CN205203399U - Battery receiving device and unmanned vehicles - Google Patents
Battery receiving device and unmanned vehicles Download PDFInfo
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- CN205203399U CN205203399U CN201520970384.XU CN201520970384U CN205203399U CN 205203399 U CN205203399 U CN 205203399U CN 201520970384 U CN201520970384 U CN 201520970384U CN 205203399 U CN205203399 U CN 205203399U
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- battery
- substrate
- locking structure
- fixing frame
- connecting hole
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- 239000000758 substrate Substances 0.000 claims description 120
- 238000005192 partition Methods 0.000 claims description 38
- 125000006850 spacer group Chemical group 0.000 claims description 6
- 239000003054 catalyst Substances 0.000 claims description 4
- 239000011541 reaction mixture Substances 0.000 claims description 4
- 230000002708 enhancing effect Effects 0.000 claims description 2
- 230000003014 reinforcing effect Effects 0.000 abstract 1
- 238000009434 installation Methods 0.000 description 3
- 230000004308 accommodation Effects 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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- Battery Mounting, Suspending (AREA)
Abstract
The utility model provides a battery receiving device, includes first base plate, second base plate and a plurality of battery fixed frame. A plurality of battery fixed frame be radial set up in between first base plate and the second base plate. Each it accepts the chamber to be formed with power supply pond male on the battery fixed frame, it is used for acceping the battery to accept the chamber. The utility model discloses still relate to an use the unmanned vehicles of battery receiving device. The utility model discloses a battery receiving device is through being radial setting with a plurality of battery fixed frame, but the quantity of battery is used in the according to actual need increase and decrease in practical application, when lightening complete machine weight, has guaranteed still that the body nodal point is balanced, the flight or the travelling performance of the carrier that the reinforcing was used.
Description
Technical Field
The utility model relates to a battery assembly technical field, in particular to battery accommodation device and use battery accommodation device's unmanned vehicles.
Background
The battery installation scheme of current aircraft is mostly through magic subsides with the battery bonding at the top or the bottom of aircraft, but such bonding mode can make between battery and the aircraft be connected insecure, leads to the battery to deviate from the aircraft easily in the aircraft flight process. Secondly, in order to prolong the flight time of the aircraft, the battery capacity is generally increased, which results in an excessively large battery volume, inconvenient installation in the fuselage, wasted fuselage space, occupation of the top and bottom space, and no installation position of the external extension piece. Meanwhile, in order to enhance the rigidity of the fuselage, a plurality of structural connecting pieces are required to be added in the fuselage, so that the additional weight is increased, and the endurance of the aircraft is reduced. In addition, the batteries bonded by the bonding mode cannot ensure the repeated precision of bonding every time, so that the center of gravity of the aircraft body is changed frequently, and the flight performance of the aircraft is influenced.
SUMMERY OF THE UTILITY MODEL
In view of the above, it is necessary to provide a battery accommodating device and an unmanned aerial vehicle using the battery accommodating device to solve the above problems.
A battery containment device comprising:
a first substrate and a second substrate;
the battery fixing frames are radially arranged between the first substrate and the second substrate, and each battery fixing frame is provided with an accommodating cavity for inserting a battery, and the accommodating cavity is used for accommodating the battery.
Further, the plurality of cell fixing frames are uniformly arranged between the first substrate and the second substrate; or,
the plurality of cell fixing frames are arranged between the first substrate and the second substrate in a central symmetry manner.
Further, the plurality of cell fixing frames are arranged along the same plane; or, the plurality of battery fixing frames are disposed between the first substrate and the second substrate in a stacked manner.
Furthermore, a first locking structure is arranged on the inner wall of the accommodating cavity and used for being matched with a second locking structure on the battery when the battery is inserted into the accommodating cavity, so that the battery is locked in the accommodating cavity.
The battery accommodating device further comprises a plurality of partition plates, the partition plates are radially arranged and supported between the first substrate and the second substrate, each battery fixing frame is arranged between the far ends of the two adjacent partition plates, the accommodating cavity on each battery fixing frame is a through hole with openings at two ends, and the near ends of the two adjacent partition plates respectively abut against the ends of the battery penetrating through the accommodating cavity when the battery is inserted into the accommodating cavity.
Furthermore, a plurality of through holes are respectively formed on the partition board and/or the battery fixing frame.
Further, the partition plates are detachably connected with the first substrate and the second substrate, respectively.
Furthermore, the partition board is provided with connecting holes, the first substrate and the second substrate are respectively provided with connecting holes opposite to the connecting holes on the partition board, the first substrate and the partition board are fixed together through the matching of connecting pieces and the first substrate and the opposite connecting holes on the partition board, and the second substrate and the partition board are fixed together through the matching of connecting pieces and the second substrate and the opposite connecting holes on the partition board.
Furthermore, the clapboard is also provided with a supporting rod vertical to the clapboard on one side contacted with the first substrate or the second substrate, and the supporting rod is detachably connected with the first substrate or the second substrate and is used for avoiding the clapboard from twisting between the first substrate or the second substrate and enhancing the supporting force provided by the clapboard between the first substrate and the second substrate.
Further, the battery fixing frame is detachably connected with the first substrate and the second substrate, respectively.
Furthermore, the battery fixing frame is provided with connecting holes, the first substrate and the second substrate are respectively provided with connecting holes opposite to the connecting holes on the battery fixing frame, the first substrate and the battery fixing frame are fixed together through the matching of connecting pieces and the first substrate and the opposite connecting holes on the battery fixing frame, and the second substrate and the battery fixing frame are fixed together through the matching of connecting pieces and the second substrate and the opposite connecting holes on the battery fixing frame.
Furthermore, the connecting hole is a threaded hole, and the connecting piece is a screw.
An unmanned aerial vehicle comprising a battery receptacle as described above, the battery receptacle constituting a fuselage of the unmanned aerial vehicle.
Furthermore, the unmanned aerial vehicle also comprises a plurality of batteries, each battery comprises a battery body, an elastic sheet and a second locking structure, the elastic sheet is arranged on the side face of one end of the battery body, and the elastic sheet is far away from the battery body in a natural state; the second locking structure is arranged on the elastic sheet, the elastic sheet abuts against the inner wall of the accommodating cavity of the battery accommodating device when the battery is inserted into the accommodating cavity of the battery accommodating device, and the second locking structure on the elastic sheet is matched with the first locking structure on the battery accommodating device, so that the battery is locked in the accommodating cavity.
Furthermore, the elastic sheet is elastically deformed under the action of external force and moves towards the direction close to the battery body, and the second locking structure on the elastic sheet is separated from the first locking structure on the battery accommodating device along with the movement of the elastic sheet, so that the battery is separated from the accommodating cavity of the battery accommodating device.
Furthermore, the elastic sheet extends from at least one side surface of the battery body to the direction of inserting the battery body into the end part of the accommodating cavity, the extending tail end is separated from the battery body, and the second locking structure is arranged at the free end of the elastic sheet; or,
the elastic sheet is convexly arranged on at least one side face of one end of the battery body, and the second locking structure is arranged on the position, far away from the battery body, of the elastic sheet.
Furthermore, the first locking structure on the battery fixing frame is a rib or a clamping groove, and the second locking structure on the battery is a hook structure; or,
the first locking structure on the battery fixing frame is a convex structure, and the second locking structure on the battery is a groove structure; or,
the first locking structure on the battery fixing frame is of a groove structure, and the second locking structure on the battery is of a protrusion structure.
Furthermore, two or more batteries are integrated in a splicing mode and then are accommodated in the accommodating cavity of the battery fixing frame.
Furthermore, each battery is accommodated in a battery box, or the batteries and the battery boxes are integrally formed, a splicing structure is arranged on the side face of each battery box, and the battery boxes are spliced with one or more battery boxes through the splicing structures.
Further, the first base plate and the second base plate of the battery accommodating device respectively form an upper cover plate and a lower cover plate of the unmanned aerial vehicle body.
Further, the unmanned aerial vehicle further comprises a plurality of arms, and the plurality of arms are respectively installed between two adjacent battery fixing frames of the battery accommodating device; and/or the presence of a catalyst in the reaction mixture,
the unmanned aerial vehicle further comprises a landing gear mounted on the second substrate of the battery receptacle; and/or the presence of a catalyst in the reaction mixture,
the unmanned aerial vehicle further comprises a load connection mechanism, and the load connection mechanism is mounted on the outer surface of the second substrate of the battery accommodating device.
The utility model discloses a battery accommodate device uses the mode replacement of the great single battery continuation of journey of capacity to adopt the mode of the relatively less a plurality of batteries continuation of journey of capacity through with current aircraft, is radial setting at the fuselage middle part with a plurality of battery fixed frame, through the rigidity of battery and battery fixed frame self, can strengthen the holistic structural strength of aircraft to make full use of unmanned vehicles's inner space, for unmanned vehicles extension outside subassembly has reserved the space. In addition, through the radial arrangement of a plurality of battery fixed frames, the quantity of batteries that can increase and decrease according to actual need uses in practical application, when lightening complete machine weight, has still guaranteed fuselage focus balance, strengthens the carrier that applies to, for example the flight performance of unmanned vehicles.
Drawings
Fig. 1 is a perspective view of a battery accommodating apparatus according to an embodiment of the present invention.
Fig. 2 is an internal structural view of the battery housing device of fig. 1.
Fig. 3 is an exploded view of the battery housing device of fig. 1.
Fig. 4 is a perspective view of a battery according to an embodiment of the present invention.
Fig. 5 is a perspective view of a battery pack according to an embodiment of the present invention.
Fig. 6 is a perspective view of a plurality of batteries according to an embodiment of the present invention spliced together by a battery box.
Fig. 7 is a perspective view of an unmanned aerial vehicle including the battery receptacle of fig. 1 according to an embodiment of the present invention.
Fig. 8 is a partial cross-sectional view of an electronic device including the battery receiving device of fig. 1 according to an embodiment of the present invention.
Description of the main elements
| Battery holding device | 20 |
| First substrate | 21 |
| Connecting hole | 211 |
| Second substrate | 22 |
| Connecting hole | 221 |
| Partition board | 23 |
| Connecting hole | 231 |
| Through hole | 232 |
| Support rod | 233 |
| Battery fixing frame | 24 |
| Containing cavity | 241 |
| First locking structure | 242 |
| Connecting hole | 243 |
| Through hole | 244 |
| Battery with a battery cell | 30 |
| Battery body | 31 |
| Spring plate | 32 |
| Second locking structure | 33 |
| Battery box | 34 |
| Aircraft with a flight control device | 1 |
| Machine arm | 101 |
| Landing gear | 102 |
| Load connecting mechanism | 103 |
| Antenna with a shield | 104 |
| Electronic device | 2 |
| Fuselage body | 12 |
The following detailed description of the invention will be further described in conjunction with the above-identified drawings.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only 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.
Fig. 1-2 are perspective views of a battery accommodating device 20 according to an embodiment of the present invention. The battery receiving device 20 includes a first substrate 21, a second substrate 22, and a plurality of battery fixing frames 24. The plurality of battery fixing frames 24 are radially disposed and supported between the first substrate 21 and the second substrate 22. In the present embodiment, each of the battery fixing frames 24 is formed with a receiving cavity 241 (as shown in fig. 3) for receiving the battery 30, and the receiving cavity 241 is used for receiving the battery 30.
In the present embodiment, the plurality of cell fixing frames 24 are uniformly arranged between the first substrate 21 and the second substrate 22. In other embodiments, the plurality of cell fixing frames 24 may be arranged between the first substrate 21 and the second substrate 22 in a central symmetry.
In the present embodiment, the plurality of cell fixing frames 24 are arranged along the same plane so as to reduce the interval between the first and second substrates 21 and 22, thereby reducing the overall thickness of the cell housing device 20. In other embodiments, the plurality of cell fixing frames 24 may also be disposed between the first substrate 21 and the second substrate 22 in a stacked manner, that is, a portion of the plurality of cell fixing frames 24 is arranged along the same plane, another portion is arranged along another plane, and two portions of the cell fixing frames 24 are stacked in a direction from the first substrate 21 to the second substrate 22. The two portions of the battery fixing frame 24 may be completely overlapped or partially overlapped in a direction from the first substrate 21 to the second substrate 22. In other embodiments, the battery fixing frames 24 may be stacked in three or more layers.
Referring to fig. 3, in the present embodiment, a first locking structure 242 is disposed on an inner wall of the receiving cavity 241, and the first locking structure 242 is configured to cooperate with a second locking structure 33 (shown in fig. 4) on the battery 30 when the battery 30 is inserted into the receiving cavity 241, so as to lock the battery 30 in the receiving cavity 241.
Referring to fig. 4, the battery 30 includes a battery body 31, a spring plate 32, and a second locking structure 33. The elastic sheet 32 is disposed on a side surface of one end of the battery body 31, and the elastic sheet 32 is away from the battery body 31 in a natural state. The second locking structure 33 is disposed on the elastic sheet 32.
When the battery 30 is inserted into the accommodating cavity 241, the elastic sheet 32 can be elastically deformed and move toward the battery body 31 under the action of external force. When the external force disappears, the elastic sheet 32 recovers deformation under the action of the resilience force and abuts against the inner wall of the accommodating cavity 241, and the second locking structure 33 on the elastic sheet 32 is matched with the first locking structure 242, so that the battery 30 is locked in the accommodating cavity 241.
Similarly, when the battery 30 needs to be taken out, the elastic sheet 32 can be deformed and move in a direction approaching the battery body 31 under the action of an external force, and the second locking structure 33 on the elastic sheet 32 is separated from the first locking structure 242 on the battery accommodating device 20 following the movement of the elastic sheet 32, so that the battery 30 is separated from the accommodating cavity 241 of the battery accommodating device 20.
In this embodiment, the elastic piece 32 extends from at least one side surface of the battery body 31 in a direction in which the battery body 31 is inserted into the end portion of the accommodating cavity 241, and an extending end is separated from the battery body 31, and the second locking structure 33 is disposed at a free end of the elastic piece 32.
In other embodiments, the elastic sheet 32 may be protruded from at least one side of one end of the battery body 31, and the second locking structure 33 is disposed at a position where the elastic sheet 32 is far away from the battery body 31.
In this embodiment, the first locking structure 242 on the battery fixing frame 24 is a rib, and the second locking structure 33 on the battery 30 is a hook structure. In other embodiments, the first locking structure 242 on the battery fixing frame 24 can be a locking slot, and the second locking structure 33 on the battery 30 can be a hook structure. Alternatively, the first locking structure 242 on the battery fixing frame 24 may be a protrusion structure, and correspondingly, the second locking structure 33 on the battery 30 may be a groove structure. Alternatively, the first locking structure 242 on the battery fixing frame 24 may be a groove structure, and correspondingly, the second locking structure 33 on the battery 30 may be a protrusion structure.
In other embodiments, two or more batteries 30 may be assembled into a whole and then received in the receiving cavity 241 of the battery fixing frame 24. In the other embodiments, as shown in fig. 5, each of the batteries 30 may be received in a battery compartment 34, or the batteries 30 may be integrally formed with the battery compartment 34. The battery box 34 is provided with a splicing structure (not shown) on the side surface, and as shown in fig. 6, the battery box 34 can be spliced with one or more battery boxes 34 through the splicing structure.
Referring to fig. 3 again, the battery receiving device 20 further includes a plurality of spacers 23 radially disposed and supported between the first substrate 21 and the second substrate 22. In this embodiment, each battery fixing frame 24 is disposed between the far ends of the two adjacent partition boards 23, the receiving cavity 241 on the battery fixing frame 24 is a through hole with openings at both ends, and the shortest distance between the two adjacent partition boards 23 is smaller than or equal to the width of the battery 30, so that the ends of the two adjacent partition boards 23 with the shorter distance respectively abut against the ends of the battery 30 passing through the receiving cavity 241 when the battery 30 is inserted into the receiving cavity, thereby fixing the battery 30 in the receiving cavity more firmly.
The utility model discloses a battery accommodate device 20 is through battery fixed frame 24 with set up corresponding locking structure on the battery 30, and through adjacent two the baffle 23 support at a distance from nearer one end in battery 30 inserts accept the tip of chamber 241, thereby can guarantee battery 30 inserts the reliability and stability after accepting chamber 241 avoids taking place battery 30 to follow effectively in removal or the flight process accept the accident of deviating from in the chamber 241.
In the present embodiment, the partition 23 is detachably connected to the first substrate 21 and the second substrate 22, respectively. In this embodiment, the partition 23 is provided with a connection hole 231, the first substrate 21 and the second substrate 22 are respectively provided with connection holes 211 and 221 facing the connection hole 231 of the partition 23, the first substrate 21 and the partition 23 are fixed together by a connection member (not shown) engaging with the connection holes 211 and 231 facing the first substrate 21 and the partition 23, and the second substrate 22 and the partition 23 are fixed together by a connection member (not shown) engaging with the connection holes 221 and 231 facing the second substrate 22 and the partition 23.
In the present embodiment, the battery fixing frame 24 is detachably connected to the first substrate 21 and the second substrate 22, respectively. In this embodiment, the battery fixing frame 24 is provided with a connecting hole 243, the first substrate 21 and the second substrate 22 are respectively provided with connecting holes 212 and 222 opposite to the connecting hole 243 on the battery fixing frame 24, the first substrate 21 and the battery fixing frame 24 are fixed together by a connecting member (not shown) matching with the connecting holes 212 and 243 on the first substrate 21 and the battery fixing frame 24, and the second substrate 22 and the battery fixing frame 24 are fixed together by a connecting member (not shown) matching with the connecting holes 222 and 243 on the second substrate 22 and the battery fixing frame 24.
In this embodiment, the connection holes 211, 212, 221, 222, 231, and 243 are screw holes, and the connection member is a screw.
In the present embodiment, the partition 23 and the battery fixing frame 24 are respectively provided with a plurality of through holes 232 and 244, so that the overall weight of the battery housing device 20 is reduced while ensuring sufficient supporting force between the first base plate 21 and the second base plate 22.
In this embodiment, the partition 23 is further provided with a support rod 233 substantially perpendicular to the partition 23 on a side contacting with the first substrate 21 or the second substrate 22, and the support rod 233 is detachably connected to the first substrate 21 or the second substrate 22, so as to prevent the partition 23 from twisting between the first substrate 21 and the second substrate 22 and enhance a supporting force provided by the partition 23 between the first substrate 21 and the second substrate 22. In other embodiments, the support bar 233 may be omitted.
In the present embodiment, as shown in fig. 7, the battery housing device 20 may be applied to an unmanned aerial vehicle 1. Wherein the unmanned aerial vehicle 1 further comprises a plurality of the batteries 30. In the present embodiment, the battery housing device 20 constitutes the fuselage of the unmanned aerial vehicle 1 and is configured to house the battery 30. In the present embodiment, the first base plate 21 and the second base plate 22 of the battery housing device 20 can be used as an upper cover plate and a lower cover plate of the fuselage of the unmanned aerial vehicle 1, respectively, so that the overall weight of the unmanned aerial vehicle 1 can be reduced.
In the present embodiment, the unmanned aerial vehicle 1 further includes, but is not limited to, a horn 101, a landing gear 102, and a load connection mechanism 103, wherein the number of the horn 101 may be plural, and the horns are respectively installed between two adjacent battery fixing frames 24 of the battery receiving device 20. The landing gear 102 may be mounted on the second base plate 22 of the battery receptacle 20, and the load attachment mechanism 103, such as a cradle head, may be mounted on an outer surface of the second base plate 22 of the battery receptacle 20.
The battery fixing frame 24 may also serve as a carrier for other functional hardware of the unmanned aerial vehicle 1, for example, the outer surface of the first substrate 21 of the battery fixing frame 24 may be used for mounting the antenna 104 of the unmanned aerial vehicle 1.
Because a plurality of battery fixed frame 24 are radial even arrangement or are central symmetry and arrange, make accept in battery fixed frame 24 battery 30 also is radial even or be central symmetry and set up on unmanned vehicles 1 fuselage, thereby can guarantee unmanned vehicles 1's the focus with unmanned vehicles 1's the center coincidence improves the stability of flight.
It is understood that when the unmanned aerial vehicle 1 requires only a short dead time, all the accommodating cavities 241 of the battery accommodating device 20 do not need to be loaded with the batteries 30 at the same time, so that the overall weight of the unmanned aerial vehicle 1 is reduced and the endurance is prolonged.
The utility model discloses a mode replacement that battery accommodate device 20 continued the journey through the great single battery 30 of the aircraft 1 use capacity that will be used now is the mode of adopting the relatively less a plurality of batteries 30 of capacity to continue the journey, and is radial setting at the fuselage middle part with a plurality of battery fixed frame 24, through battery 30 and the rigidity of battery fixed frame 24 self can strengthen the holistic structural strength of aircraft 1, and make full use of unmanned vehicles 1's inner space, for unmanned vehicles 1 extension outside subassembly has reserved the space. In addition, through the radial arrangement of a plurality of battery fixed frames 24, the quantity of batteries that can increase and decrease according to actual need uses in practical application, when lightening complete machine weight, has still guaranteed fuselage focus balance, strengthens unmanned vehicles 1's flight performance.
In other embodiments, as shown in fig. 8, the battery receiving apparatus 20 may also be applied to an electronic apparatus 2. The electronic device 2 may be a remote controller or a mobile device such as a remote control combat tank, and the electronic device 2 further includes a body 12 and a plurality of the batteries 30. The battery receptacle 20 is mounted in the middle of the main body 12 and forms a part of the main body 12, that is, the first base plate 21 and/or the second base plate 22 of the battery receptacle 20 may be an upper cover plate and/or a lower cover plate of the main body 12, thereby reducing the overall weight of the electronic device 2. The battery receiving device 20 is used for receiving the battery 30. By radially disposing the plurality of battery fixing frames 24 in the middle of the body 12 of the electronic device 2, the internal space of the electronic device 2 can be fully utilized, and space is reserved for expanding external components of the electronic device 2. In addition, the battery 30 can be reduced according to actual needs, so that the weight of the whole machine is reduced, the gravity center balance of the whole machine is ensured, and the moving performance of the electronic device 2 is improved.
Finally, it should be noted that the above embodiments are only used for illustrating the technical solutions of the present invention and not for limiting, and although the present invention has been described in detail with reference to the preferred embodiments, it should be understood by those skilled in the art that modifications or equivalent substitutions can be made on the technical solutions of the present invention without departing from the spirit and scope of the technical solutions of the present invention.
Claims (21)
1. A battery containment device comprising:
a first substrate and a second substrate;
the battery fixing frames are radially arranged between the first substrate and the second substrate, and each battery fixing frame is provided with an accommodating cavity for inserting a battery, and the accommodating cavity is used for accommodating the battery.
2. The battery housing device of claim 1, wherein the plurality of battery securing frames are evenly arranged between the first substrate and the second substrate; or,
the plurality of cell fixing frames are arranged between the first substrate and the second substrate in a central symmetry manner.
3. The battery housing device of claim 2, wherein said plurality of battery holding frames are arranged along a common plane; or, the plurality of battery fixing frames are disposed between the first substrate and the second substrate in a stacked manner.
4. The battery containment apparatus of claim 2, wherein the interior wall of the housing cavity has a first locking structure for engaging a second locking structure on the battery when the battery is inserted into the housing cavity to lock the battery in the housing cavity.
5. The battery receiving device according to claim 2, wherein the battery receiving device further comprises a plurality of partition plates, the partition plates are radially arranged and supported between the first substrate and the second substrate, each battery fixing frame is arranged between the ends of two adjacent partition plates that are far away from each other, the receiving cavities on the battery fixing frames are through holes with openings at two ends, and the ends of two adjacent partition plates that are near to each other respectively abut against the ends of the batteries that pass through the receiving cavities when the batteries are inserted into the receiving cavities.
6. The battery housing apparatus of claim 5, wherein the separator and/or the battery mounting frame each have a plurality of through holes.
7. The battery containment apparatus of claim 5, wherein the spacer is removably attached to the first substrate and the second substrate, respectively.
8. The battery housing device according to claim 7, wherein the partition plate is provided with a connecting hole, the first substrate and the second substrate are respectively provided with a connecting hole opposite to the connecting hole of the partition plate, the first substrate and the partition plate are fixed together by a connecting member engaged with the first substrate and the connecting hole opposite to the partition plate, and the second substrate and the partition plate are fixed together by a connecting member engaged with the second substrate and the connecting hole opposite to the partition plate.
9. The battery housing apparatus of claim 5, wherein the spacer is further provided with a support bar perpendicular to the spacer on a side contacting the first substrate or the second substrate, the support bar being detachably connected to the first substrate or the second substrate for preventing the spacer from twisting between the first substrate or the second substrate and enhancing a supporting force provided by the spacer between the first substrate and the second substrate.
10. The battery containment apparatus of claim 1, wherein the battery securing frame is removably attached to the first substrate and the second substrate, respectively.
11. The battery housing apparatus according to claim 10, wherein the battery fixing frame is provided with a connecting hole, the first substrate and the second substrate are respectively provided with a connecting hole opposite to the connecting hole of the battery fixing frame, the first substrate and the battery fixing frame are fixed together by a connecting member engaged with the first substrate and the connecting hole of the battery fixing frame, and the second substrate and the battery fixing frame are fixed together by a connecting member engaged with the second substrate and the connecting hole of the battery fixing frame.
12. The battery housing apparatus of claim 8 or 11, wherein the attachment holes are threaded holes and the attachment members are screws.
13. An unmanned aerial vehicle comprising:
the battery receptacle of any of claims 1-11, constituting a fuselage of the UAV.
14. The unmanned aerial vehicle of claim 13, further comprising a plurality of batteries, wherein the batteries comprise a battery body, a spring plate and a second locking structure, the spring plate is disposed on a side surface of one end of the battery body, and the spring plate is naturally away from the battery body; the second locking structure is arranged on the elastic sheet, the elastic sheet abuts against the inner wall of the accommodating cavity of the battery accommodating device when the battery is inserted into the accommodating cavity of the battery accommodating device, and the second locking structure on the elastic sheet is matched with the first locking structure on the battery accommodating device, so that the battery is locked in the accommodating cavity.
15. The unmanned aerial vehicle of claim 14, wherein the resilient tab is elastically deformed by an external force and moves in a direction approaching the battery body, and the second locking structure on the resilient tab disengages from the first locking structure on the battery receptacle following the movement of the resilient tab, so that the battery is removed from the receiving cavity of the battery receptacle.
16. The UAV of claim 15, wherein the resilient tab extends from at least one side of the battery body in a direction in which the battery body is inserted into the receiving cavity, and has an extended end separated from the battery body, and the second locking structure is disposed at a free end of the resilient tab; or,
the elastic sheet is convexly arranged on at least one side face of one end of the battery body, and the second locking structure is arranged on the position, far away from the battery body, of the elastic sheet.
17. The UAV of claim 14 wherein the first locking feature on the battery mounting frame is a rib or a slot and the second locking feature on the battery is a hook; or,
the first locking structure on the battery fixing frame is a convex structure, and the second locking structure on the battery is a groove structure; or,
the first locking structure on the battery fixing frame is of a groove structure, and the second locking structure on the battery is of a protrusion structure.
18. The UAV of claim 14 wherein two or more batteries are assembled into a unit and then received in the receiving cavity of the battery mounting frame.
19. The UAV of claim 18 wherein each battery is housed in a battery compartment or the batteries are integrally formed with the battery compartment, and the battery compartment has a splicing structure on its side, and the battery compartment is spliced with one or more battery compartments by the splicing structure.
20. The UAV of claim 13 wherein the first and second base plates of the battery receptacle constitute upper and lower cover plates, respectively, of a fuselage of the UAV.
21. The unmanned aerial vehicle of claim 13 or 20, further comprising a plurality of horn mounted between two adjacent battery securing frames of the battery receptacle device, respectively; and/or the presence of a catalyst in the reaction mixture,
the unmanned aerial vehicle further comprises a landing gear mounted on the second substrate of the battery receptacle; and/or the presence of a catalyst in the reaction mixture,
the unmanned aerial vehicle further comprises a load connection mechanism, and the load connection mechanism is mounted on the outer surface of the second substrate of the battery accommodating device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520970384.XU CN205203399U (en) | 2015-11-30 | 2015-11-30 | Battery receiving device and unmanned vehicles |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520970384.XU CN205203399U (en) | 2015-11-30 | 2015-11-30 | Battery receiving device and unmanned vehicles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205203399U true CN205203399U (en) | 2016-05-04 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520970384.XU Expired - Fee Related CN205203399U (en) | 2015-11-30 | 2015-11-30 | Battery receiving device and unmanned vehicles |
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| Country | Link |
|---|---|
| CN (1) | CN205203399U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018103576A1 (en) * | 2016-12-05 | 2018-06-14 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
| CN108860626A (en) * | 2018-06-12 | 2018-11-23 | 天津天喜科技有限公司 | Battery installation device for civil unmanned aircraft |
-
2015
- 2015-11-30 CN CN201520970384.XU patent/CN205203399U/en not_active Expired - Fee Related
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018103576A1 (en) * | 2016-12-05 | 2018-06-14 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
| EP3369658A4 (en) * | 2016-12-05 | 2018-12-05 | Autel Robotics Co., Ltd. | Unmanned aerial vehicle |
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