CN107161352A - A kind of rotor flying robot landing platform of float type four - Google Patents
A kind of rotor flying robot landing platform of float type four Download PDFInfo
- Publication number
- CN107161352A CN107161352A CN201710309044.6A CN201710309044A CN107161352A CN 107161352 A CN107161352 A CN 107161352A CN 201710309044 A CN201710309044 A CN 201710309044A CN 107161352 A CN107161352 A CN 107161352A
- Authority
- CN
- China
- Prior art keywords
- flying robot
- floating body
- landing platform
- float type
- rotor flying
- 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.)
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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 47
- 238000007667 floating Methods 0.000 claims abstract description 42
- 229920001971 elastomer Polymers 0.000 claims abstract description 30
- 239000005060 rubber Substances 0.000 claims abstract description 30
- 230000008859 change Effects 0.000 claims description 11
- 230000001681 protective effect Effects 0.000 claims description 8
- 239000011521 glass Substances 0.000 claims description 4
- 238000013016 damping Methods 0.000 abstract description 7
- 230000033001 locomotion Effects 0.000 abstract description 4
- 230000005484 gravity Effects 0.000 abstract description 3
- 230000009471 action Effects 0.000 abstract description 2
- 230000000630 rising effect Effects 0.000 abstract description 2
- 238000012544 monitoring process Methods 0.000 description 8
- 230000000694 effects Effects 0.000 description 5
- 230000007613 environmental effect Effects 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 2
- 230000001105 regulatory effect Effects 0.000 description 2
- 241000607479 Yersinia pestis Species 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 201000010099 disease Diseases 0.000 description 1
- 208000037265 diseases, disorders, signs and symptoms Diseases 0.000 description 1
- 239000003814 drug Substances 0.000 description 1
- 229940079593 drug Drugs 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 229910052500 inorganic mineral Inorganic materials 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000011707 mineral Substances 0.000 description 1
- 230000000116 mitigating effect Effects 0.000 description 1
- 238000012806 monitoring device Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000005070 sampling Methods 0.000 description 1
Classifications
-
- 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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
- B64D45/06—Landing aids; Safety measures to prevent collision with earth's surface mechanical
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Manipulator (AREA)
Abstract
The invention discloses a kind of rotor flying robot landing platform of float type four, including water tank, the inwall of the guide cylinder is provided with non-slip rubber layer, and the upper end of friction lever is provided with non-slip rubber block, and the non-slip rubber block is in circular arc.The invention, after flying robot is sideling fallen on floating body from side, floating body starts to move downward, simultaneous with lateral movement, at this moment universal wheel can rise along the inwall of pallet, slowly slowed down under gravity, rubber bar, which is straightened, during certain position aids in floating body being withdrawn into middle part, recoil strength is not too large, if direct vertical drop, universal wheel can glide along guide cylinder, under the action of the spring, friction is produced between non-slip rubber block and non-slip rubber layer on friction lever, along with the resistance of water, so as to slowly slow down, milder, speed is then gone up after lowering in the presence of buoyancy and rubber bar, at this moment frictional force plays acting in opposition, prevent that rising is too fast, milder, damping milder.
Description
Technical field
The invention belongs to four rotor flying robots landing technical field, it is related to four rotor flying robot landing platforms,
Specifically related to a kind of rotor flying robot landing platform of float type four.
Background technology
Aircraft is to be manufactured by the mankind, can fly away from ground, controlled in endoatmosphere or big in space flight and by people
The apparatus flying object of the gas-bearing formation external space (space) flight, aircraft is divided into airborne vehicle, spacecraft, rocket, guided missile and guided weapon；
Unmanned plane is also one kind of aircraft, and unmanned plane is manipulated not using radio robot and the presetting apparatus provided for oneself
Manned aircraft, from technical standpoint definition can be divided into depopulated helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, nobody
Dirigible and unmanned parasol etc.；By application field can be divided into it is military with it is civilian, military aspect unmanned plane is divided into reconnaissance plane and target drone；
At present, unmanned plane can be widely applied to national ecological environmental protection, aeroplane photography, mapping, mineral resources exploration, the condition of a disaster monitoring,
Traffic patrolling, power-line patrolling, security monitoring, emergent mitigation, emergency command, rain making, national defense safety, land resources exploration,
Town planning, seismic survey, environmental monitoring, forest fire protection, Crop Estimation, the monitoring of protection zone wild animal, air sampling, sea
Thing scouting, border tour, prohibition of drug scouting, fire inspection, ecological environmental protection, marine environmental monitoring, land use survey, water money
It is source exploitation, crop growth monitoring and the yield by estimation, agricultural operation, Natural calamity monitoring and assessment, urban planning and municipal administration, gloomy
The field such as the protection of woods pest and disease damage and monitoring, digital city.Belong to for four rotor flying robots in unmanned multi-rotor aerocraft
One kind, the long continuation of the journey of flying robot's flight is to return to be charged after a problem, therefore certain time, is entered simultaneously
Row maintenance conditions, in case flight next time, this is accomplished by using landing platform, and the damping of landing platform is related to flying robot
Protection because being loaded with many monitoring devices and electric elements above, impact during landing they can be caused to damage or
Person is reduction service life, and in the market also has many landing platforms with damping, is largely that still, spring is also by spring
It is too stiff, and bounce, than larger, can equally produce anti-force during resilience.
The content of the invention
According to above the deficiencies in the prior art, the technical problems to be solved by the invention are to propose a kind of rotor of float type four
Flying robot's landing platform, by frictional connection between floating body and guide rod and guide cylinder, solves damping effect bad
The problem of, the characteristics of with good damping effect.
In order to solve the above-mentioned technical problem, the technical solution adopted by the present invention is：A kind of rotor flying machine of float type four
Provided with the opening-like pallet in upper end in the middle part of people's landing platform, including water tank, the inner chamber of the water tank, and the lower end of pallet is opened
Mouthful, the lower ending opening of the pallet, which is connected with guide cylinder straight down, the water tank, is provided with floating body, and floating body is located at pallet
Surface, be provided with universal wheel provided with guide rod straight down, the lower end of the guide rod in the middle part of the lower end of the floating body, and
The diameter of guide rod and universal wheel is respectively less than the internal diameter of guide cylinder, and it is upward that the lower end of the guide rod is circumferentially hingedly connected with outer end
Thread barrel is threaded with the friction lever of tilting, the guide rod, and the lower end of thread barrel is rotatably connected to change, described turn
Ring set connects on the guide bar, and change is located at the upside of friction lever, is connected between the side wall of the friction lever and change by spring
Connect, connected between the outer end circumference of the floating body and the inwall of water tank by rubber bar, the inwall of the guide cylinder is provided with anti-
Sliding rubber layer, and the upper end of friction lever is provided with non-slip rubber block, the non-slip rubber block is in circular arc.
In said apparatus, the lower end of the floating body is in the arc-shaped, and provided with pendant block in the middle part of the lower end of floating body.
In said apparatus, the lower end side of the water tank is provided with water valve.
In said apparatus, connected between the circumferential upper end of the floating body and the upper end circumference of water tank by the anti-drop net of annular
Connect.
In said apparatus, the upper end of the floating body is circumferentially with protective plate, and the inner side of protective plate is provided with elastic insert.
In said apparatus, clear glass is connected with the side wall of the water tank.
In said apparatus, water inlet is offered on the side wall of the floating body, and water inlet is threaded with spin-block, it is described
The outer end of spin-block is provided with moving block.
In said apparatus, the lower end of the water tank is provided with slipmat.
Present invention has the advantages that:The invention, after flying robot is sideling fallen on floating body from side, floating body start to
Lower motion, simultaneous with lateral movement, at this moment universal wheel can rise along the inwall of pallet, carry out under gravity slow
Slow down, rubber bar, which is straightened, during certain position aids in floating body being withdrawn into middle part, and recoil strength is not too large, if directly vertical drop
Fall, universal wheel can glide along guide cylinder, under the action of the spring, between the non-slip rubber block and non-slip rubber layer on friction lever
Produce friction, along with the resistance of water, so as to slowly slow down, milder, speed lower after then in buoyancy and rubber bar
In the presence of go up, at this moment frictional force rise acting in opposition, prevent rise too fast, milder, damping milder, effect more preferably, very
Good protects flying robot, by water inlet water filling, just can adjust the falling speed of floating body, rotates thread barrel, just may be used
To adjust the extruding dynamics of spring, regulating friction force, so as to adjust gliding speed.
Brief description of the drawings
The mark in the content and figure expressed by this specification accompanying drawing is briefly described below：
Fig. 1 is the structural representation of the embodiment of the present invention.
Fig. 2 is the front view of the embodiment of the present invention.
In figure：1 water tank, 2 pallets, 3 guide cylinders, 4 floating bodies, 5 guide rods, 6 universal wheels, 7 friction levers, 8 thread barrels, 9 changes,
10 springs, 11 rubber bars, 12 non-slip rubbers layer, 13 non-slip rubber blocks, 14 pendant blocks, 15 water valves, 16 anti-drop nets, 17 protective plates, 18
Clear glass, 19 spin-blocks, 20 non-slipping blocks.
Embodiment
Below against accompanying drawing, by the description to embodiment, embodiment of the invention such as involved each component
Shape, construction, the mutual alignment between each several part and annexation, the effect of each several part and operation principle, manufacturing process and
Operate with method etc., is described in further detail, to help those skilled in the art to inventive concept of the invention, technology
Scheme has more complete, accurate and deep understanding.
A kind of rotor flying robot landing platform of float type four, including water tank 1, the lower end of water tank 1 are provided with slipmat 20,
Anti-skidding, the lower end side of water tank 1 is provided with water valve 15, is easy to be connected with clear glass 18 on draining, the side wall of water tank 1, is easy to see
Examine and the opening-like pallet 2 in upper end is provided with the middle part of the inner case of water tank 1, the inner chamber of water tank 1, and the lower ending opening of pallet 2, support
The lower ending opening of disk 2, which is connected with guide cylinder 3 straight down, water tank 1, is provided with floating body 4, and floating body 4 is hollow structure inside, from
And with buoyancy, and floating body 4 is located at the surface of pallet 2, the lower end of floating body 4 is in the arc-shaped, and is provided with the middle part of the lower end of floating body 4
Block 14 is fallen, is so easy to the balance of floating body 4, it is not easy to tilt, is led between the circumferential upper end of floating body 4 and the upper end circumference of water tank 1
The anti-drop net 16 for crossing annular is connected, and prevents flying robot from falling into water tank 1.
The upper end of floating body 4 is circumferentially with protective plate 17, and the inner side of protective plate 17 is provided with elastic insert, and protective action is floated
Water inlet is offered on the side wall of body 4, and water inlet is threaded with spin-block 19, the outer end of spin-block 19 is provided with moving block, can
To intake, so as to adjust the water inlet buffer speed of floating body 4, provided with guide rod 5 straight down in the middle part of the lower end of floating body 4, it is oriented to
The lower end of bar 5 is provided with universal wheel 6, and the diameter of guide rod 5 and universal wheel 6 is respectively less than under the internal diameter of guide cylinder 3, guide rod 5
Circumferential be hingedly connected with the friction lever 7 that outer end is upturned, guide rod 5 in end is threaded with thread barrel 8, and thread barrel 8
Lower end is rotatably connected to change 9, and change 9 is socketed on guide rod 5, and change 9 is located at the upside of friction lever 7, the side of friction lever 7
Connected, connected between the outer end circumference of floating body 4 and the inwall of water tank 1 by rubber bar 11 by spring 10 between wall and change 9,
The inwall of guide cylinder 3 is provided with non-slip rubber layer 12, and the upper end of friction lever 7 is provided with non-slip rubber block 13, non-slip rubber block 13
In circular arc.
The invention, after flying robot is sideling fallen on floating body 4 from side, floating body 4 starts to move downward, simultaneous with
Lateral movement, inwall of the at this moment meeting of universal wheel 6 along pallet 2 rises, and is slowly slowed down under gravity, certain position
When the auxiliary that is straightened of rubber bar 11 floating body 4 is withdrawn into middle part, recoil strength is not too large, if directly vertical drop, universal wheel 6
It can be glided along guide cylinder 3, in the presence of spring 10, between the non-slip rubber block 13 and non-slip rubber layer 12 on friction lever 7
Produce friction, along with the resistance of water, so as to slowly slow down, milder, speed lower after then in buoyancy and rubber bar
Go up in the presence of 11, at this moment frictional force plays acting in opposition, prevent from rising too fast, milder, damping milder, effect is more preferable,
Flying robot is protected well, by water inlet water filling, the falling speed of floating body 4 just can be adjusted, rotate thread barrel 8,
Just the extruding dynamics of spring 10, regulating friction force, so as to adjust gliding speed can be adjusted.
The present invention is exemplarily described above in conjunction with accompanying drawing, it is clear that the present invention is implemented not by aforesaid way
Limitation, as long as the improvement of the various unsubstantialities of inventive concept and technical scheme of the present invention progress is employed, or without changing
Enter and the design of the present invention and technical scheme are directly applied into other occasions, within protection scope of the present invention.This hair
Bright protection domain should be determined by the scope of protection defined in the claims.
Claims (8)
1. a kind of rotor flying robot landing platform of float type four, including water tank (1), it is characterised in that the water tank (1)
Provided with the pallet (2) that upper end is opening-like in the middle part of inner chamber, and the lower ending opening of pallet (2), the lower ending opening company of the pallet (2)
Be connected to guide cylinder (3) straight down, be provided with floating body (4) in the water tank (1), and floating body (4) be located at pallet (2) just on
Provided with guide rod (5) straight down in the middle part of side, the lower end of the floating body (4), the lower end of the guide rod (5) is provided with universal wheel
(6), and the diameter of guide rod (5) and universal wheel (6) is respectively less than the internal diameters of guide cylinder (3), the lower end of the guide rod (5) is circumferential
It is hingedly connected with the friction lever (7) that outer end is upturned, the guide rod (5) and is threaded with thread barrel (8), and thread barrel
(8) lower end is rotatably connected to change (9), and the change (9) is socketed on guide rod (5), and change (9) is located at friction lever
(7) upside, is connected, the outer end of the floating body (4) between the side wall of the friction lever (7) and change (9) by spring (10)
Circumferentially with being connected between the inwall of water tank (1) by rubber bar (11), the inwall of the guide cylinder (3) is provided with non-slip rubber layer
(12), and friction lever (7) upper end be provided with non-slip rubber block (13), the non-slip rubber block (13) be in circular arc.
2. the rotor flying robot landing platform of a kind of float type four according to claim 1, it is characterised in that described floating
The lower end of body (4) is in the arc-shaped, and provided with pendant block (14) in the middle part of the lower end of floating body (4).
3. a kind of rotor flying robot landing platform of float type four according to claim 1, it is characterised in that the water
The lower end side of case (1) is provided with water valve (15).
4. the rotor flying robot landing platform of a kind of float type four according to claim 1, it is characterised in that described floating
It is connected between the circumferential upper end of body (4) and the upper end circumference of water tank (1) by the anti-drop net (16) of annular.
5. the rotor flying robot landing platform of a kind of float type four according to claim 1, it is characterised in that described floating
The upper end of body (4) is circumferentially with protective plate (17), and the inner side of protective plate (17) is provided with elastic insert.
6. a kind of rotor flying robot landing platform of float type four according to claim 1, it is characterised in that the water
Clear glass (18) is connected with the side wall of case (1).
7. the rotor flying robot landing platform of a kind of float type four according to claim 1, it is characterised in that described floating
Water inlet is offered on the side wall of body (4), and water inlet is threaded with spin-block (19), the outer end of the spin-block (19) is provided with
Moving block.
8. a kind of rotor flying robot landing platform of float type four according to claim 1, it is characterised in that the water
The lower end of case (1) is provided with slipmat (20).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710309044.6A CN107161352B (en) | 2017-05-04 | 2017-05-04 | Floating body type four-rotor flying robot landing platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710309044.6A CN107161352B (en) | 2017-05-04 | 2017-05-04 | Floating body type four-rotor flying robot landing platform |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107161352A true CN107161352A (en) | 2017-09-15 |
| CN107161352B CN107161352B (en) | 2023-08-18 |
Family
ID=59813111
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710309044.6A Active CN107161352B (en) | 2017-05-04 | 2017-05-04 | Floating body type four-rotor flying robot landing platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107161352B (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108363409A (en) * | 2018-02-01 | 2018-08-03 | 沈阳无距科技有限公司 | Unmanned plane inspection control method, apparatus and system |
| CN111516895A (en) * | 2020-04-29 | 2020-08-11 | 北京华力创通科技股份有限公司 | Accurate take-off and landing equipment for mooring unmanned aerial vehicle |
| CN113651238A (en) * | 2021-07-15 | 2021-11-16 | 巨力索具研究院(天津)有限公司 | Guiding, positioning and buffering device for integral hoisting of offshore wind turbine generator system |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1511741A (en) * | 1966-01-31 | 1968-02-02 | British Aircraft Corp Ltd | Advanced installation of fuel tanks, for airplanes |
| US20070221790A1 (en) * | 2006-03-27 | 2007-09-27 | Honeywell International Inc. | Ducted Fan Air Data System |
| US20100181431A1 (en) * | 2009-01-16 | 2010-07-22 | Masatsugu Ishiba | Flight assistance apparatus |
| CN103043220A (en) * | 2011-10-13 | 2013-04-17 | 王力丰 | Taking-off and landing system of shipboard aircraft of aircraft carrier and taking-off and landing method thereof |
| CN206719566U (en) * | 2017-05-04 | 2017-12-08 | 安徽工程大学 | A kind of rotor flying robot landing platform of float type four |
-
2017
- 2017-05-04 CN CN201710309044.6A patent/CN107161352B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1511741A (en) * | 1966-01-31 | 1968-02-02 | British Aircraft Corp Ltd | Advanced installation of fuel tanks, for airplanes |
| US20070221790A1 (en) * | 2006-03-27 | 2007-09-27 | Honeywell International Inc. | Ducted Fan Air Data System |
| US20100181431A1 (en) * | 2009-01-16 | 2010-07-22 | Masatsugu Ishiba | Flight assistance apparatus |
| CN103043220A (en) * | 2011-10-13 | 2013-04-17 | 王力丰 | Taking-off and landing system of shipboard aircraft of aircraft carrier and taking-off and landing method thereof |
| CN206719566U (en) * | 2017-05-04 | 2017-12-08 | 安徽工程大学 | A kind of rotor flying robot landing platform of float type four |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108363409A (en) * | 2018-02-01 | 2018-08-03 | 沈阳无距科技有限公司 | Unmanned plane inspection control method, apparatus and system |
| CN111516895A (en) * | 2020-04-29 | 2020-08-11 | 北京华力创通科技股份有限公司 | Accurate take-off and landing equipment for mooring unmanned aerial vehicle |
| CN111516895B (en) * | 2020-04-29 | 2022-02-25 | 北京华力创通科技股份有限公司 | Accurate take-off and landing equipment for mooring unmanned aerial vehicle |
| CN113651238A (en) * | 2021-07-15 | 2021-11-16 | 巨力索具研究院(天津)有限公司 | Guiding, positioning and buffering device for integral hoisting of offshore wind turbine generator system |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107161352B (en) | 2023-08-18 |
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