CN215622709U

CN215622709U - Unmanned aerial vehicle for full path planning and capturing

Info

Publication number: CN215622709U
Application number: CN202122415716.6U
Authority: CN
Inventors: 黎剑
Original assignee: Mianyang Yaozhou Technology Co ltd
Current assignee: Mianyang Yaozhou Technology Co ltd
Priority date: 2021-10-08
Filing date: 2021-10-08
Publication date: 2022-01-25
Anticipated expiration: 2031-10-08

Abstract

The utility model discloses an unmanned aerial vehicle for full path planning and capturing in the technical field of unmanned aerial vehicles, which comprises an unmanned aerial vehicle main body; the rain-proof anti-collision building assembly comprises an installation rod detachably fixed in the center of the top of an unmanned aerial vehicle main body, a side ring is sleeved on the outer side of a top seat, a plurality of groups of reinforcing rods are arranged between the top of the outer wall of the top seat and the top of the side ring in an annular array mode, and a waterproof breathable film is arranged between every two adjacent groups of reinforcing rods; the landing assembly is arranged at the bottom of the unmanned aerial vehicle main body. According to the utility model, the rain-proof anti-collision module is arranged at the top of the main body of the unmanned aerial vehicle, and is contacted through the side ring or the elastic contact plate during collision, so that the wings are effectively prevented from being damaged by collision, and meanwhile, the collision force is buffered through the elastic contact plate, the spring and the anti-collision elastic ring, so that the collision damage to the main body of the unmanned aerial vehicle is further reduced.

Description

Unmanned aerial vehicle for full path planning and capturing

Technical Field

The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle for full path planning and capturing.

Background

Unmanned aerial vehicles are simply called "drones", and "UAVs" in english, are unmanned aerial vehicles operated by radio remote control equipment and self-contained program control devices, or are operated autonomously, either completely or intermittently, by an onboard computer, and currently unmanned aerial vehicles for full path planning and capture have the following drawbacks in use: at unmanned aerial vehicle flight in-process, often cause colliding with and striking phenomenon of unmanned aerial vehicle because the operator operates carelessly or because of topography and air current etc. cause, cause the damage of certain degree to unmanned aerial vehicle's fuselage, the rainwater can cause the influence to the rotation of unmanned aerial vehicle's wing when raining simultaneously, arouse easily that unmanned aerial vehicle is out of control for unmanned aerial vehicle life is lower, and still receives the vibrations damage when some unmanned aerial vehicle early falls to the ground. To this end, we propose a drone for full path planning and capture.

SUMMERY OF THE UTILITY MODEL

The utility model aims to provide an unmanned aerial vehicle for full path planning and capturing, so as to solve the problems in the background technology.

In order to achieve the purpose, the utility model provides the following technical scheme: a drone for full path planning and capture, comprising,

the unmanned aerial vehicle comprises an unmanned aerial vehicle main body, wherein an electric device is arranged at the bottom of the unmanned aerial vehicle main body;

the rain-proof anti-collision building assembly comprises an installation rod detachably fixed in the center of the top of an unmanned aerial vehicle main body, a top seat is fixed at the top of the installation rod, a side ring is sleeved outside the top seat and is positioned below the top seat, a plurality of groups of reinforcing rods are arranged between the top of the outer wall of the top seat and the top of the side ring in an annular array mode, and a waterproof breathable film is arranged between every two adjacent groups of reinforcing rods;

the landing assembly is arranged at the bottom of the unmanned aerial vehicle main body.

Further, the fixed cover of side ring outer wall is equipped with crashproof elastic ring, and crashproof elastic ring outer wall annular array integrated into one piece has multiunit elastic bulge, side bottom of the ring portion outer wall annular array has multiunit curved curb plate, the curb plate has curved elastic contact plate with the wing one-to-one of unmanned aerial vehicle main part, the curb plate outer wall has curved elastic contact plate through multiunit spring coupling.

Further, unmanned aerial vehicle main part top central authorities are fixed with the mount pad, and the installation pole activity is inserted and is established in the mount pad, the equal screw thread of side is inserted and is equipped with the screw thread round pin around the mount pad, the both sides outer wall bottom of installation pole all seted up with screw thread round pin complex screw hole.

Further, the subassembly that falls to the ground includes the U-shaped frame fixed with unmanned aerial vehicle main part bottom, the left and right sides end symmetry rotation slope of U-shaped frame front and back side is provided with the link, and the front and back side the one end of keeping away from the U-shaped frame between the link is provided with the contact wheel through the axis body rotation.

Furthermore, the front side and the rear side are connected with the connecting frame top jointly and accept the board, and accept and be provided with the arc spring between board and the U-shaped frame bottom, the one side of accepting the board and keeping away from the arc spring is fixed with the rectangular plate parallel with the connecting frame, and runs through around on the rectangular plate and has seted up the waist hole.

Further, the longitudinal movement in the waist hole is provided with the loose axle of looks adaptation, and the loose axle longitudinal fixation sets up one end in the adapting rod, U-shaped frame bottom central authorities are fixed with the sleeve through the support, and sleeve inner chamber middle part is fixed with inserts, controls the side the relative one end of adapting rod activity respectively runs through the sleeve left and right sides, controls the side the relative one end of adapting rod all is provided with reset spring, and the reset spring other end with insert fixedly.

Compared with the prior art, the utility model has the beneficial effects that: the utility model is provided with a rain-proof anti-collision building assembly at the top of the main body of the unmanned aerial vehicle, the rain-proof anti-collision building assembly is contacted through a side ring or an elastic contact plate during collision, thereby effectively avoiding the wings from being damaged by collision, simultaneously realizing collision buffering through the elastic contact plate, a spring and an anti-collision elastic ring, further reducing the collision damage of the main body of the unmanned aerial vehicle, and the rain-proof anti-collision building assembly is provided with a waterproof breathable film at a reinforcing rod between a top seat and the side ring, so that rainwater can slide down from the side edge, effectively preventing the interference of the rainwater on the wings, ensuring the stable operation of the main body of the unmanned aerial vehicle during rainy days, and is provided with a landing assembly, when the main body of the unmanned aerial vehicle contacts the ground, the arc-shaped spring is extruded by the swinging of a connecting frame to realize preliminary buffering of the vibration force, and the connecting frame also drives a bearing rod, and a reset spring are used for realizing further buffering of the landing vibration force of the main body of the unmanned aerial vehicle, the life of this unmanned aerial vehicle main part has been prolonged.

Drawings

FIG. 1 is a perspective view of the structure of the present invention;

FIG. 2 is a perspective view of the rain-proof anti-collision assembly structure of the utility model;

fig. 3 is a perspective view of the floor assembly structure of the present invention.

In the figure: 1. an unmanned aerial vehicle main body; 2. an electrical device; 3. a rain-proof anti-collision assembly; 31. a mounting seat; 32. mounting a rod; 33. a top seat; 34. a reinforcing bar; 35. a waterproof breathable film; 36. an anti-collision elastic ring; 37. a side plate; 38. a resilient contact plate; 39. a side ring; 4. a landing assembly; 41. a U-shaped frame; 42. a connecting frame; 43. a contact wheel; 44. a bearing plate; 45. an arc-shaped spring; 46. a sleeve; 47. a bearing rod.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

Example 1

Referring to fig. 1-3, the present invention provides a technical solution: an unmanned aerial vehicle for full path planning and capturing comprises an unmanned aerial vehicle main body 1, wherein the unmanned aerial vehicle main body 1 is widely applied in the field and is not detailed in any other way, an electric device 2 is arranged at the bottom of the unmanned aerial vehicle main body 1, the electric device 2 is a device which enables the unmanned aerial vehicle to carry out full path planning and capturing, selection is carried out according to actual conditions, the unmanned aerial vehicle is widely applied in the field and is not detailed in any other way; rain-proof prevents bumping a subassembly 3, rain-proof prevents bumping a subassembly 3 and includes can dismantle the installation pole 32 of fixing in the central authorities of unmanned aerial vehicle main part 1 top, installation pole 32 top is fixed with footstock 33, footstock 33 outside cover is equipped with side ring 39, and side ring 39 is located footstock 33 below, the outside of side ring 39 is in the outside of unmanned aerial vehicle main part 1 wing, make the contact during collision be side ring 39, annular array is provided with multiunit stiffener 34 between footstock 33 outer wall top and the side ring 39 top, stiffener 34 is the slope, be provided with waterproof ventilated membrane 35 between two sets of stiffener 34 adjacently, waterproof ventilated membrane 35 makes rainwater can not interfere unmanned aerial vehicle main part 1 normal flight, make rainwater slide from the side, on the other hand the gas permeability is strong, the air current that the wing produced can smoothly pass through waterproof ventilated membrane 35, guarantee the stability of unmanned aerial vehicle main part 1 flight; fall to the ground subassembly 4, fall to the ground subassembly 4 and set up in unmanned aerial vehicle main part 1 bottom.

As shown in fig. 2: the outer wall of the side ring 39 is fixedly sleeved with an anti-collision elastic ring 36 and is made of rubber materials, the damage caused by received impact force is further reduced, multiple groups of elastic bulges are integrally formed on the outer wall annular array of the anti-collision elastic ring 36, multiple groups of arc-shaped side plates 37 are arranged on the outer wall annular array at the bottom of the side ring 39, the side plates 37 correspond to the wings of the unmanned aerial vehicle main body 1 one by one, the wings are protected, the unmanned aerial vehicle main body 1 can fly normally, the outer walls of the side plates 37 are connected with arc-shaped elastic contact plates 38 through multiple groups of springs, and the damage caused by collision is reduced;

as shown in fig. 2: 1 top central authorities of unmanned aerial vehicle main part are fixed with mount pad 31, and the activity of installation pole 32 is inserted and is established in mount pad 31, and the equal screw thread of side is inserted and is equipped with the screw thread round pin around mount pad 31, and the outer end of screw thread round pin is fixed with and supplies the manual pivoted driving-disc of user of service, and the both sides outer wall bottom of installation pole 32 all seted up with screw thread round pin complex screw hole, conveniently realizes fast that the rain-proof prevents bumping the dismouting of subassembly 3 and unmanned aerial vehicle main part 1.

Example 2

As shown in fig. 3: the landing assembly 4 comprises a U-shaped frame 41 fixed to the bottom of the unmanned aerial vehicle main body 1, the U-shaped frame 41 plays a role in supporting and installing a structure, the left end and the right end of the front side and the rear side of the U-shaped frame 41 are symmetrically rotated and inclined to form connecting frames 42, one end, far away from the U-shaped frame 41, of each connecting frame 42 on the front side and the rear side is rotatably provided with a contact wheel 43 through a shaft body, the unmanned aerial vehicle main body 1 is in contact with the ground through the contact wheels 43 when landing, and is in sliding contact with the ground when landing, so that the damage of landing vibration force of the unmanned aerial vehicle main body 1 is reduced while contact wear is reduced;

as shown in fig. 3: the top of the front side connecting frame 42 and the top of the rear side connecting frame 42 are connected with a bearing plate 44 together, an arc spring 45 is arranged between the bearing plate 44 and the bottom of the U-shaped frame 41, the unmanned aerial vehicle main body 1 is in contact with the ground in a floor mode, the connecting frame 42 swings to extrude the arc spring 45 to achieve preliminary vibration force buffering, damage caused by the floor vibration force of the unmanned aerial vehicle main body 1 is further reduced, a rectangular plate parallel to the connecting frame 42 is fixed on one side, away from the arc spring 45, of the bearing plate 44, and waist holes (not shown in the figure) are formed in the rectangular plate in a penetrating mode from front to back so that the bearing rod 47 is driven to move outwards when the connecting frame 42 swings;

as shown in fig. 3: the vertical activity in the waist hole is provided with the loose axle of looks adaptation, and the loose axle vertical fixation sets up one end in adapting rod 47, the assembly mouth has been seted up to adapting rod 47's outer end, U-shaped frame 41 bottom central authorities are fixed with sleeve 46 through the support, and sleeve 46 inner chamber middle part is fixed with inserts (not shown in the figure), the relative one end of adapting rod 47 of left and right sides activity respectively runs through sleeve 46 left and right sides, the relative one end of adapting rod 47 of left and right sides all is provided with reset spring, and the reset spring other end is fixed with inserts, thereby make adapting rod 47 outside lateral shifting pulling reset spring during the link 42 swing, thereby realize further unmanned aerial vehicle main part 1 and fall to the ground the vibrations power buffering.

The rest of the structure is the same as in example 1.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.

Claims

1. An unmanned aerial vehicle for full path planning and capture, its characterized in that: comprises the steps of (a) preparing a mixture of a plurality of raw materials,

the unmanned aerial vehicle comprises an unmanned aerial vehicle main body (1), wherein an electric device (2) is arranged at the bottom of the unmanned aerial vehicle main body (1);

the rain-proof anti-collision assembly (3) comprises an installation rod (32) detachably fixed in the center of the top of the unmanned aerial vehicle main body (1), a top seat (33) is fixed to the top of the installation rod (32), a side ring (39) is sleeved on the outer side of the top seat (33), the side ring (39) is located below the top seat (33), multiple groups of reinforcing rods (34) are arranged between the top of the outer wall of the top seat (33) and the top of the side ring (39) in an annular array mode, and a waterproof breathable film (35) is arranged between every two adjacent groups of reinforcing rods (34);

fall to the ground subassembly (4), fall to the ground subassembly (4) and set up in unmanned aerial vehicle main part (1) bottom.

2. A drone for full path planning and capture according to claim 1, characterised in that: fixed cover of side ring (39) outer wall is equipped with anticollision elastic ring (36), and anticollision elastic ring (36) outer wall annular array integrated into one piece has multiunit elastic bulge, side ring (39) bottom outer wall annular array has multiunit curved curb plate (37), curb plate (37) and the wing one-to-one of unmanned aerial vehicle main part (1), curb plate (37) outer wall has curved elastic contact board (38) through multiunit spring coupling.

3. A drone for full path planning and capture according to claim 2, characterised in that: unmanned aerial vehicle main part (1) top central authorities are fixed with mount pad (31), and install pole (32) activity and insert and establish in mount pad (31), the equal screw thread of front and back side of mount pad (31) is inserted and is equipped with the screw thread round pin, the both sides outer wall bottom of mount pad (32) all seted up with screw thread round pin complex screw hole.

4. A drone for full path planning and capture according to claim 3, characterised in that: the ground component (4) comprises a U-shaped frame (41) fixed to the bottom of the unmanned aerial vehicle main body (1), the left end and the right end of the front side and the rear side of the U-shaped frame (41) are symmetrically rotated and inclined to form connecting frames (42), and one ends, far away from the U-shaped frame (41), of the connecting frames (42) are provided with contact wheels (43) in a rotating mode through shaft bodies.

5. A drone for full path planning and capture according to claim 4, characterised in that: front and back side link span (42) top is connected with jointly and accepts board (44), and accepts and is provided with between board (44) and U-shaped frame (41) bottom curved spring (45), it is fixed with the rectangular plate parallel with link span (42) to accept one side that curved spring (45) were kept away from in board (44), and runs through around on the rectangular plate and seted up the waist hole.

6. A drone for full path planning and capture according to claim 5, characterised in that: the vertical activity in the waist hole is provided with the loose axle of looks adaptation, and the vertical fixed one end that sets up in adapting rod (47) of loose axle, U-shaped frame (41) bottom central authorities are fixed with sleeve (46) through the support, and sleeve (46) inner chamber middle part is fixed with inserts, controls the side the relative one end of adapting rod (47) activity respectively runs through sleeve (46) left and right sides, controls the side the relative one end of adapting rod (47) all is provided with reset spring, and the reset spring other end with insert fixedly.