CN218967215U - Unmanned aerial vehicle battery installation component - Google Patents

Abstract

The utility model provides an unmanned aerial vehicle battery mounting assembly, which comprises a battery compartment, a positioning chute plate and two lock catches, wherein the two lock catches are respectively hinged to the side face of the battery compartment, and the battery compartment is used for accommodating a battery core for supplying power to an unmanned aerial vehicle; the surface of the positioning chute plate is provided with a slide bar, the bottom of the battery compartment is provided with a chute, and the slide bar is matched with the chute so that the battery compartment can only slide along the positioning chute plate; one end of the positioning chute plate is provided with a limit baffle which is abutted against the end part of the battery compartment, and the lock catch is connected to the limit baffle in a clamping way so as to lock the battery compartment and the positioning chute plate; the unmanned aerial vehicle battery is firmly installed and easily disassembled through the double fixing modes of the sliding groove and the lock catch.

Description

Unmanned aerial vehicle battery installation component

Technical Field

The utility model belongs to the technical field of unmanned aerial vehicle device manufacturing and unmanned aerial vehicle parts, and particularly relates to an unmanned aerial vehicle battery mounting assembly.

Background

Almost all unmanned aerial vehicle all adopt battery powered, and the problem that faces at first is how to install the battery on unmanned aerial vehicle fuselage, and most unmanned aerial vehicle battery's on the market fixed mode adopts the fixed mode of rolling area to bind at present, and this mode is too crude, has because of fixed insecure and leads to the not hard up class potential safety hazard of battery in the flight.

Disclosure of Invention

Based on the above state of the art, the present utility model aims to provide an unmanned aerial vehicle battery installation component, which realizes stable installation and easy disassembly of an unmanned aerial vehicle battery through a double fixing mode of a chute and a lock catch.

The technical scheme adopted by the utility model is as follows: the battery installation assembly of the unmanned aerial vehicle is characterized by comprising a battery compartment, a positioning chute plate and two lock catches, wherein the two lock catches are respectively hinged to the side face of the battery compartment, and the battery compartment is used for accommodating a battery core for supplying power to the unmanned aerial vehicle;

the surface of the positioning chute plate is provided with a slide bar, the bottom of the battery compartment is provided with a chute, and the slide bar is matched with the chute so that the battery compartment can only slide along the positioning chute plate; the sectional shapes of the slide bar and the slide groove are configured into shapes which enable the slide bar of the positioning slide groove plate to slide along the length direction of the slide bar slide groove and not to be separated from other directions after being matched with the slide groove of the battery compartment, for example, the cross section of the slide bar is in a T shape, the cross section of the slide groove is in an inverted T shape, or the cross section of the slide bar is in an inverted ladder shape, and the cross section of the slide groove is in a trapezoid with a wide bottom surface and a narrow opening.

One end of the positioning chute plate is provided with a limit baffle which is abutted with the end part of the battery compartment, and the lock catch is connected to the limit baffle in a clamping way, so that the battery compartment and the positioning chute plate are locked. The two sides of the battery compartment are also provided with a lock catch installation position, the lock catch installation position accommodates and installs the lock catch, the middle part of the lock catch is provided with a pin hole, and the pin hole is used for a pin shaft to pass through so as to install the lock catch in the lock catch installation position in a hinged manner; the front end of the lock catch extends inwards to form a clamping head, two sides of the positioning sliding groove plate are respectively provided with a lock catch bayonet, and the clamping head is connected with the lock catch bayonet in a clamping mode.

A spring is arranged between the inner side of the rear end of the lock catch and the lock catch installation position, and the lock catch is kept in a state that the clamping head is clamped with the lock catch bayonet of the positioning sliding groove plate by the spring. In order to prevent the shifting and slipping of the spring, the inner side of the rear end of the lock catch is provided with a spring positioning seat, the end part of the spring is sleeved on the spring positioning seat, preferably, the inner bottom surface of the lock catch installation position is also provided with a spring positioning seat, namely, the two ends of the spring are respectively positioned and installed by one spring positioning seat.

One side of the battery compartment is opened to form a mounting port, a power supply core is put in and taken out, the battery compartment extends below the mounting port to form a power supply leading-out cavity, and a lead of the power supply core is electrically connected with parts such as an external plug and the like from the power supply leading-out cavity; the installation port and one side of the power supply leading-out cavity are closed by the battery tail plate, the other side of the power supply leading-out cavity is closed by the plug installation plate, and the connecting plug of the power supply circuit is fixedly inserted on the plug installation plate so as to realize that the power supply circuit connects the electric core power inside the battery compartment.

The technical scheme of the utility model has the advantages that: the double fixing modes of the sliding chute and the lock catch are utilized to realize reliable installation of the unmanned aerial vehicle battery, so that the battery is prevented from falling off due to factors such as vibration, and meanwhile, the lock catch type locking mode is convenient for the disassembly of the unmanned aerial vehicle battery and more convenient for use; in addition, all the parts can be produced in batches and then assembled and installed on unmanned aerial vehicle bodies of various models, so that the standardization of unmanned aerial vehicle parts is facilitated.

Drawings

FIG. 1 is a schematic view of the overall structure of the unmanned aerial vehicle battery mounting assembly of the present utility model;

FIG. 2 is a schematic view of an exploded construction of the unmanned aerial vehicle battery mounting assembly of the present utility model;

FIG. 3 is a schematic view of the battery compartment of the unmanned aerial vehicle battery mounting assembly of the present utility model in a disassembled state;

FIG. 4 is a schematic view of a positioning runner plate in the unmanned aerial vehicle battery mounting assembly of the present utility model;

FIG. 5 is a schematic view of a latch structure in the unmanned aerial vehicle battery mounting assembly of the present utility model;

in the figure: 1. 1-1 parts of battery bin, 1-2 parts of mounting port, 1-3 parts of power supply leading-out cavity, 1-4 parts of lock catch mounting position and 1-4 parts of chute;

2. positioning a chute plate, 2-1, a slide bar, 2-2 and a lock catch bayonet; 3. a battery tail plate; 4. the device comprises a lock catch, 4-1, a clamping head, 4-2, a pin hole, 4-3 and a spring positioning seat; 5. and a plug mounting plate.

Detailed Description

The following describes in further detail the embodiments of the present utility model with reference to the drawings and examples. The following examples are illustrative of the utility model and are not intended to limit the scope of the utility model.

In the description of the present application, it should be understood that the terms "center," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like indicate orientations or positional relationships based on the orientation or positional relationships shown in the drawings, merely to facilitate description of the present application and simplify the description, and do not indicate or imply that the devices or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and therefore should not be construed as limiting the present application.

The terms "first," "second," and the like, 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 defining "a first" or "a second" may explicitly or implicitly include one or more such feature. In the description of the present application, unless otherwise indicated, the meaning of "a plurality" is two or more.

In the description of the present application, it should be noted that, unless explicitly specified and limited otherwise, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be either fixedly connected, detachably connected, or integrally connected, for example; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the terms in this application will be understood by those of ordinary skill in the art in a specific context.

Fig. 1 is a schematic diagram of the overall structure of an unmanned aerial vehicle battery mounting assembly according to the utility model, fig. 2 is a schematic diagram of the explosion structure of the unmanned aerial vehicle battery mounting assembly according to the utility model, and as shown in fig. 1 and 2, the unmanned aerial vehicle battery mounting assembly according to the utility model comprises a battery compartment 1, a positioning chute plate 2 and a lock catch 4, wherein the positioning chute plate 2 is fixedly arranged with an unmanned aerial vehicle body, the battery compartment 1 is slidably arranged on the positioning chute plate 2, the lock catch 4 is hinged on the side surface of the battery compartment 1, and the locking and unlocking of the battery compartment 1 and the positioning chute plate 2 are controllably realized.

Fig. 3 is a schematic diagram of a battery compartment in the battery installation assembly of the unmanned aerial vehicle, the battery compartment 1 is configured as a shell for accommodating a battery cell for supplying power to the unmanned aerial vehicle, one side of the battery compartment 1 is opened with a mounting opening 1-1, the mounting opening 1-1 is used for loading and unloading the battery cell, the battery compartment 1 extends to form a power supply leading-out cavity 1-2 at a position below the mounting opening 1-1, one side of the mounting opening 1-1 and one side of the power supply leading-out cavity 1-2 are sealed by a battery tail plate 3, the other side of the power supply leading-out cavity 1-2 is sealed by a plug mounting plate 5, and a connecting plug of a power supply circuit is fixedly inserted on the plug mounting plate 5 so as to realize that the power supply circuit connects the battery cell in the battery compartment 1. Referring to fig. 1, a plurality of screw holes are formed in the side wall of the battery compartment 1, a plurality of screw counter bores are formed in the battery tail plate 3, and the battery tail plate 3 is fixedly mounted on the battery compartment 1 through screws; the battery compartment 1 is also provided with a latch mounting position 1-3 on both sides, the latch mounting position 1-3 is hinged with a latch 4, see fig. 5, which is a latch structure schematic diagram in the unmanned aerial vehicle battery mounting assembly, a pin hole 4-2 is arranged at the upper middle position of the latch 4, a pin shaft passes through the pin hole 4-2 to hinge the latch 4 at the latch mounting position 1-3, the front end of the latch 4 extends inwards to form a chuck 4-1, the chuck 4-1 is in clamping connection with a positioning slide plate 2, when the rear end of the latch 4 is pressed, the latch 4-1 rotates around a pin shaft, the chuck 4-1 is lifted up to release the lock with the positioning slide plate 2, see fig. 5, a spring positioning seat 4-3 is arranged at the inner side of the rear end of the latch 4, a spring is arranged between the spring positioning seat 4-3 and the latch mounting position 1-3, the spring keeps the latch 4 in a state of being clamped with the positioning slide plate 2, and the end of the spring is sleeved on the spring positioning seat 4-3, so that the latch 4-1 is prevented from falling off, and the latch 4 is separated from the front end of the latch 4-1 when the latch 4 is pressed, and the latch 4 is separated from the front end of the battery compartment is pressed, and the latch 4 is separated from the front end of the latch 4-1, and the latch is separated from the front end of the latch 4 when the latch is pressed, and the latch 4 is moved towards the front end of the battery compartment. Preferably, the inner side surface of the lock catch 4 is provided with an arc-shaped surface at a position corresponding to the pin hole 4-2, so that the lock catch 4 can rotate around the pin shaft when the rear end of the lock catch 4 is pressed.

As shown in fig. 4, a schematic diagram of a positioning sliding chute board structure in the installation assembly of the unmanned aerial vehicle battery according to the present utility model is shown, wherein a sliding strip 2-1 is provided on the upper surface of the positioning sliding chute board 2, preferably, the section of the sliding strip 2-1 is T-shaped, and the sliding strip 2-1 cooperates with a sliding chute 1-4 at the bottom of the battery compartment 1, so that the battery compartment 1 can only slide along the axial direction of the sliding strip 2-1; one end of the positioning slide groove plate 2 forms a limit baffle, the limit baffle enables the battery compartment 1 to be in sliding fit along the slide bar 2-1 and then to be abutted against the battery compartment 1, lock catch bayonets 2-2 are respectively arranged on two sides of the limit baffle, and the lock catch bayonets 2-2 are clamped with clamping heads 4-1 of the lock catches 4 after the battery compartment 1 is in place (the end of the battery compartment is abutted against the limit baffle), so that the battery compartment 1 is locked on the positioning slide groove plate 2.

When the battery is installed, the bottom sliding groove 1-4 of the battery compartment 1 is matched with the sliding bar 2-1 of the positioning sliding groove plate, the battery compartment 1 slides along the sliding bar to be abutted with the limit baffle, and then the rear end of the lock catch 4 is pressed to enable the clamping head 4-1 of the lock catch 4 to be clamped into the lock catch bayonet 2-2 of the limit baffle, so that the battery is installed; when dismantling, press hasp 4 rear end, chuck 4-1 perk breaks away from hasp bayonet socket 2-2, then move battery compartment 1 and make its slippage go out the spacing of draw runner, can accomplish the dismantlement, compare in prior art, the battery installation after-fixing is more firm, and installation and dismantlement are all more convenient.

The foregoing is merely a preferred embodiment of the present utility model, and it should be noted that modifications and substitutions can be made by those skilled in the art without departing from the technical principles of the present utility model, and these modifications and substitutions should also be considered as being within the scope of the present utility model.

Claims (8)

1. The battery installation assembly of the unmanned aerial vehicle is characterized by comprising a battery compartment, a positioning chute plate and two lock catches, wherein the two lock catches are respectively hinged to the side face of the battery compartment, and the battery compartment is used for accommodating a battery core for supplying power to the unmanned aerial vehicle;

the surface of the positioning chute plate is provided with a slide bar, the bottom of the battery compartment is provided with a chute, and the slide bar is matched with the chute so that the battery compartment can only slide along the positioning chute plate;

one end of the positioning chute plate is provided with a limit baffle which is abutted with the end part of the battery compartment, and the lock catch is connected to the limit baffle in a clamping way, so that the battery compartment and the positioning chute plate are locked.

2. The unmanned aerial vehicle battery mounting assembly of claim 1, wherein one side of the battery compartment is open to a mounting port, and the battery compartment extends below the mounting port to form a power extraction cavity, one side of the mounting port and the power extraction cavity being closed by a battery tail plate, and the other side of the power extraction cavity being closed by a plug mounting plate.

3. The unmanned aerial vehicle battery mounting assembly of claim 1 or 2, wherein a latch mounting location is provided on both sides of the battery compartment, the latch mounting location accommodates and mounts the latch, a pin hole is provided at a central position on the latch, and a pin hole is provided for a pin to pass through to hinge-mount the latch at the latch mounting location.

4. The unmanned aerial vehicle battery mounting assembly of claim 3, wherein the front end of the lock catch extends inwards to form a clamp head, two sides of the limit baffle of the positioning chute plate are respectively provided with a lock catch bayonet, and the clamp head is in clamping connection with the lock catch bayonet.

5. The unmanned aerial vehicle battery mounting assembly of claim 4, wherein a spring is disposed between the inside of the rear end of the lock catch and the lock catch mounting location, the spring maintaining the lock catch in a state in which the chuck engages the lock catch bayonet of the positioning chute plate.

6. The unmanned aerial vehicle battery mounting assembly of claim 5, wherein a spring positioning seat is provided on the inside of the rear end of the latch, and the end of the spring is sleeved on the spring positioning seat.

7. The unmanned aerial vehicle battery mounting assembly of claim 1, wherein the slide has a T-shaped cross-section and the chute has an inverted T-shaped cross-section.

8. The unmanned aerial vehicle battery mounting assembly of claim 1, wherein the cross section of the runner is inverted trapezoidal and the cross section of the runner is trapezoidal with a wide bottom surface and a narrow opening.

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