CN212243871U

CN212243871U - Unmanned aerial vehicle launcher

Info

Publication number: CN212243871U
Application number: CN202021078877.XU
Authority: CN
Inventors: 曹雷
Original assignee: Zhuhai Sv Tech Co ltd
Current assignee: Zhuhai Sv Tech Co ltd
Priority date: 2020-06-12
Filing date: 2020-06-12
Publication date: 2020-12-29
Anticipated expiration: 2030-06-12

Abstract

An unmanned aerial vehicle launcher can be mounted on an automobile for use and used for bearing an unmanned aerial vehicle, and comprises a mounting base, a stabilizing mechanism, a bearing platform and a fastening mechanism; the mounting base can be mounted on an automobile; one end of the stabilizing mechanism is installed on the installation base, the other end of the stabilizing mechanism is connected with the bearing platform, so that the bearing platform keeps an inclination angle unchanged, and the bearing platform is used for bearing the unmanned aerial vehicle; fastening device installs on accepting the platform for the fixed unmanned aerial vehicle that is located on accepting the platform. The launching angle of the launching cradle of the unmanned aerial vehicle is automatically adjusted through the stabilizing mechanism, so that the normal take-off and landing of the unmanned aerial vehicle can be supported when the automobile is located on uneven terrain.

Description

Unmanned aerial vehicle launcher

Technical Field

The utility model relates to an unmanned aerial vehicle field specifically is an unmanned aerial vehicle launcher.

Background

With the continuous progress of the science and technology society, the unmanned aerial vehicle trade is gradually becoming bigger and bigger, and many rotor crafts are fast owing to advantages such as mechanical structure is simple, and driving system is simple, can rise perpendicularly and descend, and the very young of researcher becomes radiant in time, and the many rotor crafts begin to be studied in dispute, all have the heat tide of commercialization of many rotors in the global scope. And wherein, the unmanned aerial vehicle of partial great volume because it is inconvenient to carry, sometimes still needs on-vehicle unmanned aerial vehicle launcher to bear the weight of the transportation, still can directly take off or land on-vehicle unmanned aerial vehicle launcher even when having the needs. But when the terrain is uneven, the road surface is rugged or the slope appears, because current on-vehicle unmanned aerial vehicle launcher does not possess the ability of automatically regulated transmission angle, consequently also will lead to being located the whole slope that appears of unmanned aerial vehicle on this on-vehicle unmanned aerial vehicle launcher, to the unmanned aerial vehicle of vertical lift, this can lead to unmanned aerial vehicle to launch failure or tumble and damage.

SUMMERY OF THE UTILITY MODEL

Technical problem to be solved

In order to solve the above problem, the utility model provides a pair of unmanned aerial vehicle launcher can automatic adjustment unmanned aerial vehicle's launch angle.

(II) technical scheme

In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle launcher can be mounted on an automobile for use and used for bearing an unmanned aerial vehicle, and comprises a mounting base, a stabilizing mechanism, a bearing platform and a fastening mechanism; the mounting base can be mounted on an automobile; one end of the stabilizing mechanism is installed on the installation base, the other end of the stabilizing mechanism is connected with the bearing platform, so that the bearing platform keeps an inclination angle unchanged, and the bearing platform is used for bearing the unmanned aerial vehicle; fastening device installs on accepting the platform for the fixed unmanned aerial vehicle that is located on accepting the platform.

Preferably, the stabilizing mechanism comprises a first tripod head motor, a first support column is arranged on the mounting base, a second support column is arranged on the bearing platform, one end of the first tripod head motor is arranged on the first support column, and the other end of the first tripod head motor is arranged on the second support column, so that the second support column can swing relative to the first support column.

Preferably, the stabilizing mechanism further comprises a second pan-tilt motor and a connecting piece, wherein one end of the first pan-tilt motor, which is far away from the first support column, is mounted on the connecting piece, so that the connecting piece can swing relative to the first support column; and one end of the second tripod head motor is arranged on the connecting piece, and the other end of the second tripod head motor is arranged on the second support column, so that the second support column can swing relative to the connecting piece.

Preferably, the fastening mechanism comprises an electromagnet, which is mounted on the receiving platform.

Preferably, the electromagnet is embedded on the bearing platform.

Preferably, the fastening mechanism further comprises a magnetic reinforcing part, the electromagnet is attached to the magnetic reinforcing part, the electromagnet can be magnetically attracted with the magnetic reinforcing part, and the magnetic reinforcing part is installed on the top of the bearing platform.

Preferably, the magnetic reinforcement is made of silicon steel.

Advantageous effects

The utility model has the advantages that: an unmanned aerial vehicle launcher can be mounted on an automobile for use and used for bearing an unmanned aerial vehicle, and comprises a mounting base, a stabilizing mechanism, a bearing platform and a fastening mechanism; the mounting base can be mounted on an automobile; one end of the stabilizing mechanism is installed on the installation base, the other end of the stabilizing mechanism is connected with the bearing platform, so that the bearing platform keeps an inclination angle unchanged, and the bearing platform is used for bearing the unmanned aerial vehicle; fastening device installs on accepting the platform for the fixed unmanned aerial vehicle that is located on accepting the platform. The launching angle of the launching cradle of the unmanned aerial vehicle is automatically adjusted through the stabilizing mechanism, so that the normal take-off and landing of the unmanned aerial vehicle can be supported when the automobile is located on uneven terrain.

Drawings

The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description, do not constitute a limitation of the invention, in which:

FIG. 1 is a schematic view of an embodiment of the present invention installed on a vehicle;

fig. 2 is a schematic view of the embodiment of the present invention when carrying an unmanned aerial vehicle;

fig. 3 is a schematic overall structure diagram of an embodiment of the present invention;

fig. 4 is a schematic view of an explosive assembly according to an embodiment of the present invention;

fig. 5 is another schematic illustration of an explosive assembly according to an embodiment of the present invention;

FIG. 6 is a schematic structural view of a stabilization mechanism;

FIG. 7 is a first schematic view illustrating a state of the embodiment of the present invention when the vehicle is on a horizontal plane;

fig. 8 is a first schematic view of a state of the embodiment of the present invention when the vehicle is on a slope;

FIG. 9 is a schematic view of a second state of the embodiment of the present invention when the vehicle is on a horizontal plane;

FIG. 10 is a schematic view of a second state of the embodiment of the present invention when the vehicle is on a slope;

in the drawing, a car, b unmanned aerial vehicle, 1 mounting base, 2 stabilizing mechanism, 3 take on the platform, 4 fastening device, 10 first pillar, 21 first cloud platform motor, 22 second cloud platform motor, 23 connecting piece, 30 second pillar, 40 electro-magnet, 41 magnetism reinforcement.

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 work belong to the protection scope of the present invention.

Referring to fig. 1-6, an unmanned aerial vehicle launcher, which can be mounted on a vehicle a for use, for carrying an unmanned aerial vehicle b, comprises a mounting base 1, a stabilizing mechanism 2, a carrying platform 3 and a fastening mechanism 4; the mounting base 1 can be mounted on an automobile a; one end of the stabilizing mechanism 2 is installed on the installation base 1, the other end of the stabilizing mechanism is connected with the bearing platform 3, so that the bearing platform 3 keeps the inclination angle unchanged, and the bearing platform 3 is used for bearing the unmanned aerial vehicle b; fastening device 4 installs on accepting platform 3 for fix the unmanned aerial vehicle b that is located on accepting platform 3. The utility model discloses in, mounting base 1 can install and use on arbitrary loading end, and in this embodiment, mounting base installs and uses on the automobile top surface.

Specifically, current on-vehicle type unmanned aerial vehicle launcher when the car is located uneven topography, rugged or slope section, because current on-vehicle unmanned aerial vehicle launcher does not possess the ability of automatically regulated launch angle, consequently also will lead to the unmanned aerial vehicle that is located on this on-vehicle unmanned aerial vehicle launcher whole to appear inclining, to the unmanned aerial vehicle of vertical lift, this can lead to unmanned aerial vehicle launch failure or tumble and damage.

Therefore the utility model discloses in, come automatic adjustment to accept the inclination of platform 3 through stabilizing mean 2 to make the top surface of accepting platform 3 all the time approach to the horizontality, so that fix and to take off or descend at car a top directly at unmanned aerial vehicle b on accepting platform 3, because stabilizing mean 2 has the function at automatically regulated inclination, go the in-process that advances at car a even, unmanned aerial vehicle b also can follow this unmanned aerial vehicle launcher at car a top and normally take off. The fastening mechanism 4 can fix the unmanned aerial vehicle b on the bearing platform 3, and when the unmanned aerial vehicle b needs to take off, the fastening mechanism 4 unlocks the unmanned aerial vehicle b; after unmanned aerial vehicle b descends to accepting on the platform 3, fastening device 4 locks unmanned aerial vehicle b again. And wherein, fastening device 4 is fixed or unblock unmanned aerial vehicle b to unmanned aerial vehicle b's fixed and unblock operation, accessible manual control's mode, also can fix or unblock unmanned aerial vehicle b automatically through automatically controlled subassembly.

Specifically, referring to fig. 6, 7 and 8, the stabilizing mechanism 2 includes a first pan/tilt motor 21, a first support column 10 is disposed on the mounting base 1, a second support column 30 is disposed on the receiving platform 3, one end of the first pan/tilt motor 21 is mounted on the first support column 10, and the other end of the first pan/tilt motor 21 is mounted on the second support column 30, so that the second support column 30 can swing relative to the first support column 10. The automatic adjustment operation of the stabilizing mechanism 2 is realized by the rotation of the first pan/tilt motor 21, wherein the swinging direction of the bearing platform 3 swings towards the front and back direction of the automobile a, so when the automobile a runs on a slope road section, the mounting base 1 and the top surface of the automobile a both have a certain inclination angle with the horizontal plane, the first pan/tilt motor 21 can rotate and automatically adjust the inclination angle of the bearing platform 3, so that the bearing platform 3 can swing relative to the mounting base 1, thereby the top surface of the bearing platform 3 is always close to the horizontal state, and the unmanned aerial vehicle b borne on the automobile a can normally take off on the slope road section.

Further, referring to fig. 6, 9 and 10, the stabilizing mechanism 2 further includes a second pan/tilt motor 22 and a connecting member 23, wherein an end of the first pan/tilt motor 21 away from the first support column 10 is mounted on the connecting member 23, so that the connecting member 23 can swing relative to the first support column 10; one end of the second pan/tilt motor 22 is mounted on the connecting member 23, and the other end of the second pan/tilt motor 22 is mounted on the second support column 30, so that the second support column 30 can swing relative to the connecting member 23. The second pan/tilt motor 22 is arranged to enable the receiving platform 3 to swing towards the left and right directions of the automobile a, so that the top surface of the receiving platform 3 is always close to the horizontal state when the automobile a shakes or inclines left and right. Therefore, the arrangement of the first tripod head motor 21 and the second tripod head motor 22 can enable the automobile loaded with the launcher of the unmanned aerial vehicle to normally take off or land the unmanned aerial vehicle b borne by the automobile a when the automobile runs on most rugged or uneven road sections.

It should also be noted that the stabilizing mechanism 2 may further include a third pan/tilt motor, a fourth pan/tilt motor, or even more pan/tilt motors, and when one pan/tilt motor is additionally provided, the swinging direction of the receiving platform 3 is more diversified, and the stability of the receiving platform 3 will be improved.

Specifically, the fastening mechanism 4 comprises an electromagnet 40, and the electromagnet 40 is installed on the bearing platform 3. This fastening device 4 is applicable to the unmanned aerial vehicle that has iron unmanned aerial vehicle undercarriage, and wherein, electro-magnet 40 can inlay or glue and locate on the top surface of accepting platform 3. After the electromagnet 40 is powered on, the landing gear of the unmanned aerial vehicle can be adsorbed and fixed, and after the electromagnet 40 is powered off, the landing gear of the unmanned aerial vehicle can be quickly unlocked. This kind of unmanned aerial vehicle's fixed or unblock mode convenient to use and swift can fix the iron unmanned aerial vehicle undercarriage of arbitrary shape, and application scope is wide.

It should be noted that, still can be equipped with built-in power supply and control element in this unmanned aerial vehicle launcher, this built-in power supply can provide the energy for the operation of stabilizing mean 2 or fastening device 4, and also can control the running state of first cloud platform motor 21 and second cloud platform motor 22 through the procedure of predetermineeing in advance in the control element, with the circular telegram and the outage state of electro-magnet 40.

Further, the fastening mechanism 4 further includes a magnetic reinforcement 41, the electromagnet 40 is attached to the magnetic reinforcement 41, the electromagnet 40 can be magnetically attracted to the magnetic reinforcement 41, and the magnetic reinforcement 41 is installed on the top of the receiving platform 3. This magnetism reinforcing part 41 is platelike structure, and unmanned aerial vehicle b accepts on the top surface of this magnetism reinforcing part 41, and the laminating of electro-magnet 40 is in the bottom surface of this magnetism reinforcing part 41 to through the setting of this magnetism reinforcing part 41, improved fastening device 4's adsorption area and adsorption strength, thereby can make things convenient for operations such as descending and fixed of unmanned aerial vehicle b on this accepts platform 3 more.

Further, magnetism reinforcing piece 41 is the silicon steel material, because silicon steel is soft magnetic material, and the demagnetization speed is very fast, prevents that this magnetism reinforcing piece 41 of electro-magnet 40 from still having magnetism after the outage demagnetization to continue adsorbing unmanned aerial vehicle b, thereby led to unmanned aerial vehicle b to take off the failure.

It is noted that the terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of example embodiments according to the present application. As used herein, the singular forms "a", "an" and "the" are intended to include the plural forms as well, and it should be understood that when the terms "comprises" and/or "comprising" are used in this specification, they specify the presence of stated features, steps, operations, devices, components, and/or combinations thereof, unless the context clearly indicates otherwise.

The relative arrangement of the components and steps, the numerical expressions, and numerical values set forth in these embodiments do not limit the scope of the present application unless specifically stated otherwise. Meanwhile, it should be understood that the sizes of the respective portions shown in the drawings are not drawn in an actual proportional relationship for the convenience of description. Techniques, methods, and apparatus known to those of ordinary skill in the relevant art may not be discussed in detail but are intended to be part of the specification where appropriate. In all examples shown and discussed herein, any particular value should be construed as merely illustrative, and not limiting. Thus, other examples of the exemplary embodiments may have different values. It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, further discussion thereof is not required in subsequent figures.

In the description of the present application, it is to be understood that the orientation or positional relationship indicated by the directional terms such as "front, rear, upper, lower, left, right", "lateral, vertical, horizontal" and "top, bottom", etc., are generally based on the orientation or positional relationship shown in the drawings, and are used for convenience of description and simplicity of description only, and in the case of not making a reverse description, these directional terms do not indicate and imply that the device or element being referred to must have a particular orientation or be constructed and operated in a particular orientation, and therefore, should not be considered as limiting the scope of the present application; the terms "inner and outer" refer to the inner and outer relative to the profile of the respective component itself.

Spatially relative terms, such as "above … …," "above … …," "above … …," "above," and the like, may be used herein for ease of description to describe one device or feature's spatial relationship to another device or feature as illustrated in the figures. It will be understood that the spatially relative terms are intended to encompass different orientations of the device in use or operation in addition to the orientation depicted in the figures. For example, if a device in the figures is turned over, devices described as "above" or "on" other devices or configurations would then be oriented "below" or "under" the other devices or configurations. Thus, the exemplary term "above … …" can include both an orientation of "above … …" and "below … …". The device may be otherwise variously oriented (rotated 90 degrees or at other orientations) and the spatially relative descriptors used herein interpreted accordingly.

It should be noted that the terms "first", "second", and the like are used to define the components, and are only used for convenience of distinguishing the corresponding components, and the terms have no special meanings unless otherwise stated, and therefore, the scope of protection of the present application is not to be construed as being limited.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. An unmanned aerial vehicle launcher can be mounted on an automobile (a) for use and used for bearing an unmanned aerial vehicle (b), and is characterized by comprising a mounting base (1), a stabilizing mechanism (2), a bearing platform (3) and a fastening mechanism (4);

the mounting base (1) can be mounted on an automobile (a); one end of the stabilizing mechanism (2) is installed on the installation base (1), the other end of the stabilizing mechanism is connected with the bearing platform (3) so that the bearing platform (3) keeps the inclination angle unchanged, and the bearing platform (3) is used for bearing the unmanned aerial vehicle (b);

fastening device (4) are installed on accepting platform (3) for fix unmanned aerial vehicle (b) that is located on accepting platform (3).

2. An unmanned aerial vehicle launcher according to claim 1, wherein the stabilizing mechanism (2) comprises a first cradle head motor (21), the mounting base (1) is provided with a first support column (10), the receiving platform (3) is provided with a second support column (30), one end of the first cradle head motor (21) is mounted on the first support column (10), and the other end of the first cradle head motor (21) is mounted on the second support column (30), so that the second support column (30) can swing relative to the first support column (10).

3. An unmanned aerial vehicle launcher according to claim 2, wherein the stabilizing mechanism (2) further comprises a second pan-tilt motor (22) and a connecting member (23), and an end of the first pan-tilt motor (21) remote from the first strut (10) is mounted on the connecting member (23) so that the connecting member (23) can swing relative to the first strut (10); one end of the second tripod head motor (22) is mounted on the connecting piece (23), and the other end of the second tripod head motor (22) is mounted on the second support column (30), so that the second support column (30) can swing relative to the connecting piece (23).

4. An unmanned aerial vehicle launcher according to claim 1, wherein the fastening mechanism (4) comprises an electromagnet (40), the electromagnet (40) being mounted on the receiving platform (3).

5. An unmanned aerial vehicle launcher according to claim 4, wherein the electromagnet (40) is embedded in the receiving platform (3).

6. An unmanned aerial vehicle launcher according to claim 4, wherein the fastening mechanism (4) further comprises a magnetic reinforcement (41), the electromagnet (40) is attached to the magnetic reinforcement (41), and the electromagnet (40) can be magnetically attracted to the magnetic reinforcement (41), and the magnetic reinforcement (41) is mounted on top of the receiving platform (3).

7. An unmanned aerial vehicle launcher according to claim 6, wherein the magnetic reinforcement (41) is silicon steel.