CN210027957U - Multi-unmanned aerial vehicle hangar - Google Patents
Multi-unmanned aerial vehicle hangar Download PDFInfo
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- CN210027957U CN210027957U CN201920642485.2U CN201920642485U CN210027957U CN 210027957 U CN210027957 U CN 210027957U CN 201920642485 U CN201920642485 U CN 201920642485U CN 210027957 U CN210027957 U CN 210027957U
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Abstract
The utility model provides a multimachine unmanned aerial vehicle hangar, include: a body defining a chamber therein; a plurality of machine that stops, it is a plurality of the one end of stopping the machine respectively with but the circumference pivot ground of body links to each other, and is a plurality of it has the recess that is used for accomodating unmanned aerial vehicle to inject respectively on the machine that stops, when release or retrieve the state, stop the machine rotatory to horizontal position in order to release or retrieve unmanned aerial vehicle, when accomodating the state, stop the machine rotatory to with the side parallel position of body is in order to accomodate unmanned aerial vehicle. According to the utility model discloses multimachine unmanned aerial vehicle hangar has the cavity through injecing at this internal, and a plurality of machine of stopping pivot ground are established in the week of body, and this multimachine unmanned aerial vehicle hangar is simple structure not only, can realize parking, location and the fixing of a plurality of unmanned aerial vehicles simultaneously moreover, and complementary interference.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to a multimachine unmanned aerial vehicle hangar.
Background
With the rapid development of the multi-rotor unmanned aerial vehicle technology and the continuous expansion of the application range of the multi-rotor unmanned aerial vehicle, the pursuit of people on the multi-rotor unmanned aerial vehicle technology is developed from the independent pursuit of performance indexes to the aspect of simultaneously pursuing the use convenience degree and the intellectualization. The degree of automation determines the convenience of using the unmanned aerial vehicle, so that a product concept of an unmanned aerial vehicle hangar is provided, and the existing multi-rotor unmanned aerial vehicle hangars developed at home and abroad generally have one hangar and one machine, namely one parking garage is used for storing and maintaining one unmanned aerial vehicle; in addition, a concept of multiple machines is proposed, but no more perfect product is available at present.
SUMMERY OF THE UTILITY MODEL
In view of this, the utility model provides a multimachine unmanned aerial vehicle hangar, this multimachine unmanned aerial vehicle hangar simple structure can realize a plurality of unmanned aerial vehicle accomodate the function.
According to the utility model discloses multimachine unmanned aerial vehicle hangar, include: a body defining a chamber therein; a plurality of machine that stops, it is a plurality of the one end of stopping the machine respectively with but the circumference pivot ground of body links to each other, and is a plurality of it has the recess that is used for accomodating unmanned aerial vehicle to inject respectively on the machine that stops, when release or retrieve the state, stop the machine rotatory to horizontal position in order to release or retrieve unmanned aerial vehicle, when accomodating the state, stop the machine rotatory to with the side parallel position of body is in order to accomodate unmanned aerial vehicle.
According to the utility model discloses multimachine unmanned aerial vehicle hangar has the cavity through injecing at this internal, and a plurality of machine of stopping pivot ground are established in the week of body, and this multimachine unmanned aerial vehicle hangar is simple structure not only, can realize parking, location and the fixing of a plurality of unmanned aerial vehicles simultaneously moreover, and complementary interference.
According to the utility model discloses multimachine unmanned aerial vehicle hangar can also have following additional technical characterstic:
according to an embodiment of the invention, the body is formed as a cuboid.
According to the utility model discloses an embodiment, the board that stops is four.
According to the utility model discloses an embodiment, the platform of stopping is formed into the rectangular plate, the recess is established the middle part of stopping the platform.
According to the utility model discloses an embodiment, stop the upper end of board with but the circumference pivot ground of body upper end links to each other during the state of accomodating, the recess is located in the cavity.
According to the utility model discloses an embodiment, stop the platform the lower extreme with but the circumference pivot ground of body lower extreme links to each other during the state of accomodating, the recess orientation the cavity sets up.
According to the utility model discloses an embodiment, the shape of recess with unmanned aerial vehicle's shape is corresponding.
According to the utility model discloses an embodiment, it is right with being used for in the cavity a plurality of mouths that charge.
According to the utility model discloses an embodiment, multimachine unmanned aerial vehicle hangar still includes: the protection casing, protection casing movably establish the outside of body is in order to protect the body stop the board with unmanned aerial vehicle.
According to an embodiment of the invention, the bottom surface of the body is fixed to the ground.
Drawings
Fig. 1 is a top view of a multi-drone hangar in accordance with an embodiment of the present invention;
fig. 2 is a front view of a multi-drone hangar in accordance with an embodiment of the present invention;
fig. 3 is a schematic view of a state structure of a multi-drone hangar according to an embodiment of the present invention;
fig. 4 is a schematic view of another state structure of the multi-drone hangar according to an embodiment of the present invention;
fig. 5 is a schematic view of a further state structure of the multi-drone hangar according to an embodiment of the present invention;
fig. 6 is a top view of a multiple drone hangar in a released state in accordance with an embodiment of the present invention;
FIG. 7 is a front view of FIG. 6;
fig. 8 is a schematic structural view of yet another multi-drone hangar in a released or recovered state according to an embodiment of the present invention;
fig. 9 is a schematic view of a mechanism of yet another multi-drone hangar in a stowed state according to an embodiment of the present invention.
Reference numerals:
a multi-drone hangar 100; a body 10; stopping the machine 20; a groove 21; a drone 30.
Detailed Description
Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are exemplary only for the purpose of explaining the present invention, and should not be construed as limiting the present invention.
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", "axial", "radial", "circumferential", and the like, indicate the orientation or positional relationship indicated based on the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention. Furthermore, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless otherwise specified.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
The multi-drone hangar 100 according to the embodiments of the present invention will be described first in detail with reference to the accompanying drawings.
As shown in fig. 1 to 5, a multi-drone hangar 100 according to an embodiment of the present invention includes a body 10 and a plurality of docking stations 20.
Specifically, be injectd the cavity in the body 10, a plurality of one end that stop the platform 20 link to each other with the circumference pivot ground of body 10 respectively, be injectd the recess 21 that is used for accomodating unmanned aerial vehicle 30 on a plurality of stops the platform 20 respectively, when release or recovery state, stop the platform 20 and rotate to horizontal position in order to release or retrieve unmanned aerial vehicle 30, when accomodating the state, stop the platform 20 and rotate to the side parallel position with body 10 in order to accomodate unmanned aerial vehicle 30.
In other words, multimachine unmanned aerial vehicle hangar 100 mainly comprises body 10 and shut down platform 20, wherein, the installation cavity has been injectd in the body 10, a plurality of shut down platforms 20 rotatably establish in the circumference of body 10, shut down and be equipped with recess 21 on the platform 20, when retrieving unmanned aerial vehicle 30, shut down platform 20 rotatory to horizontal position, and relatively fixed with body 10 through fixing device, after unmanned aerial vehicle 30 falls to the recess 21 on the shut down platform 20, shut down platform 20 rotatory to the parallel position with the body 10 side in order to accomodate unmanned aerial vehicle 30, when releasing unmanned aerial vehicle 30, shut down platform 20 and rotate to horizontal position again, and relatively fixed with body 10 through fixing device, unmanned aerial vehicle 30 rises from recess 21, accomplish unmanned aerial vehicle 30's release. This multimachine unmanned aerial vehicle hangar 100 not only realizes a plurality of unmanned aerial vehicles 30 operations such as take off simultaneously more easily, and mutual noninterference, has reduced unmanned aerial vehicle 30 in the use intervention of people moreover, has simplified the operation of using, has also improved the quick response ability that unmanned aerial vehicle 30 was on duty.
From this, according to the utility model discloses multimachine unmanned aerial vehicle hangar 100 has the cavity through injecing in body 10, but a plurality of machine 20 pivot ground of stopping establish in the week of body 10, and this multimachine unmanned aerial vehicle hangar 100 is simple structure not only, can realize parking, location and fixed of a plurality of unmanned aerial vehicles 30 simultaneously moreover, and complementary interference.
According to the utility model discloses a some concrete embodiments, body 10 can form into the cuboid, and square simple structure is convenient for process, is injectd in the body 10 to have the cavity that corresponds with recess 21.
Preferably, the number of the stopping stations 20 is four, and the four stopping stations 20 are pivotally connected to four circumferential sides of the body 10, respectively, that is, the multi-drone aircraft library 100 can accommodate and release at most four drones 30 at the same time.
The utility model discloses an in the embodiment, shut down platform 20 and form to the rectangular plate, recess 21 is established at the middle part of stopping platform 20, simple structure, the processing of being convenient for.
According to an embodiment of the present invention, as shown in fig. 6 and 7, the upper end of the parking table 20 is pivotally connected to the upper end of the body 10 in the circumferential direction, and the groove 21 is located in the chamber in the storage state. That is, when the docking station 20 is rotated to the stowed state, the groove 21 is disposed facing away from the body 10, and the wings of the drone 30 protrude out of the groove 21.
According to a further embodiment of the invention, as shown in fig. 8 and 9, the lower end of the parking table 20 is pivotably connected to the circumference of the lower end of the body 10, the recess 21 being arranged towards the chamber in the stowed position. That is, when the docking station 20 rotates to the storage state, the groove 21 is disposed toward the body 10, and the wings of the unmanned aerial vehicle 30 are located in the cavity.
Preferably, the shape of recess 21 corresponds with the shape of unmanned aerial vehicle 30, and from this, the accurate location and the accomodation of unmanned aerial vehicle 30 are convenient, have simplified the complexity of system.
The utility model discloses an in the embodiment, be equipped with a plurality of mouths that charge in the cavity, can also charge to unmanned aerial vehicle 30 when the rotatory unmanned aerial vehicle 30 of accomodating to the body 10 side of stopping 20.
Optionally, the multi-drone hangar 100 further comprises: the protection casing, protection casing movably establish in the outside of body 10 in order to protect body 10, shut down platform 20 and unmanned aerial vehicle 30. That is to say, unmanned aerial vehicle 30 is accomodating the in-process, and a plurality of stops the board 20 rotation and draw in, and unmanned aerial vehicle 30 exposes in the environment this moment, can further unmanned aerial vehicle 30 through setting up the protection casing.
Optionally, the bottom surface of the body 10 is fixed on the ground, and the structure is stable.
In conclusion, according to the utility model discloses multimachine unmanned aerial vehicle hangar 100, through having limited the cavity in body 10, but a plurality of stops board 20 pivot establish in the circumference of body 10, this multimachine unmanned aerial vehicle hangar 100 is simple structure not only, can realize parking, location and the fixing of a plurality of unmanned aerial vehicles 30 simultaneously moreover, and complementary interference.
The foregoing is a preferred embodiment of the present invention, and it should be noted that, for those skilled in the art, a plurality of improvements and decorations can be made without departing from the principle of the present invention, and these improvements and decorations should also be regarded as the protection scope of the present invention.
Claims (10)
1. A multi-machine unmanned aerial vehicle hangar, comprising:
a body defining a chamber therein;
a plurality of machine that stops, it is a plurality of the one end of stopping the machine respectively with but the circumference pivot ground of body links to each other, and is a plurality of it has the recess that is used for accomodating unmanned aerial vehicle to inject respectively on the machine that stops, when release or retrieve the state, stop the machine rotatory to horizontal position in order to release or retrieve unmanned aerial vehicle, when accomodating the state, stop the machine rotatory to with the side parallel position of body is in order to accomodate unmanned aerial vehicle.
2. The multi-drone hangar of claim 1, wherein the body is formed as a cuboid.
3. The multi-drone hangar of claim 2, wherein the number of docking stations is four.
4. The multi-drone hangar of claim 1, wherein the docking station is formed as a rectangular plate, the recess being provided in the middle of the docking station.
5. The multi-drone hangar of claim 1, wherein an upper end of the docking station is pivotably connected to a circumference of the upper end of the body, the recess being located within the chamber in the stowed condition.
6. The multi-drone hangar of claim 1, wherein a lower end of the docking station is pivotably connected to a circumference of the lower end of the body, the recess being disposed toward the cavity in the stowed condition.
7. The multi-drone hangar of claim 1, wherein the shape of the groove corresponds to the shape of the drone.
8. The multi-drone hangar of claim 1, wherein a plurality of charging ports are provided in the chamber for charging the drones.
9. The multi-drone hangar of claim 1, further comprising:
the protection casing, protection casing movably establish the outside of body is in order to protect the body stop the board with unmanned aerial vehicle.
10. The multi-drone hangar of claim 1, wherein the bottom surface of the body is fixed to the ground.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920642485.2U CN210027957U (en) | 2019-05-07 | 2019-05-07 | Multi-unmanned aerial vehicle hangar |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920642485.2U CN210027957U (en) | 2019-05-07 | 2019-05-07 | Multi-unmanned aerial vehicle hangar |
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| CN210027957U true CN210027957U (en) | 2020-02-07 |
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| CN201920642485.2U Active CN210027957U (en) | 2019-05-07 | 2019-05-07 | Multi-unmanned aerial vehicle hangar |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111572795A (en) * | 2020-05-25 | 2020-08-25 | 北京华力创通科技股份有限公司 | Unmanned aerial vehicle takes off device and unmanned aerial vehicle conveyer |
| CN112051808A (en) * | 2020-07-29 | 2020-12-08 | 成都震风航空技术有限公司 | Unmanned aerial vehicle landing method based on automatic hangar of unmanned aerial vehicle |
| CN113428376A (en) * | 2021-08-03 | 2021-09-24 | 广东电网有限责任公司 | Unmanned aerial vehicle parking equipment |
-
2019
- 2019-05-07 CN CN201920642485.2U patent/CN210027957U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111572795A (en) * | 2020-05-25 | 2020-08-25 | 北京华力创通科技股份有限公司 | Unmanned aerial vehicle takes off device and unmanned aerial vehicle conveyer |
| CN111572795B (en) * | 2020-05-25 | 2022-04-22 | 北京华力创通科技股份有限公司 | Unmanned aerial vehicle takes off device and unmanned aerial vehicle conveyer |
| CN112051808A (en) * | 2020-07-29 | 2020-12-08 | 成都震风航空技术有限公司 | Unmanned aerial vehicle landing method based on automatic hangar of unmanned aerial vehicle |
| CN113428376A (en) * | 2021-08-03 | 2021-09-24 | 广东电网有限责任公司 | Unmanned aerial vehicle parking equipment |
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