CN216301495U - Unmanned aerial vehicle safety flight platform - Google Patents
Unmanned aerial vehicle safety flight platform Download PDFInfo
- Publication number
- CN216301495U CN216301495U CN202123368391.7U CN202123368391U CN216301495U CN 216301495 U CN216301495 U CN 216301495U CN 202123368391 U CN202123368391 U CN 202123368391U CN 216301495 U CN216301495 U CN 216301495U
- Authority
- CN
- China
- Prior art keywords
- unmanned aerial
- aerial vehicle
- plate
- damping
- arc
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Landscapes
- Vibration Dampers (AREA)
Abstract
The utility model discloses an unmanned aerial vehicle safe flying platform, which comprises an unmanned aerial vehicle, a damping plate, an arc-shaped protection plate, a pressure plate, a buffering component and an arching base, wherein two sides of the unmanned aerial vehicle are respectively provided with a support rod, the upper surface of the unmanned aerial vehicle is fixedly connected with a fixed plate, the upper surfaces of the fixed plate and the two support rods are respectively provided with wings, the bottom surface of the unmanned aerial vehicle is fixedly connected with the upper surface of the damping plate, two ends of the upper part of the damping plate are respectively fixedly connected with the pressure plate, two side surfaces of the upper part of the pressure plate are respectively provided with the buffering component, two side surfaces of the bottom of the support rods are respectively and symmetrically hinged with pneumatic telescopic links through semicircular hinge plates, one end surface of the pneumatic telescopic links, which is far away from the semicircular hinge plates, is hinged with the buffering component, the bottom of the unmanned aerial vehicle is provided with the damping plate and the arching base, and the buffering component is matched with the pneumatic telescopic links for use, the gravity buffering effect of the unmanned aerial vehicle in take-off and landing is ensured.
Description
Technical Field
The utility model relates to a safe flight platform of an unmanned aerial vehicle, and belongs to the technical field of unmanned aerial vehicles.
Background
The unmanned plane is an unmanned plane for short, and is an unmanned aerial vehicle operated by utilizing a radio remote control device and a self-contained program control device. Unmanned aerial vehicle is unmanned vehicles's the general name in fact, in unmanned aerial vehicle flight in-process, receive the striking of hindrance easily to and come from descending and receive the vibrations power of diving, arouse easily that unmanned aerial vehicle internal component damages, and the supporting collection equipment who uses of unmanned aerial vehicle takes place the skew, influence data acquisition, need have the buffering protection when the hindrance striking, and have the protector use of shock attenuation noise reduction when descending.
SUMMERY OF THE UTILITY MODEL
Aiming at the problems in the prior art, the utility model provides an unmanned aerial vehicle safety flight platform, wherein an unmanned aerial vehicle is provided with an arc-shaped protection plate and a fan-shaped compression spring, the unmanned aerial vehicle has the shock absorption and protection effects when the unmanned aerial vehicle is impacted and blocked, the bottom of the unmanned aerial vehicle is provided with a shock absorption plate, an arched base and a buffer assembly which are matched with a pneumatic telescopic rod for use, the gravity buffering effect of taking off and landing of the unmanned aerial vehicle is ensured, the internal damage caused by the vibration of the unmanned aerial vehicle is reduced, and the technical problems that the vibration force is large and an impact blocking object is easy to damage are solved.
In order to achieve the purpose, the utility model is realized by the following technical scheme: an unmanned aerial vehicle safe flying platform comprises an unmanned aerial vehicle, a damping plate, arc-shaped protection plates, pressure plates, a buffering assembly and an arching base, wherein two sides of the unmanned aerial vehicle are respectively provided with a supporting rod, the upper surface of the unmanned aerial vehicle is fixedly connected with a fixing plate, the upper surfaces of the fixing plate and the two supporting rods are respectively provided with wings, the bottom surface of the unmanned aerial vehicle is fixedly connected with the upper surface of the damping plate, two ends of the upper part of the damping plate are respectively fixedly connected with the pressure plates, two side surfaces of the upper part of the pressure plates are respectively provided with the buffering assembly, two side surfaces of the bottom of the supporting rods are respectively and symmetrically hinged with a pneumatic telescopic rod through semicircular hinged sheets, one end surface of the pneumatic telescopic rod, which is far away from the semicircular hinged with the buffering assembly, one end, which is far away from each other, of the two pressure plates is welded with the arc-shaped protection plates, one end surface, which is far away from the unmanned aerial vehicle, of the supporting rod is connected with the arc-shaped protection plates through at least four damping springs, the damping plate bottom fixed surface connect at least three damping support pole, damping support pole bottom threaded connection arch the base, arch base bottom surface joint have the shock attenuation sponge.
The buffering component comprises two positioning grooves symmetrically welded on the pressure plate, sliding shaft rods are arranged in the positioning grooves, buffering compression springs are sleeved on the surfaces of the sliding shaft rods, one end surfaces, close to each other, of the two sliding shaft rods are connected with positioning blocks in a sliding mode, and the two positioning blocks are correspondingly hinged to the bottom end surfaces of the two pneumatic telescopic rods.
The bracing piece keep away from unmanned aerial vehicle's an end surface and connect the arc guard plate through four damping spring, four damping spring expand towards arc guard plate side surface for fan-shaped structure.
The damping plate is arranged in a minor arc structure, and a damping spring layer is arranged in the damping plate.
The bracing piece keep away from four damping spring in unmanned aerial vehicle's one end surface all be articulated.
In conclusion, the utility model provides an unmanned aerial vehicle safe flight platform, wherein the unmanned aerial vehicle is provided with the arc-shaped protection plate and the fan-shaped compression spring, the unmanned aerial vehicle has the shock absorption and protection effects when the unmanned aerial vehicle is impacted and blocked, the shock absorption plate, the arched base and the buffering component are arranged at the bottom of the unmanned aerial vehicle and are matched with the pneumatic telescopic rod for use, the gravity buffering effect of the unmanned aerial vehicle during takeoff and landing is ensured, the internal damage caused by the vibration of the unmanned aerial vehicle is reduced, and the protection effect on the unmanned aerial vehicle is achieved.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic diagram of the structure A of FIG. 1;
FIG. 3 is a schematic diagram of the structure B in FIG. 2;
in the figure: unmanned aerial vehicle 1, bracing piece 11, fixed plate 12, wing 13, semicircle articulated piece 14, air telescopic rod 15, shock attenuation board 2, shock attenuation bracing piece 21, damping spring layer 22, arc guard plate 3, damping spring 31, pressure plate 4, buffer unit 5, positioning groove 51, slide shaft pole 52, buffering compression spring 53, locating piece 54, hunch up base 6, shock attenuation sponge 61.
Detailed Description
As shown in fig. 1 to 3, the utility model is an unmanned aerial vehicle safe flying platform, comprising an unmanned aerial vehicle 1, a damping plate 2, an arc-shaped protection plate 3, a pressure plate 4, a buffering component 5 and an arching base 6, wherein two sides of the unmanned aerial vehicle 1 are respectively provided with a support rod 11, the upper surface of the unmanned aerial vehicle 1 is fixedly connected with a fixed plate 12, the upper surfaces of the fixed plate 12 and the two support rods 11 are respectively provided with a wing 13, the bottom surface of the unmanned aerial vehicle 1 is fixedly connected with the upper surface of the damping plate 2, two ends of the upper part of the damping plate 2 are respectively fixedly connected with the pressure plate 4, two side surfaces of the upper part of the pressure plate 4 are respectively provided with the buffering component 5, two side surfaces of the bottom of the support rods 11 are respectively and symmetrically hinged with pneumatic telescopic rods 15 through semicircular hinge pieces 14, one end surface of the pneumatic telescopic rod 15 far away from the semicircular hinge pieces 14 is hinged with the buffering component 5, the pneumatic telescopic rod 15 is respectively hinged with the semicircular hinged sheets 14 and the buffering component 5, the aim is realized that the pneumatic telescopic rod has a movable connection mode and can provide more damping and buffering functions for the unmanned aerial vehicle, one end of the two pressure plates 4, which is far away from each other, is welded with the arc-shaped protection plate 3, the arc-shaped structure of the arc-shaped protection plate 3 is arranged, even if the protection surface is increased, the resistance caused by impact of obstacles is buffered, the unmanned aerial vehicle is greatly protected from being damaged, one end surface of the support rod 11, which is far away from the unmanned aerial vehicle 1, is connected with the arc-shaped protection plate 3 through at least four damping springs 31, the bottom surface of the damping plate 2 is fixedly connected with at least three damping support rods 21, the three damping support rods 21 are arranged to play a triangular role in supporting the unmanned aerial vehicle, the bottom end of each damping support rod 21 is in threaded connection with the arched base 6, and the upper part of the arched base 6 is arranged in an arched arc-shaped structure, the purpose plays the atress big, the shock attenuation cushions the effect to shock attenuation sponge 61 on, 6 bottom surface joints of hunch-up base have shock attenuation sponge 61, shock attenuation sponge 61 has the shock attenuation buffering to and inhale the effect of sound.
Buffering subassembly 5 including two positioning groove 51 of symmetry welding on pressure plate 4, positioning groove 51 inside set up slide shaft pole 52, slide shaft pole 52 surface cup joint buffering compression spring 53, the mutual terminal surface sliding connection locating piece 54 that is close to of two slide shaft poles 52, locating piece 54 owing to receive the cushion effect that comes from pneumatic telescopic handle, sliding promotion buffering compression spring 53 on slide shaft pole 52 plays buffering unmanned aerial vehicle self gravity, gives unmanned aerial vehicle certain cushioning effect, two locating pieces 54 correspond the articulated bottom surface that corresponds two pneumatic telescopic handle 15.
The damping plate 2 is arranged in a minor arc structure, and a damping spring layer 22 is arranged in the damping plate 2.
In summary, the utility model provides an unmanned aerial vehicle safety flight platform, the unmanned aerial vehicle is provided with an arc-shaped protection plate and a fan-shaped compression spring, when the unmanned aerial vehicle is impacted and blocked, the unmanned aerial vehicle has a shock absorption and protection effect, the bottom of the unmanned aerial vehicle is provided with a shock absorption plate, an arched base and a buffer assembly which are matched with a pneumatic telescopic rod for use, the gravity buffering effect of the unmanned aerial vehicle during taking off and landing is ensured, the internal damage caused by the vibration of the unmanned aerial vehicle is reduced, and the unmanned aerial vehicle is protected.
Claims (5)
1. The safe flying platform of the unmanned aerial vehicle is characterized by comprising an unmanned aerial vehicle (1), a damping plate (2), an arc-shaped protection plate (3), a pressure plate (4), a buffering component (5) and an arch base (6), wherein supporting rods (11) are respectively arranged on two sides of the unmanned aerial vehicle (1), the upper part of the unmanned aerial vehicle (1) is fixedly connected with a fixing plate (12), wings (13) are respectively arranged on the upper surfaces of the fixing plate (12) and the two supporting rods (11), the bottom surface of the unmanned aerial vehicle (1) is fixedly connected with the upper surface of the damping plate (2), two ends of the upper part of the damping plate (2) are respectively fixedly connected with the pressure plate (4), the two side surfaces of the upper part of the pressure plate (4) are respectively provided with the buffering component (5), the two side surfaces of the bottom of the supporting rods (11) are respectively and symmetrically hinged with pneumatic telescopic rods (15) through semicircular hinged pieces (14), pneumatic telescopic link (15) keep away from articulated piece of semicircle (14) one end surface and articulate buffering subassembly (5), two pressure plates (4) one end welding arc guard plate (3) of keeping away from each other, bracing piece (11) keep away from the one end surface of unmanned aerial vehicle (1) and connect arc guard plate (3) through four at least damping spring (31), damping plate (2) bottom fixed surface connect at least three shock attenuation bracing piece (21), shock attenuation bracing piece (21) bottom threaded connection arch base (6), arch base (6) bottom surface joint have shock attenuation sponge (61).
2. The unmanned aerial vehicle safe flying platform of claim 1, wherein the buffer assembly (5) comprises two positioning grooves (51) symmetrically welded on the pressure plate (4), a sliding shaft rod (52) is arranged inside the positioning groove (51), a buffer compression spring (53) is sleeved on the surface of the sliding shaft rod (52), one end surface of the two sliding shaft rods (52) close to each other is slidably connected with a positioning block (54), and the two positioning blocks (54) are correspondingly hinged to the bottom end surfaces of the two pneumatic telescopic rods (15).
3. An unmanned aerial vehicle safe flight platform according to claim 1, characterized in that, the surface of one end of the support rod (11) far away from the unmanned aerial vehicle (1) is connected with the arc-shaped protection plate (3) through four damping springs (31), and the four damping springs (31) are unfolded towards one side surface of the arc-shaped protection plate (3) in a fan-shaped structure.
4. An unmanned aerial vehicle safe flight platform according to claim 1, characterized in that, the shock attenuation board (2) be the minor arc column structure setting, shock attenuation board (2) inside be provided with damping spring layer (22).
5. An unmanned aerial vehicle safe flight platform according to claim 2, wherein the support rod (11) is hinged with four damping springs (31) on the end surface away from the unmanned aerial vehicle (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123368391.7U CN216301495U (en) | 2021-12-29 | 2021-12-29 | Unmanned aerial vehicle safety flight platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123368391.7U CN216301495U (en) | 2021-12-29 | 2021-12-29 | Unmanned aerial vehicle safety flight platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216301495U true CN216301495U (en) | 2022-04-15 |
Family
ID=81084827
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202123368391.7U Active CN216301495U (en) | 2021-12-29 | 2021-12-29 | Unmanned aerial vehicle safety flight platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216301495U (en) |
-
2021
- 2021-12-29 CN CN202123368391.7U patent/CN216301495U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN113772083B (en) | Unmanned aerial vehicle for personnel tracking | |
| CN216301495U (en) | Unmanned aerial vehicle safety flight platform | |
| CN214138939U (en) | Unmanned aerial vehicle take-off and landing shock attenuation buffer | |
| CN206307266U (en) | A kind of multi-rotor unmanned aerial vehicle double damping undercarriage | |
| CN209667380U (en) | A kind of agricultural unmanned plane anticollision device, collision-prevention device | |
| CN208085999U (en) | A kind of plant protection drone damping undercarriage | |
| CN209938977U (en) | Unmanned aerial vehicle's protector | |
| CN210761306U (en) | Old city reforms transform and uses unmanned aerial vehicle shock-absorbing structure | |
| CN205872452U (en) | A support for among unmanned aerial vehicle | |
| CN213566447U (en) | Traffic investigation is with shooting unmanned aerial vehicle | |
| CN213200087U (en) | Carbon fiber unmanned machine shell | |
| CN211001806U (en) | Unmanned aerial vehicle undercarriage | |
| CN113716028A (en) | Shock attenuation undercarriage and unmanned aerial vehicle | |
| CN219134546U (en) | Unmanned aerial vehicle main part frame is with preventing falling mechanism | |
| CN213768957U (en) | Forest fire monitoring device for fixed-wing unmanned aerial vehicle | |
| CN219545103U (en) | Unmanned aerial vehicle with protection machanism | |
| CN221068447U (en) | Unmanned aerial vehicle buffer | |
| CN110271687A (en) | Portable, lightweight unmanned plane blocks recyclable device and application method | |
| CN215399311U (en) | Undercarriage for unmanned aerial vehicle with buffer function | |
| CN214216128U (en) | A bradyseism device for adverse circumstances unmanned aerial vehicle descends | |
| CN216253616U (en) | Unmanned aerial vehicle flight controller | |
| CN217864717U (en) | Improved generation unmanned aerial vehicle for aerial survey | |
| CN218578043U (en) | Unmanned aerial vehicle | |
| CN214824090U (en) | Multi-rotor meteorological unmanned aerial vehicle | |
| CN219857627U (en) | Unmanned aerial vehicle with good protection function |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |