CN107310726B - A kind of unmanned plane in operation process convenient for stopping - Google Patents
A kind of unmanned plane in operation process convenient for stopping Download PDFInfo
- Publication number
- CN107310726B CN107310726B CN201710498342.4A CN201710498342A CN107310726B CN 107310726 B CN107310726 B CN 107310726B CN 201710498342 A CN201710498342 A CN 201710498342A CN 107310726 B CN107310726 B CN 107310726B
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- CN
- China
- Prior art keywords
- block
- motor
- sucker
- gear
- electromagnet
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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
- 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
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Abstract
The unmanned plane that the present invention relates to a kind of in operation process convenient for stopping, stopping mechanism includes adsorbing mechanism, PLC and testing agency, the adsorbing mechanism includes fixed block, first motor, Knucle-gear, bar gear, first walks block, first sucker and reinforcement absorbent module, the reinforcement absorbent module includes the second motor, first screw rod, second walks block, connecting rod and the second sucker, the testing agency includes fixed link, first electromagnet, second electromagnet, spring, third walks block, third motor, second screw rod and push rod, this is in operation process convenient for the unmanned plane of stop, through the first sucker in adsorbing mechanism and the second sucker suction on building, so as to lasting operation in the sky, rotor mechanism is set to close, save the energy, increase cruising ability and working efficiency, suction has been ensured by testing agency Random structure good can be adsorbed on building, ensure that safety.
Description
Technical field
The present invention relates to unmanned plane field, in particular to a kind of unmanned plane in operation process convenient for stopping.
Background technique
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft, or fully or intermittently automatically operated by car-mounted computer, at present take photo by plane, it is agricultural, plant protection, micro-
Type self-timer, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief,
The application in the fields such as movies-making, manufacture romance, has greatly expanded the purposes of unmanned plane itself.
When carrying out some work taken photo by plane or monitored, rotor mechanism long-play is needed, energy consumption is increased,
And cruising ability is bad, and rest in unmanned function on aerial building, it undoubtedly can be reduced consumption, and
Convenient working.
Summary of the invention
The technical problem to be solved by the present invention is for overcome the deficiencies in the prior art, providing one kind in operation process
Convenient for the unmanned plane of stop.
The technical solution adopted by the present invention to solve the technical problems is: it is a kind of in operation process convenient for stop nobody
Machine including fuselage and the rotor mechanism being arranged on fuselage and stops mechanism, the stop mechanism include adsorbing mechanism, PLC and
Testing agency；
The adsorbing mechanism include fixed block, first motor, Knucle-gear, gear, first walk block, the first sucker and add
Strong absorbent module, the fixed block are fixed at the side of fuselage, and the first motor is arranged on fixed block, and described first
The rotation of motor driven Knucle-gear, the Knucle-gear and bar gear engage, and described first block that walks is located at the side of a gear, described
Bar gear is slidably connected with fixed block, and described gear is horizontally disposed, and the first side for walking block is arranged in first sucker,
Described first walks block between gear and the first sucker；
The reinforcement absorbent module includes the second motor, the first screw rod, second walks block, connecting rod and the second sucker, described
The rotation of second the first screw rod of motor driven, described second walks block equipped with the hole that walks, and the hole that walks is equipped with internal screw thread, institute
It states the internal screw thread that second walks on block to match with the external screw thread on the first screw rod, one end of first screw rod penetrates second and walks
Block, second sucker are arranged in second and walk the one end of block far from the first screw rod, and the reinforcement absorbent module has several, institute
It states and reinforces absorbent module and be connected to first by connecting rod and walk on block, second sucker is parallel with the first sucker；
The testing agency includes that fixed link, the first electromagnet, the second electromagnet, spring, third walk block, third electricity
The two sides of fixed block are arranged in machine, the second screw rod and push rod, the fixed link, and the fixed link is horizontally disposed, the fixed link
Side far from fuselage is equipped with detection slot, and the slot bottom of detection slot is arranged in first electromagnet, and second electromagnet passes through
Spring is connected on the first electromagnet, and the magnetic direction of first electromagnet and the second electromagnet is on the contrary, second electromagnetism
Iron is slidably connected with fixed link, and the third block that walks is located at side of second electromagnet far from the first electromagnet, the third
The rotation of the second screw rod of motor driven, the side of the push rod be equipped with the matched internal screw thread of the second screw rod, second screw rod
One end penetrates push rod；
The first motor, the second motor, third motor and rotor mechanism are electrically connected with PLC.
Preferably, in order to preferably be adsorbed on building, described first, which walks, is additionally provided with air pump and air guide among block
One end of pipe, the air pump is connected to by gas-guide tube with the inside of the first sucker, and the other end of the air pump is connected to outside, institute
Air pump is stated to be electrically connected with PLC.
It is general that first sucker is pushed by gear, make the first sucker suction on building, it, can be with when adsorbing difficult
The air in the first sucker is drawn by air pump, makes the inside and outside formation draught head of sucker, to make the first sucker suction
On building.
Preferably, second, which walks, is additionally provided with gag lever post, the limit on block in order to make second block that walks walk more steady
One end of position bar is fixed on second and walks on block, and the other end of the gag lever post penetrates connecting rod, the gag lever post and the first screw rod
In parallel.
Preferably, in order to protect push rod, the push rod is equipped with anticollison block far from the side of the second screw rod.
Preferably, in order to increase the firmness and resistance to practicality of the first sucker and the second sucker, first sucker and
The making material of second sucker is nitrile rubber.
Nitrile rubber mainly uses emulsion polymerization at low temperature to produce, and oil resistivity is fabulous, and wearability is higher, and heat resistance is preferable,
Bonding force is strong.
Preferably, controlling for convenience, the first motor, the second motor and third motor are servo motor.
Preferably, landing for convenience, support frame is additionally provided with below the fuselage.
Preferably, being also coated with machine oil between the Knucle-gear and gear to protect Knucle-gear and gear
Preferably, being additionally provided with rain cover above the stop mechanism for rain-proof.
It as preferably, connects with remote terminal terminal, to facilitate operation, is equipped in the fuselage wireless for convenience
Communication module.
The invention has the advantages that should be in operation process convenient for the unmanned aerial vehicle design clever structure stopped, practicability
Height, so as to lasting operation in the sky, makes through the first sucker in adsorbing mechanism and the second sucker suction on building
Rotor mechanism can close, and save the energy, increase cruising ability and working efficiency, ensured adsorbing mechanism by testing agency
It good can be adsorbed on building, ensure that safety, when needing to leave, the first sucker and are pushed open by push rod
Two suckers, to continue flight operation.
Detailed description of the invention
Present invention will be further explained below with reference to the attached drawings and examples.
Fig. 1 is the structural schematic diagram of the unmanned plane of the invention for being convenient for stopping in operation process；
Fig. 2 is the structural schematic diagram of the stop mechanism of the unmanned plane of the invention for being convenient for stopping in operation process；
Fig. 3 is the portion the A enlarged drawing of Fig. 2；
Fig. 4 is the portion the B enlarged drawing of Fig. 2；
Fig. 5 is the first sucker of the unmanned plane of the invention for being convenient for stopping in operation process and the connection knot of the second sucker
Structure schematic diagram.
In figure: 1. rotor mechanisms, 2. fuselages, 3. support frames, 4. stop mechanism, 5. fixed links, 6. first motors, 7. knuckle-tooth
Wheel, 8. push rods, 9. first walk block, 10. air pumps, 11. gas-guide tubes, 12. first suckers, 13. fixed blocks, 14. gears, and 15.
First electromagnet, 16. springs, 17. second electromagnet, 18. thirds walk block, 19. third motors, 20. second screw rods, and 21.
Two motors, 22. first screw rods, 23. gag lever posts, 24. second walk block, 25. second suckers, 26. connecting rods.
Specific embodiment
In conjunction with the accompanying drawings, the present invention is further explained in detail.These attached drawings are simplified schematic diagram, only with
Illustration illustrates basic structure of the invention, therefore it only shows the composition relevant to the invention.
As shown in Figs. 1-5, a kind of unmanned plane for being convenient for stopping in operation process, including fuselage 2 and setting are on fuselage 2
Rotor mechanism 1 and stop mechanism 4, the stops mechanism 4 include adsorbing mechanism, PLC and testing agency；
The adsorbing mechanism includes fixed block 13, first motor 6, Knucle-gear 7, gear 14, first walks block 9, first
Sucker 12 and reinforcement absorbent module, the fixed block 13 are fixed at the side of fuselage 2, and the setting of first motor 6 is solid
Determine on block 13, the first motor 6 drives Knucle-gear 7 to rotate, and the Knucle-gear 7 and gear 14 engage, and described first walks
Block 9 is located at the side of a gear 14, and described gear 14 is slidably connected with fixed block 13, and described gear 14 is horizontally disposed, institute
It states the first sucker 12 and first side for walking block 9 is set, described first walks block 9 between gear 14 and sucker；
The reinforcement absorbent module include the second motor 21, the first screw rod 22, second walk block 24, connecting rod 26 and second inhale
Disk 25, second motor 21 drive the rotation of the first screw rod 22, and described second walks block 24 equipped with the hole that walks, the hole that walks
It is equipped with internal screw thread, the described second internal screw thread to walk on block 24 is matched with the external screw thread on the first screw rod 22, and described first
One end of bar 22 penetrates second and walks block 24, second sucker 25 be arranged in second walk block 24 far from the first screw rod 22 one
End, the reinforcement absorbent module have several, and the reinforcement absorbent module is connected to first by connecting rod 26 and walks on block 9, institute
It is parallel with the first sucker 12 to state the second sucker 25；
The testing agency includes that fixed link 5, the first electromagnet 15, the second electromagnet 17, spring 16, third walk block
18, the two sides of fixed block 13,5 water of fixed link is arranged in third motor 19, the second screw rod 20 and push rod 8, the fixed link 5
Flat setting, the fixed link 5 are equipped with detection slot far from the side of fuselage 2, and the slot of detection slot is arranged in first electromagnet 15
Bottom, second electromagnet 17 are connected on the first electromagnet 15 by spring 16, first electromagnet 15 and the second electromagnetism
For the magnetic direction of iron 17 on the contrary, second electromagnet 17 is slidably connected with fixed link 5, the third walks block 18 positioned at second
Side of the electromagnet 17 far from the first electromagnet 15, the third motor 19 drive the second screw rod 20 to rotate, and the one of the push rod 8
Side be equipped with the matched internal screw thread of the second screw rod 20, one end of second screw rod 20 penetrates push rod 8；
The first motor 6, the second motor 21, third motor 19 and rotor mechanism 1 are electrically connected with PLC.
Preferably, in order to preferably be adsorbed on building, described first, which walks, is additionally provided with air pump 10 among block 9 and leads
One end of tracheae 11, the air pump 10 is connected to by gas-guide tube 11 with the inside of the first sucker 12, the other end of the air pump 10
It is connected to outside, the air pump 10 is electrically connected with PLC.
The first sucker 12 is generally pushed by gear 14, is adsorbed on the first sucker 12 on building, when absorption is difficult
When, the air in the first sucker 12 can be drawn by air pump 10, make the inside and outside formation draught head of sucker, to make the
One sucker 12 is adsorbed on building.
Preferably, second, which walks, is additionally provided with gag lever post 23 on block 24 in order to make second block 24 that walks walk more steady,
One end of the gag lever post 23 is fixed on second and walks on block 24, and the other end of the gag lever post 23 penetrates connecting rod 26, the limit
Position bar 23 is parallel with the first screw rod 22.
Preferably, in order to protect push rod 8, the push rod 8 is equipped with anticollison block far from the side of the second screw rod 20.
Preferably, described first inhales in order to increase the firmness and resistance to practicality of the first sucker 12 and the second sucker 25
The making material of disk 12 and the second sucker 25 is nitrile rubber.
Nitrile rubber mainly uses emulsion polymerization at low temperature to produce, and oil resistivity is fabulous, and wearability is higher, and heat resistance is preferable,
Bonding force is strong.
Preferably, controlling for convenience, the first motor 6, the second motor 21 and third motor 19 are servo electricity
Machine.
Preferably, landing for convenience, support frame 3 is additionally provided with below the fuselage 2.
Preferably, being also coated with machine between the Knucle-gear 7 and gear 14 to protect Knucle-gear 7 and gear 14
Oil
Preferably, being additionally provided with rain cover above the stop mechanism 4 for rain-proof.
It as preferably, is connected for convenience with remote terminal terminal, to facilitate operation, is equipped with nothing in the fuselage 2
Line communication module.
When the unmanned plane in operation process convenient for stopping enters designated position, first motor 6 is controlled by PLC and is opened
It opens, first motor 6 drives Knucle-gear 7 to rotate, and Knucle-gear 7 and gear 14 engage, and makes a gear 14 that the first sucker 12 be pushed to inhale
It is attached on the wall or window of building, then the rotation of the first screw rod 22 is driven by the second motor 21, to make second to walk
Block 24 is subjected to displacement, and the second sucker 25 is pushed to be adsorbed on window, then passes through the first electromagnet 15 and the second electricity in testing agency
Magnet 17 is opened, because of the magnetic direction of the first electromagnet 15 and the second electromagnet 17 on the contrary, being subjected to displacement the second electromagnet 17,
So that push rod 8 is handed over light promotion window, when the first sucker 12 and the second sucker 25 are not pushed away from, illustrate that adsorption effect is good,
Rotor mechanism 1 can be closed, makes this that the unmanned plane stopped is convenient for be adsorbed on window in operation process and carries out operation, work as needs
When flying away from, PLC controls rotor unlatching first, then drives the rotation of the second screw rod 20 by third motor 19, makes push rod 8 that position occur
It moves, 8 thrust of push rod is very big at this time, and the first sucker 12 and the second sucker 25 is made to leave window.
Compared with prior art, should be in operation process convenient for the unmanned aerial vehicle design clever structure stopped, practicability is high, leads to
The first sucker 12 and the second sucker 25 crossed in adsorbing mechanism are adsorbed on building, so as to lasting operation in the sky, are made
Rotor mechanism 1 can close, and save the energy, increase cruising ability and working efficiency, ensured adsorption machine by testing agency
Structure good can be adsorbed on building, ensure that safety, when needing to leave, push the first sucker open by push rod 8
12 and second sucker 25, to continue flight operation.
Taking the above-mentioned ideal embodiment according to the present invention as inspiration, through the above description, relevant staff is complete
Various changes and amendments can be carried out without departing from the scope of the technological thought of the present invention' entirely.The technology of this invention
Property range is not limited to the contents of the specification, it is necessary to which the technical scope thereof is determined according to the scope of the claim.
Claims (10)
1. a kind of unmanned plane in operation process convenient for stopping, which is characterized in that including fuselage (2) and be arranged in fuselage (2)
On rotor mechanism (1) and stop mechanism (4), the stop mechanism (4) includes adsorbing mechanism, PLC and testing agency；
The adsorbing mechanism includes fixed block (13), first motor (6), Knucle-gear (7), gear (14), first walks block
(9), the first sucker (12) and reinforce absorbent module, the fixed block (13) is fixed at the side of fuselage (2), and described first
Motor (6) is arranged on fixed block (13), first motor (6) driving Knucle-gear (7) rotation, the Knucle-gear (7) and item
Gear (14) engagement, described first walk block (9) be located at the side of gear (14), described gear (14) and fixed block (13)
It is slidably connected, described gear (14) is horizontally disposed, the side that the first sucker (12) setting walks block (9) first, institute
It states first and walks block (9) between gear (14) and the first sucker (12)；
The reinforcement absorbent module includes the second motor (21), the first screw rod (22), second walks block (24), connecting rod (26) and the
Two suckers (25), second motor (21) driving the first screw rod (22) rotation, described second walk block (24) be equipped with and walk
Hole, the hole that walks are equipped with internal screw thread, the outer spiral shell on the described second internal screw thread and the first screw rod (22) to walk on block (24)
Line matching, one end of first screw rod (22) penetrate second and walk block (24), and the second sucker (25) setting is walked second
The one end of position block (24) far from the first screw rod (22), the reinforcement absorbent module have several, and the reinforcement absorbent module passes through
Connecting rod (26) is connected to first and walks on block (9), and second sucker (25) is parallel with the first sucker (12)；
The testing agency includes that fixed link (5), the first electromagnet (15), the second electromagnet (17), spring (16), third walk
Block (18), third motor (19), the second screw rod (20) and push rod (8), the fixed link (5) are arranged the two of fixed block (13)
Side, the fixed link (5) is horizontally disposed, and the fixed link (5) is equipped with detection slot, first electricity far from the side of fuselage (2)
The slot bottom of detection slot is arranged in magnet (15), and second electromagnet (17) is connected to the first electromagnet (15) by spring (16)
On, the magnetic direction of first electromagnet (15) and the second electromagnet (17) is on the contrary, second electromagnet (17) and fixation
Bar (5) is slidably connected, the third walk block (18) be located at the second electromagnet (17) far from the first electromagnet (15) side, institute
Third motor (19) driving the second screw rod (20) rotation is stated, the side of the push rod (8) is equipped with matched with the second screw rod (20)
One end of internal screw thread, second screw rod (20) penetrates push rod (8)；
The first motor (6), the second motor (21), third motor (19) and rotor mechanism (1) are electrically connected with PLC.
2. the unmanned plane in operation process convenient for stopping as described in claim 1, which is characterized in that described first walks block
(9) intermediate to be additionally provided with air pump (10) and gas-guide tube (11), one end of the air pump (10) passes through gas-guide tube (11) and the first sucker
(12) inside connection, the other end of the air pump (10) are connected to outside, and the air pump (10) is electrically connected with PLC.
3. the unmanned plane in operation process convenient for stopping as described in claim 1, which is characterized in that second walks block (24)
On be additionally provided with gag lever post (23), one end of the gag lever post (23) is fixed on second and walks on block (24), the gag lever post (23)
The other end penetrate connecting rod (26), the gag lever post (23) is parallel with the first screw rod (22).
4. the unmanned plane in operation process convenient for stopping as described in claim 1, which is characterized in that the push rod (8) is remote
Side from the second screw rod (20) is equipped with anticollison block.
5. the unmanned plane in operation process convenient for stopping as described in claim 1, which is characterized in that first sucker
(12) and the making material of the second sucker (25) is nitrile rubber.
6. the unmanned plane in operation process convenient for stopping as described in claim 1, which is characterized in that the first motor
(6), the second motor (21) and third motor (19) are servo motor.
7. the unmanned plane in operation process convenient for stopping as described in claim 1, which is characterized in that under the fuselage (2)
Side is additionally provided with support frame (3).
8. the unmanned plane in operation process convenient for stopping as described in claim 1, which is characterized in that the Knucle-gear (7)
Machine oil is also coated between gear (14).
9. the unmanned plane in operation process convenient for stopping as described in claim 1, which is characterized in that the stop mechanism
(4) top is additionally provided with rain cover.
10. the unmanned plane in operation process convenient for stopping as described in claim 1, which is characterized in that in the fuselage (2)
Equipped with wireless communication module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710498342.4A CN107310726B (en) | 2017-06-27 | 2017-06-27 | A kind of unmanned plane in operation process convenient for stopping |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710498342.4A CN107310726B (en) | 2017-06-27 | 2017-06-27 | A kind of unmanned plane in operation process convenient for stopping |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107310726A CN107310726A (en) | 2017-11-03 |
| CN107310726B true CN107310726B (en) | 2019-11-22 |
Family
ID=60180210
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710498342.4A Active CN107310726B (en) | 2017-06-27 | 2017-06-27 | A kind of unmanned plane in operation process convenient for stopping |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107310726B (en) |
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| CN204688427U (en) * | 2015-02-14 | 2015-10-07 | 尹澍 | A kind of shooting unmanned plane with vacuum cup |
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| CN106419772A (en) * | 2016-11-02 | 2017-02-22 | 深圳职业技术学院 | Unmanned aerial vehicle device for cleaning high-altitude glass |
| CN106510565A (en) * | 2016-11-08 | 2017-03-22 | 苏州大学 | Air automatic scrubbing device, cleaning group, and suitable wall surface |
| CN106882377A (en) * | 2017-03-29 | 2017-06-23 | 深圳市雷凌广通技术研发有限公司 | A kind of unmanned plane for glass cleaning |
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2017
- 2017-06-27 CN CN201710498342.4A patent/CN107310726B/en active Active
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0524584A (en) * | 1991-07-22 | 1993-02-02 | Mitsubishi Heavy Ind Ltd | Working airship |
| WO2013068575A2 (en) * | 2011-11-10 | 2013-05-16 | Michael Bieder | Cleaning machine for windows, façade elements, solar modules, and smooth-surfaced surface elements of that kind |
| CN103192987A (en) * | 2013-04-07 | 2013-07-10 | 南京理工大学 | Amphibious robot capable of flying and climbing wall and control method of amphibious robot |
| CN204688427U (en) * | 2015-02-14 | 2015-10-07 | 尹澍 | A kind of shooting unmanned plane with vacuum cup |
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| CN205931240U (en) * | 2016-06-21 | 2017-02-08 | 深圳市博飞航空科技有限公司 | Unmanned vehicles's curtain adsorption equipment |
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Also Published As
| Publication number | Publication date |
|---|---|
| CN107310726A (en) | 2017-11-03 |
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