that extends is internally provided with the hollow chamber that fumicants is drawn in export, and a pair of of empennage is hinged on the connecting plate
Both sides, be equipped with groove in the middle part of the connecting plate, the structure of a pair of of empennage of locking be equipped in the groove.
Further, the storage accumulator is fastenedly connected with the fuselage by screw, the positioning support leg with it is described
Fuselage is fastenedly connected by screw.
Further, the coulometric detector is fastenedly connected with the fuselage by screw, described information processor and institute
It states fuselage to be fastenedly connected by screw, the order lock is fastenedly connected with the fuselage by screw.
Further, the wireless charging receiver is fastenedly connected with the fuselage by screw, the positioning shooting head
It is fastenedly connected by screw with the fuselage.
Further, the landing gear is bolted with support frame as described above, the signal projector and the support
Frame is fastenedly connected by screw.
Further, the power module is fastenedly connected with support frame as described above by screw, the wireless charging transmitter
It is fastenedly connected by screw with support frame as described above.
Further, the pressure inductor is connect with the wireless charging transmitter by conducting wire.
Further, the other end for extending frame is equipped with baffle straight up, and a pair of of baffle is located at a pair of of extension frame
Outside.
Further, two groups of telescopic rods and a pair of 4th motor are equipped in the groove, the 4th motor drives one group
Telescopic rod is flexible, and one end of every group of telescopic rod is connected to described extend on the medial surface of frame.
Further, the free end of a pair of of empennage is mutually matched cambered surface, the free end of one of empennage be convex surface,
The free end of another empennage is concave surface.
Further, further include undercarriage, the undercarriage is arranged to be set inside the bottom of the fuselage, the undercarriage
There are multi-staged air damper and spring.
Further, second motor is opposite with the rotation direction of output shaft of third motor.
Compared with prior art, the advantageous effect of the invention reached is：
1), the present invention will be set gradually before and after head and fuselage, and flank, top the first balance wing of setting and the is arranged in both sides
Two balance wings, tail portion setting balance tailstock increase nobody using lightweight material in own physical structure and aerodynamics angle
The balance of machine optimizes flight structure and traction power, and flank is symmetrical arranged, the first balance wing and the second balance wing are coaxial up and down
Setting, makes that unmanned plane during flying is more steady, can fly to switch rapidly between the state of flights such as rotation in hovering, side, balances tailstock
Structural strength, the dispersion stress for increasing unmanned plane, form strength and support, greatly improve reliability of structure and load-bearing capacity；
2), head be mounted with perception, disturbance in judgement object information multiple element, it is ensured that the efficient and reliability of inspection, machine
Body is mounted with accumulator and signal tube, and accumulator provides stable cruising ability, and signal tube, which loads, draws fumicants, head element compared with
Gently, body element is heavier, and center of gravity is made to fall the position to the rear in the middle part of unmanned plane, is conducive to unmanned plane in gradually release electric energy and export
Balance is kept during drawing fumicants, the first propeller, the second propeller are fixed on fuselage roof, final assembly by mounting base
Stablize, ensure fuselage intensity, the first propeller is controlled by the second motor, the second propeller is controlled by third motor, different
Driving device adjusts rotating speed, and convenient for completing, the various flare maneuvers of unmanned plane, landing is more stable, power is more longlasting；
3), unmanned plane in the case that encounter it is set can by spraying draw fumicants remind rear aircraft pay attention to convert course line, prolong
Long frame is connected to by feed tube with the signal tube of fuselage, is formed for drawing long and narrow flue derived from fumicants, and making smog more has type strong,
Awing centre of lift moves unmanned plane with the angle of attack and velocity variations, empennage distance center farther out, just with the lift of very little
Can holding torque balance, a pair of of empennage is hinged, is rotated within the scope of 90 ° by adjusting established angle, forms vertical tail or level
Empennage generates the torque opposite with deflection direction, keeps original posture, locking mechanism when having crosswind or sinuous flow upsets straight trip
Ensure the storage of empennage level, does not swing awing；
4), baffle forms the position limiting structure of empennage, and it is vertical state to make empennage full swing angle；The driving of 4th motor is stretched
Contracting bar stretches within the scope of certain amplitude, and telescopic rod is rigid structure, provides stable support force and convergent force；Arc surfaced edge
Reduction corner angle, convex surface are convenient for a pair of of empennage to be collapsed simultaneously to middle part, the two are avoided to rub with concave surface；Undercarriage takes off in unmanned plane
Unmanned plane is supported to provide buffer protection work when ground moving, air damper and spring land to unmanned plane when landing or sliding
With；Second motor, third motor output rotational axis direction on the contrary, make unmanned plane horizontal direction equalising torque, flight is more steady
It is fixed；
5) it, is not necessarily to plug wire, that is, chargeable, avoids dangerous caused by due to charging wire does not pull out, and can realize self-filling
Electricity has locking mechanism, can not avoid generating pendant due to unmanned plane has consumed electricity when the external world instructs from the external world's input instruction when locking
It falls, it is safer, it is more energy saving and safe by sensing switch circuit.
Description of the drawings
Attached drawing is used to provide further understanding of the present invention, and a part for constitution instruction, the reality with the present invention
It applies example to be used to explain the present invention together, not be construed as limiting the invention.In the accompanying drawings：
Fig. 1 is the structural diagram of the present invention；
Fig. 2 is the vertical view of the present invention；
Fig. 3 is the structural schematic diagram that tailstock is balanced in the present invention；
Fig. 4 is the structural schematic diagram of charging unit in the present invention；
Fig. 5 is the top view of landing gear in the present invention；
Fig. 6 is the local part schematic diagram of the present invention.
In figure：1, head, 2, fuselage, 3, a pair of of flank, 31, first motor, the 4, first balance wing, the 5, second balance wing,
61, a pair of to extend frame, 62, a pair of of empennage, 63, connecting plate, 64, telescopic rod, 65, feed tube, 9, accumulator, 10, electric power detection
Device, 11, positioning support leg, 12, message handler, 13, wireless charging receiver, 14, signal receiver, 15, positioning shooting head,
16, order lock, 17, landing gear, 18, wireless charging transmitter, 19, landing mark, 20, locator, 21, pressure sensitive
Device, 22, supporting rack, 23, power module, 24, signal projector.
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.
- Fig. 6 is please referred to Fig.1, the present invention provides a kind of technical solution：A kind of air traffic air route prospecting unmanned plane, including
Head 1, fuselage 2, a pair of of flank 3, the first balance wing 4, the second balance wing 5 and balance tailstock, the head 1 are internally provided with
Radar altitude sensor, Big Dipper alignment sensor, ultrasonic detector and infrared detector, the fuselage 2 are internally provided with storage
Battery and signal tube, coulometric detector 10 is arranged in 9 lower section of accumulator, for detecting 9 electricity of unmanned plane accumulator, coulometric detector
10 side setting information processors 12, for handling various feedback informations, 12 side setting command lock of message handler
16, for locking aviation mechanism athletic posture, 16 following setting signal receiver 14 of order lock, for receiving signal transmitting
The signal that device 24 is sent out, wireless charging receiver 13 is arranged in signal receiver 14 below, for receiving wireless charging transmitter 18
The electric power sent out, 13 side setting positioning shooting head 15 of wireless charging receiver, for positioning shooting, the setting of 7 lower end of fuselage is fixed
Position support leg 11, is used to support and positions, and landing gear 17 is arranged in 22 top of supporting rack, for unmanned plane landing and carries upper part
Wireless charging transmitter 18 is arranged in part, 17 centre of landing gear, is used for transmitting electric power, and the setting landing of 17 top of landing gear identifies 19,
For facilitating unmanned plane landing to provide identification, locator 20 is arranged in landing 19 surroundings of mark, for positioning unmanned plane landing place,
For 20 following settings pressure inductor 21 of locator for judging pressure with break-make circuit, power module is arranged in 22 lower end of supporting rack
23, for providing electric power, 22 side setting signal transmitter 24 of supporting rack is accommodated with drawing for emitting signal in the signal tube
Fumicants, the pair of flank 3 are symmetricly set on the both sides of the head 1, and the free end of the flank 3 is equipped with first motor 31,
First balance wing 4 includes the first propeller and the second motor, and second motor is fixed on the head 1 by mounting base
Top, second motor drives the first propeller rotation, second balance wing 5 to be mounted on first balance wing
4 top, second balance wing 5 include the second propeller and third motor, and the third motor is mounted on the mounting base
Top, the third motor drives the second propeller rotation, and the balance tailstock includes a pair of extending frame 61, a pair of tail
The wing 62 and connecting plate 63, a pair extends frame 61 and is horizontally disposed with, along the length direction distribution of the fuselage 2, and a pair extends frame 61
One end be separately fixed on a pair of of flank 3, the other end is fixedly connected by the connecting plate 63, the extension frame 61 passes through one
Feed tube 65 is connected to the signal tube, and the frame 61 that extends is internally provided with the hollow chamber that fumicants is drawn in export, a pair of of empennage 62
The both sides of the connecting plate 63 are hinged on, 63 middle part of the connecting plate is equipped with groove, and a pair of of empennage of locking is equipped in the groove
62 structure.
In the present embodiment, coulometric detector 10 detects 9 remaining capacity situation of unmanned plane accumulator always, and feeds back to information
Processor 12 starts order lock 16, order when message handler 12 obtains 9 remaining capacity deficiency of unmanned plane accumulator
Lock 16 locks aviation mechanism motion state, rejects external operation signal, and signal receiver 14 receives signal projector
24 signals, and message handler 12 is fed back to, 12 automatic setting path of message handler makes unmanned plane go to nearest wireless charging
Motor structure, when unmanned plane is close to wireless charging mechanism, positioning shooting head 15 detects landing mark 18, message handler first
12 carry out first stage landing by this message command unmanned plane, and floating state is entered when unmanned plane drops to designated position,
Positioning shooting head 15 judges that the position of locator 20, subsequent unmanned plane adjust posture again at this time, carries out second stage landing, directly
To landing gear 17 is dropped to, at this point, positioning support leg 11 drops down onto on locator 20, pressure inductor 21 is experienced pressure and is connected back
Road, power module 23 provide electric power, are sent out by wireless charging transmitter 18, and it is nobody that wireless charging receiver 13, which receives electric power,
Machine accumulator 9 charges, and when coulometric detector 10 detects that unmanned plane accumulator 9 has enough electricity, order lock 16 closes
Lock-out state is closed, unmanned plane is flown away from, and pressure inductor 21 experiences pressure disappearance, then disconnects circuit, wireless charging transmitter
18 are stopped.
In the present embodiment, with fuselage 2 by axis connection, unmanned plane accumulator 9 is fastened with fuselage 2 by screw aviation mechanism
Connection, positioning support leg 11 are fastenedly connected with fuselage 2 by screw, and coulometric detector 10 is fastenedly connected with fuselage 2 by screw,
Message handler 12 is fastenedly connected with fuselage 2 by screw, and order lock 16 is fastenedly connected with fuselage 2 by screw, wirelessly
Charging receiver 13 is fastenedly connected with fuselage 2 by screw, and positioning shooting head 15 is fastenedly connected with fuselage 2 by screw, landing
Frame 17 is bolted with supporting rack 22, and signal projector 24 is fastenedly connected with supporting rack 22 by screw, power module 23
It is fastenedly connected by screw with supporting rack 22, wireless charging transmitter 18 is fastenedly connected with supporting rack 22 by screw, feeling of stress
Device 21 is answered to be connect by conducting wire with wireless charging transmitter 18.
It in the present embodiment, will be set gradually before and after head 1 and fuselage 2, flank 3, the first balance of top setting is arranged in both sides
The wing 4 and the second balance wing 5, tail portion setting balance tailstock, using lightweight material, in own physical structure and aerodynamics angle
Degree increases the balance of unmanned plane, optimizes flight structure and traction power, and flank 3 is symmetrical arranged, the first balance wing 4 and second is flat
About 5 wing that weighs is coaxially disposed, and makes that unmanned plane during flying is more steady, can fly between the state of flights such as rotation rapidly in hovering, side
Switching, balance tailstock increase the structural strength of unmanned plane, dispersion stress, form strength and support, greatly improve reliability of structure
And load-bearing capacity.
In the present embodiment, head 1 be mounted with perception, disturbance in judgement object information multiple element, it is ensured that inspection it is efficient with
Reliability, fuselage 2 are mounted with accumulator and signal tube, and accumulator provides stable cruising ability, and signal tube, which loads, draws fumicants, machine
First 1 element is relatively light, 2 element heavy of fuselage, so that center of gravity is fallen the position to the rear in the middle part of unmanned plane, is conducive to unmanned plane and is gradually releasing
Electric discharge keeps balance during capable of and exporting drawing fumicants, and the first propeller, the second propeller are fixed on fuselage 2 by mounting base
Top, final assembly is stable, ensures 2 intensity of fuselage, and the first propeller is controlled by the second motor, the second propeller passes through third
Motor controls, and the various flare maneuvers of unmanned plane, landing be more stable, power is more held convenient for completing for different driving device adjustment rotating speed
Long.
In the present embodiment, unmanned plane in the case that encounter it is set can by spraying draw fumicants remind rear aircraft pay attention to converting
Course line extends frame 61 and is connected to the signal tube of fuselage 2 by feed tube 65, formed for drawing long and narrow flue derived from fumicants, make cigarette
Mist more has type strong, and awing centre of lift moves unmanned plane with the angle of attack and velocity variations, 62 distance center of empennage farther out,
With the lift of very little can holding torque balance, a pair of of empennage 62 is hinged, is rotated within the scope of 90 ° by adjusting established angle, shape
At vertical tail 62 or tailplane 62, when having crosswind or sinuous flow upsets straight trip, the torque opposite with deflection direction is generated, is protected
Hold original posture, locking mechanism can in order to control the L-shaped limited block of device control, can device control in order to control tension spring, etc., protect
The horizontal storage of empennage 62 is demonstrate,proved, is not swung awing.
In the present embodiment, unmanned plane is reconnoitred in the air traffic air route, and it is vertical that the other end for extending frame 61 is equipped with
Upward baffle, a pair of of baffle are located at a pair of outside for extending frame 61.Baffle forms the position limiting structure of empennage 62, makes empennage 62 most
Big swing angle is vertical state.
In the present embodiment, unmanned plane is reconnoitred in the air traffic air route, and two groups of 64 Hes of telescopic rod are equipped in the groove
A pair of 4th motor, the 4th motor drive one group of telescopic rod 64 flexible, and one end of every group of telescopic rod 64 is connected to described prolong
On the medial surface of long frame 61.4th motor drives telescopic rod 64 to stretch within the scope of certain amplitude, and telescopic rod 64 is that rigidity is tied
Structure provides stable support force and convergent force.
In the present embodiment, unmanned plane is reconnoitred in the air traffic air route, and the free end of a pair of of empennage 62 is to cooperate
Cambered surface, the free end of one of empennage 62 be convex surface, another empennage 62 free end be concave surface.It reduces at arc surfaced edge
Corner angle, convex surface are convenient for a pair of of empennage 62 to be collapsed simultaneously to middle part, the two are avoided to rub with concave surface.
In the present embodiment, unmanned plane is reconnoitred in the air traffic air route, further includes：Undercarriage is arranged in the machine
The bottom of body 2, the undercarriage are internally provided with multi-staged air damper and spring.Undercarriage takes off landing or cunning in unmanned plane
Unmanned plane is supported to provide buffer protection function when ground moving, air damper and spring land to unmanned plane when row.
In the present embodiment, unmanned plane, second motor and the third motor are reconnoitred in the air traffic air route
The rotation direction of output shaft is opposite.Second motor, third motor output rotational axis direction on the contrary, making unmanned plane horizontal direction power
Square balances, and flight is more stablized.
Finally it should be noted that：The foregoing is only a preferred embodiment of the present invention, is not intended to restrict the invention,
Although the present invention is described in detail referring to the foregoing embodiments, for those skilled in the art, still may be used
With technical scheme described in the above embodiments is modified or equivalent replacement of some of the technical features.
All within the spirits and principles of the present invention, any modification, equivalent replacement, improvement and so on should be included in the present invention's
Within protection domain.
Claims (10)
1. unmanned plane is reconnoitred in a kind of air traffic air route, it is characterised in that：Including head, fuselage, a pair of of flank, the first balance
The wing, the second balance wing and balance tailstock, the head are internally provided with radar altitude sensor, Big Dipper alignment sensor, ultrasound
Wave detector and infrared detector, the fuselage interior, which is equipped with, stores accumulator and signal tube, setting below the storage accumulator
Coulometric detector, coulometric detector side setting information processor, described information processor side setting command lock,
The wireless charging receiver, institute is arranged in the following setting signal receiver of order lock, the signal receiver below
It states and positioning shooting head is set beside wireless charging receiver, the fuselage lower end setting positioning support leg, support frame as described above top
The landing gear is set, the wireless charging transmitter, the landing gear top setting landing mark are set among the landing gear
Know, locator, the locator following settings pressure inductor, the setting of support frame as described above lower end is arranged in the landing mark surrounding
Power module, setting signal transmitter beside support frame as described above are accommodated with drawing fumicants, the pair of flank pair in the signal tube
Title is arranged in the both sides of the head, and the free end of the flank is equipped with first motor, first balance wing, including the first spiral shell
Paddle and the second motor are revolved, second motor is fixed on the top of the head by mounting base, and second motor drives institute
The rotation of the first propeller is stated, second balance wing is mounted on the top of first balance wing, and second balance wing includes
Second propeller and third motor, the third motor are mounted on the top of the mounting base, described in third motor driving
Second propeller rotates, and the balance tailstock includes a pair of of extension frame, a pair of of empennage and connecting plate, and a pair extends frame level and sets
It sets, along the length direction distribution of the fuselage, and a pair of one end for extending frame is separately fixed on a pair of of flank, the other end passes through
The connecting plate is fixedly connected, and the extension frame is connected to by a feed tube with the signal tube, and the extension frame is internally provided with
Export draws the hollow chamber of fumicants, a pair of of empennage to be hinged on the both sides of the connecting plate, groove, institute are equipped in the middle part of the connecting plate
State the structure that a pair of of empennage of locking is equipped in groove.
2. unmanned plane is reconnoitred in a kind of air traffic air route according to claim 1, it is characterised in that：The storage accumulator with
The fuselage is fastenedly connected by screw, and the positioning support leg is fastenedly connected with the fuselage by screw；The electricity inspection
It surveys device to be fastenedly connected by screw with the fuselage, described information processor is fastenedly connected with the fuselage by screw, described
Order lock is fastenedly connected with the fuselage by screw.
3. unmanned plane is reconnoitred in a kind of air traffic air route according to claim 1, it is characterised in that：The wireless charging connects
It receives device to be fastenedly connected by screw with the fuselage, the positioning shooting head is fastenedly connected with the fuselage by screw；It is described
Landing gear is bolted with support frame as described above, and the signal projector is fastenedly connected with support frame as described above by screw.
4. unmanned plane is reconnoitred in a kind of air traffic air route according to claim 1, it is characterised in that：The power module with
Support frame as described above is fastenedly connected by screw, and the wireless charging transmitter is fastenedly connected with support frame as described above by screw.
5. unmanned plane is reconnoitred in a kind of air traffic air route according to claim 1, it is characterised in that：The pressure inductor
It is connect by conducting wire with the wireless charging transmitter.
6. unmanned plane is reconnoitred in a kind of air traffic air route according to claim 1, it is characterised in that：It is described to extend the another of frame
One end is equipped with baffle straight up, and a pair of of baffle is located at a pair of outside for extending frame.
7. unmanned plane is reconnoitred in a kind of air traffic air route according to claim 1, it is characterised in that：It is equipped in the groove
Two groups of telescopic rods and a pair of 4th motor, the 4th motor drive one group of telescopic rod flexible, one end connection of every group of telescopic rod
Extend on the medial surface of frame described.
8. unmanned plane is reconnoitred in a kind of air traffic air route according to claim 1, it is characterised in that：The freedom of a pair of of empennage
End is mutually matched cambered surface, the free end of one of empennage be convex surface, another empennage free end be concave surface.
9. unmanned plane is reconnoitred in a kind of air traffic air route according to claim 1, it is characterised in that：Further include undercarriage,
The undercarriage is arranged in the bottom of the fuselage, and the undercarriage is internally provided with multi-staged air damper and spring.
10. unmanned plane is reconnoitred in a kind of air traffic air route according to claim 1, it is characterised in that：Second motor
It is opposite with the rotation direction of output shaft of third motor.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201810632738.8A CN108639330A (en) | 2018-06-20 | 2018-06-20 | A kind of air traffic air route prospecting unmanned plane |
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| CN201810632738.8A CN108639330A (en) | 2018-06-20 | 2018-06-20 | A kind of air traffic air route prospecting unmanned plane |
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Application publication date: 20181012 |