CN205707289U - Unmanned plane battery hatch structure and unmanned plane - Google Patents
Unmanned plane battery hatch structure and unmanned plane Download PDFInfo
- Publication number
- CN205707289U CN205707289U CN201620532134.2U CN201620532134U CN205707289U CN 205707289 U CN205707289 U CN 205707289U CN 201620532134 U CN201620532134 U CN 201620532134U CN 205707289 U CN205707289 U CN 205707289U
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- battery hatch
- locking piece
- battery
- unmanned plane
- locating part
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Abstract
This utility model relates to a kind of unmanned plane battery hatch structure and unmanned plane, this unmanned plane battery hatch structure includes body, battery hatch, the first locking piece being arranged on body, the second locking piece being arranged in battery hatch and can be mutually locked with the first locking piece, the first locating part being arranged on body, the second locating part being arranged in battery hatch and the button being arranged on body release assembly, body is provided with battery flat, battery hatch is slidably connected on body and can cover the opening of battery flat, the spacing cooperation of the first locating part and the second locating part is used for stoping battery hatch opposing body to slide, button release assembly includes release button and the back-moving spring being slidably arranged on body, spacing cooperation between first locating part and the second locating part can be released by pressing release button.Unmanned plane battery hatch structure of the present utility model, it is not necessary to use specific purpose tool, battery hatch opens conveniently, simple, and opening time is shorter.
Description
Technical field
This utility model belongs to vehicle technology field, particularly relates to a kind of unmanned plane battery hatch structure and unmanned
Machine.
Background technology
Existing unmanned plane, the flight time enough in order to ensure unmanned plane, battery is typically designed to removable mode,
Battery is arranged in the battery flat that body interior is formed, and is provided with battery hatch at the outside opening of battery flat.Due to unmanned plane
Vibration frequency during flight is the highest in the sky, and it is firm that this requires that battery hatch is connected with body, and otherwise battery hatch once departs from
Body, will cause battery loosen, power down, unmanned plane will lose efficacy, cause unmanned plane to fall or ground control lost efficacy, consequence is tight
Weight.
Thus, existing a part of unmanned plane, between battery hatch and body, commonly used snap fit is fixed, by snap fit
Crimp thus open battery hatch, in order to ensure unmanned plane performance safety, snap fit design very difficult releasing, it usually needs borrow
Assistant engineer's tool can release the locking of snap fit, the most just can take off battery hatch, and opening of battery hatch is difficult and loaded down with trivial details, this
Sample, needs take off battery be replaced or charge time, need the longer time.
Utility model content
Technical problem to be solved in the utility model is for existing unmanned plane its battery hatch of battery hatch structure
Open the defect of more difficulty, it is provided that a kind of unmanned plane battery hatch structure.
The technical scheme that the above-mentioned technical problem of this utility model solution is used is:
There is provided a kind of unmanned plane battery hatch structure, including body, battery hatch, setting the first lock on the body
Stop member, be arranged in described battery hatch and can with the second locking piece that described first locking piece is mutually locked, be arranged on described
The first locating part on body, the second locating part being arranged in described battery hatch and setting button on the body
Release assembly, is provided with battery flat in described body, described battery hatch is slidably connected on the body and can cover described
The opening of battery flat, the locking of described first locking piece and the second locking piece and unlocking direction and the glide direction one of battery hatch
Causing, the spacing cooperation of described first locating part and the second locating part is used for stoping battery hatch opposing body to slide, described button
Release assembly includes release button and the back-moving spring for described release push-button reset, the institute being slidably arranged on described body
State the spacing cooperation between the first locating part and the second locating part to be released by pressing described release button.
Further, described body being provided with through hole, described release button is slidably arranged in described through hole, described logical
The outer openings in hole and the ft connection of described body.
Further, described first locating part includes the limit arranging on the body and can sliding along body height direction
Position block, the upper end of described limited block forms the spacing preiection passing described body upper surface, and described second locating part includes arranging
Lock described first at the first postive stop baffle of described battery hatch glide direction side, described limited block and the first postive stop baffle
Abut when stop member and the second locking piece locking, to stop battery hatch opposing body to described first locking piece and the second lock
The unlocking direction of stop member slides；Described back-moving spring upwardly limited block, a side surface of described limited block acts against release
The medial extremity of button, described limited block can when described release button is pressed slide downward depart from described first limiting block
Plate.
Further, described first locating part also includes the second postive stop baffle arranged on the body, described second
Postive stop baffle and described limited block lay respectively at the opposite sides of described body along described battery hatch glide direction, and described second
Locating part includes the 3rd postive stop baffle being arranged on described battery hatch glide direction opposite side, described second postive stop baffle and
Three postive stop baffles abut when described first locking piece and the second locking piece locking, with stop battery hatch opposing body to
Slide in the locking direction of described first locking piece and the second locking piece.
Further, the medial extremity of described release button is formed as the first inclined-plane, and a side surface of described limited block is formed
For the second inclined-plane with described first inclined-plane laminating, described first inclined-plane can push down on the second inclined-plane and drive with this described spacing
Block opposing body's slide downward.
Further, described first locking piece includes being arranged on body and first draw-in groove of release button the same side, institute
State the second locking piece to include being arranged on battery hatch glide direction side and the first snap fit in described first draw-in groove can being snapped in.
Further, described second locking piece also includes the second draw-in groove being arranged on battery hatch glide direction opposite side,
Described first locking piece also includes being arranged on body and can snap in the second snap fit in described second draw-in groove.
Further, the inner surface of described body is formed with the first confined planes and second extended along body height direction
Confined planes, described battery hatch is respectively formed with the first guide plate corresponding to the position of described first confined planes and the second confined planes
And second guide plate, described first guide plate and the second guide plate can respectively with the first confined planes and the second confined planes against, institute
State the first guide plate and the first confined planes against and the second guide plate and the second confined planes against to described battery hatch
Spacing direction be perpendicular to the glide direction of described battery hatch.
Further, described body is provided with protrudes from the first of described first confined planes and the second confined planes respectively and lead
The first guide groove and the second guide groove, institute it is respectively arranged with on muscle and the second guiding rib, described first guide plate and the second guide plate
State the first guiding rib and the second guiding rib can slide respectively and be interspersed in described first guide groove and the second guide groove.
According to unmanned plane battery hatch structure of the present utility model, battery hatch is slidably connected on the body of unmanned plane,
Be provided with on body the first locking piece, the first locating part and button release assembly, battery hatch is provided with the second locking piece and
Second locating part, the locking of the first locking piece and the second locking piece and unlocking direction are consistent with the glide direction of battery hatch, the
The spacing cooperation of one locating part and the second locating part is used for stoping battery hatch opposing body to slide, this first locking piece and second
Locking piece is mutually locked to close battery hatch, and when battery hatch is closed, the opening of the battery flat on covering body, discharges button
Outboard end expose outside body, the release button of pressing button release assembly can release the first locating part and the second locating part it
Between spacing cooperation, and then battery hatch glide direction is spacing is released from, and pulls battery hatch can make to unlocking direction
One locking piece and the second locking piece separate unblock, and battery hatch is opened, and battery can take out from battery flat, relative to existing
Technology, it is not necessary to use specific purpose tool, battery hatch opens conveniently, simple, and opening time is shorter, so, takes off at needs
When battery is replaced or charges, time-consuming less.Further, the first locking piece and the locking of the second locking piece and the first locating part
Spacing with the second locating part coordinates the connection reliability also being able between guarantee battery hatch and body, and battery hatch is difficult to pine
De-, it is ensured that the flight safety of unmanned plane.
It addition, this utility model additionally provides a kind of unmanned plane, it includes above-mentioned unmanned plane battery hatch structure.
Accompanying drawing explanation
Fig. 1 is the unmanned plane battery hatch structure sectional elevation in the first direction that this utility model one embodiment provides
Figure；
Fig. 2 is the enlarged drawing in Fig. 1 at a；
Fig. 3 is the enlarged drawing in Fig. 1 at b；
Fig. 4 is the structural representation of unmanned plane battery hatch its body of structure that this utility model one embodiment provides；
Fig. 5 is the structural representation of unmanned plane battery hatch its battery hatch of structure that this utility model one embodiment provides
Figure；
Fig. 6 is the unmanned plane battery hatch structure sectional elevation in a second direction that this utility model one embodiment provides
Figure；
Fig. 7 is the enlarged drawing in Fig. 6 at c；
Fig. 8 is that unmanned plane its battery hatch of battery hatch structure that this utility model one embodiment provides opens the first stage
Schematic diagram；
Fig. 9 is that unmanned plane its battery hatch of battery hatch structure that this utility model one embodiment provides opens second stage
Schematic diagram；
Figure 10 is the schematic diagram that the unmanned plane battery hatch structure that this utility model one embodiment provides takes out battery；
Figure 11 is the structural representation of the unmanned plane that this utility model one embodiment provides.
Reference in description is as follows:
1, body；11, battery flat；12, through hole；13, the second postive stop baffle；14, the first draw-in groove；15, the second snap fit；16、
First confined planes；17, the second confined planes；18, the first guiding rib；19, the second guiding rib；2, battery hatch；21, the first limiting block
Plate；22, the 3rd postive stop baffle；23, the first snap fit；24, the second draw-in groove；25, the first guide plate；251, the first guide groove；26, second
Guide plate；261, the second guide groove；3, button release assembly；31, release button；311, the first inclined-plane；32, back-moving spring；4, limit
Position block；41, spacing preiection；42, the second inclined-plane；
10, battery；
20, horn；
30, motor is driven；
40, propeller.
Detailed description of the invention
In order to make this utility model be solved the technical problem that, technical scheme and beneficial effect clearer, below
In conjunction with drawings and Examples, this utility model is described in further detail.Should be appreciated that concrete reality described herein
Execute example only in order to explain this utility model, be not used to limit this utility model.
As shown in Figures 1 to 5, this utility model one embodiment provide unmanned plane battery hatch structure, including body 1,
Battery hatch 2, the first locking piece being arranged on described body 1, be arranged in described battery hatch 2 and can with described first lock
The second locking piece, the first locating part being arranged on described body 1 that stop member is mutually locked, it is arranged in described battery hatch 2
The second locating part and be arranged on described body 1 button release assembly 3, described body 1 is provided with battery flat 11, institute
State the opening that battery hatch 2 is slidably connected on described body 1 and can cover described battery flat 11, described first locking piece and
The locking of two locking piece is consistent with the glide direction of battery hatch 2 with unlocking direction, described first locating part and the second locating part
Spacing cooperation be used for stoping battery hatch 2 opposing body 1 to slide, described button release assembly 3 includes being slidably arranged in described
Discharging button 31 and being used for the back-moving spring 32 that described release button 31 resets, described first locating part and second on body 1
Spacing cooperation between locating part can be released by pressing described release button 31.
In the present embodiment, as in figure 2 it is shown, be provided with through hole 12 on described body 1, described release button 31 is slidably arranged in
In described through hole 12, the outer openings of described through hole 12 and the ft connection of described body 1.
In the present embodiment, as shown in Figures 1 to 5, described first locating part includes being arranged on described body 1 and can be along this
The limited block 4 that slides in height direction and the second postive stop baffle 13 of being arranged on described body 1, described second postive stop baffle 13
With the opposite sides that described limited block 4 lays respectively at described body 1 along described battery hatch 2 glide direction, described limited block 4
Upper end forms the spacing preiection 41 passing described body 1 upper surface.Described second locating part includes being arranged on described battery hatch 2
First postive stop baffle 21 of glide direction side and be arranged on the 3rd postive stop baffle of described battery hatch 2 glide direction opposite side
22, described limited block 4 abuts when described first locking piece and the second locking piece locking with the first postive stop baffle 21, with resistance
Only battery hatch 2 opposing body 1 slides to the unlocking direction of described first locking piece and the second locking piece；Described back-moving spring 32
Upwardly limited block 4, a side surface of described limited block 4 acts against the medial extremity of release button 31, and described limited block 4 can be
Slide downward depart from described first postive stop baffle 21 when described release button 31 is pressed.Described second postive stop baffle 13 and
Three postive stop baffles 22 abut when described first locking piece and the second locking piece locking, to stop battery hatch 2 the most originally
Body 1 slides to the locking direction of described first locking piece and the second locking piece.So, at described first locking piece and the second locking
During part locking, abutted by limited block 4 and the first postive stop baffle 21 and the second postive stop baffle 13 and the 3rd postive stop baffle
22 abut, it is possible to stop battery hatch 2 opposing body 1 to described first locking piece and the unblock of the second locking piece and locking
Sliding in direction, so, battery hatch 2 is lower high with the connection reliability of body 1 in off position.
In the present embodiment, as in figure 2 it is shown, the medial extremity of described release button 31 is formed as the first inclined-plane 311, described spacing
One side surface of block 4 is formed as and the second inclined-plane 42 of described first inclined-plane 311 laminating, when pressing release button 31, described
First inclined-plane 311 can push down on the second inclined-plane 42 and drive described limited block 4 opposing body 1 slide downward with this.Set on body 1
Being equipped with the spacing position limiting structure (not indicating in figure) that slides for limited block 4, this position limiting structure makes limited block 4 can only be edge
The short transverse of body 1 is slided.
In the present embodiment, as Fig. 1 is to shown in 5, and described first locking piece includes being arranged on body 1 same with release button 31
First draw-in groove 14 of side and being arranged on body 1 and the second snap fit 15 of the first draw-in groove 14 opposite side, described second locking
Part includes being arranged on battery hatch 2 glide direction side and can snapping in the first snap fit 23 in described first draw-in groove 14 and arrange
At the second draw-in groove 24 of battery hatch 2 glide direction opposite side, described second snap fit 15 can snap in described second draw-in groove 24.
As shown in Fig. 4, Fig. 6 and Fig. 9, the inner surface of described body 1 is formed with first extended along body height direction
Confined planes 16 and the second confined planes 17, described battery hatch 2 is corresponding to described first confined planes 16 and the position of the second confined planes 17
Put and be respectively formed with the first guide plate 25 and the second guide plate 26, described first guide plate 25 and the second guide plate 26 can respectively with
First confined planes 16 and the second confined planes 17 against.
As shown in Fig. 4, Fig. 6 and Fig. 9, described body 1 is provided with and protrudes from described first confined planes 16 and second respectively
First guiding rib 18 and the second guiding rib 19 of confined planes 17, described first guide plate 25 and the second guide plate 26 are respectively provided with
Have the first guide groove 251 and the second guide groove 261, described first guiding rib 18 and the second guiding rib 19 can slide respectively be interspersed in described
In first guide groove 251 and the second guide groove 261, to realize being slidably connected of battery hatch 2 and body 1.Described first guide groove 251 with
The position of the first guiding rib 18 contact can arrange curved surfaces (such as semi-cylindrical), so that battery hatch 2 and the cunning of body 1
Dynamic more smooth and easy；In like manner, the position that the second guide groove 261 contacts with the second guiding rib 19 may also set up curved surfaces (such as semicircle
Cylinder).
As shown in Figures 4 and 5, in the present embodiment, the first draw-in groove 14 and the first snap fit 23 arrange two groups, the second snap fit 15 with
Second draw-in groove 24 arranges two groups equally, and during in such manner, it is possible to guarantor's reinforcement battery hatch 2 is closed further, the connection with body 1 is reliable
Property.
As it is shown in figure 1, the glide direction of described release button 31 is identical with the glide direction of battery hatch 2, battery hatch 2
Glide direction hereinafter referred to as first direction.First snap fit 23 and the first draw-in groove the 14, second snap fit 15 and lock of the second draw-in groove 24
The most consistent with first direction with unlocking direction.
As shown in Figure 6, described first guide plate 25 and the first confined planes 16 against and the second guide plate 26 and second
Confined planes 17 against being the left and right directions in Fig. 6, hereinafter referred to as second direction to the spacing direction of described battery hatch 2.The
Two directions are vertical with first direction.The plane at first direction and the second place is parallel to horizontal plane.The short transverse of body 1 is vertical
In horizontal plane.
Below in conjunction with Fig. 1 to Figure 10, the operation principle of the unmanned plane battery hatch structure of the present embodiment is illustrated.
Original state (battery hatch 2 is closed): as shown in Figures 1 to 7, the first snap fit 23 snaps in the first draw-in groove 14, the
Two snap fits 15 snap in described second draw-in groove 24, and the first guiding rib 18 and the second guiding rib 19 can slide respectively and be interspersed in described
In one guide groove 251 and the second guide groove 261 so that the battery hatch 2 displacement in body 1 short transverse is limited.In first party
Upwards, limited block 4 abuts with the first postive stop baffle 21 and the second postive stop baffle 13 mutually supports with the 3rd postive stop baffle 22
Leaning on, thus, the battery hatch 2 displacement on the first direction of body 1 is limited.It addition, in a second direction, described first leads
To plate 25 and the second guide plate 26 respectively with the first confined planes 16 and the second confined planes 17 against, thus, battery hatch 2 is at body
Displacement in the second direction of 1 is limited.Visible, under the closed mode of battery hatch 2, battery hatch 2 relative to body 1,
In a first direction, second direction and body height direction all obtained good spacing, battery hatch 2 in off position lower with this
The connection of body 1 is the most firm, and battery hatch 2 is difficult to get loose, it is possible to avoids result in the unmanned plane that battery loosens, power down is caused and loses
Effect, it is ensured that the flight safety of unmanned plane.
Sliding opening principle (battery hatch 2 opening procedure): as can be seen from figures 8 and 9, operator press release button 31
And keep (spacing preiection 41 on limited block 4 follows limited block 4 opposing body 1 slide downward), then to the first locking piece with
The unlocking direction of the second locking piece pulls battery hatch 2, when pulling force is more than the locking power of the first locking piece and the second locking piece,
Unlock between battery hatch 2 with body 1 and can relative slide, due to the first guiding rib 18 and the second guiding rib 19 on body 1
Slide respectively in the first guide groove 251 and the second guide groove 261 that are interspersed in battery hatch 2, thus, after this, battery hatch 2 phase
Sliding to unlocking direction for body, Fig. 8 show battery hatch 2 and opens the schematic diagram of first stage, in fig. 8, battery flat
The first guiding rib 18 and the second guiding rib 19 on lid 2 the most do not completely disengage from first guide groove 251 and second of battery hatch 2 and lead
Groove 261.As it is shown in figure 9, the first guiding rib 18 and second after slip certain distance (such as 15mm), in battery hatch 2
Guiding rib 19 completely disengages from the first guide groove 251 and the second guide groove 261 of battery hatch 2, and battery hatch 2 is kept completely separate with body 1.
As shown in Figure 10, the short transverse along body 1 takes out battery 10.
Battery hatch 2 closes principle: battery hatch 2 closing process is contrary with battery hatch 2 opening procedure.
It addition, as shown in figure 11, this utility model one embodiment additionally provides a kind of unmanned plane, and it includes above-described embodiment
Unmanned plane battery hatch structure.
As shown in figure 11, at the top of described body 1 circumferentially on be evenly arranged with four horns 20 (four rotors),
The end of horn 20 is provided with driving motor 30, and driving to connect on the output shaft of motor 30 has propeller 40.
Body 1 arranges battery flat 11, battery flat 11 is provided with battery 10, battery 10 usually rechargeable battery.Battery
10 are arranged in battery flat 11 by similar connectors such as buckles.
Certainly, unmanned plane also should include the parts such as the panel not shown in other parts, such as figure.
The foregoing is only preferred embodiment of the present utility model, not in order to limit this utility model, all at this
Any amendment, equivalent and the improvement etc. made within the spirit of utility model and principle, should be included in this utility model
Protection domain within.
Claims (10)
1. a unmanned plane battery hatch structure, it is characterised in that include that body, battery hatch, setting are on the body
First locking piece, the second locking piece being arranged in described battery hatch and can being mutually locked with described first locking piece, setting
The first locating part on the body, the second locating part being arranged in described battery hatch and setting are on the body
Button release assembly, described body is provided with battery flat, described battery hatch is slidably connected on the body and can cover
Cover the opening of described battery flat, the locking of described first locking piece and the second locking piece and unlocking direction and the slip of battery hatch
Direction is consistent, and the spacing cooperation of described first locating part and the second locating part is used for stoping battery hatch opposing body to slide, institute
State release button and the reset for described release push-button reset that button release assembly includes being slidably arranged on described body
Spring, the spacing cooperation between described first locating part and the second locating part can be released by pressing described release button.
Unmanned plane battery hatch structure the most according to claim 1, it is characterised in that be provided with through hole on described body,
Described release button is slidably arranged in described through hole, the outer openings of described through hole and the ft connection of described body.
Unmanned plane battery hatch structure the most according to claim 1, it is characterised in that described first locating part includes arranging
On the body and the limited block that can slide along body height direction, the upper end of described limited block is formed and passes on described body
The spacing preiection on surface, described second locating part includes the first limiting block being arranged on described battery hatch glide direction side
Plate, described limited block and the first postive stop baffle abut when described first locking piece and the second locking piece locking, to stop
Battery hatch opposing body slides to the unlocking direction of described first locking piece and the second locking piece；Described back-moving spring is pushed up
Dynamic limited block, a side surface of described limited block acts against the medial extremity of release button, and described limited block can be pressed in described release
Slide downward depart from described first postive stop baffle when button is pressed.
Unmanned plane battery hatch structure the most according to claim 3, it is characterised in that described first locating part also includes setting
Putting the second postive stop baffle on the body, described second postive stop baffle and described limited block are along described battery hatch slip side
To laying respectively at the opposite sides of described body, described second locating part include being arranged on described battery hatch glide direction another
3rd postive stop baffle of side, described second postive stop baffle and the 3rd postive stop baffle are locked at described first locking piece and the second locking piece
Abut time only, to stop battery hatch opposing body sliding to the locking direction of described first locking piece and the second locking piece
Dynamic.
Unmanned plane battery hatch structure the most according to claim 3, it is characterised in that the medial extremity shape of described release button
Becoming the first inclined-plane, a side surface of described limited block is formed as and the second inclined-plane of described first inclined-plane laminating, and described first
Inclined-plane can push down on the second inclined-plane and drive described limited block opposing body's slide downward with this.
Unmanned plane battery hatch structure the most according to claim 1, it is characterised in that described first locking piece includes arranging
On body with release button the same side the first draw-in groove, described second locking piece includes being arranged on battery hatch glide direction one
Side also can snap in the first snap fit in described first draw-in groove.
Unmanned plane battery hatch structure the most according to claim 6, it is characterised in that described second locking piece also includes setting
Putting the second draw-in groove at battery hatch glide direction opposite side, described first locking piece also includes being arranged on body and can snapping in
The second snap fit in described second draw-in groove.
8. according to the unmanned plane battery hatch structure described in claim 1-7 any one, it is characterised in that described body interior
Side surface is formed with the first confined planes and the second confined planes extended along body height direction, and described battery hatch is corresponding to described
The position of the first confined planes and the second confined planes is respectively formed with the first guide plate and the second guide plate, described first guide plate and
Second guide plate can respectively with the first confined planes and the second confined planes against, described first guide plate and the first confined planes against
And second guide plate and the second confined planes be perpendicular to described battery hatch against to the spacing direction of described battery hatch
Glide direction.
Unmanned plane battery hatch structure the most according to claim 8, it is characterised in that be provided with on described body and dash forward respectively
For described first confined planes and the first guiding rib of the second confined planes and the second guiding rib, described first guide plate and second is led
On plate, it is respectively arranged with the first guide groove and the second guide groove, described first guiding rib and the second guiding rib can slide respectively and be interspersed in
In described first guide groove and the second guide groove.
10. a unmanned plane, it is characterised in that include the unmanned plane battery hatch structure described in claim 1-9 any one.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620532134.2U CN205707289U (en) | 2016-06-02 | 2016-06-02 | Unmanned plane battery hatch structure and unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620532134.2U CN205707289U (en) | 2016-06-02 | 2016-06-02 | Unmanned plane battery hatch structure and unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205707289U true CN205707289U (en) | 2016-11-23 |
Family
ID=57300444
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
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| CN201620532134.2U Active CN205707289U (en) | 2016-06-02 | 2016-06-02 | Unmanned plane battery hatch structure and unmanned plane |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107200117A (en) * | 2017-04-12 | 2017-09-26 | 杭州迅蚁网络科技有限公司 | A kind of aircraft that easing gear is filled with recession formula |
| CN108482697A (en) * | 2018-06-06 | 2018-09-04 | 深圳草莓创新技术有限公司 | A kind of unmanned plane automatic positioning charging unit and its method |
| CN108513564A (en) * | 2017-04-26 | 2018-09-07 | 深圳市大疆创新科技有限公司 | Electronic equipment |
| CN108878715A (en) * | 2018-06-28 | 2018-11-23 | 芜湖新尚捷智能信息科技有限公司 | A kind of unmanned plane battery thermal device |
-
2016
- 2016-06-02 CN CN201620532134.2U patent/CN205707289U/en active Active
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107200117A (en) * | 2017-04-12 | 2017-09-26 | 杭州迅蚁网络科技有限公司 | A kind of aircraft that easing gear is filled with recession formula |
| CN108513564A (en) * | 2017-04-26 | 2018-09-07 | 深圳市大疆创新科技有限公司 | Electronic equipment |
| CN108513564B (en) * | 2017-04-26 | 2023-05-02 | 深圳市大疆创新科技有限公司 | Electronic equipment |
| CN108482697A (en) * | 2018-06-06 | 2018-09-04 | 深圳草莓创新技术有限公司 | A kind of unmanned plane automatic positioning charging unit and its method |
| CN108482697B (en) * | 2018-06-06 | 2023-09-19 | 深圳草莓创新技术有限公司 | Unmanned aerial vehicle automatic positioning charging device and method thereof |
| CN108878715A (en) * | 2018-06-28 | 2018-11-23 | 芜湖新尚捷智能信息科技有限公司 | A kind of unmanned plane battery thermal device |
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