CN111498134A - Self-adaptive unmanned aerial vehicle take-off and landing platform - Google Patents
Self-adaptive unmanned aerial vehicle take-off and landing platform Download PDFInfo
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- CN111498134A CN111498134A CN202010354199.3A CN202010354199A CN111498134A CN 111498134 A CN111498134 A CN 111498134A CN 202010354199 A CN202010354199 A CN 202010354199A CN 111498134 A CN111498134 A CN 111498134A
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- 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
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- 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
- B64F1/007—Helicopter portable landing pads
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- 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
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Abstract
The invention provides a self-adaptive unmanned aerial vehicle take-off and landing platform, which is characterized in that: comprises a base unit including a first elongated member formed to protrude from a side surface of the base unit, the base unit having a center of gravity lower than an upper surface thereof; and a first telescopic unit provided on the base unit, the first telescopic unit being movable up and down in the first elongate member, the first telescopic unit being fixable at an arbitrary position.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle lifting, in particular to a self-adaptive unmanned aerial vehicle take-off and landing platform.
Background
In recent years, a large number of unmanned aerial vehicles are used for operation, the variety of the unmanned aerial vehicles is diversified, and operators can hardly find a flat terrain to take off when working in the field. The position and the posture of a takeoff point are automatically recorded before the unmanned aerial vehicle takes off, and the flying state of the plane flying in the air is unstable if the takeoff posture is inclined.
In the field of some special areas, the unmanned aerial vehicle safety work is hardly realized to the many bottom leveling's of going into the mountain condition, for guaranteeing that unmanned aerial vehicle can have a fine gesture of taking off when taking off and can reduce the possibility of exploding the machine (unmanned aerial vehicle drops or falls in the water, leads to totally unable flight, and this kind of condition is called the machine of exploding), so need an unmanned aerial vehicle platform that takes off and land that can adjust.
In other schemes, the unmanned aerial vehicle take-off and landing platform is great and is difficult to drag, inconvenient transportation or operating procedure are more, and the time that the operating personnel who use unmanned aerial vehicle used the machine is longer, has caused the inconvenience of operation.
Disclosure of Invention
This section is for the purpose of summarizing some aspects of embodiments of the invention and to briefly introduce some preferred embodiments. In this section, as well as in the abstract and the title of the invention of this application, simplifications or omissions may be made to avoid obscuring the purpose of the section, the abstract and the title, and such simplifications or omissions are not intended to limit the scope of the invention.
Therefore, the invention aims to overcome the defect that the unmanned aerial vehicle take-off and landing platform in the prior art is too complex to operate, and thereby provides a self-adaptive unmanned aerial vehicle take-off and landing platform.
In order to solve the technical problems, the invention provides the following technical scheme: the utility model provides an unmanned aerial vehicle platform that takes off and land of self-adaptation which characterized in that: comprises a base unit including a first elongated member formed to protrude from a side surface of the base unit, the base unit having a center of gravity lower than an upper surface thereof; and a first telescopic unit provided on the base unit, the first telescopic unit being movable up and down in the first elongate member, the first telescopic unit being fixable at an arbitrary position.
As a preferred scheme of the self-adaptive unmanned aerial vehicle take-off and landing platform, the method comprises the following steps: the vertical cross section of the base unit is semi-elliptical, a vertex M is arranged at the bottom of the base unit, and the base unit can keep the upper surface balance through the vertex M.
As a preferred scheme of the self-adaptive unmanned aerial vehicle take-off and landing platform, the method comprises the following steps: the base unit further comprises a first protruding part protruding from one side of the base unit, and the first elongated part is connected with the bottom end of the first protruding part.
As a preferred scheme of the self-adaptive unmanned aerial vehicle take-off and landing platform, the method comprises the following steps: the first extension part and the first telescopic unit are provided with a plurality of groups, and the first extension part and the first telescopic unit are uniformly connected with the first protruding part.
As a preferred scheme of the self-adaptive unmanned aerial vehicle take-off and landing platform, the method comprises the following steps: the suction unit is arranged on the base unit; the first telescopic unit further comprises a moving part and a rolling part, the moving part can move up and down in the first elongated part, the rolling part is arranged in the first elongated part, the suction unit can suck the rolling part to move upwards, and the rolling part is fixedly locked with the moving part.
As a preferred scheme of the self-adaptive unmanned aerial vehicle take-off and landing platform, the method comprises the following steps: the suction unit comprises a power component and a magnetic component, the power component is arranged in the base unit, the magnetic component is arranged on the first protruding component, and the magnetic component is uniformly distributed on the first protruding component.
As a preferred scheme of the self-adaptive unmanned aerial vehicle take-off and landing platform, the method comprises the following steps: the vertical distance X from the bottom end of the first elongate member to the first protruding member is less than the vertical distance Y from the apex M to the first protruding member.
As a preferred scheme of the self-adaptive unmanned aerial vehicle take-off and landing platform, the method comprises the following steps: the vertical distance Z of the moving member from the bottom of the first elongate member furthest to the first projecting member is greater than the distance Y.
As a preferred scheme of the self-adaptive unmanned aerial vehicle take-off and landing platform, the method comprises the following steps: the rolling part is adsorbable material, the suction unit can drive the rolling part upwards.
As a preferred scheme of the self-adaptive unmanned aerial vehicle take-off and landing platform, the method comprises the following steps: the friction force between the first protruding component and the rolling component driven by the suction unit to move can bear the pressure of the base unit and the articles borne by the base unit.
The invention has the beneficial effects that:
1. the invention provides a self-adaptive unmanned aerial vehicle take-off and landing platform, which is convenient to install, enables a base unit to quickly reach a horizontal state, is simple to operate, and can achieve the using effect without excessive operation of a user.
2. The invention provides a self-adaptive unmanned aerial vehicle take-off and landing platform, a suction unit can provide higher suction to achieve the effect of stable support, and a moving part can be fixed at a fixed position by a rolling part to prevent the stability of a base unit from being damaged by larger pressure generated by the unmanned aerial vehicle during take-off or landing.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings needed to be used in the description of the embodiments will be briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings based on these drawings without inventive exercise. Wherein:
FIG. 1 is a schematic diagram of the overall structure of a self-adaptive unmanned aerial vehicle take-off and landing platform;
FIG. 2 is a schematic diagram of an overall structure of an adaptive unmanned aerial vehicle take-off and landing platform with an unmanned aerial vehicle;
FIG. 3 is a schematic view of a cutting structure of a self-adaptive unmanned aerial vehicle take-off and landing platform;
fig. 4 is a schematic structural diagram of the adaptive unmanned aerial vehicle take-off and landing platform in a state of the first telescopic unit and the base unit;
fig. 5 is a schematic structural diagram of the adaptive unmanned aerial vehicle take-off and landing platform in another state with the first telescopic unit and the base unit being independent;
fig. 6 is a schematic structural diagram of a first telescopic unit and a first protruding part of an adaptive unmanned aerial vehicle take-off and landing platform;
Detailed Description
In order to make the aforementioned objects, features and advantages of the present invention comprehensible, embodiments accompanied with figures are described in detail below.
In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present invention, but the present invention may be practiced in other ways than those specifically described and will be readily apparent to those of ordinary skill in the art without departing from the spirit of the present invention, and therefore the present invention is not limited to the specific embodiments disclosed below.
Example 1
The embodiment provides an adaptive unmanned aerial vehicle take-off and landing platform, and referring to fig. 1-2,
including base unit 100 and first flexible unit 200, base unit 100 is the base of the platform of unmanned aerial vehicle take off and land, base unit 100 can bear unmanned aerial vehicle in order to realize unmanned aerial vehicle's take off and land, first flexible unit 200 is the extension pipeline that can freely stretch out and draw back and can fix, can stabilize self earlier through base unit 100 between base unit 100 and the first flexible unit 200, thereby first flexible unit 200 stretches out and fixes by oneself and stabilizes base unit 100.
Preferably, the base unit 100 includes a first elongated member 101, the first elongated member 101 is an elongated protrusion around the base unit 100, the first elongated member 101 is a fixed protrusion that can be connected to other components, the center of gravity of the base unit 100 is lower, the base unit 100 is lower because the bottom of the base unit 100 is higher in mass than the top of the base unit 100, and the base unit 100 can provide a surface stabilization effect after a period of motion. The first telescopic unit 200 is disposed on the base unit 100, and the first telescopic unit 200 can be fixed at any position, so that the base unit 100 can be stabilized after the base unit 100 is stabilized. Preferably, the purpose of fixing the first telescopic unit 200 by the electromagnet, inserting other parts, and the like can be selected.
In actual operation, the operator takes out self-adaptation unmanned aerial vehicle platform of taking off and land, places base unit 100 in the position that needs put unmanned aerial vehicle, and base unit 100 this moment rocks to stable state, and first telescoping unit 200 on the first extension 101 this moment contacts ground, adopts foretell method to fix first telescoping unit 200 to firm base unit 100, unmanned aerial vehicle can be put on base unit 100 and take off the landing.
Example 2
The embodiment provides an adaptive unmanned aerial vehicle take-off and landing platform, and referring to fig. 1 to 6,
the suction unit 300 is a power part capable of providing strong suction to the rolling member 202, the suction unit 300 has no suction to the rolling member 202 when not activated, and when the suction unit 300 opens the east, the rolling member 202 is attracted to the suction unit and provides a larger suction force.
Preferably, the vertical very section of the base unit 100 is a semi-ellipse, here it can also be a semicircle, etc., and the bottom vertex of the base unit 100 is a vertex M, because the base unit 100 is in the shape of a semi-football or a hemisphere, etc. because the center of gravity is low and the bottom contact placement surface is a vertex, the base unit 100 will finally form a balance on the vertex M and finally form a state of top balance of the base unit 100.
The base unit 100 further includes a first protrusion member 102, the first protrusion member 102 is formed to protrude from an outer side of the base unit 100, the first protrusion member 102 is a housing in which the first telescopic unit 200 is placed, and the first protrusion member 102 is connected to the first elongated member 101.
The first elongated members 101 and the first telescopic units 200 are provided with a plurality of sets, and the plurality of sets of the first elongated members 101 and the first telescopic units 200 are uniformly distributed on the periphery of the base unit 100 to maintain the balanced state of the base unit 100 when stationary, so that when the base unit 100 stops not shaking, the upper surface of the base unit 100 is horizontal to be suitable for smooth take-off and landing of the unmanned aerial vehicle.
The suction unit 300 is a portion provided on the base unit 100 to fix and stabilize the first telescopic unit 200 to the rolling member 202. The first telescopic unit 200 further comprises a moving part 201 and a rolling part 202, the moving part 201 is a moving block capable of moving up and down in the first protruding part 102, the rolling part 202 is arranged in the first protruding part 102 and distributed around the periphery of the first telescopic unit 200, the suction unit 300 can suck the rolling part 202 to fix the moving part 201, and the suction unit 300 can suck the rolling part 202 by suction and fix the moving part firmly.
The suction unit 300 includes a power component 301 and a magnetic component 302, the power component 301 can provide power, the magnetic component 302 can convert the power of the power component 301 into magnetic force, when the power component 301 is started, the magnetic component 302 receives the power of the power component 301 and converts the power into magnetic force, and attracts the rolling component 202 to rise, thereby fixing the rolling component.
Preferably, the inner side of the first protruding part 102 is a curved surface which shrinks upwards, that is, the rolling part 202 presses the moving part 201 when moving upwards, the moving part 201 is a moving block which is straight upwards and downwards, and the moving part 201 is fixed and limited at a fixed position when the rolling part 202 moves inside the first protruding part 102.
The vertical distance X from the bottom end of the first elongate member 101 to said first projecting member 102 is less than the vertical distance Y from the apex M to the first projecting member 102, i.e. the first elongate member 101 is not in contact with the ground when the base unit 100 and the first elongate member 101 are both upright, which gives sufficient distance for movement of the movable member 201 within the first elongate member 101.
The vertical distance Z from the longest distance that the moving member 201 extends beyond the first elongated member 101 to the first protruding member 102 is greater than the vertical distance Y from the vertex M to the first protruding member 102, i.e. the longest distance that the moving member 201 extends beyond the first protruding member 102 will be longer by the vertex M, and when the maximum distance is reached, the moving member 201 needs to be extended to the contact surface for the stability of the base unit 100.
Since the rolling member 202 needs to be attracted by the magnetic member 302, the rolling member 202 is made of a magnetically attractive metal such as iron, nickel, or cobalt, and the attraction unit 300 can attract the rolling member 202 to move upward to fix the moving member 201.
The friction between the first protruding member 102 and the rolling member 202 and between the rolling member 202 and the moving member 201 can support the pressure of the sum of the base unit 100 and the drone, so that the landing platform can support the landing of the drone.
Preferably, the inner wall of the first protruding member 102 is contacted with the rolling member 202 by increasing the friction coefficient, such as but not limited to, roughening the inner wall, using a material with high friction such as rubber, etc., the rolling member 202 is roughened, the moving member 201 is made of a material that cannot be attracted by the electromagnet, and the surface is roughened or made of a material with high friction such as rubber.
In actual operation, the operator places base unit 100 on the subaerial of unmanned aerial vehicle that needs take off and land, base unit 100's bottom top surface M contacts ground, base unit 100's first telescoping unit 200 stretches out to first bulge 102 outsidely, after base unit 100 is stable, moving part 201 is inserted subaerial, open power part 301 this moment, magnetic part 302 changes the electric energy into magnetic energy, rolling part 202 rises along first bulge 102 inner wall, and extrude moving part 201, the platform this moment can adapt to unmanned aerial vehicle take off and land, unmanned aerial vehicle can realize the function of taking off and land on the platform.
It should be noted that the above-mentioned embodiments are only for illustrating the technical solutions of the present invention and not for limiting, and although the present invention has been described in detail with reference to the preferred embodiments, it should be understood by those skilled in the art that modifications or equivalent substitutions may be made on the technical solutions of the present invention without departing from the spirit and scope of the technical solutions of the present invention, which should be covered by the claims of the present invention.
Claims (10)
1. The utility model provides an unmanned aerial vehicle platform that takes off and land of self-adaptation which characterized in that: comprises the steps of (a) preparing a mixture of a plurality of raw materials,
a base unit (100) comprising a first elongate member (101), said first elongate member (101) being formed to project laterally from said base unit (100), the centre of gravity of said base unit (100) being lower than the upper surface thereof; and
a first telescopic unit (200), wherein the first telescopic unit (200) is arranged on the base unit (100), the first telescopic unit (200) can move up and down in the first extension part (101), and the first telescopic unit (200) can be fixed at any position.
2. The adaptive unmanned aerial vehicle take-off and landing platform of claim 1, wherein: the vertical cross section of the base unit (100) is semi-elliptical, a vertex M is arranged at the bottom of the base unit (100), and the base unit (100) can keep the upper surface balance through the vertex M.
3. The adaptive unmanned aerial vehicle take-off and landing platform of claim 1 or 2, wherein: the base unit (100) further comprises a first protruding part (102), the first protruding part (102) is formed by protruding from one side of the base unit (100), and the first elongated part (101) is connected with the bottom end of the first protruding part (102).
4. The adaptive unmanned aerial vehicle take-off and landing platform of claim 3, wherein: the first elongated member (101) and the first telescopic unit (200) are provided with a plurality of sets, the first elongated member (101) and the first telescopic unit (200) being uniformly connected to the first protruding member (102).
5. The adaptive unmanned aerial vehicle take-off and landing platform of claim 1 or 4, wherein: also comprises the following steps of (1) preparing,
a suction unit (300), the suction unit (300) being disposed on the base unit (100);
the first telescopic unit (200) further comprises a moving part (201) and a rolling part (202), the moving part (201) can move up and down in the first elongated part (101), the rolling part (202) is arranged in the first elongated part (101), the suction unit (300) can suck the rolling part (202) to move upwards, and the rolling part (202) is fixedly locked on the moving part (201).
6. The adaptive unmanned aerial vehicle take-off and landing platform of claim 5, wherein: the suction unit (300) comprises a power component (301) and a magnetic component (302), wherein the power component (301) is arranged in the base unit (100), the magnetic component (302) is arranged on the first protruding component (102), and the magnetic component (302) is uniformly distributed on the first protruding component (102).
7. An adaptive unmanned aerial vehicle take-off and landing platform as defined in any of claims 4 or 6, wherein: the vertical distance X of the bottom end of the first elongate member (101) to the first protruding member (102) is less than the vertical distance Y of the apex M to the first protruding member (102).
8. The adaptive unmanned aerial vehicle take-off and landing platform of claim 7, wherein: the vertical distance Z of the moving part (201) from the bottom of the longest distance of the first elongated part (101) to the first protruding part (102) is larger than the distance Y.
9. The adaptive unmanned aerial vehicle take-off and landing platform of claim 6 or 8, wherein: the rolling component (202) is made of adsorbable materials, and the suction unit (300) can drive the rolling component (202) to move upwards.
10. The adaptive unmanned aerial vehicle take-off and landing platform of claim 6 or 8, wherein: the friction force between the first protruding part (102) and the rolling part (202) driven by the suction unit (300) can bear the pressure of the base unit (100) and the articles carried by the base unit.
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| CN202010354199.3A CN111498134B (en) | 2020-04-29 | 2020-04-29 | Self-adaptive unmanned aerial vehicle take-off and landing platform |
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| CN202010354199.3A CN111498134B (en) | 2020-04-29 | 2020-04-29 | Self-adaptive unmanned aerial vehicle take-off and landing platform |
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| CN111498134B (en) | 2023-09-01 |
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