CN209814286U

CN209814286U - Removable unmanned aerial vehicle spray lance structure

Info

Publication number: CN209814286U
Application number: CN201920627683.1U
Authority: CN
Inventors: 杨丁
Original assignee: Shandong Zhongxiang Intelligent Technology Co Ltd
Current assignee: Shandong Zhongxiang Intelligent Technology Co Ltd
Priority date: 2019-05-05
Filing date: 2019-05-05
Publication date: 2019-12-20
Anticipated expiration: 2029-05-05

Abstract

The utility model provides a detachable unmanned aerial vehicle spray lance structure, which comprises a mounting seat, an elastic belt and a fixed seat, wherein the fixed seat and the mounting seat are oppositely arranged and are all fixed on a wing, the starting end of the elastic belt is hinged on the mounting seat, and the tail end of the elastic belt is fixedly connected with a metal sleeve; the fixing seat forms a slot and an opening which are communicated with each other, the metal sleeve is inserted into the slot, and the elastic band extends out of the slot from the opening. The detachable unmanned aerial vehicle spray lance structure of the utility model is spliced by the metal sleeve, so that the spray lance is held by the elastic band, and the splicing mode is convenient to detach and install; meanwhile, the diameter of the spray rod can be changed due to the elasticity of the elastic band.

Description

Removable unmanned aerial vehicle spray lance structure

Technical Field

The utility model belongs to the unmanned aerial vehicle field especially relates to a removable unmanned aerial vehicle spray lance structure.

Background

An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", 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.

The existing unmanned aerial vehicle water tank is hung at the bottom of the body through a support, and the spray rod is fixed at the bottom of the wing through a hoop, so that the spray rod is difficult to detach and replace.

SUMMERY OF THE UTILITY MODEL

In view of this, the utility model aims at providing a removable unmanned aerial vehicle spray lance structure to the spray lance is changed in the dismantlement.

In order to achieve the above purpose, the technical scheme of the utility model is realized like this:

a detachable unmanned aerial vehicle spray lance structure comprises a mounting seat, an elastic belt and a fixed seat, wherein the fixed seat and the mounting seat are oppositely arranged and are fixed on wings, the starting end of the elastic belt is hinged to the mounting seat, and the tail end of the elastic belt is fixedly connected with a metal sleeve; the fixing seat forms a slot and an opening which are communicated with each other, the metal sleeve is inserted into the slot, and the elastic band extends out of the slot from the opening.

Furthermore, the installation seat comprises a bottom rod, the starting end of the elastic band is bent around the bottom rod and sewn with the starting end of the elastic band to form a sleeve ring part, and the sleeve ring part is sleeved on the bottom rod and rotates around the bottom rod.

Furthermore, the two sides of the bottom rod are bent to form side rods, the two side rods are arranged oppositely, and the tail ends of the two side rods are fixedly connected to the wings.

Further, the fixed seat comprises an inner plate and an outer plate which are parallel to each other; the upper ends of the inner plate and the outer plate horizontally extend to the space between the inner plate and the outer plate to form a flanging; the opening is located between two flanges, and the slot is located between the inner plate, the outer plate and the flanges.

Furthermore, the adjacent surfaces of the inner plate and the outer plate are bonded with rubber layers, and the rubber layers are pressed to generate elastic deformation along with the insertion of the metal sleeve into the slot.

Furthermore, the inner plate and the outer plate are provided with symmetrical through holes, positioning pins which penetrate through the metal sleeve are inserted in the through holes, strong magnets are adhered to one side, far away from the outer plate, of the inner plate, and the strong magnets adsorb the positioning pins.

Furthermore, the metal sleeve is rectangular, an inlet is formed in one side end face of the metal sleeve, the tail end of the elastic band is inserted into the metal sleeve from the inlet, and the metal sleeve is riveted with the elastic band.

Compared with the prior art, removable unmanned aerial vehicle spray lance structure have following advantage:

the detachable unmanned aerial vehicle spray lance structure of the utility model is spliced by the metal sleeve, so that the spray lance is held by the elastic band, and the splicing mode is convenient to detach and install; meanwhile, the diameter of the spray rod can be changed due to the elasticity of the elastic band.

Drawings

The accompanying drawings, which form a part hereof, are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the invention without undue limitation. In the drawings:

fig. 1 is the embodiment of the utility model provides a removable unmanned aerial vehicle spray lance structure schematic diagram.

Description of reference numerals:

1. a mounting seat; 11. a bottom bar; 12. a side lever; 2. an elastic band; 21. a collar portion; 22. a metal sheath; 3. a fixed seat; 31. an inner plate; 32. an outer plate; 33. flanging; 4. a rubber layer; 5. positioning pins; 7. a strong magnet.

Detailed Description

It should be noted that, in the present invention, the embodiments and features of the embodiments may be combined with each other without conflict.

In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are used merely for convenience of description and for simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention. Furthermore, the terms "first", "second", etc. are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first," "second," etc. may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless otherwise specified.

In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be, for example, 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 meaning of the above terms in the present invention can be understood by those of ordinary skill in the art through specific situations.

The present invention will be described in detail below with reference to the accompanying drawings in conjunction with embodiments.

A removable unmanned aerial vehicle spray lance structure, includes mount pad 1, elastic webbing 2 and fixing base 3.

The mounting base 1 is fixed on the wing, as shown in fig. 1, the mounting base 1 includes a bottom bar 11, side bars 12 are formed by bending two sides of the bottom bar 11, the two side bars 12 are arranged oppositely, and the tail ends of the two side bars 12 are fixedly connected to the wing. The starting end of the elastic band 2 is bent around the bottom rod 11 and sewn with the starting end to form a sleeve ring part 21, the sleeve ring part 21 is sleeved on the bottom rod 11 and rotates around the bottom rod 11, and therefore the starting end of the elastic band 2 is hinged to the mounting base 1.

The fixed seat 3 is arranged opposite to the mounting seat 1 and fixedly connected to the other side of the wing. The fixed seat 3 comprises an inner plate 31 and an outer plate 32 which are parallel to each other; the upper ends of the inner plate 31 and the outer plate 32 extend horizontally therebetween, and are formed with beads 33. An opening is formed between the two flanges 33, and a slot is defined by the inner plate 31, the outer plate 32 and the flanges 33 and is communicated with the opening. The end of the elastic band 2 is fixedly connected with a metal sleeve 22. The metal sleeve 22 is rectangular and has an entrance formed on one end face, the end of the elastic band 2 is inserted into the metal sleeve 22 through the entrance, and the metal sleeve 22 is riveted with the elastic band 2. The metal sleeve 22 is inserted into the slot and the elastic band 2 is extended out of the slot from the opening.

In order to prevent the metal sleeve 22 from being removed from the slot, the rubber layer 4 is adhered to the adjacent surfaces of the inner plate 31 and the outer plate 32, and the rubber layer 4 is elastically deformed when the metal sleeve 22 is inserted into the slot. The inner plate 31 and the outer plate 32 are provided with symmetrical through holes at two sides of the rivet, positioning pins 5 penetrating through the metal sleeve 22 are inserted in the through holes, a strong magnet 7 is adhered to one side of the inner plate 31 far away from the outer plate 32, and the strong magnet adsorbs the positioning pins 5.

The above description is only a preferred embodiment of the present invention, and should not be taken as limiting the invention, and any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. The utility model provides a removable unmanned aerial vehicle spray lance structure, includes mount pad (1), elastic band (2) and fixing base (3), fixing base (3) set up and all fix on the wing with mount pad (1) relatively, its characterized in that: the starting end of the elastic band (2) is hinged with the mounting seat (1), and the tail end of the elastic band (2) is fixedly connected with a metal sleeve (22); the fixing seat (3) forms a slot and an opening which are communicated with each other, the metal sleeve (22) is inserted into the slot, and the elastic band (2) extends out of the slot from the opening.

2. The removable unmanned aerial vehicle boom structure of claim 1, wherein: the mounting seat (1) comprises a bottom rod (11), the starting end of the elastic band (2) is bent around the bottom rod (11) and sewn with the elastic band to form a sleeve ring part (21), and the sleeve ring part (21) is sleeved on the bottom rod (11) and rotates around the bottom rod (11).

3. The removable unmanned aerial vehicle boom structure of claim 2, wherein: two sides of the bottom rod (11) are bent to form side rods (12), the side rods (12) are arranged oppositely, and the tail ends of the side rods (12) are fixedly connected to the wings.

4. The removable unmanned aerial vehicle boom structure of claim 1, wherein: the fixed seat (3) comprises an inner plate (31) and an outer plate (32) which are parallel to each other; the upper ends of the inner plate (31) and the outer plate (32) horizontally extend to the space between the upper ends and the outer plate to form a flanging (33); the opening is positioned between the two flanges (33), and the slot is positioned between the inner plate (31), the outer plate (32) and the flanges (33).

5. The removable unmanned aerial vehicle boom structure of claim 4, wherein: the adjacent surfaces of the inner plate (31) and the outer plate (32) are adhered with rubber layers (4), and the rubber layers (4) are pressed to generate elastic deformation along with the insertion of the metal sleeve (22) into the slot.

6. The removable unmanned aerial vehicle boom structure of claim 4, wherein: the inner plate (31) and the outer plate (32) are provided with symmetrical through holes, positioning pins (5) which simultaneously penetrate through the metal sleeve (22) are inserted in the through holes, a strong magnet (7) is adhered to one side of the inner plate (31) far away from the outer plate (32), and the strong magnet adsorbs the positioning pins (5).

7. The removable unmanned aerial vehicle boom structure of claim 1, wherein: the metal sleeve (22) is rectangular, an inlet is formed in one side end face, the tail end of the elastic band (2) is inserted into the metal sleeve (22) from the inlet, and the metal sleeve (22) is riveted with the elastic band (2).