CN216397395U

CN216397395U - Unmanned aerial vehicle for high-altitude deicing

Info

Publication number: CN216397395U
Application number: CN202121577811.XU
Authority: CN
Inventors: 赵雯
Original assignee: Individual
Current assignee: Hubei Warring Wolf Airlines Co ltd
Priority date: 2021-07-13
Filing date: 2021-07-13
Publication date: 2022-04-29
Anticipated expiration: 2031-07-13

Abstract

The utility model discloses an unmanned aerial vehicle for high-altitude deicing, which belongs to the field of unmanned aerial vehicles and comprises a body, wherein the body comprises a base, a rectangular groove is fixedly connected in the middle of the base, a first motor is fixedly installed at the rear end of the rectangular groove, a T-shaped groove is formed at the lower end of the rectangular groove, buckle grooves are formed in the left and right parts of the front end of the rectangular groove, cross rods are respectively and fixedly connected with the left and right ends of the body, one end, away from the body, of each cross rod is fixedly connected with a flying device, an L-shaped rod is fixedly connected in the middle of the flying device, a sheath is fixedly connected at the upper end of each L-shaped rod, and a limiting device is fixedly installed at the output end of each motor. The safety problem caused by high-altitude ice blocks is reduced.

Description

Unmanned aerial vehicle for high-altitude deicing

Technical Field

The utility model relates to the field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle for high-altitude deicing.

Background

An unmanned aircraft, referred to as "drone", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft.

Icing in high altitude often is a very dangerous natural phenomenon, when the icicle that produces drops, causes the bad things such as personnel's injury very easily, and unmanned aerial vehicle also has very extensive application in the aspect of deicing in high altitude.

Traditional unmanned aerial vehicle can only carry out simple article transportation work on the market, and when needs carried out the high altitude deicing, ordinary unmanned aerial vehicle just can't satisfy the condition, causes the high altitude deicing difficulty, appears the safety problem easily.

SUMMERY OF THE UTILITY MODEL

1. Technical problem to be solved

Aiming at the problems in the prior art, the utility model aims to provide an unmanned aerial vehicle for high-altitude deicing, which is characterized in that impact crushing of an impact rod on a high-altitude ice block and limit pulling of a limiting device on the impact rod are realized, so that impact crushing work of the impact rod on the ice block is realized, a high-altitude deicing task of the unmanned aerial vehicle is completed, and safety problems caused by the high-altitude ice block are reduced.

2. Technical scheme

In order to solve the above problems, the present invention adopts the following technical solutions.

An unmanned aerial vehicle for high-altitude deicing comprises a body, wherein the body comprises a base, a rectangular groove is fixedly connected in the middle of the base, a first motor is fixedly installed at the rear end of the rectangular groove, a T-shaped groove is formed at the lower end of the rectangular groove, buckling grooves are formed in the left and right parts of the front end of the T-shaped groove, a cross rod is fixedly connected at the left and right ends of the body, a flying device is fixedly connected at one end of the cross rod away from the body, an L-shaped rod is fixedly connected in the middle of the flying device, a sheath is fixedly connected at the upper end of the L-shaped rod, a limiting device is fixedly installed at the output end of the motor, a T-shaped sliding block is slidably connected in the middle of the T-shaped groove, an impact rod is fixed at the upper end of the T-shaped sliding block, a limiting groove is formed in the middle of the impact rod, linkage rods are fixedly connected in the left and right parts of the front end of the body, and a cylindrical rod is rotatably connected in the middle of the linkage rods, the middle part of the cylindrical rod is fixedly connected with an elastic rope.

Furthermore, stop device includes the tray, tray upper end fixedly connected with second motor, second motor output end fixedly connected with push rod, tray front end middle part fixedly connected with dwang, the dwang outer end is rotated and is connected with the buckle piece for stop device can carry out spacing portable to the impact rod.

Furthermore, the front end of the push rod limits the upper end of the clamping block, and the lower end of the clamping block is clamped in the middle of the limiting groove, so that the clamping block can control the movement and emission of the impact rod.

Furthermore, the front end of the impact rod is fixedly connected with a punch, and the punch is conical in shape, so that the impact rod can effectively impact and crush the high-altitude ice blocks.

Furthermore, the middle part of the elastic rope is connected with the middle part of the impact rod in a clamped mode, and the elastic rope is made of high-elasticity rubber, so that the impact rod can be popped up by the elastic rope, and the elastic rope cannot be damaged by stress.

Further, the sheath is located simultaneous high with the flying device, and the diameter of sheath is five centimetres for unmanned aerial vehicle flight in-process prevents the striking damage.

3. Advantageous effects

Compared with the prior art, the utility model has the advantages that:

(1) this scheme is broken through the impact of impact rod to the high altitude ice-cube to and stop device is to the spacing pulling of impact rod, thereby realize impacting the broken work of impact rod to the ice-cube, thereby accomplish unmanned aerial vehicle's high altitude deicing task, reduce the safety problem that the high altitude ice-cube produced.

(2) Stop device includes the tray, tray upper end fixedly connected with second motor, and second motor output end fixedly connected with push rod, tray front end middle part fixedly connected with dwang, dwang outer end rotate be connected with the buckle piece for stop device can carry out spacing portable to the impact pole.

(3) The front end of the push rod limits the upper end of the clamping block, and the lower end of the clamping block is clamped in the middle of the limiting groove, so that the clamping block can control the movement and emission of the impact rod.

(4) The front end of the impact rod is fixedly connected with a punch, and the punch is conical in shape, so that the impact rod can effectively impact and crush the high-altitude ice blocks.

(5) The middle part of the elastic rope is clamped with the middle part of the impact rod, and the elastic rope is made of high-elasticity rubber, so that the impact rod can be popped up by the elastic rope, and the elastic rope cannot be damaged by stress.

(6) The sheath is located simultaneous high with the flying device, and the diameter of sheath is five centimetres for unmanned aerial vehicle flight in-process prevents the striking damage.

Drawings

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

FIG. 2 is a schematic side view of the present invention;

FIG. 3 is a schematic illustration of the fuselage structure of the present invention;

FIG. 4 is a partial schematic structural view of the present invention;

fig. 5 is a schematic structural view of the limiting device of the present invention.

The reference numbers in the figures illustrate:

1. a body; 101. a base; 102. a rectangular groove; 103. a first motor; 104. a T-shaped groove; 105. a snap groove; 2. a cross bar; 3. a flying device; 4. an L-shaped rod; 5. a sheath; 6. a limiting device; 601. a support block; 602. a second motor; 603. a push rod; 604. rotating the rod; 605. a buckling block; 7. a T-shaped slider; 8. an impact bar; 9. a limiting groove; 10. a linkage rod; 11. a cylindrical rod; 12. an elastic rope.

Detailed Description

The technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention; it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all embodiments, and all other embodiments obtained by those skilled in the art without any inventive work are within the scope of the present invention.

In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "top/bottom", and the like indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the referred device or element must have a specific orientation, be constructed in a specific orientation, and be operated, and thus should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.

In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "sleeved/connected," "connected," and the like are to be construed broadly, e.g., "connected," which may be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.

Example 1:

referring to fig. 1-4, an unmanned aerial vehicle for high-altitude deicing comprises a body 1, the body 1 comprises a base 101, a rectangular groove 102 is fixedly connected to the middle of the base 101, a first motor 103 is fixedly installed at the rear end of the rectangular groove 102, a T-shaped groove 104 is formed at the lower end of the rectangular groove 102, a buckle groove 105 is formed at the left and right portions of the front end of the T-shaped groove 104, a cross rod 2 is fixedly connected to the left and right ends of the body 1, a flying device 3 is fixedly connected to one end of the cross rod 2 away from the body 1, an L-shaped rod 4 is fixedly connected to the middle of the flying device 3, a sheath 5 is fixedly connected to the upper end of the L-shaped rod 4, a limiting device 6 is fixedly installed at the output end of the motor 103, a T-shaped slider 7 is slidably connected to the middle of the T-shaped groove 104, an impact rod 8 is fixed to the upper end of the T-shaped slider 7, a limiting groove 9 is formed at the middle of the impact rod 8, and a linkage rod 10 is fixedly connected to the left and right portions of the front end of the body 1, the middle part of the linkage rod 10 is rotatably connected with a cylindrical rod 11, and the middle part of the cylindrical rod 11 is fixedly connected with an elastic rope 12.

Referring to fig. 1-2, the limiting device 6 includes a supporting block 601, a second motor 602 is fixedly connected to an upper end of the supporting block 601, a push rod 603 is fixedly connected to an output end of the second motor 602, a rotating rod 604 is fixedly connected to a middle portion of a front end of the supporting block 601, and a fastening block 605 is rotatably connected to an outer end of the rotating rod 604, so that the limiting device can limit the impact rod movably. The front end of the push rod 603 limits the upper end of the buckling block 605, and the lower end of the buckling block 605 is clamped in the middle of the limiting groove 9, so that the buckling block can control the movement and the emission of the impact rod.

Referring to fig. 1-3, a punch is fixedly connected to the front end of the impact rod 8, and the punch is conical, so that the impact rod can effectively impact and crush the high-altitude ice blocks. The middle part of the elastic rope 12 is clamped with the middle part of the impact rod 8, and the elastic rope 12 is made of high-elasticity rubber, so that the impact rod can be popped up by the elastic rope, and the elastic rope cannot be damaged by stress. Sheath 5 and flying device 3 are located simultaneous height, and the diameter of sheath 5 is five centimetres for unmanned aerial vehicle flight in-process prevents the striking damage.

Referring to fig. 1-5, in use, the flying device 3 is opened, the unmanned aerial vehicle is remotely controlled to a proper position, the impact rod 8 is aligned to a position to be deiced, the second motor 602 is operated to withdraw the push rod 603, the buckling block 605 rotates around the rotating rod 604, the impact rod 8 is ejected out under the action of the elastic rope 12, the punch at the front end of the impact rod 8 impacts and breaks an ice block, the first motor 103 is operated to extend the limiting device 6, the buckling block 605 is clamped into the limiting groove 9, the second motor 602 is operated to extend the push rod 603, the buckling block 605 is limited, and finally the first motor 103 drives the limiting device 6 to withdraw, so that the impact rod 8 resets and the ice block breaking work is completed. The high-altitude ice removing device is characterized in that impact crushing of the impact rod 8 on high-altitude ice blocks and limiting pulling of the limiting device 6 on the impact rod 8 are achieved, so that impact crushing work of the impact rod 8 on the ice blocks is achieved, high-altitude ice removing tasks of the unmanned aerial vehicle are completed, and safety problems caused by the high-altitude ice blocks are reduced.

The foregoing is only a preferred embodiment of the present invention; the scope of the utility model is not limited thereto. Any person skilled in the art should be able to cover the technical scope of the present invention by equivalent or modified solutions and modifications within the technical scope of the present invention.

Claims

1. An unmanned aerial vehicle for high altitude deicing, includes fuselage (1), its characterized in that: the aircraft body (1) comprises a base (101), a rectangular groove (102) is fixedly connected to the middle of the base (101), a first motor (103) is fixedly mounted at the rear end of the rectangular groove (102), a T-shaped groove (104) is formed in the lower end of the rectangular groove (102), buckle grooves (105) are formed in the left and right portions of the front end of the T-shaped groove (104), transverse rods (2) are fixedly connected to the left and right portions of the aircraft body (1), a flying device (3) is fixedly connected to one end, far away from the aircraft body (1), of each transverse rod (2), an L-shaped rod (4) is fixedly connected to the middle of the flying device (3), a sheath (5) is fixedly connected to the upper end of each L-shaped rod (4), a limiting device (6) is fixedly mounted at the output end of the motor (103), a T-shaped sliding block (7) is slidably connected to the middle of the T-shaped groove (104), and an impact rod (8) is fixedly connected to the upper end of the T-shaped sliding block (7), the novel multifunctional impact machine is characterized in that a limiting groove (9) is formed in the middle of the impact rod (8), linkage rods (10) are fixedly connected to the left portion and the right portion of the front end of the machine body (1), a cylindrical rod (11) is rotatably connected to the middle of each linkage rod (10), and an elastic rope (12) is fixedly connected to the middle of each cylindrical rod (11).

2. A drone for deicing high altitude according to claim 1, characterized in that: stop device (6) are including tray (601), tray (601) upper end fixedly connected with second motor (602), second motor (602) output end fixedly connected with push rod (603), tray (601) front end middle part fixedly connected with dwang (604), dwang (604) outer end rotates and is connected with buckle piece (605).

3. A drone for deicing high altitude according to claim 2, characterized in that: the front end of the push rod (603) limits the upper end of the clamping block (605), and the lower end of the clamping block (605) is clamped in the middle of the limiting groove (9).

4. A drone for deicing high altitude according to claim 1, characterized in that: the front end of the impact rod (8) is fixedly connected with a punch, and the punch is conical.

5. A drone for deicing high altitude according to claim 1, characterized in that: the middle part of the elastic rope (12) is connected with the middle part of the impact rod (8) in a clamping mode, and the elastic rope (12) is made of high-elasticity rubber.

6. A drone for deicing high altitude according to claim 1, characterized in that: the sheath (5) and the flying device (3) are located at the same height, and the diameter of the sheath (5) is five centimeters.