CN220843050U - Landing buffer device for unmanned aerial vehicle spare landing - Google Patents

Landing buffer device for unmanned aerial vehicle spare landing Download PDF

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Publication number
CN220843050U
CN220843050U CN202322753235.5U CN202322753235U CN220843050U CN 220843050 U CN220843050 U CN 220843050U CN 202322753235 U CN202322753235 U CN 202322753235U CN 220843050 U CN220843050 U CN 220843050U
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fixedly connected
landing
unmanned aerial
aerial vehicle
buffer device
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CN202322753235.5U
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Chinese (zh)
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刘帆
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Tianjin Ouxun Technology Co ltd
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Tianjin Ouxun Technology Co ltd
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Abstract

The utility model relates to the technical field of unmanned aerial vehicles and discloses a landing buffer device for standby landing of an unmanned aerial vehicle, which comprises a bottom plate, wherein two groups of sliding groove frames, two groups of electric push rods and a storage battery are fixedly connected to the upper surface of the bottom plate respectively, sliding frames are slidingly connected to the inside of each sliding groove frame, the telescopic ends of each electric push rod are fixedly connected with the inner top wall of each sliding frame, fixing frames are fixedly connected to the top ends of the sliding frames together, telescopic springs which are arranged at equal distances are fixedly connected to the upper surface of the fixing frames, and supporting plates are fixedly connected to the top ends of the telescopic springs of each group together. According to the utility model, the supporting plate is arranged, so that the unmanned aerial vehicle can lift and fall, meanwhile, the storage battery is utilized, when the electric push rod is used for providing power, the sliding frame can be driven to move up and down in the sliding groove frame through the expansion and contraction of the electric push rod, and meanwhile, the sliding frame can be driven to move up and down by utilizing the sliding frame, so that the sliding frame can drive the supporting plate to lift and adjust.

Description

Landing buffer device for unmanned aerial vehicle spare landing
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a landing buffer device for standby landing of an unmanned aerial vehicle.
Background
The unmanned plane is called as unmanned plane for short, and is a unmanned plane operated by radio remote control equipment and a self-contained program control device.
The utility model discloses an unmanned aerial vehicle landing buffer device in China patent publication No. CN213800225U, which comprises a bottom plate, two sliding rods which are distributed in a horizontal structure are inserted into two sides of the outer wall of the top of the bottom plate, a top plate is mounted on the top end of each sliding rod through bolts, springs positioned between the outer walls of the bottom of the top plate and the outer wall of the top of the bottom plate are sleeved outside the sliding rods, and guide grooves are formed in two sides of the outer wall of the top plate.
With respect to the related art in the above, the applicant believes that the following drawbacks exist: unmanned aerial vehicle plays and falls the support, when using, need remove to open place, need keep spacious around, and the support can not be according to unmanned aerial vehicle's needs with the height adjustment of device when using, if take off in pressing close to ground department, the flying dust that the screw brought can influence the sight to influence unmanned aerial vehicle's take off.
Disclosure of utility model
The utility model provides a landing buffer device for unmanned aerial vehicle standby landing, which aims to solve the technical problem that the height of the device cannot be adjusted according to the requirement of the unmanned aerial vehicle and the buffer effect is not good enough.
The utility model is realized by adopting the following technical scheme: the utility model provides an unmanned aerial vehicle is prepared for falling and is used buffer that rises and falls, includes the bottom plate, two sets of slide groove frame of upper surface fixedly connected with respectively and two sets of electric putter and battery, every the inside equal sliding connection of slide groove frame has the slide frame, every electric putter's flexible end all with the interior roof fixed connection of slide frame, every group the common fixedly connected with mount in top of slide frame, the last fixedly connected with equidistance of mount is arranged telescopic spring, every group telescopic spring's the common fixedly connected with backup pad in top.
As a further improvement of the scheme, the bottom surface of the bottom plate is fixedly connected with two groups of fixing columns, and the bottom surface of each fixing column is fixedly connected with a stabilizing ring.
As a further improvement of the scheme, the outer surface of each electric push rod is fixedly connected with a reinforcing ring, and the bottom surface of each reinforcing ring is fixedly connected with the upper surface of the bottom plate.
As a further improvement of the scheme, the upper surface of the bottom plate is fixedly connected with a battery box, and the inner wall of the battery box is contacted with the outer surface of the storage battery.
As a further improvement of the scheme, the upper surface of the battery box is movably hinged with a protective door, and the upper surface of the protective door is provided with radiating holes which are arranged at equal intervals.
As a further improvement of the scheme, the upper surface of the supporting plate is fixedly connected with an anti-slip pad, and the anti-slip pad is required to be in a soft rubber shape.
As a further improvement of the scheme, the upper surface of the supporting plate is fixedly connected with two groups of fixing seats, and the upper surface of each fixing seat is fixedly connected with an illuminating lamp.
Compared with the prior art, the utility model has the beneficial effects that:
According to the utility model, the support plate is arranged, so that the unmanned aerial vehicle can lift and fall, meanwhile, when the storage battery is utilized, the electric push rod is powered for use, and the sliding frame can be driven to move up and down in the sliding groove frame through the expansion and contraction of the electric push rod, and meanwhile, the sliding frame can be driven to move up and down by utilizing the upward and downward movement of the sliding frame, so that the sliding frame can drive the support plate to lift and adjust, the unmanned aerial vehicle can be far away from the ground when lifting and falling, and the unmanned aerial vehicle can buffer when lifting and falling on the support plate through the expansion and contraction of the expansion spring, and further the unmanned aerial vehicle can have stability when lifting and falling.
Drawings
FIG. 1 is a schematic diagram of the overall structure of the present utility model;
FIG. 2 is a schematic view of a cross-sectional structure of a support plate according to the present utility model;
FIG. 3 is a schematic view of a telescopic spring according to the present utility model;
fig. 4 is a schematic structural view of a battery according to the present utility model.
Main symbol description:
1. A bottom plate; 2. fixing the column; 3. a support plate; 4. an anti-slip pad; 5. a stabilizing ring; 6. a fixing seat; 7. a lighting lamp; 8. a fixing frame; 9. a telescopic spring; 10. a sliding groove rack; 11. an electric push rod; 12. a reinforcing ring; 13. a battery case; 14. a heat radiation port; 15. a storage battery; 16. a carriage; 17. a protective door.
Detailed Description
The present utility model will be further described with reference to the accompanying drawings and detailed description, wherein it is to be understood that, on the premise of no conflict, the following embodiments or technical features may be arbitrarily combined to form new embodiments.
Example 1:
Please combine fig. 1-4, the landing buffer device for unmanned aerial vehicle spare landing of this embodiment, including bottom plate 1, the upper surface of bottom plate 1 is two sets of slide groove frame 10 and two sets of electric putter 11 and battery 15 of fixedly connected with respectively, the inside of every slide groove frame 10 all sliding connection has carriage 16, the flexible end of every electric putter 11 all with the interior roof fixed connection of carriage 16, the common fixedly connected with mount 8 in top of every group carriage 16, the last surface fixedly connected with equidistance extension spring 9 of mount 8 is arranged, the common fixedly connected with backup pad 3 in top of every group extension spring 9.
Example 2:
With reference to fig. 1, this embodiment is further improved on the basis of embodiment 1 in that: the bottom surface fixedly connected with two sets of fixed columns 2 of bottom plate 1, the equal fixedly connected with solid fixed ring 5 in bottom surface of every fixed column 2, through fixed column 2, can fix on bottom plate 1 to fix solid fixed ring 5, can make solid fixed ring 5 support bottom plate 1.
Example 3:
With reference to fig. 3, this embodiment is further improved on the basis of embodiment 1 in that: the surface of every electric putter 11 all fixedly connected with reinforcing ring 12, the bottom surface of every reinforcing ring 12 all with the last fixed surface of bottom plate 1 be connected, through reinforcing ring 12, can fix electric putter 11 on bottom plate 1, can make electric putter 11 can have the fastness when using.
Example 4:
With reference to fig. 3-4, this embodiment is further improved on the basis of embodiment 1 in that: the upper surface fixedly connected with battery case 13 of bottom plate 1, the inner wall of battery case 13 contacts with the surface of battery 15, through battery case 13, can fix on bottom plate 1 to can make battery 15 place, thereby can make battery 15 have stability when using.
Example 5:
With reference to fig. 3, this embodiment is further improved on the basis of embodiment 4 in that: the upper surface of the battery box 13 is movably hinged with a protective door 17, the upper surface of the protective door 17 is provided with radiating ports 14 which are arranged at equal intervals, the battery box 13 can be opened or closed through the protective door 17, and the inside of the battery box 13 can radiate heat by utilizing the radiating ports 14.
Example 6:
With reference to fig. 2, this embodiment is further improved on the basis of embodiment 1 in that: the upper surface fixedly connected with slipmat 4 of backup pad 3, slipmat 4 need become soft rubber form, utilizes slipmat 4, can fix on backup pad 3 to utilize the material of self, play the effect that can skid.
Example 7:
with reference to fig. 2, this embodiment is further improved on the basis of embodiment 1 in that: the upper surface fixedly connected with of backup pad 3 is two sets of fixing base 6, and the upper surface fixedly connected with light 7 of every fixing base 6 utilizes fixing base 6, can fix light 7 on backup pad 3 to use of illumination when can making unmanned aerial vehicle rise and fall through light 7.
The embodiment of the application provides a landing buffer device for unmanned aerial vehicle standby landing, which is implemented by the following principle: when the unmanned aerial vehicle is used, firstly, the storage battery 15 is connected with a power supply, when equipment is needed to be used, the protective door 17 is opened, the storage battery 15 is installed in the battery box 13, after the installation is finished, the electric push rod 11 and the illuminating lamp 7 are communicated with the storage battery 15 through wires, the base plate 1 is placed at a proper using position through the fixing post 2 and the fixing ring 5, then the unmanned aerial vehicle is placed on the anti-slip pad 4, when the height of the supporting plate 3 is needed to be adjusted after the placement is finished, the electric push rod 11 is opened to stretch, the electric push rod 11 stretches and simultaneously drives the sliding frame 16 to lift in the sliding groove frame 10, the supporting plate 3 is driven to move upwards through the lifting of the sliding groove frame 10, and when the unmanned aerial vehicle needs to fall onto the anti-slip pad 4 and the supporting plate 3, the falling force can be buffered through the support of the telescopic matching fixing frame 8 of the telescopic spring 9, so that the unmanned aerial vehicle is used.
The above embodiments are only preferred embodiments of the present utility model, and the scope of the present utility model is not limited thereto, but any insubstantial changes and substitutions made by those skilled in the art on the basis of the present utility model are intended to be within the scope of the present utility model as claimed.

Claims (7)

1. The utility model provides an unmanned aerial vehicle is with taking-off and landing buffer, its characterized in that, including bottom plate (1), the upper surface of bottom plate (1) is two sets of slide groove frame (10) and two sets of electric putter (11) and battery (15) of fixedly connected with respectively, every the inside of slide groove frame (10) is all sliding connection has slide frame (16), every electric putter's (11) flexible end all with the interior roof fixed connection of slide frame (16), every group the common fixedly connected with mount (8) in top of slide frame (16), the last fixedly connected with equidistance of mount (8) extension spring (9), every group the common fixedly connected with backup pad (3) in top of extension spring (9).
2. The landing buffer device for unmanned aerial vehicle spare landing as claimed in claim 1, wherein the bottom surface of the bottom plate (1) is fixedly connected with two groups of fixing columns (2), and the bottom surface of each fixing column (2) is fixedly connected with a stabilizing ring (5).
3. The landing buffer device for the unmanned aerial vehicle standby landing as claimed in claim 1, wherein the outer surface of each electric push rod (11) is fixedly connected with a reinforcing ring (12), and the bottom surface of each reinforcing ring (12) is fixedly connected with the upper surface of the bottom plate (1).
4. The landing buffer device for unmanned aerial vehicle spare landing as claimed in claim 1, wherein the battery box (13) is fixedly connected to the upper surface of the base plate (1), and the inner wall of the battery box (13) is in contact with the outer surface of the storage battery (15).
5. The landing buffer device for unmanned aerial vehicle spare landing as claimed in claim 4, wherein the upper surface of the battery box (13) is movably hinged with a protective door (17), and the upper surface of the protective door (17) is provided with heat dissipation ports (14) which are arranged at equal intervals.
6. The landing buffer device for unmanned aerial vehicle spare landing as claimed in claim 1, wherein the upper surface of the supporting plate (3) is fixedly connected with an anti-slip pad (4), and the anti-slip pad (4) is required to be in a soft rubber shape.
7. The landing buffer device for unmanned aerial vehicle spare landing as claimed in claim 1, wherein the upper surface of the supporting plate (3) is fixedly connected with two groups of fixing seats (6), and the upper surface of each fixing seat (6) is fixedly connected with an illuminating lamp (7).
CN202322753235.5U 2023-10-13 2023-10-13 Landing buffer device for unmanned aerial vehicle spare landing Active CN220843050U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202322753235.5U CN220843050U (en) 2023-10-13 2023-10-13 Landing buffer device for unmanned aerial vehicle spare landing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202322753235.5U CN220843050U (en) 2023-10-13 2023-10-13 Landing buffer device for unmanned aerial vehicle spare landing

Publications (1)

Publication Number Publication Date
CN220843050U true CN220843050U (en) 2024-04-26

Family

ID=90776774

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202322753235.5U Active CN220843050U (en) 2023-10-13 2023-10-13 Landing buffer device for unmanned aerial vehicle spare landing

Country Status (1)

Country Link
CN (1) CN220843050U (en)

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