CN210047614U - Battery compartment subassembly reaches fixed wing unmanned aerial vehicle who contains it - Google Patents

Battery compartment subassembly reaches fixed wing unmanned aerial vehicle who contains it Download PDF

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Publication number
CN210047614U
CN210047614U CN201920607397.9U CN201920607397U CN210047614U CN 210047614 U CN210047614 U CN 210047614U CN 201920607397 U CN201920607397 U CN 201920607397U CN 210047614 U CN210047614 U CN 210047614U
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Prior art keywords
battery
battery compartment
top shell
compartment
groove
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CN201920607397.9U
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Chinese (zh)
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尹亮亮
龚成
张羽
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Nanjing Tuoxing Intelligent Control Technology Co Ltd
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Nanjing Tuoxing Intelligent Control Technology Co Ltd
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Abstract

The utility model belongs to the technical field of unmanned aerial vehicle, concretely relates to battery compartment subassembly and contain its fixed wing unmanned aerial vehicle, battery compartment subassembly includes battery and battery compartment, and the battery compartment includes the storehouse body, has seted up the storage tank of accommodating the battery on the storehouse body, and the storage tank top is equipped with the bin mouth, and the bin mouth supplies the battery to pack into the storage tank from the battery compartment top; the battery comprises a top shell and an electric core, the electric core is fixed on the lower portion of the top shell, an elastic insertion piece protrudes outwards from the side portion of the top shell, and a slot matched with the elastic insertion piece is formed in the corresponding position of the accommodating groove. The utility model discloses a battery compartment subassembly reaches fixed wing unmanned aerial vehicle who contains it is equipped with independent battery compartment on the fuselage, and the top shell of battery belongs to the partly of fuselage, and forms pneumatic conformal structure with the fuselage, and the storehouse lid of battery compartment is regarded as simultaneously to the top shell, and when the storage tank of battery compartment was packed into to electric core, the door in top shell sealed battery compartment, convenient and swift was changed to the battery.

Description

Battery compartment subassembly reaches fixed wing unmanned aerial vehicle who contains it
Technical Field
The utility model relates to an unmanned air vehicle technique field, concretely relates to battery compartment subassembly reaches fixed wing unmanned aerial vehicle who contains it.
Background
A drone is an unmanned aerial vehicle that is operated by a radio remote control device or by its own programmed control means. With the rapid development of the unmanned aerial vehicle industry, more and more unmanned aerial vehicles are applied to industries such as agriculture, forestry, electric power, surveying and mapping, remote measurement and the like. The fixed wing unmanned aerial vehicle is an unmanned aerial vehicle, has the advantages of high flying speed, long endurance time, large load and the like, and is widely applied to various industries.
Fixed wing unmanned aerial vehicle includes the fuselage, is equipped with the cabin in the fuselage, installs flight control device in the cabin and for the battery of unmanned aerial vehicle power supply, and the battery passes through screw or bolt snap-on usually in the cabin, changes the battery at every turn, all need open the hatch door in cabin, and the operation is inconvenient, and dismouting efficiency is lower.
SUMMERY OF THE UTILITY MODEL
The utility model discloses a solve above-mentioned technical problem, provide a battery compartment subassembly and contain its fixed wing unmanned aerial vehicle, battery easy dismounting and swift, it is firm to install.
In order to achieve the technical effects, the utility model adopts the following technical scheme: in a first aspect, the utility model provides a battery compartment assembly, the battery compartment assembly includes battery and battery compartment, the battery compartment includes the storehouse body, seted up the storage tank that holds the battery on the storehouse body, the storage tank top is equipped with the bin mouth, the bin mouth supplies the battery to pack into the storage tank from the battery compartment top; the battery comprises a top shell and an electric core, the electric core is fixed at the lower part of the top shell, an elastic insertion piece protrudes outwards from the side part of the top shell, and a slot matched with the elastic insertion piece is arranged at the corresponding position of the accommodating groove; when the battery is installed in the battery compartment, the top shell seals the compartment opening, and the elastic insertion piece is inserted in the slot to fix the battery in the battery compartment.
The utility model provides a battery compartment subassembly includes battery and battery compartment, and the battery includes fixed connection's top shell and electric core, and the top shell uses as the cang gai of battery compartment simultaneously, and when electric core installed in the storage tank of battery compartment, the cang kou of top shell sealed battery compartment, elasticity inserted sheet on the top shell correspond insert the slot that corresponds on the battery compartment in to fix the battery on the battery compartment.
As the preferred structure of the utility model, the elastic inserting piece is hinged on the side edge of the top shell, and the elastic inserting piece moves up and down relative to the side part of the top shell; the notch of the slot is arranged at the inner side edge of the bin opening, and the slot is formed from the notch to the bin body.
As the utility model discloses structural improvement, the elasticity inserted sheet with be connected with the spring between the electric core.
The spring coupling is between elasticity inserted sheet and electric core, is favorable to strengthening the inseparable nature of pegging graft between elasticity inserted sheet and the slot to the fastness in the battery compartment has been improved to the battery.
As a further improvement of the structure of the utility model, the surface of the elastic insertion piece is provided with a groove, a positioning button is arranged in the groove, the positioning button comprises a pressing bulge and a pressure spring, the pressing bulge is arranged in the groove and moves relative to the groove, and the pressure spring is connected between the bottom of the pressing bulge and the bottom of the groove; the top of the slot is provided with a positioning hole for the positioning button to pass through from the inside of the slot. Through setting up the positioning button, be convenient for take out the battery fast in the battery compartment.
Preferably, the elastic insertion pieces are two and are oppositely arranged in the middle of two sides of the top shell.
Preferably, the size of the accommodating groove is matched with the battery cell, and each side surface of the battery cell is arranged in the accommodating groove along each inner side surface of the accommodating groove; the top shell seals the bin opening, and the outer edge of each side part of the top shell is in seamless butt joint with the inner edge of the bin opening.
Furthermore, the corners of the accommodating groove are rounded corners, and the corners of the battery core are matched with the rounded corners.
The corner of storage tank is established to the fillet, and the electricity core corresponds the position and agrees with the fillet mutually, and the friction that produces when having reduced the battery dismouting is favorable to putting into the holding storehouse of battery compartment with the battery core fast in, avoids being blocked.
On the other hand, the utility model provides a fixed wing unmanned aerial vehicle, which comprises a vehicle body and the battery cabin assembly; the battery compartment assembly comprises a battery and a battery compartment, the battery compartment comprises a compartment body, the compartment body is a part of a machine body or is arranged on the machine body, and the compartment body is provided with a containing groove for containing the battery; the top of the containing groove is provided with a bin opening, and the bin opening is used for the battery to be loaded into the containing groove from the top of the battery bin.
The utility model provides a fixed wing unmanned aerial vehicle, the storehouse body of battery compartment can be fused into an organic whole with the fuselage, becomes a part of fuselage, and the storehouse body of battery compartment also can solitary individuality, installs on the fuselage, during the dismouting battery, need not to open the cabin again, only need open the battery compartment dismouting on the fuselage can, convenient operation and swift.
Furthermore, the battery comprises a top shell and an electric core, the electric core is fixed at the lower part of the top shell, an elastic insertion piece protrudes outwards from the side part of the top shell, and a slot matched with the elastic insertion piece is arranged at the corresponding position of the accommodating groove; the top shell is arc-shaped, is a part of the machine body and seals the bin opening.
Furthermore, a pull ring is arranged on the top shell. The convenience of disassembling and assembling the battery can be improved through the pull ring.
By adopting the technical scheme, the method has the following beneficial effects: the utility model provides a battery compartment subassembly and contain its fixed wing unmanned aerial vehicle, battery compartment subassembly include battery and battery compartment, and the battery includes fixed connection's top shell and electric core, and the top shell uses as the cang gai of battery compartment simultaneously, easy dismounting between battery and the battery compartment, and the inserted sheet on the top shell is pegged graft in the slot on the battery compartment for electric core fixed mounting is in the storage tank of battery compartment. The utility model provides a fixed wing unmanned aerial vehicle is equipped with independent battery compartment on the fuselage, and the top shell of battery belongs to the partly of fuselage, and forms pneumatic conformal structure with the fuselage, and the storehouse lid of battery compartment is regarded as simultaneously to the top shell, when the storage tank of battery compartment is packed into to electric core, the door of top shell sealed battery compartment, and convenient and swift is changed to the battery.
Drawings
Fig. 1 is a schematic structural diagram of a battery in a battery compartment assembly provided by the present invention;
FIG. 2 is an enlarged view of FIG. 1 at A;
fig. 3 is a schematic structural view of a battery compartment in the battery compartment assembly provided by the present invention;
fig. 4 is a schematic view illustrating the installation of the single cell battery in cooperation with the bottom of the battery compartment according to the present invention;
fig. 5 is a schematic view of the dual-cell battery provided by the present invention installed in cooperation with the bottom of the battery compartment;
fig. 6 is the utility model provides a fixed wing unmanned aerial vehicle's schematic structure diagram.
In the figure:
100. a body; 200. a battery compartment assembly; 1. a top shell; 2. an electric core; 3. an elastic insert; 4. a spring; 5. a pull ring; 6. a first connector; 7. a second connector; 8. a bin body; 9. a containing groove; 10. a slot; 11. positioning holes; 12. pressing the protrusion; 13. a groove; 14. and (5) pressing a spring.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention clearer, the accompanying drawings in the embodiments of the present invention are combined below to clearly and completely describe the technical solutions in the embodiments of the present invention, and obviously, the described embodiments are some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts belong to the protection scope of the present invention.
In the present invention, the terms "upper", "lower", "left", "right", "front", "rear", "top", "bottom", "inner", "outer", "middle", "vertical", "horizontal", "lateral", "longitudinal", and the like indicate the orientation or positional relationship based on the orientation or positional relationship shown in the drawings. These terms are used primarily to better describe the invention and its embodiments, and are not intended to limit the indicated devices, elements or components to a particular orientation or to be constructed and operated in a particular orientation.
Moreover, some of the above terms may be used to indicate other meanings besides the orientation or positional relationship, for example, the term "on" may also be used to indicate some kind of attachment or connection relationship in some cases. The specific meaning of these terms in the present invention can be understood by those of ordinary skill in the art as appropriate.
Furthermore, the terms "mounted," "disposed," "provided," "connected," and "coupled" are to be construed broadly. For example, it may be a fixed connection, a removable connection, or a unitary construction; can be a mechanical connection, or an electrical connection; may be directly connected, or indirectly connected through intervening media, or may be in internal communication between two devices, elements or components. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.
"plurality" means two or more unless otherwise specified.
The present invention will be described in further detail below with reference to specific embodiments and with reference to the attached drawings.
The first embodiment is as follows:
referring to fig. 1, 2, 3 and 4, the battery compartment assembly 200 includes a battery and a battery compartment, the battery compartment includes a compartment body 8, the compartment body 8 is provided with a containing groove 9 for containing the battery, a compartment opening is provided at the top of the containing groove 9, and the compartment opening is used for the battery to be loaded into the containing groove 9 from the top of the battery compartment; the battery comprises a top shell 1 and an electric core 2, wherein the electric core 2 is fixed on the lower part of the top shell 1, and the electric core 2 comprises a metal shell so as to be convenient for heat dissipation, and the electric core 2 can be welded with the top shell 1 into a whole and can also be fixedly connected with the top shell by a connecting piece, such as a screw or a bolt.
An elastic insertion piece 3 protrudes outwards from the side part of the top shell 1, and a slot 10 matched with the elastic insertion piece is arranged at the corresponding position of the accommodating groove 9; when the battery is installed in the battery compartment, the top shell 1 seals the compartment opening, and the elastic insertion piece 3 is inserted into the slot 10 to fix the battery in the battery compartment. The top shell 1 of battery uses as the cang gai of battery compartment simultaneously, and when the storage tank was packed into to the electric core of battery, the inserted sheet inserted the slot in, top shell 1 just sealed cang kou, and the battery installation is swift, directly puts into storage tank 9 with electric core 2 in, and the inserted sheet is aimed at the slot position and is inserted and can realize the battery installation, need not additionally to use the cang gai of battery compartment sealed, and convenient operation has improved battery installation effectiveness. Optionally, the corresponding position in electric core bottom is equipped with first connector 6, and the holding tank bottom in battery compartment is equipped with second connector 7, second connector 7 is used for electric core 2 insert arrange in when the storage tank in with first connector 7 connect the cooperation of inserting and then realize the electricity and connect.
Example two:
on the basis of the first embodiment, preferably, the elastic inserting sheet 3 is hinged to the side edge of the top shell 1, and the elastic inserting sheet 3 moves up and down relative to the side part of the top shell 1; the notch of the slot 10 is arranged at the inner side edge of the bin opening, and the slot 10 is formed from the notch to the bin body 8. In order to improve the tightness of the insertion between the elastic insertion piece 3 and the slot 10, a spring 4 is connected between the elastic insertion piece and the battery cell.
In order to quickly take out a battery from a battery compartment, a groove 10 is formed in the surface of the elastic insertion piece 3, a positioning button is arranged in the groove 10, the positioning button comprises a pressing bulge 12 and a compression spring 14, the pressing bulge 12 is arranged in the groove 10 and moves inside and outside relative to the groove 10, and the compression spring 14 is connected between the bottom of the pressing bulge 12 and the bottom of the groove 10; the top of the slot 10 is provided with a positioning hole 11 for the positioning button to pass through from the inside of the slot 10. Preferably, the two elastic inserting pieces 3 are oppositely arranged in the middle of two sides of the top shell. Under the natural state, the protruding protrusion in elasticity inserted sheet of pressing of positioning button, when the battery core when adorning along the storage tank, the slot position is aimed at to the elasticity inserted sheet, presses the arch to push down the recess internal motion to the elasticity inserted sheet at the slot, and the pressure spring compression, when the inserted sheet inserted slot, the protruding positioning hole that gets into inwards in by the slot of pressing of positioning button, presses protruding sealed locating hole and presses protruding surface and locating hole drill way and keep level. When the battery needs to be detached, the positioning button is pressed downwards, the positioning button enters the groove 10 of the elastic insertion piece 3, the positioning button indirectly acts on the elastic insertion piece 3 to move downwards, the battery is pulled out upwards, the elastic insertion piece is separated from the slot, and meanwhile, the battery core is separated from the accommodating groove upwards. Optionally, press protruding both sides and can slide in locating the recess of elasticity inserted sheet, the notch of recess is equipped with and blocks the piece, avoids pressing the arch and breaks away from the recess.
In this embodiment, preferably, the size of the accommodating groove 9 is matched with the electrical core 2, and each side surface of the electrical core is installed in the accommodating groove along each inner side surface of the accommodating groove; the top shell 1 seals the bin opening and the outer edges of the side parts of the top shell are in seamless butt joint with the inner edge of the bin opening. The corners of the accommodating groove 9 are rounded corners, and the battery core corners are matched with the rounded corners.
Example three:
this embodiment provides a fixed wing unmanned aerial vehicle, participates in fig. 6, including fuselage 100, still includes battery compartment subassembly 200, refers to simultaneously and looks like 1-4, battery compartment group, 200 include battery and battery compartment, the battery compartment includes storehouse body 8, the storehouse body be the fuselage partly or install in fuselage 100, in this embodiment, the storehouse body is fuselage 100 partly and fuses as an organic whole with fuselage 100, seted up on the storehouse body 8 and acceptd storage tank 9 of battery, the storage tank top is equipped with the bin opening, the bin opening supplies the battery by the battery compartment top is packed into the storage tank, in this embodiment is equivalent to in that the storage tank of acceping the battery has been seted up at the fuselage top. The battery comprises a top shell 1 and an electric core 2, wherein the electric core 2 is fixed on the lower part of the top shell 1, and the electric core comprises a metal shell so as to be convenient for heat dissipation, can be welded with the top shell into a whole, and can also be fixedly connected with the top shell by adopting a connecting piece, such as a screw or a bolt. An elastic insertion piece protrudes outwards from the side part of the top shell, and a slot matched with the elastic insertion piece is formed in the position corresponding to the accommodating groove; when the battery is installed in the battery compartment, the top shell 1 seals the compartment opening, and the elastic insertion piece 3 is inserted into the insertion groove to fix the battery in the battery compartment. The top shell of battery is simultaneously used as the cang gai of battery compartment, and when the storage tank was packed into to the electricity core of battery, the inserted sheet inserted in the slot, just sealed cang kou of top shell, the battery installation was swift, directly puts into the storage tank with electric core, and the inserted sheet is aimed at slot place and is inserted and can be realized the battery installation, need not additionally to use the cang gai of battery compartment sealed, and convenient operation has improved battery installation effectiveness. Optionally, the corresponding position in electric core bottom is equipped with first connector, and the holding tank bottom in battery compartment is equipped with the second connector, the second connector clip be used for electric core insert arrange in when the storage tank in with first connector clip connect the cooperation and then realize the electricity and connect.
The fixed wing unmanned aerial vehicle that this embodiment provided has set up the battery compartment alone on the fuselage, and the battery includes fixed connection top shell and electric core as an organic whole, and the top shell is the arc, and the top shell belongs to a part of fuselage, and the battery is installed behind the battery compartment, and the top shell just seals the door and forms complete fuselage, the pneumatic conformal with the remaining part of fuselage. Convenient and swift is changed to the battery, can match corresponding unmanned aerial vehicle batch production, and when the battery was changed, the battery that directly will have the top shell changed the battery of renewal after taking off, and dismouting efficiency is higher.
Preferably, the elastic inserting sheet is hinged to the side edge of the top shell, and moves up and down relative to the side part of the top shell; the notch of the slot is arranged at the inner side edge of the bin opening, and the slot is formed from the notch to the bin body. In order to improve the tightness of the insertion between the elastic insertion piece and the slot, the elastic insertion piece is connected with a spring between the electric cores.
In order to quickly take out a battery from a battery compartment, a groove 13 is formed in the surface of the elastic insertion piece 3, a positioning button is arranged in the groove 13, the positioning button comprises a pressing bulge 12 and a pressure spring 14, the pressing bulge 12 is arranged in the groove 13 and moves inside and outside relative to the groove, and the pressure spring 14 is connected between the bottom of the pressing bulge 12 and the bottom of the groove 13; the top of the slot is provided with a positioning hole 11 for the positioning button to pass through from the inside of the slot. Preferably, the elastic insertion pieces are two and are oppositely arranged in the middle of two sides of the top shell. Under the natural state, the protruding locating hole that gets into upwards in by the slot of pressing of positioning button presses protruding sealed locating hole and presses protruding surface and locating hole drill way and keep level, and when the battery core was adorned along the storage tank, the slot position was aimed at to the elasticity inserted sheet, presses the arch and supports down the recess internal motion to the elasticity inserted sheet at the slot, and the pressure spring compression, when the inserted sheet inserted the slot, in the protruding locating hole that upwards gets into by the slot of pressing of positioning button. When the battery needs to be detached, the positioning button is pressed downwards, the positioning button enters the groove of the elastic insertion piece, the elastic insertion piece indirectly acts on the elastic insertion piece, the battery is pulled out downwards through the downward movement of the elastic insertion piece, the elastic insertion piece is separated from the slot, and meanwhile, the battery core is separated from the accommodating groove upwards. Optionally, press protruding both sides and can slide in locating the recess of elasticity inserted sheet, the notch of recess is equipped with and blocks the piece, avoids pressing the arch and breaks away from the recess.
Because current fixed wing unmanned aerial vehicle includes fixed wing screw and many rotor screws usually, many rotor screws are installed in the fuselage both sides more for fixed wing unmanned aerial vehicle VTOL, and the fixed wing screw is installed at the aircraft nose front portion usually, is used for the flight of fixed wing unmanned aerial vehicle. The current required by the multi-rotor propeller is large, the discharge rate of a battery is required to be large, and the battery endurance time is short; the fixed-wing propeller requires low battery discharge rate, relatively small current and long endurance time. At present, a battery is usually adopted to supply power to two propellers, the efficiency is low, and the power consumption requirements of the two propellers are difficult to balance. Although two batteries are separately adopted for supplying power, the two batteries are independently installed, the battery replacement efficiency is low, and the batteries are charged in a troublesome manner and waste time. To overcome this drawback, the battery provided in this embodiment includes two battery cells, and referring to fig. 5, the two battery cells are fixed to the bottom of the top case in parallel. Two electric cores can be installed at the same time in one-time installation, and the two electric cores respectively supply power for the two propellers.
In addition, in order to facilitate the operator to apply the operating force for taking out the battery from the accommodating groove, the pull ring 5 is arranged on the top shell 1, and when the battery needs to be taken out, the battery can be taken out only by pressing the positioning button and pulling the pull ring upwards.
The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention, and various modifications and changes may be made by those skilled in the art. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims (10)

1. A battery compartment assembly is characterized in that the battery compartment assembly (200) comprises a battery and a battery compartment, the battery compartment comprises a compartment body (8), a containing groove (9) for containing the battery is formed in the compartment body (8), a compartment opening is formed in the top of the containing groove (9), and the battery is filled into the containing groove (9) from the top of the battery compartment through the compartment opening; the battery comprises a top shell (1) and an electric core (2), the electric core (2) is fixed at the lower part of the top shell (1), an elastic insertion piece (3) protrudes outwards from the side part of the top shell (1), and a slot (10) matched with the elastic insertion piece (3) is arranged at the corresponding position of the accommodating groove (9); when the battery is installed in the battery compartment, the top shell (1) seals the compartment opening, and the elastic insertion piece (3) is inserted into the insertion groove (10) to fix the battery in the battery compartment.
2. The battery compartment assembly according to claim 1, wherein the elastic insertion piece (3) is hinged to the side edge of the top shell (1), and the elastic insertion piece (3) moves up and down relative to the side part of the top shell (1); the notch of the slot (10) is arranged at the inner side edge of the bin opening, and the slot (10) is formed from the notch to the bin body (8).
3. The battery compartment assembly according to claim 2, wherein a spring (4) is connected between the elastic insert (3) and the battery cell (2).
4. The battery compartment assembly according to claim 2, wherein a groove (13) is formed in the surface of the elastic insertion piece (3), a positioning button is arranged in the groove (13), the positioning button comprises a pressing protrusion (12) and a compression spring (14), the pressing protrusion (12) is arranged in the groove (13) and moves in and out relative to the groove (13), and the compression spring (14) is connected between the bottom of the pressing protrusion (12) and the bottom of the groove (13); the top of the slot (10) is provided with a positioning hole (11) for the positioning button to pass through from the inside of the slot (10).
5. The battery compartment assembly of claim 1, wherein the two elastic insertion pieces (3) are oppositely arranged in the middle of two sides of the top shell (1).
6. The battery compartment assembly according to claim 1, wherein the accommodating groove (9) is sized to fit the battery cell (2), and each side surface of the battery cell (2) is fitted into the accommodating groove (9) along each inner side surface of the accommodating groove (9); the top shell (1) seals the bin opening, and the outer edge of each side part of the top shell (1) is in seamless butt joint with the inner edge of the bin opening.
7. The battery compartment assembly according to claim 6, wherein the corners of the accommodating groove (9) are rounded corners, and the corners of the battery cell (2) are matched with the rounded corners.
8. A fixed wing drone comprising a fuselage (100), characterized by further comprising a battery compartment assembly (200) as claimed in any one of claims 1 to 7; the battery bin assembly (200) comprises a battery and a battery bin, the battery bin comprises a bin body (8), the bin body is one part of a machine body or is arranged on the machine body, and a containing groove (9) for containing the battery is formed in the bin body; the top of the accommodating groove (9) is provided with a bin opening, and the bin opening is used for the battery to be loaded into the accommodating groove from the top of the battery bin.
9. The fixed-wing unmanned aerial vehicle of claim 8, wherein the battery comprises a top case (1) and a battery cell (2), the battery cell (2) is fixed on the lower part of the top case (1), an elastic insertion sheet (3) protrudes outwards from the side part of the top case (1), and a slot (10) matched with the elastic insertion sheet (3) is arranged at a corresponding position of the accommodating groove (9); the top shell (1) is arc-shaped, is a part of the machine body (100) and seals the bin opening.
10. Fixed-wing drone according to claim 9, characterised in that the top shell (1) is provided with a pull ring (5).
CN201920607397.9U 2019-04-29 2019-04-29 Battery compartment subassembly reaches fixed wing unmanned aerial vehicle who contains it Active CN210047614U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201920607397.9U CN210047614U (en) 2019-04-29 2019-04-29 Battery compartment subassembly reaches fixed wing unmanned aerial vehicle who contains it

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201920607397.9U CN210047614U (en) 2019-04-29 2019-04-29 Battery compartment subassembly reaches fixed wing unmanned aerial vehicle who contains it

Publications (1)

Publication Number Publication Date
CN210047614U true CN210047614U (en) 2020-02-11

Family

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Application Number Title Priority Date Filing Date
CN201920607397.9U Active CN210047614U (en) 2019-04-29 2019-04-29 Battery compartment subassembly reaches fixed wing unmanned aerial vehicle who contains it

Country Status (1)

Country Link
CN (1) CN210047614U (en)

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Address after: 211100 No.1 Dongji Avenue, Jiangning Development Zone, Nanjing, Jiangsu Province

Patentee after: Nanjing Tuoxing Intelligent Control Technology Co.,Ltd.

Address before: 210008 Room 101, block B, software building, No.9 Xinghuo Road, Jiangbei new district, Nanjing City, Jiangsu Province

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