CN219565512U - Foot rest supporting device for vertical take-off and landing unmanned aerial vehicle - Google Patents
Foot rest supporting device for vertical take-off and landing unmanned aerial vehicle Download PDFInfo
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- CN219565512U CN219565512U CN202320379685.XU CN202320379685U CN219565512U CN 219565512 U CN219565512 U CN 219565512U CN 202320379685 U CN202320379685 U CN 202320379685U CN 219565512 U CN219565512 U CN 219565512U
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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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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
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- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The utility model relates to a stand strutting arrangement for unmanned aerial vehicle that takes off and land perpendicularly, including connecting plate, regulating plate, bear post, skid board, bear symmetric distribution in connecting plate axis both sides to it is articulated through elastic hinge with bearing post up end, bear the post lower terminal surface and pass through elastic hinge and skid board hinge, bear the post medial surface and establish the direction slide rail, the regulating plate passes through the direction slide rail and is connected with bearing the post medial surface, and the regulating plate is including bearing seat, connection curb plate, locating pin and couple. On the one hand, the novel unmanned aerial vehicle can effectively meet the requirements of operation matched with various unmanned aerial vehicle equipment, and is convenient and quick to install and position; on the other hand, the bearing structural strength of the unmanned aerial vehicle equipment can be effectively improved, so that the stability and reliability of the unmanned aerial vehicle during landing operation are improved.
Description
Technical Field
The utility model relates to a tripod strutting arrangement for unmanned aerial vehicle takes off and land perpendicularly belongs to unmanned aerial vehicle technical field.
Background
The foot rest structure is important equipment for taking off and landing operation and bearing positioning of the rotor unmanned aerial vehicle, the use amount is huge, the structure types are various, although the current foot rest structure can meet the operation requirement of unmanned aerial vehicle equipment, in operation, the current foot rest structure is relatively single in structure on one hand, only can meet the use requirement of the unmanned aerial vehicle equipment embryo with a specific structure, and has the advantages of high difficulty in installation, disassembly and maintenance operation and low working efficiency, and when the unmanned aerial vehicle takes off and lands, the adaptability to the topography and the attitude of the unmanned aerial vehicle is poor, so that the stability and the reliability of the unmanned aerial vehicle landing operation are greatly influenced; meanwhile, in operation, the structure of the belly of the unmanned aerial vehicle is often influenced, so that the capacity of the unmanned aerial vehicle for carrying loads through the belly is influenced;
in addition, current foot rest structure often only can satisfy unmanned aerial vehicle and bear the needs of operation, under unmanned aerial vehicle flight condition, foot rest equipment often can consume unmanned aerial vehicle certain load capacity duration to stability and the reliability that unmanned aerial vehicle equipment was operated cause harmful effects.
Therefore, in order to solve this problem, a new unmanned aerial vehicle foot stand device needs to be developed to meet the needs of practical use.
Disclosure of Invention
In order to solve the defects in the prior art, the novel foot rest supporting device for the vertical take-off and landing unmanned aerial vehicle is simple in structure, flexible and convenient to operate, good in universality, capable of effectively meeting the requirements of supporting operation operations of various unmanned aerial vehicle devices, and convenient and quick to install and position; on the other hand can effectively improve unmanned aerial vehicle equipment and bear structural strength to reach stability and the reliability when improving unmanned aerial vehicle landing operation, in addition can effectual auxiliary improvement unmanned aerial vehicle's load bearing capacity and charge energy storage efficiency in addition.
In order to achieve the above object, the present utility model is realized by the following technical scheme:
the utility model provides a perpendicular take off and land unmanned aerial vehicle foot rest strutting arrangement, which comprises a connecting plate, the regulating plate, the carrier bar, the skid board, the connecting plate is the platy frame construction that the transversal face personally submits the rectangle, the carrier bar is two altogether, the symmetric distribution is in connecting plate axis both sides, and articulated through elastic hinge with the carrier bar up end, carrier bar axis is 90 ~ 135 contained angles with connecting plate lower extreme face, and the carrier bar is located connecting plate central line position department, carrier bar lower extreme face is articulated through elastic hinge with a skid board, skid board axis and connecting plate axis parallel distribution, the guide rail is established to carrier bar medial surface, guide rail and carrier bar axis parallel distribution, the regulating plate is located between two carrier bars, and be connected with carrier bar medial surface through guide rail, and the interval is 10% -80% of carrier bar height between regulating plate and the carrier bar up end, the regulating plate includes the carrier bar, the connection curb plate, the link hinge, locating pin and couple, carrier bar and terminal surface parallel distribution under the connecting plate, left surface and right flank of carrier bar are articulated through link plate respectively with a connection curb plate, the guide slot is established to the guide rail, the guide slot cladding is outside the guide rail and is connected with a plurality of guide pin outside the guide rail, at least one side plate is connected with the side face through the hinge, a plurality of articulated connection lateral plate, the locating pin is connected with the guide pin outside the guide slot.
Further, the skid plate is additionally provided with a wireless charging coil and a wiring terminal, at least one wireless charging coil is embedded in the lower end face of the skid plate, the area of the wireless charging coil is not less than 30% of the area of the lower end face of the skid plate, and at least one wiring terminal is embedded in the upper end face of the skid plate and is electrically connected with the wireless charging coil respectively.
Further, the inner side surface and the outer side surface of the skid plate are provided with auxiliary operation cavities in addition, the auxiliary operation cavities are distributed in parallel with the axis of the skid plate, at least one inflatable air bag is arranged in the auxiliary operation cavities, the upper end surface of the skid plate corresponding to the inflatable air bag is provided with an inflatable valve, and the inflatable valve is communicated with the inflatable air bag through a guide pipe.
Further, the bearing seat is any one of a U-shaped groove-shaped structure and a rectangular closed cavity structure with a cross section, the lower end face of the bearing seat and the lower end face of the connecting side plate form an included angle of 0-90 degrees, and when the included angle between the lower end face of the bearing seat and the lower end face of the connecting side plate is 0 degrees, the lower end face of the bearing seat and the lower end face of the connecting side plate are distributed in the same plane.
Further, the connecting side plate comprises a plate body and elastic telescopic rods, the plate body is of a plate-shaped structure with a rectangular cross section, the elastic telescopic rods are connected with the outer side face of the plate body, the upper end faces of the elastic telescopic rods are connected with the connecting hinges and hinged to the side surface of the bearing seat through the connecting hinges, and each elastic telescopic rod is connected with one connecting hinge.
Further, the connecting plate comprises two bearing plates, two adjusting bolts, positioning electromagnets and connecting screw holes, wherein the two bearing plates are of a plate-shaped structure with rectangular cross sections, the two bearing plates are connected through at least two adjusting bolts, two ends of each adjusting bolt are hinged with the side surface of the bearing plate through hinges and form an included angle of 10-90 degrees with the side surface of the bearing plate, at least two connecting screw holes which are vertically distributed with the upper end surface of the bearing plate are formed in the upper end surface of the bearing plate, the positioning electromagnets are embedded in the upper end surface of the bearing plate, are coated outside the connecting screw holes and are of an annular structure which is coaxially distributed with the connecting screw holes, and the positioning electromagnets are mutually connected in parallel.
The novel unmanned aerial vehicle device has the advantages of simple structure, flexible and convenient operation, good universality, convenient and quick installation and positioning, and can effectively meet the requirements of operation matched with various unmanned aerial vehicle devices; on the other hand can effectively improve unmanned aerial vehicle equipment and bear structural strength to reach stability and the reliability when improving unmanned aerial vehicle landing operation, in addition can effectual auxiliary improvement unmanned aerial vehicle's load bearing capacity and charge energy storage efficiency in addition.
Drawings
The present utility model will be described in detail below with reference to the attached drawings and detailed description;
FIG. 1 is a schematic diagram of the novel structure;
FIG. 2 is a schematic view of a partial structure of a connecting side plate;
FIG. 3 is a schematic diagram of a skid structure.
Detailed Description
In order to facilitate the technical means, creation characteristics, achievement of the purpose and efficacy of the present utility model, the present utility model is further described below in connection with the specific embodiments.
As shown in fig. 1-3, a foot rest supporting device for a vertical lifting unmanned aerial vehicle comprises a connecting plate 1, an adjusting plate 2, bearing columns 3 and skid plates 4, wherein the connecting plate 1 is of a plate-shaped frame structure with rectangular cross sections, the two bearing columns 3 are symmetrically distributed on two sides of an axis of the connecting plate 1 and hinged with the upper end face of the bearing columns 3 through elastic hinges 5, the axis of the bearing columns 3 is in an included angle of 90-135 degrees with the lower end face of the connecting plate 1, the bearing columns 3 are positioned at the center line position of the connecting plate 1, the lower end face of the bearing columns 3 is hinged with one skid plate 4 through elastic hinges 5, the axis of the skid plates 4 is parallel to the axis of the connecting plate 1, guide sliding rails 6 are arranged on the inner side faces of the bearing columns 3, the guide sliding rails 6 are parallel to the axis of the bearing columns 3, the adjusting plate 2 is positioned between the two bearing columns 3 and connected with the inner side faces of the bearing columns 3 through the guide sliding rails 6, and the interval between the adjusting plate 2 and the upper end faces of the bearing columns 3 is 10-80% of the height of the bearing columns 3.
In this embodiment, the adjusting plate 2 includes a bearing seat 21, a connecting side plate 22, a connecting hinge 23, a positioning pin 24 and a hook 25, where the bearing seat 21 is parallel to the lower end surface of the connecting plate 1, the left side surface and the right side surface of the bearing seat 21 are hinged to one connecting side plate 22 through the connecting hinge 23, the side wall of the connecting side plate 22 is provided with a guiding groove 26, the guiding groove 26 is coated outside the guiding slide rail 6 and slidingly connected with the outer side surface of the guiding slide rail 6, the side wall of the guiding groove 26 is provided with at least one positioning pin 24, the positioning pin 24 is connected with the guiding slide rail 6, and the hook 25 is several, is connected with the lower end surfaces of the bearing seat 21 and the connecting side plate 22 and hinged to the lower end surfaces of the bearing seat 21 and the connecting side plate 22 through an elastic hinge 5.
It is mainly described that the skid plate 4 is further provided with a wireless charging coil 41, a connection terminal 43 and an electromagnetic positioning pin 44, at least one wireless charging coil 41 is embedded in the lower end surface of the skid plate 4, the area of the wireless charging coil 41 is not less than 30% of the area of the lower end surface of the skid plate 4, and at least one connection terminal 43 is embedded in the upper end surface of the skid plate 4 and is electrically connected with the wireless charging coil 41 respectively.
Further preferably, the inner side surface and the outer side surface of the skid plate 4 are provided with auxiliary working chambers 47, the auxiliary working chambers 47 are distributed in parallel with the axis of the skid plate 4, at least one inflatable air bag 48 is arranged in the auxiliary working chambers 47, the upper end surface of the skid plate 4 corresponding to the inflatable air bag 48 is provided with an inflatable valve 49, and the inflatable valve 49 is communicated with the inflatable air bag 48 through a flow guide pipe.
In this embodiment, the bearing seat 21 is any one of a rectangular closed cavity structure and a U-shaped groove structure with a cross section, the lower end surface of the bearing seat 21 forms an included angle of 0 ° to 90 ° with the lower end surface of the connecting side plate 22, and when the included angle between the lower end surface of the bearing seat 21 and the lower end surface of the connecting side plate 22 is 0 °, the lower end surface of the bearing seat 21 and the lower end surface of the connecting side plate 22 are distributed in the same plane.
Meanwhile, the connecting side plate 22 includes a plate body 221 and elastic telescopic rods 222, the plate body 221 is of a plate-shaped structure with a rectangular cross section, the elastic telescopic rods 222 are connected with the outer side surface of the plate body 221, the upper end surfaces of the elastic telescopic rods 222 are connected with the connecting hinges 23 and hinged with the side surface of the bearing seat 21 through the connecting hinges 23, and each elastic telescopic rod 222 is connected with one connecting hinge 23.
In this embodiment, the connection plate 1 includes two bearing plates 101, an adjusting bolt 102, positioning electromagnets 103 and a connection screw hole 104, the bearing plates 101 are of a plate structure with rectangular cross sections, the two bearing plates 101 are connected by at least two adjusting bolts 102, two ends of each adjusting bolt 102 are hinged to the side surface of the bearing plate 101 through a hinge 105 and form an included angle of 10-90 degrees with the side surface of the bearing plate 101, the upper end surface of the bearing plate 101 is provided with at least two connection screw holes 102 vertically distributed with the upper end surface of the bearing plate 101, the positioning electromagnets 103 are embedded in the upper end surface of the bearing plate 101, are coated outside the connection screw holes 104 and are of an annular structure coaxially distributed with the connection screw holes 104, and the positioning electromagnets 103 are mutually parallel.
In the concrete implementation of the novel structure, firstly, the novel connecting plate, the adjusting plate, the bearing column and the skid plate are assembled, then the assembled novel structure is connected with the unmanned aerial vehicle body through the connecting plate on the one hand, and when the connecting plate is connected with the unmanned aerial vehicle body, the connecting plate structure is flexibly adjusted through the adjusting bolt of the connecting plate on the other hand so as to meet the requirements of the matched operation of unmanned aerial vehicles of different bodies; on the other hand, the connection stability and the assembly connection convenience of the connecting plate and the unmanned aerial vehicle body are realized through the positioning electromagnet and the connecting screw hole of the connecting plate, finally, the included angle between the connecting plate and the bearing column is adjusted according to the use requirement, and the connection position and the relative position relation between the adjusting plate and the bearing column are synchronously adjusted when the working state of the bearing column is adjusted, so that the positioning of the adjusting plate is finished on one hand; on the other hand strengthens two bearing column connection structure's stability through the regulating plate, improves this novel overall structure intensity.
In the operation along with the unmanned aerial vehicle, on one hand, the load bearing seat of the adjusting plate and the hook assist to realize the need of carrying and positioning the load of the unmanned aerial vehicle; on the other hand, through the wireless charging coil of skid board, binding post cooperation, realize carrying out the operation of charging to unmanned aerial vehicle system, improve unmanned aerial vehicle operation's convenience of charging.
In the landing process of the unmanned aerial vehicle, on one hand, the elastic hinge connected between the skid plate and the bearing column realizes that the skid plate automatically adjusts the landing position and angle according to the terrain structure, thereby achieving the purpose of improving the landing stability; on the other hand, the contact area of landing sites on the lower end face of the skid plate and the buoyancy of the skid plate are improved by inflating the inflatable air bags in the skid plate, so that landing stability is improved, landing operation on the surface of a water body can be realized, and the flexibility and reliability of the unmanned aerial vehicle in use and operation are further improved.
The novel unmanned aerial vehicle device has the advantages of simple structure, flexible and convenient operation, good universality, convenient and quick installation and positioning, and can effectively meet the requirements of operation matched with various unmanned aerial vehicle devices; on the other hand can effectively improve unmanned aerial vehicle equipment and bear structural strength to reach stability and the reliability when improving unmanned aerial vehicle landing operation, in addition can effectual auxiliary improvement unmanned aerial vehicle's load bearing capacity and charge energy storage efficiency in addition.
The foregoing has outlined and described the basic principles and main features of the present utility model and the advantages of the present utility model. It will be appreciated by those skilled in the art that the present utility model is not limited by the foregoing embodiments, which have been described in the foregoing embodiments and description merely illustrates the principles of the utility model, and that various changes and modifications may be made therein without departing from the spirit and scope of the utility model, which is defined by the appended claims. The scope of protection of this utility model is defined by the claims that follow and equivalents thereof.
Claims (6)
1. Foot rest support device for unmanned aerial vehicle takes off and land perpendicularly, its characterized in that: the foot rest supporting device for the vertical lifting unmanned aerial vehicle comprises a connecting plate, an adjusting plate, bearing columns and skid plates, wherein the connecting plate is of a platy frame structure with a rectangular cross section, the two bearing columns are symmetrically distributed on two sides of an axis of the connecting plate and hinged with the upper end face of the bearing column through elastic hinges, the axis of the bearing column is 90-135 degrees with the lower end face of the connecting plate, the bearing columns are located at the center line position of the connecting plate, the lower end face of the bearing column is hinged with one skid plate through the elastic hinges, the axis of the skid plate is parallel to the axis of the connecting plate, the inner side face of the bearing column is provided with guide sliding rails, the guide sliding rails are parallel to the axis of the bearing column, the adjusting plate is located between the two bearing columns and connected with the inner side face of the bearing column through the guide sliding rails, the distance between the adjusting plate and the upper end face of the bearing column is 10-80% of the height of the bearing column, the adjusting plate comprises a bearing seat, a connecting side plate, a connecting hinge, a positioning pin and a hook, the left side face and the right side face of the bearing seat are parallel to the connecting plate are respectively hinged with the connecting plate through the elastic hinges, the connecting side plate is connected with the side face of the connecting plate through the connecting hinge, the guide sliding seat is connected with the side face of the side plate, and the side face of the positioning pin is connected with the side face of the side plate through the side plate, and is connected with the side face of the side plate through the hinge, and is connected with the side face of the side plate.
2. The foot rest support device for a vertical take-off and landing unmanned aerial vehicle according to claim 1, wherein: the wireless charging device comprises a skid plate, at least one wireless charging coil and a wiring terminal, wherein the wireless charging coil is embedded in the lower end face of the skid plate, the area of the wireless charging coil is not less than 30% of the area of the lower end face of the skid plate, and the wiring terminal is embedded in the upper end face of the skid plate and is electrically connected with the wireless charging coil respectively.
3. The foot rest support device for a vertical take-off and landing unmanned aerial vehicle according to claim 2, wherein: the auxiliary operation cavity is distributed in parallel with the axis of the skid plate, at least one inflatable air bag is arranged in the auxiliary operation cavity, an inflation valve is arranged on the upper end face of the skid plate corresponding to the inflatable air bag, and the inflation valve is communicated with the inflatable air bag through a guide pipe.
4. The foot rest support device for a vertical take-off and landing unmanned aerial vehicle according to claim 1, wherein: the bearing seat is any one of a U-shaped groove-shaped structure and a rectangular closed cavity structure with a cross section, the lower end face of the bearing seat and the lower end face of the connecting side plate form an included angle of 0-90 degrees, and when the included angle between the lower end face of the bearing seat and the lower end face of the connecting side plate is 0 degree, the lower end face of the bearing seat and the lower end face of the connecting side plate are distributed in the same plane.
5. The foot rest support device for a vertical take-off and landing unmanned aerial vehicle according to claim 1, wherein: the connecting side plate comprises a plate body and elastic telescopic rods, wherein the plate body is of a plate-shaped structure with a rectangular cross section, the elastic telescopic rods are connected with the outer side face of the plate body, the upper end faces of the elastic telescopic rods are connected with connecting hinges and hinged to the side surface of the bearing seat through the connecting hinges, and each elastic telescopic rod is connected with one connecting hinge.
6. The foot rest support device for a vertical take-off and landing unmanned aerial vehicle according to claim 1, wherein: the connecting plate comprises two bearing plates, two adjusting bolts, positioning electromagnets and connecting screw holes, wherein the two bearing plates are of plate-shaped structures with rectangular cross sections, the two bearing plates are connected through at least two adjusting bolts, two ends of each adjusting bolt are hinged to the side surface of the bearing plate through hinges and form an included angle of 10-90 degrees with the side surface of the bearing plate, the upper end face of each bearing plate is provided with at least two connecting screw holes which are vertically distributed with the upper end face of the bearing plate, the positioning electromagnets are embedded in the upper end face of the bearing plate, are coated outside the connecting screw holes and are of annular structures which are coaxially distributed with the connecting screw holes, and the positioning electromagnets are mutually connected in parallel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320379685.XU CN219565512U (en) | 2023-03-02 | 2023-03-02 | Foot rest supporting device for vertical take-off and landing unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320379685.XU CN219565512U (en) | 2023-03-02 | 2023-03-02 | Foot rest supporting device for vertical take-off and landing unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219565512U true CN219565512U (en) | 2023-08-22 |
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ID=87662750
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202320379685.XU Active CN219565512U (en) | 2023-03-02 | 2023-03-02 | Foot rest supporting device for vertical take-off and landing unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219565512U (en) |
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2023
- 2023-03-02 CN CN202320379685.XU patent/CN219565512U/en active Active
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