CN214986129U - Drawer type nacelle of modularized vertical take-off and landing unmanned aerial vehicle - Google Patents

Drawer type nacelle of modularized vertical take-off and landing unmanned aerial vehicle Download PDF

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CN214986129U
CN214986129U CN202121051529.8U CN202121051529U CN214986129U CN 214986129 U CN214986129 U CN 214986129U CN 202121051529 U CN202121051529 U CN 202121051529U CN 214986129 U CN214986129 U CN 214986129U
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pod
module
tracking module
aerial vehicle
unmanned aerial
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CN202121051529.8U
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王放
徐安安
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Beihang University
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Beihang University
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Abstract

The utility model discloses a drawer type pod of a modularized vertical take-off and landing unmanned aerial vehicle, which is detachably arranged in the body of the unmanned aerial vehicle and comprises a pod body, a slide rail, a pod separation button, a pan-tilt tracking module and a pan-tilt control tracking module, wherein the pod body is of a cylindrical structure with an open top, the slide rail is of a U-shaped structure and is fixed on the top end surface of the pod body, a straight notch is arranged on the slide rail, a slide groove which is matched with the slide rail and is connected with the slide rail in a sliding way is formed on the inner wall of the unmanned aerial vehicle body, a bracket is also arranged in the unmanned aerial vehicle body, a pod separating button is arranged on the outer side wall of the pod body and is electrically connected with the motor, the cradle head tracking module and the cradle head control tracking module are both arranged in the pod body, and the cradle head control tracking module is electrically connected with the cradle head tracking module and is used for controlling the cradle head tracking module.

Description

Drawer type nacelle of modularized vertical take-off and landing unmanned aerial vehicle
Technical Field
The utility model relates to an unmanned helicopter technical field of VTOL, more specifically the drawer type nacelle that relates to a modularization VTOL unmanned aerial vehicle that says so.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is autonomously operated, either completely or intermittently, by an onboard computer. VTOL fixed wing unmanned aerial vehicle can realize VTOL, has compromise fixed wing unmanned aerial vehicle and rotor unmanned aerial vehicle's advantage, is the key field of development in recent years. The vertical take-off and landing unmanned aerial vehicle can be divided into two categories of military use and civil use according to the application field, and in the aspect of military use, the unmanned aerial vehicle is divided into a reconnaissance plane and a target drone; in civilian aspect, unmanned aerial vehicle + industry application is real just need of unmanned aerial vehicle, and unmanned aerial vehicle wide application is in fields such as aerial photograph, agriculture, plant protection, miniature autodyne, express delivery transportation, disaster relief, observation wild animal, control infectious disease, survey and drawing, news report, electric power inspection, relief of disaster, movie & TV are shot, make romantic at present, has expanded unmanned aerial vehicle's use itself greatly.
However, the pod structure of the vertical take-off and landing fixed wing unmanned aerial vehicle in the prior art is inconvenient to mount and dismount in the use process, brings certain trouble to operators, and has certain defects.
Therefore, it is an urgent need to solve the problem of the art to provide a drawer type pod of a modularized vertical take-off and landing unmanned aerial vehicle with simple structure, reasonable design, convenient operation, and easy installation and disassembly.
Disclosure of Invention
In view of this, in order to solve among the prior art VTOL fixed wing unmanned aerial vehicle and install and dismantle inconvenient class of technical problem in the use, the utility model provides a simple structure, reasonable in design, convenient operation, the modularization VTOL unmanned aerial vehicle's of easily installing and dismantling drawer type nacelle.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
a drawer type pod of a modularized vertical take-off and landing unmanned aerial vehicle is detachably arranged in a body of the unmanned aerial vehicle and comprises a pod body, a slide rail, a pod separation button, a pan-tilt tracking module and a pan-tilt control tracking module, wherein the pod body is of a cylindrical structure with an open top, the slide rail is of a U-shaped structure and is fixed on the top end face of the pod body, a straight notch is formed in the slide rail, a slide groove matched with and in sliding connection with the slide rail is formed in the inner wall of the body of the unmanned aerial vehicle, a bracket is further arranged in the body of the unmanned aerial vehicle, the pod separation button is arranged on the outer side wall of the pod body and is electrically connected with the motor and used for controlling the detachable insertion of the pod into the straight notch, the pan-tilt tracking module and the pan-tilt control tracking module are both arranged in the pod body and are electrically connected with the pan-tilt tracking module, for controlling the pan-tilt tracking module.
According to the technical scheme, compare with prior art scheme, the utility model provides a modularization VTOL unmanned aerial vehicle's drawer type nacelle, through the sliding connection structure who utilizes slide rail and the inside spout of unmanned aerial vehicle fuselage, the operating personnel of being convenient for install this nacelle in the unmanned aerial vehicle fuselage fast accurately, and easily dismantle, through the electric connection structure who utilizes nacelle separation button and machine to include, be convenient for install this nacelle in the fuselage after inside the fixed connection between slide rail and the spout of assurance, can make the machine include by popping out in the straight flute through operation nacelle separation button, can realize the light separation with the slide rail spout, the setting up of module is tracked to cloud platform and cloud platform control makes this nacelle structural design reasonable, effectively slow down shake or vibrations that the unmanned aerial vehicle flight in-process caused to the camera. The utility model discloses a modularization VTOL unmanned aerial vehicle's drawer type nacelle, simple structure not only, reasonable in design, convenient operation easily installs and dismantles moreover, and structural stability is good, has good application prospect.
Furthermore, the pod body comprises a pod upper cover and a pod lower cover, the pod upper cover is connected to the top of the pod lower cover, the slide rail is formed on the top of the pod upper cover, the pod separation button is arranged on the outer side wall of the pod upper cover, and the pan-tilt tracking module and the pan-tilt control module are both arranged inside the pod lower cover.
The nacelle has the advantages of being reasonable in structural design and convenient to install and detach.
Furthermore, the straight notch is a plurality of, and is a plurality of the straight notch is evenly arranged at interval on the slide rail.
The beneficial effect who adopts above-mentioned technical scheme to produce is for this nacelle structural design is reasonable, has effectively improved nacelle and unmanned aerial vehicle fuselage mounting structure's stability.
The nacelle is connected with the nacelle lower cover, the task load module is connected to the outer wall of the nacelle lower cover, and the nacelle connection module is electrically connected with the cradle head control tracking module and the task load module.
Furthermore, a normal camera module and an oblique camera module are hung on the task load module, and the normal camera module and the oblique camera module are electrically connected with the task load module.
The nacelle has the beneficial effects that the nacelle is rich in functions and has good photographing and shooting functions.
Further, still include integrated plug, integrated plug locates on the top face of nacelle upper cover, and with the cloud platform is tracked the module with cloud platform control tracks module electric connection, just integrated plug detachably connects in the unmanned aerial vehicle fuselage.
The nacelle has the advantages of being reasonable in structural design, convenient to install and detach and convenient and fast to operate.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings required to be used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the provided drawings without creative efforts.
Fig. 1 is a schematic structural diagram of a drawer-type pod of a modular vertical take-off and landing unmanned aerial vehicle according to the present invention;
fig. 2 is a top view of a drawer-type pod of a modular vertical take-off and landing drone provided by the present invention;
fig. 3 is a side view of a drawer pod of a modular vertical take-off and landing drone provided by the present invention;
fig. 4 is a schematic structural diagram of the drawer-type pod of the modular vertical take-off and landing drone in an installation state according to the present invention.
Wherein: the unmanned aerial vehicle comprises a pod body 1, a pod upper cover 11, a pod lower cover 12, a sliding rail 2, a pod separation button 3, a pan-tilt tracking module 4, a pan-tilt control tracking module 5, a straight notch 6, a pod connection module 7, a task load module 8, an integrated plug 9 and an unmanned aerial vehicle body 100.
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 and intended to be used for 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 "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in 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, 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 limited otherwise.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," and "fixed" are to be construed broadly and may, 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 meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.
In the present disclosure, unless expressly stated or limited otherwise, the first feature "on" or "under" the second feature may comprise direct contact between the first and second features, or may comprise contact between the first and second features not directly. Also, the first feature being "on," "above" and "over" the second feature includes the first feature being directly on and obliquely above the second feature, or merely indicating that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature includes the first feature being directly under and obliquely below the second feature, or simply meaning that the first feature is at a lesser elevation than the second feature.
The utility model discloses a drawer type pod of a modularized vertical take-off and landing unmanned aerial vehicle, which is detachably arranged in an unmanned aerial vehicle body 100 and comprises a pod body 1, a slide rail 2, a pod separation button 3, a tripod head tracking module 4 and a tripod head control tracking module 5, wherein the pod body 1 is of a cylindrical structure with an open top, the slide rail 2 is of a U-shaped structure and is fixed on the top end surface of the pod body 1, a straight notch 6 is arranged on the slide rail 2, a slide groove matched and in sliding connection with the slide rail 2 is formed on the inner wall of the unmanned aerial vehicle body 100, a bracket is also arranged in the unmanned aerial vehicle body 100, the pod separation button 3 is arranged on the outer side wall of the pod body 1 and is electrically connected with a machine for detachably inserting in the straight notch 6, the tripod head tracking module 4 and the tripod head control tracking module 5 are both arranged in the pod body 1, and the tripod head control tracking module 5 is electrically connected with the tripod head tracking module 4, for controlling the pan-tilt tracking module 4.
According to the utility model discloses an optional embodiment, nacelle body 1 includes nacelle upper cover 11 and nacelle lower cover 12, and nacelle upper cover 11 is connected at nacelle lower cover 12 top, and slide rail 2 is formed at nacelle upper cover 11 top, and nacelle release button 3 locates on 11 lateral walls of nacelle upper cover, and inside nacelle lower cover 12 was all located to cloud platform tracking module 4 and cloud platform control module to make this nacelle structural design reasonable, the installation with dismantle the convenience.
According to the utility model discloses an optional embodiment, straight notch 6 is a plurality ofly, and the even interval of a plurality of straight notch 6 is arranged on slide rail 2 to make this nacelle structural design reasonable, effectively improved nacelle and unmanned aerial vehicle fuselage mounting structure's stability.
According to the utility model discloses an optional embodiment, still include nacelle connection module 7 and task load module 8, on nacelle connection module 7 located 12 bottoms inner walls of nacelle lower cover, task load module 8 is connected on 12 bottoms outer walls of nacelle lower cover, and nacelle connection module 7 tracks module 5 and task load module 8 electric connection with cloud platform control.
According to the utility model discloses an optional embodiment, carry on task load module 8 and have orthographic camera module and slope camera module, and orthographic camera module and slope camera module all with task load module 8 electric connection to make this nacelle function abundant, have good and shoot and make a video recording the function.
According to the utility model discloses an optional embodiment still includes integrated plug 9, and integrated plug 9 is located on the top face of nacelle upper cover 11 to track module 4 and the control of cloud platform and track module 5 electric connection with the cloud platform, and integrated plug 9 detachably connects in unmanned aerial vehicle fuselage 100, thereby makes this nacelle structural design reasonable, and installation and dismantlement convenience, the simple operation.
The utility model discloses a modularization VTOL unmanned aerial vehicle's drawer type nacelle, through the sliding connection structure who utilizes slide rail and the inside spout of unmanned aerial vehicle fuselage, be convenient for operating personnel install this nacelle in the unmanned aerial vehicle fuselage fast accurately, and easily dismantle, through the electric connection structure who utilizes nacelle separation button and machine to draw together, be convenient for install this nacelle inside fixed connection between guaranteeing slide rail and the spout afterwards, can make the machine draw together by popping out in the straight flute through operation nacelle separation button, can realize the light separation with the slide rail spout, the setting up of module is tracked to cloud platform tracking module and cloud platform control makes this nacelle structural design reasonable, effectively slow down shake or vibrations that unmanned aerial vehicle flight in-process caused to the camera. The drawer type pod is simple in structure, reasonable in design, convenient to operate, easy to install and detach, good in structural stability and good in application prospect.
In the description herein, references to the description of the term "one embodiment," "some embodiments," "an example," "a specific example," or "some examples," etc., mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above are not necessarily intended to refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples. Furthermore, various embodiments or examples described in this specification can be combined and combined by those skilled in the art.
Although embodiments of the present invention have been shown and described, it is understood that the above embodiments are exemplary and should not be construed as limiting the present invention, and that variations, modifications, substitutions and alterations can be made to the above embodiments by those of ordinary skill in the art without departing from the scope of the present invention.

Claims (6)

1. A drawer type pod of a modularized vertical take-off and landing unmanned aerial vehicle is detachably installed in an unmanned aerial vehicle body (100) and is characterized by comprising a pod body (1), a slide rail (2), a pod separation button (3), a pan-tilt tracking module (4) and a pan-tilt control tracking module (5), wherein the pod body (1) is of a cylindrical structure with an open top, the slide rail (2) is of a U-shaped structure and is fixed on the top end face of the pod body (1), a straight notch (6) is formed in the slide rail (2), a slide groove matched with the slide rail (2) and in sliding connection with the slide rail is formed in the inner wall of the unmanned aerial vehicle body (100), a basket is further installed in the unmanned aerial vehicle body (100), the pod separation button (3) is arranged on the outer side wall of the pod body (1) and is electrically connected with the unmanned aerial vehicle and is used for controlling the basket to be detachably inserted in the straight notch (6), the cloud platform tracking module (4) and the cloud platform control tracking module (5) are arranged in the pod body (1), and the cloud platform control tracking module (5) is electrically connected with the cloud platform tracking module (4) and used for controlling the cloud platform tracking module (4).
2. The drawer-type pod of a modular VTOL UAV of claim 1, wherein the pod body (1) comprises a pod upper cover (11) and a pod lower cover (12), the pod upper cover (11) is connected to the top of the pod lower cover (12), the slide rail (2) is formed on the top of the pod upper cover (11), the pod separation button (3) is arranged on the outer side wall of the pod upper cover (11), and the pan-tilt tracking module (4) and the pan-tilt control module are arranged inside the pod lower cover (12).
3. The drawer pod of a modular VTOL UAV according to claim 2, characterized in that the number of said slots (6) is multiple, and the multiple slots (6) are arranged on the slide rail (2) at regular intervals.
4. The drawer-type pod of a modular VTOL UAV of claim 2, further comprising a pod connection module (7) and a task load module (8), wherein the pod connection module (7) is disposed on the inner bottom wall of the pod lower cover (12), the task load module (8) is connected to the outer bottom wall of the pod lower cover (12), and the pod connection module (7) is electrically connected to the PTZ control tracking module (5) and the task load module (8).
5. The drawer-type pod of a modular VTOL UAV of claim 4, wherein the task load module (8) is hung with a forward camera module and a tilt camera module, and both the forward camera module and the tilt camera module are electrically connected with the task load module (8).
6. The drawer-type pod of a modular VTOL UAV of claim 4, further comprising an integrated plug (9), wherein the integrated plug (9) is disposed on the top end surface of the pod upper cover (11) and electrically connected to the PTZ tracking module (4) and the PTZ control tracking module (5), and the integrated plug (9) is detachably connected in the UAV body (100).
CN202121051529.8U 2021-05-17 2021-05-17 Drawer type nacelle of modularized vertical take-off and landing unmanned aerial vehicle Active CN214986129U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202121051529.8U CN214986129U (en) 2021-05-17 2021-05-17 Drawer type nacelle of modularized vertical take-off and landing unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202121051529.8U CN214986129U (en) 2021-05-17 2021-05-17 Drawer type nacelle of modularized vertical take-off and landing unmanned aerial vehicle

Publications (1)

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CN214986129U true CN214986129U (en) 2021-12-03

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CN (1) CN214986129U (en)

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