Hanging structure for unmanned aerial vehicle battery

Abstract

The invention provides a mounting structure for a battery of an unmanned aerial vehicle. The mounting structure comprises a front limiting mechanism, a middle limiting mechanism and a rear limiting mechanism, the front limiting mechanism, the middle limiting mechanism and the rear limiting mechanism are all arranged on the end face of the cabin inner bulkhead, are axially distributed in the battery mounting direction, and correspondingly abut against the front end face, the outer surface of the middle section and the rear end face of the battery body respectively; the position of the battery on the end face of the bulkhead in the cabin is cooperatively restrained. According to the mounting structure for the unmanned aerial vehicle battery, the serious power supply reliability and safety problems caused by unstable contact pressure and even failure of an interface of a connector due to inherent operation inconvenience and connection vulnerability of wire throwing connection in related technologies are solved.

Description

Technical Field

[0001] The present invention belongs to the technical field of unmanned aerial vehicle (UAV) batteries, and in particular relates to a mounting structure for UAV batteries. Background Art

[0002] Given the stringent requirements of drone systems for continuous power supply to onboard avionics, the batteries they are equipped with must not only have sufficient energy output capacity, but also require careful structural design considerations for both installation and fixation. This means ensuring that the battery cells can be quickly and easily removed and replaced by operators to accommodate frequent maintenance or mission changes. Furthermore, they must provide an extremely strong and stable restraint in complex flight environments and maneuvers, such as those encountering airflow disturbances or acceleration and deceleration shocks, effectively preventing any power outages or flight safety hazards caused by battery displacement, loosening, or even accidental detachment. Therefore, modern drone battery fixation solutions require significant optimization and upgrades based on traditional strapping methods.

[0003] In the current design, the method of connecting the battery using free-swinging cables is not only complicated to operate, but also requires effort to align the pins and straighten the wiring harness, which greatly reduces the convenience of disassembly and assembly; at the same time, this exposed cable connection is very likely to loosen or have poor contact under the vibration impact of flight, and the physical reliability of the connection is difficult to guarantee.

[0004] Due to the inherent operational inconvenience and connection fragility of the loose wire connection in the relevant technology, and the lack of effective compensation design for battery deformation in the fixed structure when responding to temperature changes, the contact pressure of the connector interface is ultimately unstable or even fails, causing serious power supply reliability and safety problems. Summary of the Invention

[0005] In view of this, the present invention aims to solve one of the related technical problems at least to a certain extent.

[0006] To achieve the above object, the technical solution of the present invention is achieved as follows:

[0007] A mounting structure for a UAV battery, comprising a front limiting mechanism, a middle limiting mechanism, and a rear limiting mechanism;

[0008] The front limiting mechanism, the middle limiting mechanism and the rear limiting mechanism are all arranged on the end surface of the cabin inner bulkhead. The front limiting mechanism, the middle limiting mechanism and the rear limiting mechanism are axially distributed along the battery installation direction and respectively abut against the front end surface, the outer surface of the middle section and the rear end surface of the battery body to cooperate to constrain the position of the battery on the end surface of the cabin inner bulkhead;

[0009] The front limit mechanism includes a front limit seat fixedly mounted on the end surface of the cabin inner bulkhead and two elastic buckle assemblies symmetrically arranged on the front limit seat;

[0010] The front end of the battery is provided with a limiting structure corresponding to the front limiting seat; the elastic snap assembly is configured to: when the limiting structure of the battery abuts against the front limiting seat, it is locked to constrain the axial displacement of the battery, and disassembly is achieved by manual release.

[0011] Furthermore, the intermediate limiting mechanism includes an intermediate limiting seat fixedly mounted on the end surface of the bulkhead in the cabin and two intermediate limiting ears fixedly arranged in the middle of the battery body;

[0012] The intermediate limiting seat is provided with intermediate limiting grooves on two opposite sides thereof;

[0013] The intermediate limiting ears can slide into and engage with the corresponding intermediate limiting grooves in a horizontal direction;

[0014] The middle limiting groove can accommodate the middle limiting ear and limit its displacement in the vertical direction.

[0015] Furthermore, the rear limit mechanism includes a rear limit base fixedly mounted on the end surface of the bulkhead in the cabin, two rear limit ears fixedly arranged at the rear of the battery body, and two locking mechanisms arranged on the rear limit base;

[0016] The rear limit base is provided with rear limit grooves on two opposite sides thereof;

[0017] The rear limiting ears can be inserted into the corresponding rear limiting grooves to achieve horizontal positioning;

[0018] The locking mechanism is used to limit the rear of the battery.

[0019] Furthermore, the locking mechanism includes a buckle base, a rear limit buckle and a glass bead top screw. The buckle base is integrally connected to the end of the rear limit base. One end of the rear limit buckle is rotatably engaged with the buckle base through a knurled pin, and the other end of the rear limit buckle is detachably connected to the buckle base through the glass bead top screw. The rear limit buckle is used to limit the rear of the battery.

[0020] Furthermore, the limiting structure includes a limiting slot and a front limiting ear that can cooperate with the limiting slot, the front limiting ear is arranged at the front end of the power supply, the limiting slot is arranged on the front limiting seat, and the shape of the limiting slot is adapted to the front limiting ear;

[0021] The front limiting ear can be inserted into the limiting slot to achieve preliminary positioning of the battery body relative to the front limiting seat;

[0022] When the front limiting ear is inserted into the limiting slot, the elastic buckle assembly is locked to restrict the axial displacement of the front limiting ear in the limiting slot.

[0023] Furthermore, the elastic buckle assembly includes a buckle body, a travel hole, a return spring and a limit screw, the end of the front limit seat is provided with a front limit groove, the top of the buckle body is provided with a pressing portion, the side of the buckle body is provided with a buckle limit ear, and the travel hole is provided in the middle of the buckle body along the vertical direction;

[0024] The lower portion of the buckle body is accommodated in the front limiting groove;

[0025] The return spring is arranged at the bottom of the front limiting groove and elastically abuts between the bottom of the limiting groove and the buckle body;

[0026] The limit screw passes through the travel hole and is threadedly connected to the front limit seat, and the head size of the limit screw is larger than the width of the travel hole, thereby slidably constraining the buckle body on the front limit seat and allowing the buckle body to move vertically along the limit groove within a limited travel;

[0027] When the buckle body is in an unpressed state, its position blocks the front limit ear inserted into the upper limit slot of the front limit seat to limit its axial displacement;

[0028] By pressing the pressing portion, the buckle body is driven to overcome the elastic force of the return spring and move downward, so that the buckle limiting ear can be separated from the obstruction of the front limiting ear, thereby achieving unlocking.

[0029] Furthermore, a baffle is provided in the middle of the front limit seat, and the baffle is provided with a notch that can cooperate with the power socket, one side of the notch is opposite to the power socket, and the other side of the notch is provided with a socket protection cover.

[0030] Furthermore, the buckle body is provided with a visual identification area, and when the buckle body is in the initial locking position under the action of the return spring, the visual identification area is exposed outside the front limit seat;

[0031] When the return spring force is overcome and the position is pressed down to the unlocked position, the visual identification area is shielded by the front limit seat;

[0032] The exposed and concealed states of the visual identification area correspond to the locked and unlocked states of the elastic buckle assembly respectively.

[0033] Compared with the prior art, the mounting structure for drone batteries described in the present invention has the following advantages:

[0034] 1. The front limit mechanism achieves initial positioning through the precise fit of the limit ear at the front end of the battery and the limit slot. Combined with the elastic snap components symmetrically distributed on both sides, they automatically lock when the battery abuts, forming a rigid constraint on the axial displacement of the battery, effectively ensuring the contact reliability of the battery connector in the vibration environment of flight.

[0035] 2. The intermediate limit mechanism uses a guided engagement method in which the limit ear in the middle of the battery slides horizontally into the limit slot, providing full-range load-bearing support for the battery body, significantly reducing the risk of deformation of the battery casing due to bending stress during flight maneuvers.

[0036] 3. After the rear limit ear is inserted into the rear limit groove to achieve precise horizontal positioning of the rear of the battery, the rotary locking mechanism applies continuous compression force through the ratchet locking effect of the glass bead top screw, forming a three-way limit (axial anti-slip, lateral anti-twist, and vertical anti-vibration).

[0037] 4. The three mechanisms are distributed along the battery installation axis, implementing targeted constraints on the front, middle and rear sections of the battery: the front section is used to achieve electrical interface protection and automatic locking, the middle section is used to achieve support stiffness and deformation compensation, and the rear section is used to achieve manual locking redundancy. BRIEF DESCRIPTION OF THE DRAWINGS

[0038] The accompanying drawings, which constitute part of the present invention, are provided to provide a further understanding of the present invention. The exemplary embodiments of the present invention and their descriptions are used to explain the present invention and do not constitute an undue limitation of the present invention. In the accompanying drawings:

[0039] Figure 1 This is a schematic diagram of a mounting structure for a UAV battery according to an embodiment of the present invention;

[0040] Figure 2 Schematic diagram of the front limiting mechanism, the middle limiting mechanism and the rear limiting mechanism according to an embodiment of the present invention;

[0041] Figure 3 This is a schematic diagram of the connection between the front limit seat and the end face of the cabin inner bulkhead according to an embodiment of the present invention;

[0042] Figure 4 This is a front view of the front limit seat according to an embodiment of the present invention;

[0043] Figure 5 This is a cross-sectional view of the elastic buckle assembly according to an embodiment of the present invention;

[0044] Figure 6 This is a schematic diagram of the front limit groove according to an embodiment of the present invention;

[0045] Figure 7 This is a schematic diagram of a buckle body according to an embodiment of the present invention;

[0046] Figure 8 Schematic diagram of the front limiting ears, middle limiting ears, and rear limiting ears according to an embodiment of the present invention.

[0047] Description of reference numerals:

[0048] 1. End face of the bulkhead in the cabin; 101. Fixing screw; 2. Front limit mechanism; 201. Front limit seat; 2011. Front limit slot; 202. Limit screw; 203. Buckle body; 2031. Visual identification area; 2032. Travel hole; 2033. Buckle limit ear; 204. Return spring; 3. Intermediate limit mechanism; 301. Intermediate limit slot; 4. Rear limit mechanism; 401. Rear limit base; 4011. Rear limit slot; 402. Rear limit buckle; 403. Knurled pin; 404. Glass bead top screw; 5. Power supply; 501. Front limit ear; 6. Socket protection cover; 601. Notch. DETAILED DESCRIPTION

[0049] It should be noted that, in the absence of conflict, the embodiments of the present invention and the features in the embodiments may be combined with each other.

[0050] In the description of the present invention, it should be understood that the terms "center", "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside" and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the accompanying drawings, and are only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as limiting the present invention. In addition, the terms "first", "second", etc. are only used for descriptive purposes and cannot be understood as indicating or implying relative importance or implicitly indicating the number of the indicated technical features. Therefore, features defined as "first", "second", etc. may explicitly or implicitly include one or more of the features. In the description of the present invention, unless otherwise specified, "multiple" means two or more.

[0051] In the description of the present invention, it should be noted that, unless otherwise expressly specified or limited, the terms "mounted," "connected," and "connected" should be understood in a broad sense. For example, they may refer to fixed connections, detachable connections, or integral connections; mechanical connections or electrical connections; direct connections or indirect connections through an intermediate medium; and internal communication between two components. Those skilled in the art will understand the specific meanings of the above terms in the present invention based on specific circumstances.

[0052] The present invention will be described in detail below with reference to the accompanying drawings and in conjunction with embodiments.

[0053] A mounting structure for a drone battery, such as Figure 1 As shown, it includes a front limiting mechanism 2, an intermediate limiting mechanism 3 and a rear limiting mechanism 4; the front limiting mechanism 2, the intermediate limiting mechanism 3 and the rear limiting mechanism 4 are all arranged on the end surface 1 of the cabin inner bulkhead, and the front limiting mechanism 2, the intermediate limiting mechanism 3 and the rear limiting mechanism 4 are axially distributed along the battery installation direction, and respectively abut against the front end surface, the outer surface of the middle section and the rear end surface of the battery body, so as to collaboratively constrain the position of the battery on the end surface 1 of the cabin inner bulkhead;

[0054] The front limiting mechanism 2 includes a front limiting seat 201 fixedly mounted on the end face 1 of the cabin bulkhead and two elastic snap-on assemblies symmetrically arranged on the front limiting seat 201. A limiting structure corresponding to the front limiting seat 201 is provided at the front end of the battery. The elastic snap-on assemblies are configured to lock together to constrain the battery's axial displacement when the battery's limiting structure abuts the front limiting seat 201, allowing for manual release to facilitate disassembly. The front limiting mechanism 2 achieves initial positioning through the precise fit of the limiting ears at the front end of the battery into the limiting slots. Combined with the symmetrically distributed elastic snap-on assemblies on both sides, they automatically lock together at the moment of battery abutment, forming a rigid constraint on the battery's axial displacement and effectively ensuring the contact reliability of the battery connector under flight vibration conditions.

[0055] The intermediate limiting mechanism 3 includes an intermediate limiting seat fixedly mounted on the end face 1 of the cabin bulkhead and two intermediate limiting ears fixedly mounted in the middle of the battery body. The intermediate limiting seat is provided with intermediate limiting grooves 301 on opposite sides. The intermediate limiting ears can slide horizontally into and engage with the corresponding intermediate limiting grooves 301. The intermediate limiting grooves 301 can accommodate the intermediate limiting ears and limit their vertical displacement. The intermediate limiting mechanism 3 provides full-range load-bearing support for the battery body by guiding the limiting ears in the middle of the battery to slide horizontally into the limiting grooves, significantly reducing the risk of deformation of the battery housing due to bending stress during flight maneuvers.

[0056] The rear limiting mechanism 4 includes a rear limiting base 401 fixedly mounted on the end face 1 of the cabin bulkhead, two rear limiting ears fixedly mounted at the rear of the battery body, and two locking mechanisms mounted on the rear limiting base 401. The rear limiting base 401 is provided with rear limiting grooves 4011 on opposite sides. The rear limiting ears can be inserted into the corresponding rear limiting grooves 4011 to achieve horizontal positioning. The locking mechanism is used to limit the rear of the battery. After the rear limiting ears are inserted into the rear limiting grooves 4011 to achieve precise horizontal positioning of the rear of the battery, the rotary locking mechanism applies continuous compressive force through the ratchet locking effect of the glass ball screw 404, forming a three-dimensional limit (axial anti-slip, lateral anti-twist, and vertical anti-vibration).

[0057] The locking mechanism includes a snap base, a rear limit snap 402 and a glass bead top screw 404. The snap base is integrally connected to the end of the rear limit base 401. One end of the rear limit snap 402 is rotatably engaged with the snap base through a knurled pin 403, and the other end of the rear limit snap 402 is detachably connected to the snap base through a glass bead top screw 404. The rear limit snap 402 is used to limit the rear of the battery.

[0058] The limiting structure includes a limiting slot and a front limiting ear 501 that can cooperate with the limiting slot. The front limiting ear 501 is arranged at the front end of the power supply 5, and the limiting slot is arranged on the front limiting seat 201. The shape of the limiting slot is adapted to the front limiting ear 501; the front limiting ear 501 can be inserted into the limiting slot to realize the preliminary positioning of the battery body relative to the front limiting seat 201; when the front limiting ear 501 is inserted into the limiting slot, the elastic snap assembly is locked to constrain the axial displacement of the front limiting ear 501 in the limiting slot.

[0059] The elastic buckle assembly includes a buckle body 203, a travel hole 2032, a return spring 204 and a limit screw 202. The end of the front limit seat 201 is provided with a front limit groove 2011, the top of the buckle body 203 is provided with a pressing part, the side of the buckle body 203 is provided with a buckle limit ear, and the travel hole 2032 is provided in the middle of the buckle body 203 in the vertical direction; the lower part of the buckle body 203 is accommodated in the front limit groove 2011; the return spring 204 is provided at the bottom of the front limit groove 2011 and elastically presses against the buckle body 203. The limit screw 202 is connected between the bottom of the limit slot and the buckle body 203; the limit screw 202 passes through the travel hole 2032 and is threadedly connected to the front limit seat 201. The head size of the limit screw 202 is larger than the width of the travel hole 2032, thereby slidably constraining the buckle body 203 on the front limit seat 201 and allowing the buckle body 203 to move vertically along the limit slot within a limited travel. When the buckle body 203 is in the unpressed state, its position blocks the front limit ear 501 inserted into the limit slot of the front limit seat 201, thereby limiting its axial displacement.

[0060] By pressing the pressing portion, the buckle body 203 is driven to overcome the elastic force of the return spring 204 and move downward, so that the buckle limiting ear 2033 can be separated from the obstruction of the front limiting ear 501, thereby achieving unlocking.

[0061] A baffle is provided in the middle of the front limit seat 201 , and the baffle is provided with a notch 601 that can cooperate with the power socket. One side of the notch 601 is opposite to the power socket, and the other side of the notch 601 is provided with a socket protection cover 6 .

[0062] The buckle body 203 is provided with a visual identification area 2031. When it is in the initial locking position under the action of the return spring 204, the visual identification area 2031 is exposed outside the front limit seat 201; when it is pressed down to the unlocking position to overcome the elastic force of the return spring 204, the visual identification area 2031 is shielded by the front limit seat 201; the exposed and shielded states of the visual identification area 2031 correspond to the locked state and unlocked state of the elastic buckle assembly respectively.

[0063] How this example works

[0064] Fasten the front stopper 201 to the end face 1 of the cabin bulkhead using eight fixing screws 101. Insert two return springs 204 into the bottom of the front stopper slot 2011. Insert the two clip bodies 203 into the front stopper slots 2011, press down gently, and screw in the two stopper screws 202. The heads of the stopper screws 202 sink into the travel holes 2032, allowing the clip bodies 203 to maintain vertical freedom of movement within the specified travel range. Anchor the intermediate stopper 3 to the end face 1 of the cabin bulkhead using four fixing screws 101.

[0065] Use six fixing screws 101 to fix the rear limit base 401 to the end face 1 of the bulkhead in the cabin; hinge the rear limit buckle 402 to the rear limit base 401 through two knurled pins 403; finally, screw in two glass ball screws 404 to complete the assembly of the locking unit.

[0066] Operation status description:

[0067] The buckle body 203 is provided with a visual identification area 2031. When it is in the initial locking position under the action of the return spring 204, the visual identification area 2031 is exposed outside the front limit seat 201; when it is pressed down to the unlocking position to overcome the elastic force of the return spring 204, the visual identification area 2031 is shielded by the front limit seat 201; the exposed and shielded states of the visual identification area 2031 correspond to the locked state and unlocked state of the elastic buckle assembly respectively.

[0068] The rear limit buckle 402 can rotate around the knurled pin 403 to switch between open and closed states; in the closed state, the head of the glass bead top screw 404 sinks into the locking hole, and the ratchet locking effect resists 20g vibration impact to prevent accidental loosening.

[0069] Battery assembly process:

[0070] Press the buckle body 203 down to the unlocked position (visual identification area 2031 is blocked), and synchronously rotate the rear limit buckle 402 to the open state; place the power supply 5 into the installation area and push it towards the front limit mechanism 2;

[0071] After the middle battery limiting ear slides into the middle limiting groove 301 and the rear battery limiting ear is inserted into the rear limiting groove 4011, release the buckle body 203;

[0072] The buckle body 203 automatically resets (the visual identification area 2031 is exposed), and the buckle limiting ear 2033 forms an axial interlock with the front limiting ear 501;

[0073] The rear limit buckle 402 is rotated to the closed position to complete the locking.

[0074] The above are only preferred embodiments of the present invention and are not intended to limit the present invention. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principles of the present invention should be included in the scope of protection of the present invention.

Claims

1. A mounting structure for a UAV battery, characterized by: It includes a front limiting mechanism (2), an intermediate limiting mechanism (3) and a rear limiting mechanism (4); The front limiting mechanism (2), the middle limiting mechanism (3) and the rear limiting mechanism (4) are all arranged on the end face (1) of the cabin inner bulkhead. The front limiting mechanism (2), the middle limiting mechanism (3) and the rear limiting mechanism (4) are axially distributed along the battery installation direction and respectively contact the front face, the outer surface of the middle section and the rear face of the battery body to cooperatively constrain the position of the battery on the end face (1) of the cabin inner bulkhead. The front limiting mechanism (2) comprises a front limiting seat (201) fixedly mounted on the end surface (1) of the cabin inner bulkhead, and two elastic buckle assemblies symmetrically arranged on the front limiting seat (201); The front end of the battery is provided with a limiting structure corresponding to the front limiting seat (201); the elastic buckle assembly is configured to: when the limiting structure of the battery abuts against the front limiting seat (201), lock to restrict the axial displacement of the battery, and realize disassembly by manual release; The middle limiting mechanism (3) has a middle limiting groove for accommodating a middle limiting ear of the battery; The rear limiting mechanism (4) has a rear limiting groove for positioning a limiting ear at the rear of the battery; The rear limiting mechanism (4) has a locking mechanism for locking the rear of the battery.

2. The mounting structure for a UAV battery according to claim 1, characterized in that: The intermediate limiting mechanism (3) comprises an intermediate limiting seat fixedly mounted on the end surface (1) of the cabin inner bulkhead and two intermediate limiting ears fixedly arranged in the middle of the battery body; The intermediate limiting seat is provided with intermediate limiting grooves (301) on two opposite sides thereof; The intermediate limiting lugs can slide into and engage with the corresponding intermediate limiting grooves (301) in a horizontal direction; The middle limiting groove (301) can accommodate the middle limiting ear and limit its displacement in the vertical direction.

3. The mounting structure for a UAV battery according to claim 1, characterized in that: The rear limiting mechanism (4) comprises a rear limiting base (401) fixedly mounted on the end surface (1) of the cabin inner bulkhead, two rear limiting ears fixedly arranged at the rear of the battery body, and two locking mechanisms arranged on the rear limiting base (401); The rear limiting base (401) is provided with rear limiting grooves (4011) on two opposite sides thereof; The rear limiting ears can be inserted into the corresponding rear limiting grooves (4011) to achieve horizontal positioning; The locking mechanism is used to limit the rear of the battery.

4. The mounting structure for a UAV battery according to claim 3, characterized in that: The locking mechanism comprises a buckle base, a rear limit buckle (402) and a glass ball top screw (404); the buckle base is integrally connected to the end of the rear limit base (401); one end of the rear limit buckle (402) is rotatably engaged with the buckle base via a knurled pin (403); the other end of the rear limit buckle (402) is detachably connected to the buckle base via the glass ball top screw (404); and the rear limit buckle (402) is used to limit the rear of the battery.

5. A mounting structure for a UAV battery according to any one of claims 1 to 4, characterized in that: The limiting structure comprises a limiting card slot and a front limiting ear (501) capable of cooperating with the limiting card slot, the front limiting ear (501) being arranged at the front end of the power supply (5), the limiting card slot being arranged on the front limiting seat (201), and the shape of the limiting card slot being adapted to the front limiting ear (501); The front limiting ear (501) can be inserted into the limiting slot to achieve preliminary positioning of the battery body relative to the front limiting seat (201); When the front limiting ear (501) is inserted into the limiting slot, the elastic buckle assembly is locked to constrain the axial displacement of the front limiting ear (501) in the limiting slot.

6. The mounting structure for a UAV battery according to claim 5, characterized in that: The elastic buckle assembly comprises a buckle body (203), a travel hole (2032), a return spring (204) and a limit screw (202); the end of the front limit seat (201) is provided with a front limit groove (2011); the top of the buckle body (203) is provided with a pressing portion; the side of the buckle body (203) is provided with a buckle limit ear; the travel hole (2032) is vertically penetrated and arranged in the middle of the buckle body (203); The lower portion of the buckle body (203) is accommodated in the front limiting groove (2011); The return spring (204) is arranged at the bottom of the front limiting groove (2011) and elastically abuts between the bottom of the limiting groove and the buckle body (203); The limiting screw (202) passes through the travel hole (2032) and is threadedly connected to the front limit seat (201), and the head size of the limiting screw (202) is larger than the width of the travel hole (2032), thereby slidably constraining the buckle body (203) on the front limit seat (201) and allowing the buckle body (203) to move vertically along the limit groove within a limited travel; When the buckle body (203) is in an unpressed state, its position blocks the front limiting ear (501) inserted into the upper limit slot of the front limiting seat (201), thereby limiting its axial displacement; By pressing the pressing portion, the buckle body (203) is driven to overcome the elastic force of the return spring (204) and move downward, so that the buckle limiting ear (2033) can be separated from the obstruction of the front limiting ear (501), thereby achieving unlocking.

7. The mounting structure for a UAV battery according to claim 5, characterized in that: A baffle is provided in the middle of the front limit seat (201), and the baffle is provided with a notch (601) capable of cooperating with a power socket, one side of the notch (601) is directly opposite to the power socket, and the other side of the notch (601) is provided with a socket protection cover (6).

8. The mounting structure for a UAV battery according to claim 6, characterized in that: The buckle body (203) is provided with a visual identification area (2031), and when in the initial locking position under the action of the return spring (204), the visual identification area (2031) is exposed outside the front limit seat (201); When the elastic force of the return spring (204) is overcome and the device is pressed down to the unlocked position, the visual identification area (2031) is shielded by the front limit seat (201); The exposed and concealed states of the visual identification area (2031) correspond to the locked state and unlocked state of the elastic buckle assembly respectively.

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