CN211893669U - Multipurpose unmanned aerial vehicle's impact structure - Google Patents

Abstract

The utility model discloses a multipurpose unmanned aerial vehicle's structure of shocking resistance, including unmanned aerial vehicle, unmanned aerial vehicle's aircraft nose department is provided with the subassembly of shocking resistance, the subassembly bilateral symmetry of shocking resistance sets up, the subassembly of shocking resistance includes the anticollision board, be equipped with the portion of bending on the anticollision board, the portion of bending extends to the place ahead of unmanned aerial vehicle's aircraft nose, be equipped with a plurality of mounting holes in the portion of bending, the installation is fixed with anticollision piece in the mounting hole rotation, part protrusion in the portion of bending of anticollision piece, there is the space between anticollision piece and the aircraft nose, be provided with the connector in two anticollision pieces in the outside, insert anticollision piece in the connector, the one end that organism was kept away from to the anticollision piece is equipped with the elasticity plectrum, be equipped. The utility model discloses stable in structure, unmanned aerial vehicle's nose portion shock resistance is good, can block the isolation to aerial floater, and is not fragile, and life is longer.

Description

Multipurpose unmanned aerial vehicle's impact structure

Technical Field

The utility model relates to an unmanned aerial vehicle field, concretely relates to multipurpose unmanned aerial vehicle's structure of shocking resistance.

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. Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.

At present, unmanned aerial vehicle often has multiple use, for example shoot, transportation etc. and current unmanned aerial vehicle effect of shocking resistance is poor, and aircraft nose department strikes the damage easily.

Disclosure of Invention

The utility model aims to solve the technical problem that a multipurpose unmanned aerial vehicle's that can solve above-mentioned problem shock-resistant structure is difficult for receiving the striking and damages, and life is longer.

The utility model discloses a realize through following technical scheme: the utility model provides a multipurpose unmanned aerial vehicle's impact structure that shocks resistance, including unmanned aerial vehicle, unmanned aerial vehicle's aircraft nose department is provided with the subassembly that shocks resistance, the subassembly that shocks resistance bilateral symmetry is called the setting, the subassembly that shocks resistance includes the anticollision board, be equipped with the portion of bending on the anticollision board, the portion of bending extends to the place ahead of unmanned aerial vehicle's aircraft nose, be equipped with a plurality of mounting holes in the portion of bending, the installation is fixed with anticollision piece in the mounting hole rotation, part protrusion in the portion of bending of anticollision piece, there is the space between anticollision piece and the aircraft nose, be provided with the connector in two anticollision pieces in the outside, insert anticollision piece in the connector, the one end that organism was kept away from to the anticollision piece is equipped with the elasticity plectrum, be equipped with a portion of reducing between anticollision piece and the elasticity plectrum, the inside cavity of portion.

As the preferred technical scheme, a bearing is fixedly arranged in the mounting hole, the bearing is a light bearing and is positioned in the mounting hole, an annular clamping groove is formed in an outer ring of the bearing, the bending part is inserted into the annular clamping groove to be fixed, the anti-collision block is arranged in a shaft hole of the bearing, and the anti-collision block and the bearing are fixed mutually.

Preferably, the anti-collision plate and the anti-collision block are made of rubber.

As the preferred technical scheme, a buffer cavity is arranged in the anti-collision block, buffer substances are stored in the buffer cavity, and the buffer cavity is not communicated with the connecting port.

As a preferred technical scheme, the thinning portion and the elastic shifting piece are of an integrated structure, one side of the thinning portion is provided with an inserting groove, and one end of the anti-collision piece is inserted into the inserting groove to be fixed.

The utility model has the advantages that: the utility model discloses stable in structure, unmanned aerial vehicle's nose portion shock resistance is good, can block the isolation to aerial floater, and is not fragile, and life is longer.

Drawings

In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.

Fig. 1 is a top view of the present invention;

FIG. 2 is a partial view of the bending part of the present invention;

fig. 3 is an enlarged view of the connection between the anti-collision plate and the elastic shifting piece of the present invention.

Detailed Description

All of the features disclosed in this specification, or all of the steps in any method or process so disclosed, may be combined in any combination, except combinations of features and/or steps that are mutually exclusive.

Any feature disclosed in this specification (including any accompanying claims, abstract and drawings), may be replaced by alternative features serving equivalent or similar purposes, unless expressly stated otherwise. That is, unless expressly stated otherwise, each feature is only an example of a generic series of equivalent or similar features.

In the description of the present invention, it is to be understood that the terms "one end", "the other end", "the outside", "upper", "inside", "horizontal", "coaxial", "central", "end", "length", "outer end", etc. indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element 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, in the description of the present invention, "a plurality" means at least two, e.g., two, three, etc., unless specifically limited otherwise.

The use of terms herein such as "upper," "above," "lower," "below," and the like in describing relative spatial positions is for the purpose of facilitating description to describe one element or feature's relationship to another element or feature as illustrated in the figures. The spatially relative positional terms may be intended to encompass different orientations of the device in use or operation in addition to the orientation depicted in the figures. For example, if the device in the figures is turned over, elements described as "below" or "beneath" other elements or features would then be oriented "above" the other elements or features. Thus, the exemplary term "below" can encompass both an orientation of above and below. The device may be otherwise oriented (rotated 90 degrees or at other orientations) and the spatially relative descriptors used herein interpreted accordingly.

In the present invention, unless otherwise explicitly specified or limited, the terms "set", "coupled", "connected", "penetrating", "plugging", and the like are to be understood in a broad sense, and may be, for example, fixedly connected, detachably connected, or integrated; can be mechanically or electrically connected; they may be directly connected or indirectly connected through intervening media, or they may be connected internally or in any other suitable relationship, unless expressly stated otherwise. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.

As shown in fig. 1 to 3, including unmanned aerial vehicle, 1 department of unmanned aerial vehicle's aircraft nose is provided with the subassembly of shocking resistance, and the subassembly bilateral symmetry that shocks resistance sets up, does benefit to unmanned aerial vehicle's steady operation: the subassembly of shocking resistance includes anticollision board 2, anticollision board 2 is last to be equipped with the portion 211 of bending, the portion 211 of bending extends to unmanned aerial vehicle's aircraft nose 1 the place ahead, the portion of bending does not shelter from the place ahead of aircraft nose completely, be equipped with a plurality of mounting holes on the portion 211 of bending, anticollision piece 3 is installed in the mounting hole rotation, anticollision piece 3's part protrusion is in the portion 211 of bending, there is the space between anticollision piece 3 and the aircraft nose 1, be provided with the connector in two anticollision pieces 3 in the outside, insert anticollision piece 5 in the connector, the one end that the organism was kept away from to anticollision piece 5 is equipped with elasticity plectrum 6, be equipped with one between anticollision piece 5 and the elasticity plectrum 6 and subtract thin portion 7, subtract the inside cavity of thin portion 7, the inside helium 16 of thin portion 7 that subtracts, the surface of elasticity plectrum 6 is equipped with.

Wherein, the installation is fixed with bearing 9 in the mounting hole, and bearing 9 is light bearing 9, for example plastics make, and is lighter, and bearing 9 is located the mounting hole, is equipped with the ring groove on the outer loop of bearing 9, and the part of portion 211 of bending inserts to ring groove internal fixation, and anticollision piece 3 sets up in the shaft hole of bearing 9, and is fixed mutually between anticollision piece 3 and the bearing 9.

Wherein, the anti-collision plate 2 and the anti-collision block 3 are made of rubber.

Wherein, be equipped with the cushion chamber in the anticollision piece 3, buffer substance 11 is stored in the cushion chamber, for example helium, and the cushion chamber does not lead to with the connector.

The thickness reducing portion 7 and the elastic shifting piece 6 are of an integrated structure, one side of the thickness reducing portion 7 is provided with a slot, and one end of the anti-collision piece 5 is inserted into the slot and fixed.

Wherein, the bearing, the anti-collision block, the anti-collision plate, the elastic shifting piece and the anti-collision piece can be fixed by strong waterproof glue.

The working principle is as follows: when the device is used, the impact-resistant protection of the head part of the whole device is realized through the impact-resistant component.

Anticollision board and the portion of bending are made by rubber for the anticollision parcel of device both sides and strong side, store the anticollision piece that has the helium and play a buffer protection's effect when taking place the striking, connect between anticollision piece and the bearing, the inner ring of bearing rotates, anticollision piece also can rotate under the drive of inner ring, under strong wind day, pivoted anticollision piece can block the air current, has promoted the wind resistance of device, makes the operation more stable.

This device is when using, the anticollision piece is that the metal is made, be used for promoting structural strength, anticollision piece and elasticity plectrum are connected, there is the portion of reducing thickness between the two, when unmanned aerial vehicle operation, the air current is used in the elasticity plectrum, make the elasticity plectrum can deal with the swing, the contact surface of elasticity plectrum with the external world has been increased, the contact of flexible adsorbed layer has also been increased, be convenient for flexible adsorbed layer adsorbs dust and steam, make dust and steam obtain keeping apart, flexible adsorbed layer also can play an anticollision effect simultaneously.

The above description is only for the specific embodiments of the present invention, but the scope of the present invention is not limited thereto, and any changes or substitutions that are not thought of through the creative work should be covered within the scope of the present invention. Therefore, the protection scope of the present invention should be subject to the protection scope defined by the claims.

Claims (5)

1. The utility model provides a multipurpose unmanned aerial vehicle's impact structure, includes unmanned aerial vehicle, and unmanned aerial vehicle's aircraft nose (1) department is provided with the subassembly that shocks resistance, and the subassembly bilateral symmetry that shocks resistance sets up its characterized in that: the utility model discloses an unmanned aerial vehicle, including anti-collision plate (2), be equipped with portion of bending (211) on anti-collision plate (2), portion of bending (211) extends to the place ahead of unmanned aerial vehicle's aircraft nose (1), be equipped with a plurality of mounting holes on portion of bending (211), anti-collision piece (3) are installed in the mounting hole rotation, the part protrusion of anti-collision piece (3) is in portion of bending (211), there is the space between anti-collision piece (3) and aircraft nose (1), be provided with the connector in two anti-collision pieces (3) in the outside, insert anti-collision piece (5) in the connector, the one end that organism was kept away from in anti-collision piece (5) is equipped with elasticity plectrum (6), be equipped with one between anti-collision piece (5) and elasticity plectrum (6) and subtract thin portion (7), the inside cavity in portion of subtracting thin (7), it has gas to subtract thin portion (7) inside storage, the surface of elasticity.

2. The impact-resistant structure of multipurpose unmanned aerial vehicle of claim 1, characterized in that: the bearing (9) is fixedly arranged in the mounting hole, the bearing (9) is a light bearing (9), the bearing (9) is positioned in the mounting hole, an annular clamping groove is formed in an outer ring of the bearing (9), the bending part (211) is inserted into the annular clamping groove to be fixed, the anti-collision block (3) is arranged in a shaft hole of the bearing (9), and the anti-collision block (3) and the bearing (9) are fixed mutually.

3. The impact-resistant structure of multipurpose unmanned aerial vehicle of claim 1, characterized in that: the anti-collision plate (2) and the anti-collision block (3) are made of rubber.

4. The impact-resistant structure of multipurpose unmanned aerial vehicle of claim 1, characterized in that: a buffer cavity is arranged in the anti-collision block (3), buffer substances (11) are stored in the buffer cavity, and the buffer cavity is not communicated with the connecting port.

5. The impact-resistant structure of multipurpose unmanned aerial vehicle of claim 1, characterized in that: the thickness reducing part (7) and the elastic shifting piece (6) are of an integrated structure, one side of the thickness reducing part (7) is provided with an inserting groove, and one end of the anti-collision piece (5) is inserted into the inserting groove to be fixed.

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