Unmanned aerial vehicle transverse projection device
阅读说明:本技术 无人机横向投射装置 (Unmanned aerial vehicle transverse projection device ) 是由 卢致辉 陈金颖 卢光宋 车嘉兴 郑学贵 于 2019-10-21 设计创作,主要内容包括:本发明属于无人机技术领域,尤其涉及一种无人机横向投射装置,该无人机横向投射装置包括壳体、连接组件和弹射机构,所述壳体设有具有开口并用于容置物品的安装腔;所述连接组件安装于所述壳体上并用于与无人机连接;所述弹射机构安装于所述安装腔内,所述弹射机构的驱动端朝向所述安装腔的开口设置并用于将位于所述安装腔内的物品从所述安装腔的开口弹射出去。该无人机横向投射装置可以解决了现有的无人机抛射装置采用自由落体式投射物品在部分应用场景存在局限性的技术问题,大大提高了无人机横向投射装置的应用范围。(The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to a transverse projection device of an unmanned aerial vehicle, which comprises a shell, a connecting assembly and an ejection mechanism, wherein the shell is provided with an installation cavity which is provided with an opening and used for accommodating articles; the connecting assembly is mounted on the shell and is used for being connected with the unmanned aerial vehicle; the ejection mechanism is installed in the installation cavity, and the driving end of the ejection mechanism faces the opening of the installation cavity and is used for ejecting the articles in the installation cavity out of the opening of the installation cavity. This horizontal projection arrangement of unmanned aerial vehicle can solve current unmanned aerial vehicle and cast the device and adopt the free fall formula to throw article and have the technical problem of limitation in some application scenes, has improved the range of application of horizontal projection arrangement of unmanned aerial vehicle greatly.)
1. The utility model provides a horizontal projection arrangement of unmanned aerial vehicle which characterized in that includes:
the device comprises a shell, a first fixing piece and a second fixing piece, wherein the shell is provided with an installation cavity which is provided with an opening and used for accommodating articles;
the connecting assembly is mounted on the shell and used for being connected with the unmanned aerial vehicle;
the ejection mechanism is installed in the installation cavity, and the driving end of the ejection mechanism faces the opening of the installation cavity and is used for ejecting the articles in the installation cavity out of the opening of the installation cavity.
2. The unmanned aerial vehicle lateral projection device of claim 1, wherein: the ejection mechanism comprises an elastic piece, the elastic piece is installed in the installation cavity, and the driving end of the elastic piece faces to the opening of the installation cavity.
3. The unmanned aerial vehicle lateral projection device of claim 2, wherein: the ejection mechanism further comprises a pushing cover, the pushing cover is located in the installation cavity, and the driving end of the elastic piece is connected with the pushing cover and used for pushing the pushing cover to move towards the opening of the installation cavity.
4. The unmanned aerial vehicle lateral projection device of claim 3, wherein: the lateral part of casing is equipped with towards the direction slot hole that the installation cavity opening extends, it is equipped with the guide arm to promote to cover, the tip of guide arm wears to locate in the direction slot hole.
5. The unmanned aerial vehicle lateral projection device of claim 4, wherein: the ejection mechanism further comprises a trigger assembly for triggering release of the elastic member in a compressed state.
6. The unmanned aerial vehicle lateral projection device of claim 5, wherein: the trigger assembly comprises a trigger rod and a lifting driving part, the driving end of the lifting driving part is connected with the trigger rod, and when the elastic part is in a compressed state, the lifting driving part drives the trigger rod to move towards the guide rod so as to limit the guide rod to move.
7. The unmanned aerial vehicle lateral projection device of claim 6, wherein: the trigger assembly further comprises a rotating rod, one end of the rotating rod is hinged with the shell, a hinge straight line of the rotating rod and the shell is arranged in parallel with the guide rod, and the trigger rod and the guide rod are respectively located on two opposite sides of the guide long hole; when the elastic part is in a compressed state, the lifting driving part drives the trigger rod to move until the free end of the rotating rod is lapped to limit the rotation of the rotating rod, and the guide rod is abutted to the side part of the rotating rod.
8. The unmanned aerial vehicle lateral projection device of claim 6, wherein: the lifting driving part comprises a rotary driving part and a gear, a plurality of gear teeth are arranged on the trigger rod along the length direction of the trigger rod, the driving end of the rotary driving part is connected with the gear, and the gear is meshed with the gear teeth.
9. The unmanned aerial vehicle transverse projection device of any one of claims 1-8, wherein: the horizontal projection arrangement of unmanned aerial vehicle still includes the high definition camera, the high definition camera install in on the casing.
10. The unmanned aerial vehicle lateral projection device of claim 9, wherein: the horizontal projection arrangement of unmanned aerial vehicle still includes controlling means, the high definition camera with ejection mechanism all with controlling means electric connection.
Technical Field
The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to a transverse projection device of an unmanned aerial vehicle.
Background
The development level of unmanned aerial vehicles in China is changing day by day, and unmanned aerial vehicles also tend to have low flying cost and are easy and convenient to control. Because the unmanned aerial vehicle can replace the manual work to carry out the task that has the particularity, consequently unmanned aerial vehicle's application also more and more extensive, combine unmanned aerial vehicle application in aspects such as fire control, public safety and obtain more development. At present, use unmanned aerial vehicle to carry out fixed point shooting, throw, observe, scenes such as rescue are increasing day by day, simultaneously, present a great deal of unmanned aerial vehicle is carrying out the task of throwing the carry, it throws to use steering wheel drive couple to carry out the fixed point more, current unmanned aerial vehicle's throwing device throwing task is numerous, the scene is different, the article that need throw also respectively has the difference, but current unmanned aerial vehicle throwing device that carries out free fall formula throwing with the help of gravity can't high-rise building middle level room, special geographical positions such as cliff platform carry out the task of throwing, there is great limitation.
Disclosure of Invention
The invention aims to provide a transverse projection device of an unmanned aerial vehicle, and aims to solve the technical problem that the unmanned aerial vehicle throwing device in the prior art is limited in partial application scenes by adopting a free-fall type projection object generally.
In order to achieve the purpose, the invention adopts the technical scheme that: an unmanned aerial vehicle lateral projection device, comprising:
the device comprises a shell, a first fixing piece and a second fixing piece, wherein the shell is provided with an installation cavity which is provided with an opening and used for accommodating articles;
the connecting assembly is mounted on the shell and used for being connected with the unmanned aerial vehicle;
the ejection mechanism is installed in the installation cavity, and the driving end of the ejection mechanism faces the opening of the installation cavity and is used for ejecting the articles in the installation cavity out of the opening of the installation cavity.
Optionally, the ejection mechanism includes an elastic member, the elastic member is installed in the installation cavity, and the driving end of the elastic member is disposed toward the opening of the installation cavity.
Optionally, the ejection mechanism further includes a pushing cover, the pushing cover is located in the installation cavity, and the driving end of the elastic member is connected with the pushing cover and used for pushing the pushing cover to move towards the opening of the installation cavity.
Optionally, a guide slot extending toward the opening of the installation cavity is formed in the side portion of the housing, a guide rod is arranged on the push cover, and the end portion of the guide rod penetrates through the guide slot.
Optionally, the ejection mechanism further comprises a trigger assembly for triggering release of the elastic member in a compressed state.
Optionally, the trigger assembly includes a trigger rod and a lifting driving part, a driving end of the lifting driving part is connected to the trigger rod, and when the elastic part is in a compressed state, the lifting driving part drives the trigger rod to move towards the guide rod so as to limit the guide rod to move.
Optionally, the trigger assembly further includes a rotating rod, one end of the rotating rod is hinged to the housing, a hinge line of the rotating rod and the housing is parallel to the guide rod, and the trigger rod and the guide rod are respectively located on two opposite sides of the guide long hole; when the elastic part is in a compressed state, the lifting driving part drives the trigger rod to move until the free end of the rotating rod is lapped to limit the rotation of the rotating rod, and the guide rod is abutted to the side part of the rotating rod.
Optionally, the lifting driving part includes a rotary driving part and a gear, the trigger rod is provided with a plurality of gear teeth arranged along the length direction of the trigger rod, the driving end of the rotary driving part is connected with the gear, and the gear is engaged with the gear teeth.
Optionally, the horizontal projection device of unmanned aerial vehicle still includes high definition camera, high definition camera install in on the casing.
Optionally, the horizontal projection arrangement of unmanned aerial vehicle still includes controlling means, the high definition camera with ejection mechanism all with controlling means electric connection.
One or more technical schemes in the transverse projection device of the unmanned aerial vehicle provided by the invention at least have one of the following technical effects: when the unmanned aerial vehicle catapult device is used, firstly, the connecting component is connected with the unmanned aerial vehicle, then the unmanned aerial vehicle is started, the unmanned aerial vehicle drives the horizontal projection device of the unmanned aerial vehicle to move to a projection point, finally, the catapulting mechanism is started, articles in the installation cavity are transversely catapulted out of the shell from the opening of the installation cavity by the driving end of the catapulting mechanism, the articles catapulted out of the shell simultaneously have certain transverse speed and free falling speed, so that the articles can be projected to the side position of the projection point, when the application scenes of the unmanned aerial vehicle face special geographic positions such as a high-rise building middle room and a cliff platform, the unmanned aerial vehicle stops at the side of the high-rise building or the cliff platform, after the articles are projected by the catapulting mechanism towards the high-rise building or the cliff platform, the articles can fall into the high-rise building middle room or the cliff platform under the action of self gravity and the transverse The technical problem of limitation has improved the range of application of the horizontal projection arrangement of unmanned aerial vehicle greatly.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings needed to be used in the embodiments or the prior art descriptions will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings based on these drawings without inventive exercise.
Fig. 1 is a schematic structural view of a lateral projection device of an unmanned aerial vehicle according to an embodiment of the present invention.
Fig. 2 is an exploded view of the unmanned aerial vehicle lateral projection device shown in fig. 1.
Fig. 3 is a schematic structural diagram of a projection mechanism of the unmanned aerial vehicle lateral projection device shown in fig. 1.
Fig. 4 is a schematic structural view of the hidden right half shell of the transverse projection device of the unmanned aerial vehicle shown in fig. 1 and the elastic member in a released state after the triggering assembly.
Fig. 5 is a schematic structural view of the hidden right half shell of the unmanned aerial vehicle transverse projection device shown in fig. 1 and the elastic member in a compressed state after the triggering assembly.
Wherein, in the figures, the respective reference numerals:
10-shell 11-installation cavity 12-guide long hole
13-left half shell 14-right half shell 15-rear shell
16-control cavity 17-cover plate 18-fastener
20-connecting component 30-ejection mechanism 31-elastic element
32-push cap 33-guide bar 34-trigger assembly
35-spacing collar 40-high definition camera 50-control device
51-control mainboard 52-power circuit board 341-trigger bar
342-lifting drive part 343-rotating rod 344-articulated shaft
3421
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 or similar 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 fig. 1-5 are exemplary and intended to be used for explanation of the invention, and should not be construed as limiting the invention.
In the description of the present invention, it is to be understood that the terms "length", "width", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on the orientation or positional relationships illustrated in the drawings, are only for convenience in describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and thus, should not be construed as limiting the present invention.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, 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 specifically defined otherwise.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," "secured," and the like are to be construed broadly and can, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.
Referring to fig. 1 to 5, in an embodiment of the present invention, there is provided a lateral projection device for an unmanned aerial vehicle, including a
Specifically, when the unmanned aerial vehicle transverse projection device of the embodiment of the invention is used, firstly, the connecting
Furthermore, when the horizontal projection device of the unmanned aerial vehicle faces application scenes of special geographic positions such as a middle room of a high-rise building, a cliff platform and the like, the unmanned aerial vehicle only needs to stay on the side face of the high-rise building or the cliff platform, and does not need to enter the high-rise building and the cliff platform, so that the difficulty of the unmanned aerial vehicle in executing a flight mission can be greatly reduced.
In this embodiment,
In another embodiment of the present invention, the connecting
In another embodiment of the present invention, referring to fig. 2, 4 and 5, an
In another embodiment of the present invention, referring to fig. 2, 4 and 5, the
Preferably, the
In another embodiment of the present invention, referring to fig. 1, 2 and 3, a lateral portion of a
Further, the quantity of
Further, outside the protruding
In another embodiment of the present invention, referring to fig. 1, 2 and 3, the
In another embodiment of the present invention, referring to fig. 1, 2 and 3, the triggering
In another embodiment of the present invention, referring to fig. 1, 2 and 3, the triggering
Further, the triggering
Further, the number of the
In another embodiment of the present invention, the
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In another embodiment of the present invention, the lateral unmanned aerial vehicle projection device further includes a
In another embodiment of the present invention, the lateral unmanned aerial vehicle projection apparatus further includes a
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Furthermore, the surface of the
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The present invention is not limited to the above preferred embodiments, and any modifications, equivalent substitutions and improvements made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
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