CN110406689A - Airplane parking area and UAV Landing system - Google Patents
Airplane parking area and UAV Landing system Download PDFInfo
- Publication number
- CN110406689A CN110406689A CN201810391255.3A CN201810391255A CN110406689A CN 110406689 A CN110406689 A CN 110406689A CN 201810391255 A CN201810391255 A CN 201810391255A CN 110406689 A CN110406689 A CN 110406689A
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- landing platform
- parking area
- airplane parking
- unmanned plane
- impeller
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- 230000007246 mechanism Effects 0.000 claims abstract description 34
- 238000003032 molecular docking Methods 0.000 claims abstract description 4
- 238000010586 diagram Methods 0.000 description 8
- 239000000428 dust Substances 0.000 description 5
- 239000000686 essence Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000000007 visual effect Effects 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000008450 motivation Effects 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
-
- 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
- B64F1/12—Ground or aircraft-carrier-deck installations for anchoring aircraft
- B64F1/125—Mooring or ground handling devices for helicopters
-
- 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
- B64F1/22—Ground or aircraft-carrier-deck installations for handling aircraft
-
- E—FIXED CONSTRUCTIONS
- E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
- E01F—ADDITIONAL WORK, SUCH AS EQUIPPING ROADS OR THE CONSTRUCTION OF PLATFORMS, HELICOPTER LANDING STAGES, SIGNS, SNOW FENCES, OR THE LIKE
- E01F3/00—Landing stages for helicopters, e.g. located above buildings
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Toys (AREA)
Abstract
The application provides a kind of airplane parking area and UAV Landing system, can the unmanned plane to landing in airplane parking area be accurately positioned.The airplane parking area includes: landing platform, equipped with the positioning area for positioning unmanned plane；And pushing mechanism, it is set to the landing platform, for the unmanned plane for docking at the landing platform to be pushed to the positioning area, the pushing mechanism includes the driving assembly that impeller and driving impeller move on the landing platform.
Description
Technical field
This application involves air vehicle technique fields, more particularly to airplane parking area and UAV Landing system applied to unmanned plane
System.
Background technique
In recent years, unmanned plane has been widely used for civilian, industrial and military field.Unmanned plane can be used for taking photo by plane, disappear
Anti-, mapping, detection, express delivery launch, takes out and launches etc., without being limited thereto.However, unmanned plane is in landing mission, existing shutdown
Level ground is difficult to unmanned plane precise positioning, that is to say, that existing airplane parking area can not be such that the unmanned plane of landing is accurately positioned to one
In specified region.So, it has not been convenient to which manipulator or other grasping mechanisms accurately grab or place the article on unmanned plane.
Summary of the invention
The application's is designed to provide a kind of airplane parking area and UAV Landing system, can be to landing in the nothing of airplane parking area
It is man-machine to be accurately positioned.
The one aspect of the application provides a kind of airplane parking area.The airplane parking area includes: landing platform, equipped with for positioning unmanned plane
Positioning area；And pushing mechanism, it is set to the landing platform, it is described for the unmanned plane for docking at the landing platform to be pushed to
Positioning area, the pushing mechanism include the driving assembly that impeller and driving impeller move on the landing platform.
Optionally, the driving component includes that screw rod, the motor for driving the screw rod rotation and the screw rod cooperate
Sliding part, the impeller is fixed on the sliding part.
Optionally, the landing platform is equipped with the sliding slot through its upper surface and the lower surface, and the driving component is fixed on institute
The lower surface of landing platform is stated, the impeller passes through the upper surface that the sliding slot protrudes from the landing platform.
Optionally, the impeller includes protruding from the ontology of landing platform upper surface and being set to below the ontology
Interconnecting piece, the interconnecting piece can be slidingly arranged in the sliding slot.
Optionally, the sliding slot extends along the direction of the longitudinally perpendicular to the ontology.
Optionally, the landing platform is square, and the landing platform includes the positionable wall set at least side, the positioning area
It is adjacent with the positionable wall.
Optionally, the landing platform includes the side wall set on the positionable wall of side and set on other three side.
Optionally, the pushing mechanism includes being set to the landing platform with respect to two the first promotion machines at two side walls
One the second pushing mechanism of structure and another side-walls.
Further aspect of the application provides a kind of UAV Landing system.The UAV Landing system include unmanned plane and
Above-mentioned airplane parking area.
Unmanned plane is pushed and is positioned exactly on the positioning area of landing platform by pushing mechanism by the application, can facilitate machine
Tool hand or other grasping mechanisms accurately grab article on unmanned plane, or accurately article is placed on unmanned plane.
Detailed description of the invention
Fig. 1 show the schematic diagram of one embodiment of the application airplane parking area；
Fig. 2 show the schematic diagram at another visual angle in airplane parking area shown in FIG. 1；
Fig. 3 show the stereogram exploded view of airplane parking area shown in FIG. 1；
Fig. 4 show the stereogram exploded view of the pushing mechanism of airplane parking area shown in FIG. 1；
The unmanned plane that Fig. 5 show the application UAV Landing system lands in the schematic diagram of airplane parking area state；
The unmanned plane that Fig. 6 show UAV Landing system shown in Fig. 5 is positioned at the schematic diagram of airplane parking area state.
Specific embodiment
Example embodiments are described in detail here, and the example is illustrated in the accompanying drawings.Following description is related to
When attached drawing, unless otherwise indicated, the same numbers in different drawings indicate the same or similar elements.Following exemplary embodiment
Described in embodiment do not represent all embodiments consistent with the application.On the contrary, they be only with it is such as appended
The example of the consistent device of some aspects be described in detail in claims, the application.
It is only to be not intended to be limiting the application merely for for the purpose of describing particular embodiments in term used in this application.
Unless otherwise defined, technical term or scientific term used in this application, which are should be in fields of the present invention, has general skill
The ordinary meaning that the personage of energy is understood." first " " second " and class used in present specification and claims
As word be not offered as any sequence, quantity or importance, and be used only to distinguish different component parts.Equally, " one
It is a " or the similar word such as " one " do not indicate that quantity limits yet, but indicate that there are at least one." multiple " or " several " table
Show two and two or more.Unless otherwise noted, the similar word such as " front ", " rear portion ", " lower part " and/or " top " is only
Convenient for explanation, and it is not limited to a position or a kind of spatial orientation.The similar word such as " comprising " or "comprising" means
It appears in element or object before " comprising " or "comprising" and covers and appear in " comprising " or "comprising" presented hereinafter
Element or object and its equivalent, it is not excluded that other elements or object.The similar word such as " connection " or " connected " is simultaneously
Non-limiting and may include electrical connection in physics or mechanical connection, either direct or indirectly.In
Present specification and the "an" of singular used in the attached claims, " described " and "the" be also intended to including
Most forms, unless the context clearly indicates other meaning.It is also understood that term "and/or" used herein refers to
It and include that one or more associated any or all of project listed may combine.
Fig. 1 show the stereoscopic schematic diagram of one embodiment of airplane parking area 100.Fig. 2 show another visual angle in airplane parking area
Stereoscopic schematic diagram.Fig. 3 show the stereogram exploded view of airplane parking area shown in FIG. 1.Fig. 4 show pushing away for airplane parking area shown in FIG. 1
The stereogram exploded view of motivation structure.
Airplane parking area 100 includes landing platform 10 and pushing mechanism 20 referring to FIG. 1 to FIG. 4,.Landing platform 10 is for parking and determining
Position unmanned plane 500.Landing platform 10 is equipped with the positioning area 11 for positioning unmanned plane 500.Pushing mechanism 20 is set to the landing
Platform 10, for the unmanned plane 500 for docking at the landing platform 10 to be pushed to the positioning area 11, the pushing mechanism 20 includes
The driving assembly 22 that impeller 21 and driving impeller 21 move on the landing platform 10.It will in this way, passing through pushing mechanism 20
Unmanned plane 500 pushes and is positioned exactly on the positioning area 11 of landing platform 10, can facilitate manipulator or other grasping mechanisms essence
Quasi- ground grabs article on unmanned plane 500, or accurately article is placed on unmanned plane 500.
In the illustrated embodiment, driving assembly 22 includes screw rod (not shown), the motor for driving the screw rod rotation
222, the sliding part 223 cooperated with the screw rod, the impeller 21 are fixed on the sliding part 223.The output end of motor 222
It is connect with screw rod one end, to drive screw rod to rotate.Screw rod is equipped with screw thread, and sliding part 223 is with screw rod by being threadedly engaged.When nobody
Machine 500 lands after landing platform 10, starts motor 222, driving screw rod rotation, sliding part 223 is therewith along the length side of screw rod
To movement, correspondingly, impeller 21 moves under the drive of sliding part 223, so that unmanned plane 500 is pushed to positioning area 11.
Due to using high-precision screw rod and sliding part 223, the positioning that unmanned plane 500 is accurately located to landing platform 10 can be realized
In area 11, and the precision that unmanned plane 500 can be made to position reaches the rank of millimeter, so that manipulator be greatly improved or grab automatically
Take the accuracy of the article on mechanism crawl unmanned plane 500.Meanwhile impeller 21 is adjusted by the revolving speed of adjusting motor 222
The efficiency for being pushed to positioning area 11 after unmanned plane 500 lands by pushing mechanism 20 can be improved in the speed of movement.
In another embodiment, driving assembly 22 be rack and pinion assembly, the rack and pinion assembly include: gear member,
Motor and transmission connection for driving gear member to rotate is in the rack member of the gear member, the rack member and impeller 21
It is fixedly connected, the rotation of gear member described in the motor driven, the rack member is under the driving of the gear member relative to landing
Platform 10 moves back and forth, and then impeller 21 is driven to move back and forth.
In another embodiment, driving assembly 22 is cylinder assembly, and the cylinder assembly includes: actuator and is connected to institute
The cylinder-driven part of impeller 21 is stated, the actuator drives the cylinder-driven part to drive the impeller 21 is relatively described to rise
Drop platform 10 moves back and forth.Above-mentioned is only some examples, however it is not limited to above-mentioned example.
In the illustrated embodiment, landing platform 10 is equipped with the sliding slot 14 through its upper surface 12 and lower surface 13.The driving
Component 22 is fixed on the lower surface 13 of the landing platform 10, and the impeller 21 passes through the sliding slot 14 and protrudes from the landing platform
10 upper surface 12.When the landing of unmanned plane 500 is behind landing platform 10, the driving component 22 drives institute along the sliding slot 14
Impeller 21 is stated, unmanned plane 500 is pushed to the positioning area 11.In another embodiment, the lower surface 13 of landing platform 10 is set
There is the groove of receiving driving assembly 22, driving assembly 22 is fixed in groove.Above-mentioned is only some examples, however it is not limited to above-mentioned
Example.
In the illustrated embodiment, driving assembly 22 further includes the dust cover 224 enclosed set on screw rod, dust cover 224 and screw rod
The fulcrum bearing at both ends is connected and fixed.The setting of dust cover 224 can be fallen on screw rod to avoid dust, so as to guarantee driving group
The precision of part 22.
In the illustrated embodiment, driving assembly 22 further comprises connector 225.Driving assembly 22 passes through connector 225
It is fixed on landing platform 10.Specifically, in the illustrated embodiment, driving assembly 22 includes 4 connectors 225, is respectively arranged at drive
The two sides of dynamic component 22.Each connector 225 includes the first connecting portion 2251 connecting with driving assembly 22 and connects with landing platform 10
The second connecting portion 2252 connect.In the present embodiment, first connecting portion 2251 and second connecting portion 2252 pass through fastener respectively
It is fixedly connected with the dust cover 224 of driving assembly 22 and landing platform 10, but not limited to this.
Impeller 21 includes protruding from the ontology 211 of 10 upper surface 12 of landing platform and being set under the ontology 211
The interconnecting piece 212 of side, the interconnecting piece 212 can be slidingly arranged in the sliding slot 14.Interconnecting piece 212 can be with ontology
211 are integrally formed, and can also be connected by modes such as welding, without being limited thereto.In one embodiment, ontology 211 and landing platform
It can have certain interval between 10 upper surface 12, to avoid frictional force is generated between ontology and landing platform.At another
In embodiment, can also not have gap, i.e. ontology 211 and landing platform 10 between the upper surface 12 of ontology 211 and landing platform 10
Upper surface 12 contact.Similarly, gap can be set between interconnecting piece 212 and the inner wall of sliding slot 14, gap can not also be set.
In the illustrated embodiment, ontology 211 is in longitudinal, and the longitudinally of ontology 211 side corresponding with positioning area 11
Side is parallel, and sliding slot 14 extends along the direction of the longitudinally perpendicular to ontology 211, in this way, impeller 21 moves same distance,
The distance that sliding part 223 needs to move is most short, is conducive to improve the efficiency for push to unmanned plane 500 positioning.In another reality
It applies in example, the angle between sliding slot 14 and ontology 211 is oblique angle, without being limited thereto.
In the illustrated embodiment, impeller 21 further comprises the mounting base 213 for fixing with the sliding part 223,
The mounting base 213 is fixed on the interconnecting piece 212.In the illustrated embodiment, the lower surface 13 of mounting base 213 and landing platform 10
Between be equipped with gap, generate frictional force to avoid between mounting base 213 and landing platform 10.In another embodiment, mounting base 213
It can be contacted with the lower surface 13 of landing platform 10.Mounting base 213 can be fixed on sliding part 223 by fastener, certainly may be used
It is without being limited thereto to be fixed on sliding part 223 by other means.In yet another embodiment, the interconnecting piece 212 of impeller 21 is straight
It connects and is fixed on sliding part 223.
In the illustrated embodiment, landing platform 10 is square.Landing platform 10 includes set on the positionable wall 15 of side and set on another
The side wall 16 of outer three side, positionable wall 15 are higher than side wall 16.Positioning area 11 and positionable wall 15 are adjacent.When unmanned plane 500 landing in
After landing platform 10, unmanned plane 500 is pushed to positioning area 11 by pushing mechanism 20, and impeller 21 and positionable wall 15 are jointly by nobody
Machine 500 is defined in the positioning area 11.
Specifically, pushing mechanism 20 includes two the first promotion machines being set at the opposite two side walls of the landing platform 10
One the second pushing mechanism 26 of structure 25 and another side-walls, two the first pushing mechanisms 25 are symmetrical arranged.Correspondingly, it is arranged
It include cooperating with the first sliding groove 141 of the first pushing mechanism 25 cooperation and with the second pushing mechanism 26 in the sliding slot 14 of landing platform 10
Second sliding slot 142.In the illustrated embodiment, the middle position of two first sliding grooves 141 from corresponding side wall 16 is opposite extends, and
Projection of two first sliding grooves 141 on positionable wall 15 is connected or at least partly Chong Die with positioning area 11 with positioning area 11, so
Ensure that unmanned plane 500 can be pushed to positioning area 11 by the first impeller 251 and the cooperation of the second impeller 261, avoids first
Impeller 251 pushes situation not in place.Second sliding slot 142 extends to positioning area 11 from corresponding side wall 16.Second impeller 261
It is corresponding with the position of the positioning area 11, and the length of second impeller 261 is not more than the length of the positioning area 11,
In this way, can be sent out during carrying out promotion positioning to unmanned plane 500 to avoid the second impeller 261 and the first impeller 251
Raw interference.In the illustrated embodiment, positioning area 11 is located at the middle position of positionable wall 15, but not limited to this.
When the landing of unmanned plane 500 is before landing platform 10, the first impeller 251 is located at corresponding side wall with the second impeller 261
At 16.When the landing of unmanned plane 500 is after landing platform 10, the first impeller 251 is driven with the second impeller 261 towards far from corresponding
The direction of side wall 16 moves.
In another embodiment, landing platform 10 is not provided with positionable wall 15, and positioning area 11 is set in landing platform 10
4 pushing mechanisms 20 are arranged on landing platform 10, are located at four sides of landing platform 10 for portion position.When unmanned plane 500 landing in
After landing platform 10, unmanned plane 500 is pushed jointly and is defined in positioning area 11 by 4 pushing mechanisms 20.In this way, landing platform 10 is not required to
Positionable wall 15 is set, the volume and weight of landing platform 10, convenient transportation and storage can be reduced, while simplifying landing platform 10
Structure reduces manufacturing cost.
In yet another embodiment, two positionable walls 15 being vertically connected are arranged in the adjacent two sides of landing platform 10, will position
Area 11 is set to the junction of two positionable walls 15, and 2 pushing mechanisms 20 are arranged in the other two sides of landing platform 10.Work as unmanned plane
After landing platform 10, unmanned plane 500 is pushed to positioning area 11, and 2 impellers 21 jointly by 2 pushing mechanisms 20 for 500 landing
Unmanned plane 500 is defined in the positioning area 11 jointly with 2 positionable walls 15.So, it is only necessary to two pushing mechanisms 20 are set,
Structure is simple, at low cost.
The unmanned plane that Fig. 5 show the application UAV Landing system 600 lands in the schematic diagram of airplane parking area state.Fig. 6
The unmanned plane for showing UAV Landing system shown in Fig. 5 600 is positioned at the schematic diagram of airplane parking area state.
Fig. 5 and Fig. 6 is please referred to, the embodiment of the present invention also provides a kind of UAV Landing system 600, the UAV Landing system
System 600 includes: unmanned plane 500 and such as above-mentioned airplane parking area 100 as described in the examples.The unmanned plane 500 include fuselage 510,
Be connected to the wing 520 of fuselage 510 and be set to the propeller component 530 of wing 520, the bottom size of the fuselage 510 with
11 size of positioning area matches.When unmanned plane 500 lands in airplane parking area 100, pushing mechanism 20 pushes unmanned plane 500
Fuselage 510 is pushed to positioning area 11 by fuselage 510, to realize the precise positioning to unmanned plane 500.
The foregoing is merely the preferred embodiments of the application, not to limit the application, all essences in the application
Within mind and principle, any modification, equivalent substitution, improvement and etc. done be should be included within the scope of the application protection.
Claims (9)
1. a kind of airplane parking area, it is characterised in that: comprising:
Landing platform, equipped with the positioning area for positioning unmanned plane；And
Pushing mechanism is set to the landing platform, for the unmanned plane for docking at the landing platform to be pushed to the positioning area,
The pushing mechanism includes the driving assembly that impeller and driving impeller move on the landing platform.
2. airplane parking area as described in claim 1, it is characterised in that: the driving component includes screw rod, for driving the silk
The motor of bar rotation, the sliding part with screw rod cooperation, the impeller are fixed on the sliding part.
3. airplane parking area as claimed in claim 1 or 2, it is characterised in that: the landing platform, which is equipped with, runs through its upper surface and following table
The sliding slot in face, the driving component are fixed on the lower surface of the landing platform, and the impeller passes through the sliding slot and protrudes from institute
State the upper surface of landing platform.
4. airplane parking area as claimed in claim 3, it is characterised in that: the impeller includes protruding from landing platform upper surface
Ontology and the interconnecting piece that is set to below the ontology, the interconnecting piece can be slidingly arranged in the sliding slot.
5. airplane parking area as claimed in claim 4, it is characterised in that: the sliding slot is along the longitudinally perpendicular to the ontology
Direction extends.
6. airplane parking area as described in claim 1, it is characterised in that: the landing platform is square, and the landing platform includes being set to
At least positionable wall of side, the positioning area and the positionable wall are adjacent.
7. airplane parking area as claimed in claim 6, it is characterised in that: the landing platform includes being set to the positionable wall of side and being set to
The side wall of other three side.
8. airplane parking area as claimed in claim 7, it is characterised in that: the pushing mechanism is opposite including being set to the landing platform
One the second pushing mechanism of two the first pushing mechanisms at two side walls and another side-walls.
9. a kind of UAV Landing system, comprising:
Unmanned plane；And
Airplane parking area as claimed in any one of claims 1 to 8.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810391255.3A CN110406689A (en) | 2018-04-27 | 2018-04-27 | Airplane parking area and UAV Landing system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810391255.3A CN110406689A (en) | 2018-04-27 | 2018-04-27 | Airplane parking area and UAV Landing system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110406689A true CN110406689A (en) | 2019-11-05 |
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ID=68345843
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810391255.3A Pending CN110406689A (en) | 2018-04-27 | 2018-04-27 | Airplane parking area and UAV Landing system |
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| CN113879695A (en) * | 2021-10-21 | 2022-01-04 | 河北汉光重工有限责任公司 | Adjustable stopping device |
| WO2023272526A1 (en) * | 2021-06-29 | 2023-01-05 | 深圳市大疆创新科技有限公司 | Charging base station, flight vehicle, and flight vehicle system |
| WO2023015233A1 (en) * | 2021-08-06 | 2023-02-09 | Alarm.Com Incorporated | Landing pad for aerial vehicles |
| CN115743664A (en) * | 2022-11-24 | 2023-03-07 | 中科蓝光科技(广州)有限公司 | Portable unmanned aerial vehicle air park |
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