CN214216154U - Unmanned aerial vehicle mounting structure - Google Patents

Abstract

The utility model provides an unmanned aerial vehicle carries structure belongs to unmanned air vehicle technical field. It has solved the inconvenient and heavy problem of weight of current unmanned aerial vehicle carry structure dismouting battery. This unmanned aerial vehicle carries structure includes the support plate, support plate one end integrated into one piece has a plurality of dogs that can supply the battery to lean on, set up on the dog and supply battery male slot, integrated into one piece has a plurality of can prevent the spacing arch of battery displacement on the support plate face, install the clamp plate on the support plate, the clamp plate can compress tightly the battery and through fastener demountable installation on the support plate, a plurality of lightening holes that are the bar are seted up to the support plate both sides, a plurality of louvres one that are the bar and a plurality of circular shape louvre two are seted up at the middle part of support plate. This unmanned aerial vehicle carries simple structure, lightweight more, dismouting battery are more convenient.

Description

Unmanned aerial vehicle mounting structure

Technical Field

The utility model belongs to the technical field of unmanned aerial vehicle, a unmanned aerial vehicle carry structure is related to.

Background

Unmanned aerial vehicles, known as pilotless aircraft, are unmanned aircraft operated by radio remote control devices and self-contained program control devices. The machine has no cockpit, but is provided with an automatic pilot, a program control device and other equipment. The personnel on the ground, the naval vessel or the mother aircraft remote control station can track, position, remotely control, telemeter and digitally transmit the personnel through equipment such as a radar. The aircraft can take off like a common airplane under the radio remote control or launch and lift off by a boosting rocket, and can also be thrown into the air by a mother aircraft for flying. During recovery, the aircraft can land automatically in the same way as the common aircraft landing process, and can also be recovered by a parachute or a barrier net for remote control. Can be repeatedly used for many times. The method is widely used for aerial reconnaissance, monitoring, communication, anti-submergence, electronic interference and the like.

Along with unmanned aerial vehicle technique is ripe gradually, manufacturing cost reduces with getting into the threshold, and unmanned aerial vehicle has begun civilization, and current civilian many rotor unmanned aerial vehicle of civilian generally divide into three kinds of power modes: pure electronic, oil moves and hybrid, pure oil moves unmanned aerial vehicle and can install the engine on the fuselage, make it turn into kinetic energy with chemical energy, guarantee unmanned aerial vehicle's rising and falling and flight, pure electronic unmanned aerial vehicle can install the lithium cell on the fuselage, through electric energy conversion for kinetic energy, guarantee unmanned aerial vehicle's rising and falling and flight, and hybrid's unmanned aerial vehicle has both installed the engine on the fuselage, install the lithium cell again, can enough use petrol as the power energy, by can using the electric energy as the energy, unmanned aerial vehicle's continuation of the journey performance is higher has been guaranteed.

Aiming at the hybrid power unmanned aerial vehicle, because the engine is arranged on the vehicle body as the main power source, and the battery is arranged on the vehicle body as the auxiliary power source, but the battery can not provide energy permanently, when the energy in the battery is used up, the battery needs to be disassembled for replacement, the battery has various installation modes in the prior art, one of the installation modes is that the mounting structure is arranged on the battery body, the mounting structure and the battery are integrated, the vehicle body is provided with the loading plate, the loading plate is clamped and fixed with the mounting structure through the loading plate, the detachable installation of the battery is ensured, but the installation mode has very high requirement on the whole design space of the unmanned aerial vehicle, and the design structure of the mounting structure is complex, the weight of the aircraft is increased, so that the endurance loss of the aircraft is caused, besides, the installation mode of the battery can also be fixed through a ribbon, the arrangement mode also comprises a support plate, the surface of the support plate is provided with a magic tape and a ribbon, the outer wall of one side of the battery is also provided with the magic tape, the support plate and the battery are fastened and fixed through the ribbon on the support plate after being fastened and fixed through the magic tape, although the fastening is simple, the fixing effect of the magic tape and the ribbon cannot ensure that the battery is firm in the vibration process because the unmanned aerial vehicle cannot avoid vibration in the operation process, and the battery is likely to lose efficacy due to the matching between the magic tape and the ribbon, so that the battery falls off; in addition, because the battery is installed inside unmanned aerial vehicle, all be provided with spare part all around, no matter be the fixed mode of the cooperation ribbon is pasted to the joint of integral type carry structure or magic, all do not have sufficient space to supply people's hand to stretch into when the battery needs to be changed and carry out the dismouting to the battery, can only disassemble unmanned aerial vehicle from the extroversion and change, it is very inconvenient to change the battery.

Disclosure of Invention

The utility model discloses a there is above-mentioned problem to current technique, has proposed unmanned aerial vehicle carry structure, the utility model aims to solve the technical problem that: how to guarantee that the dismouting is convenient under the firm prerequisite of battery installation, and make unmanned aerial vehicle carry structure lightweight.

The purpose of the utility model can be realized by the following technical proposal: the utility model provides an unmanned aerial vehicle carries structure, is used for installing the support plate of battery including one side, its characterized in that, integrated into one piece has a plurality of dogs that can supply the battery to support to lean on the support plate, install the clamp plate on the support plate, the clamp plate can support with the battery and lean on and compress tightly the battery on the support plate through the fastener.

The unmanned aerial vehicle mounting structure comprises a support plate for mounting a battery, the battery is mounted on one side plate surface of the support plate, violent vibration can be generated in the operation process of the unmanned aerial vehicle, and the vibration can be transmitted to the carrier plate and then transmitted to the battery, but because the arrangement of the carrier plate can offset part of the vibration and ensure that the battery is installed more stably, a plurality of stop blocks are integrally formed on the carrier plate, when the battery is installed on the carrier plate, the battery can be abutted against the stop block to ensure that the battery is firmly arranged on the support plate, the support plate is provided with the pressing plate, the pressing plate is fixed on the support plate through the fastening piece, after the fastening piece is screwed and fixed, the pressing plate can tightly press the battery to prevent the battery from falling off in the operation process of the unmanned aerial vehicle, when the battery needs to be replaced, the user can take out the battery from the support plate only by unscrewing the fastener so that the battery is not compressed any more, and the disassembly and assembly are more convenient.

In foretell unmanned aerial vehicle carries structure, the support plate is the quadrilateral, dog integrated into one piece just is located both sides respectively in support plate one end, the clamp plate is rectangular form, just the clamp plate middle part is leaned on with the battery counterbalance, clamp plate both ends lateral wall pastes and screws up fixedly through the fastener with the support plate mutually.

The support plate is the quadrilateral, dog integrated into one piece is in the both sides of support plate one end, when leaning on with the battery counterbalance, the dog that is located support plate one end both sides leans on with the both sides of battery one end respectively counterbalance, it is more stable to guarantee that the battery is installed on the support plate, be long banding clamp plate and support through the surface of middle part with the battery and lean on, and the lateral wall at its both ends offsets with the support plate and leans on, when needs are fixed, constantly screw up through the fastener, make the clamp plate middle part compress tightly the battery, guarantee that the battery is firm to be installed on the support plate, when needs dismantle change battery, only need unscrew the fastener, clamp plate middle part limit no longer is in the state of compressing tightly, user of service alright with directly with the battery take out from the not integrated into one piece of support plate have the one end of dog can, the dismouting is more convenient.

In foretell unmanned aerial vehicle carry structure, the slot has been seted up to dog one end, battery one end can insert the slot and lean on with the slot inner wall counterbalance, integrated into one piece has a plurality of spacing archs on the side face that the battery was installed to the support plate, spacing arch is located the battery both sides.

The one end of dog is seted up and is supplied battery male slot, the slot can increase the area of contact between dog and the battery, it is more stable to guarantee that the battery is installed on the support plate, it has a plurality of spacing archs still integrated into one piece on one side face of battery is installed to the support plate, spacing protruding distribution is in the both sides of battery, spacing arch can guarantee that the battery is installed after on the support plate, can not take place the skew in the direction of its both sides, the mounted position of battery has been injectd, it is more stable to guarantee to assemble.

In foretell unmanned aerial vehicle carries structure, the clamp plate both sides are turned over and are rolled over and form the turn-ups.

The two sides of the pressing plate are turned over to form flanges, the battery is mounted on the support plate and is dismounted in a drawing mode, the flanges formed by turning over the two sides of the pressing plate can play a role in guiding, and the battery cannot be blocked with the pressing plate in the mounting process.

In foretell unmanned aerial vehicle carry structure, a plurality of lightening holes that are the bar are seted up to the face both sides that the battery was installed to the support plate.

Set up the lightening hole that a plurality of is the bar on the both sides face of support plate, alleviateed the weight of support plate to a certain extent, guarantee more lightweight when guaranteeing support plate structural strength.

In the unmanned aerial vehicle mounting structure, the support plate is provided with a plurality of first strip-shaped heat dissipation holes and a plurality of second circular heat dissipation holes.

The support plate is provided with a plurality of first heat dissipation holes and second heat dissipation holes, the first heat dissipation holes are in a strip shape, the second heat dissipation holes are in a circular shape, when the battery is installed on the support plate and works for a long time, the battery can generate a large amount of heat, the battery can volatilize the heat through the first heat dissipation holes and the second heat dissipation holes, and the battery is prevented from being scrapped due to overheating.

In foretell unmanned aerial vehicle carries structure, support plate and clamp plate constitute by aluminum alloy material.

The clamp plate is all made through aluminum alloy material with the support plate, can guarantee this unmanned aerial vehicle carry structure firm while guarantee that unmanned aerial vehicle carry structure is more lightweight.

Compared with the prior art, this unmanned aerial vehicle mounting structure has following advantage:

one, this unmanned aerial vehicle carries structure one end integrated into one piece has two dogs, and the dog is located its both sides respectively, set up battery male slot on the dog, can be compressed tightly on the support plate through the clamp plate after the battery inserts the slot, and it is fixed to screw up through the fastener, the installer only need insert under the state that the fastener was unscrewed or take out the installation that the battery can accomplish the battery, just can guarantee under the state that the fastener was screwed up that the battery is compressed tightly by the clamp plate and fixes on the support plate, it is more convenient to guarantee to dismantle under the firm prerequisite of installation.

And secondly, a plurality of limiting bulges are integrally formed on the surface of the support plate and can clamp the two sides of the battery, so that the left side and the right side of the battery can be limited by the limiting bulges, and the battery is more firmly arranged on the support plate.

And the pressing plate is in a long strip shape, the two sides of the pressing plate are turned over to form flanges, and the flanges can play a role in guiding when the battery is inserted in the process of installing the battery, so that the battery is more convenient to install, and the battery cannot be blocked in the installation process.

Fourthly, set up the lightening hole of a plurality of bars on the support plate, the lightening hole is located the both sides edge of support plate, and is lighter-weighted more when can guaranteeing support plate structural strength.

Fifthly, a plurality of first heat dissipation holes and second heat dissipation holes are further formed in the surface, at the position where the support plate abuts against the battery, of the plate, the first heat dissipation holes and the second heat dissipation holes can assist the battery in heat dissipation, and the support plate can be further light.

And sixthly, the support plate and the pressing plate are made of aluminum alloy materials, and the aluminum alloy materials have high hardness and light weight.

Drawings

Fig. 1 is a schematic structural diagram of the mounting structure of the unmanned aerial vehicle.

Fig. 2 is a schematic structural diagram of a carrier plate in the mounting structure of the unmanned aerial vehicle.

Fig. 3 is a schematic structural diagram of a pressing plate in the mounting structure of the unmanned aerial vehicle.

In the figure, 1, a carrier plate; 1a, a battery; 1b, a stop block; 1b1, slot; 1c, pressing a plate; 1c1, flanging; 1d, limiting bulges; 1e, lightening holes; 1f, radiating holes I; 1g, radiating holes II; 1h, connecting columns.

Detailed Description

The following are specific embodiments of the present invention and the accompanying drawings are used to further describe the technical solution of the present invention, but the present invention is not limited to these embodiments.

As shown in fig. 1-3, this unmanned aerial vehicle mounting structure includes a support plate 1 of being made by aluminum alloy material, support plate 1 specifically is square shape, and each integrated into one piece has two spliced poles 1h on the lateral wall of the both sides of support plate 1, the spread groove has all been seted up on every spliced pole 1h lateral wall, support plate 1 can hold tightly on unmanned aerial vehicle's inside connecting rod through this spread groove lock, rethread connecting piece cooperation spliced pole holds the inside connecting rod of unmanned aerial vehicle tightly and fixes through the fastener, guarantee that support plate 1 demountable installation is in unmanned aerial vehicle again and the installation is firm.

As shown in fig. 1-3, a battery 1a is mounted in the middle of a carrier plate 1, the battery 1a and the carrier plate 1 are only abutted together, at least two stoppers 1b are integrally formed at one end of the carrier plate 1, the stoppers 1b are rectangular and located at two sides of one end of the carrier plate 1, the end of the stopper 1b connected with the carrier plate 1 and one side opening of the stopper 1b form a slot 1b1, one end of the battery 1a is inserted into the slot 1b1, the top of the battery 1a is abutted against the inner top wall of the slot 1b1, the bottom of the battery is abutted against the inner bottom wall of the slot 1b1, the rest outer side walls are abutted against the inner side wall of one side of the slot 1b1, so as to ensure that one end of the battery 1a can be pre-fixed, a fixing hole is respectively formed at each of two side edges of one side plate surface of the carrier plate 1, a strip-shaped pressing plate 1c made of aluminum alloy is mounted on the carrier plate 1, a second fixing hole is respectively formed on each side wall at each of each end of the pressing plate 1c, and both ends of the pressing plate 1c are attached to the plate surface of the support plate 1, and the first fixing hole on the support plate 1 corresponds to the second fixing hole on the pressing plate 1c, the middle part of the pressing plate 1c can be pressed on the battery 1a, the pressing plate 1c sequentially penetrates through the first fixing hole and the second fixing hole through fasteners and is screwed and fixed, so that the pressing plate 1c presses the battery 1a, the battery 1a is ensured to be detachably mounted on the support plate 1 more firmly, the fasteners are bolts and nuts, when the battery 1a needs to be dismounted, the nut needs to be slightly loosened to enable the pressing plate 1c to be loosened, the battery 1a can be pulled out from one side of the pressing plate 1c without the stop block 1b, when the battery 1a needs to be fixed, the battery 1a can be mounted firmly by screwing through eyes, and the dismounting is more convenient.

As shown in fig. 1 and fig. 3, the two side walls of the pressing plate 1c are bent to form the flanges 1c1, and the flanges 1c1 can ensure guiding function when a new battery 1a is installed, so as to prevent the battery 1a from being blocked with the side walls of the pressing plate 1 c.

As shown in fig. 1-2, at least two limiting protrusions 1d are further integrally formed on the surface of one side of the carrier plate 1 on which the battery 1a is mounted, the limiting protrusions 1d are close to the side walls of the two sides of the battery 1a, and in the operation process of the unmanned aerial vehicle, the battery 1a is further ensured not to be displaced in the left and right directions.

As shown in fig. 1-2, at least four strip-shaped lightening holes 1e are formed at two side edges of a board surface on one side of the carrier board 1, so that the weight of the carrier board 1 can be effectively lightened and the strength of the carrier board 1 can be ensured, and 6 strip-shaped first heat dissipation holes 1f and 3 circular second heat dissipation holes 1g are formed at the joint of the middle part of the carrier board 1 and the battery 1a, so that not only can effective heat dissipation be ensured when the battery 1a works, but also the carrier board 1 can be ensured to be lighter.

When the battery 1a is mounted, one end of a new battery 1a is inserted into the slot 1b1 of the stop block 1b on the support plate 1, and the nut is screwed down to enable the bolt and the nut to clamp and fix the battery 1a inwards.

The specific embodiments described herein are merely illustrative of the spirit of the invention. Various modifications, additions and substitutions for the specific embodiments described herein may be made by those skilled in the art without departing from the spirit of the invention or exceeding the scope of the invention as defined in the accompanying claims.

Although the terms of the carrier plate 1, the battery 1a, the stopper 1b, the slot 1b1, the pressing plate 1c, the flange, the 1c1 limiting protrusion 1d, the lightening hole 1e, the first heat dissipation hole 1f, the second heat dissipation hole 1g, etc. are used more herein, the possibility of using other terms is not excluded. These terms are used merely to more conveniently describe and explain the nature of the present invention; they are to be construed in a manner that is inconsistent with the spirit of the invention.

Claims (7)

1. The utility model provides an unmanned aerial vehicle carries structure, is used for installing support plate (1) of battery (1a) including one side, its characterized in that, integrated into one piece has a plurality of dogs (1b) that can supply battery (1a) to support to lean on support plate (1), install clamp plate (1c) on support plate (1), clamp plate (1c) can support with battery (1a) and lean on and compress tightly battery (1a) on support plate (1) through the fastener.

2. The unmanned aerial vehicle mounting structure of claim 1, wherein the carrier plate (1) is quadrilateral, the stop blocks (1b) are integrally formed at one end of the carrier plate (1) and located at two sides respectively, the pressing plate (1c) is strip-shaped, the middle part of the pressing plate (1c) abuts against the battery (1a), and the side walls at two ends of the pressing plate (1c) are attached to the carrier plate (1) and are screwed and fixed by fasteners.

3. The unmanned aerial vehicle carries structure of claim 1 or 2, characterized in that slot (1b1) has been seted up to dog (1b) one end, battery (1a) one end can insert slot (1b1) and lean on with slot (1b1) inner wall counterbalance, the one side face that battery (1a) was installed in carrier plate (1) goes up integrated into one piece has a plurality of spacing archs (1d), spacing archs (1d) are located battery (1a) both sides.

4. The unmanned aerial vehicle mounting structure of claim 2, wherein the pressure plate (1c) is folded at two sides to form flanges (1c 1).

5. The unmanned aerial vehicle mounting structure of claim 3, wherein a plurality of strip-shaped lightening holes (1e) are formed on two sides of the surface of the carrier plate (1) on which the battery (1a) is mounted.

6. The unmanned aerial vehicle mounting structure of claim 5, wherein the carrier plate (1) is provided with a plurality of first strip-shaped heat dissipation holes (1f) and second circular heat dissipation holes (1 g).

7. The unmanned aerial vehicle mounting structure of claim 1 or 2, wherein the carrier plate (1) and the pressure plate (1c) are both composed of an aluminum alloy material.

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