CN214729736U - Multi-functional for unmanned aerial vehicle nacelle - Google Patents
Multi-functional for unmanned aerial vehicle nacelle Download PDFInfo
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- CN214729736U CN214729736U CN202120926367.1U CN202120926367U CN214729736U CN 214729736 U CN214729736 U CN 214729736U CN 202120926367 U CN202120926367 U CN 202120926367U CN 214729736 U CN214729736 U CN 214729736U
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Abstract
The utility model discloses a nacelle for a multifunctional unmanned aerial vehicle, which relates to the field of fire fighting and comprises a mounting rack, a shell, a lighting module, a camera module, a laser aiming module, a distance detection module and a rotary driving piece, wherein both ends of the shell can be rotatably mounted on the mounting rack; the rotation action end of the rotation driving piece acts on the shell; when the pod is installed on the unmanned aerial vehicle, the mounting frame is fixedly connected with the unmanned aerial vehicle, and the camera module, the laser aiming module, the distance detection module and the rotary driving piece are electrically connected with the unmanned aerial vehicle; set up lighting module, camera module and distance detection module through the installation in the shell, and lighting direction, video image acquisition direction, laser aim the direction and, the measuring direction is the same, and when the calamity took place, after the installation nacelle on the unmanned aerial vehicle, it is overhead to reach the scene of an accident, patrols the calamity accident region for a long time through camera module, and the scene of a disaster image is passback in real time, and the distance is surveyed to the excess distance detection module, provides the foundation for the scene of a fire commander decision.
Description
Technical Field
The utility model relates to a fire control field especially relates to a multi-functional for unmanned aerial vehicle nacelle.
Background
The nacelle is mounted on an airplane and is hung on a streamline short cabin section of the airplane body or below the airplane body. The pod is used as a photoelectric device provided with certain airborne equipment or weapons, and can be additionally arranged on the unmanned aerial vehicle to enable the unmanned aerial vehicle to have functions which are not possessed by the pod.
At present, photoelectric pods for expanding the functions of fire-fighting unmanned aerial vehicles are designed and generated, the photoelectric pods mainly comprise a visible light pod, an infrared pod and a laser range finder lamp, and various optical sensors, when a disaster happens, the unmanned aerial vehicle arrives above an accident scene at the first time, long-time patrol is carried out on the disaster accident area by using the airborne photoelectric pod, live images are returned in real time, and a basis is provided for fire scene command decision; the existing pod of the fire-fighting unmanned aerial vehicle can only realize a single function, and the fire-fighting unmanned aerial vehicle generally needs to realize a plurality of functions, so that a plurality of pods are mounted on the unmanned aerial vehicle at the same time, and the load of the unmanned aerial vehicle is increased.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the problem of designing a nacelle for multifunctional unmanned aerial vehicle.
The utility model discloses a following technical scheme realizes above-mentioned purpose:
a pod for a multi-function drone, comprising:
a mounting frame;
a housing; both ends of the shell can be rotatably arranged on the mounting rack;
the camera module is used for acquiring video images;
a lighting module;
the laser aiming module is used for aiming the working target by laser;
the distance detection module is used for measuring the distance between the target object and the unmanned aerial vehicle; the camera module and the distance detection module are both arranged in the shell, and the illumination direction of the illumination module, the video image acquisition direction of the camera module, the aiming direction of the laser aiming module and the measurement direction of the distance detection module are all the same;
the rotary driving piece is used for driving the shell to rotate; the rotation action end of the rotation driving piece acts on the shell; when the nacelle is installed on unmanned aerial vehicle, mounting bracket and unmanned aerial vehicle fixed connection, camera module, laser aim module, distance detection module and rotation driving piece all with unmanned aerial vehicle electrical connection.
The beneficial effects of the utility model reside in that: through the installation set up lighting module in the shell, camera module, laser aim module and distance detection module, and lighting module's direction of illumination, camera module's video image acquisition direction, laser aim direction and distance detection module's direction of measurement is the same, when the calamity takes place, after unmanned aerial vehicle goes up the installation nacelle, arrive the scene of accident overhead for the very first time, carry out long-time patrolling to calamity accident area through camera module, pass back scene of a scene image in real time, also can be through distance detection module measurement distance, provide the basis for the scene of a fire commander decision-making, also can confirm the concrete position of operation target through laser aim module simultaneously, guarantee fire control unmanned aerial vehicle real-time operation's accuracy and high efficiency.
Drawings
Fig. 1 is a perspective view of a pod for a multi-function unmanned aerial vehicle according to the present invention;
fig. 2 is an exploded view of the pod for a multi-function unmanned aerial vehicle according to the present invention;
wherein corresponding reference numerals are:
1-camera, 2-electronic plug-in, 3-second radiator fan, 4-upper radiator plate, 5-side plate, 6-lower radiator plate, 7-lampshade, 8-range finder, 9-lamp bead radiator, 10-lamp bead, 11-first radiator fan, 12-mounting frame, 13-shaft clamp spring, 14-steering engine, 15-front mounting plate, 16-rear mounting plate, 17-connecting shaft, 18-bearing, 19-radiator block and 20-data processing module.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the drawings in the embodiments of the present invention are combined below to clearly and completely describe the technical solutions in the embodiments of the present invention. It is to be understood that the embodiments described are only some of the embodiments of the present invention, and not all of them. The components of embodiments of the present invention, as generally described and illustrated in the figures herein, may be arranged and designed in a wide variety of different configurations.
Thus, the following detailed description of the embodiments of the present invention, presented in the accompanying drawings, is not intended to limit the scope of the invention, as claimed, but is merely representative of selected embodiments of the invention. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts belong to the protection scope of the present invention.
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, it need not be further defined and explained in subsequent figures.
In the description of the present invention, it is to be understood that the terms "upper", "lower", "inner", "outer", "left", "right", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, or orientations or positional relationships that are conventionally placed when the products of the present invention are used, or orientations or positional relationships that are conventionally understood by those skilled in the art, and are merely for convenience of description of the present invention and simplifying the description, but do not indicate or imply that the device or element that is referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention.
Furthermore, the terms "first," "second," and the like are used merely to distinguish one description from another, and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it should be further noted that, unless explicitly stated or limited otherwise, the terms "disposed" and "connected" are to be interpreted broadly, and for example, "connected" may be a fixed connection, a detachable connection, or an integral connection; can be mechanically or electrically connected; the connection may be direct or indirect via an intermediate medium, and may be a communication between the two elements. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.
The following describes in detail embodiments of the present invention with reference to the accompanying drawings.
As shown in fig. 1 and 2, a pod for a multifunctional unmanned aerial vehicle includes:
a mounting frame 12;
a housing; both ends of the housing can be rotatably mounted on the mounting frame 12;
the camera module is used for acquiring video images;
a lighting module;
the laser aiming module is used for aiming the working target by laser;
the distance detection module is used for measuring the distance between the target object and the unmanned aerial vehicle; the camera module and the distance detection module are both arranged in the shell, and the illumination direction of the illumination module, the video image acquisition direction of the camera module, the aiming direction of the laser aiming module and the measurement direction of the distance detection module are all the same;
the rotary driving piece is used for driving the shell to rotate; the rotation action end of the rotation driving piece acts on the shell; when the nacelle is installed on unmanned aerial vehicle, mounting bracket 12 and unmanned aerial vehicle fixed connection, camera module, laser aim module, distance detection module and rotation driving piece all with unmanned aerial vehicle electrical connection.
The shell includes heating panel 4, lower heating panel 6, two blocks of curb plates 5, preceding mounting panel 15 and back mounting panel 16, the opening of making a video recording has been seted up to preceding mounting panel 15, the illumination opening, laser opening and range finding opening, it all is provided with two curved installation concave stations with the side that heating panel 6 is relative down to go up heating panel 4, both ends respectively with the installation concave station extrusion contact of last heating panel 4 and lower heating panel 6 about two lighting lamp covers 7 of lighting module, the distance detection module, laser aims module and camera module fixed mounting respectively at last heating panel 4 and the side that heating panel 6 is relative down, two blocks of curb plates 5 all can rotate and install on mounting bracket 12.
The camera module comprises a camera 1, a camera fixing frame and a camera lens, a screw mounting hole is formed in the middle of an upper heat dissipation plate 4, the camera 1 is fixedly mounted in the middle of the upper heat dissipation plate 4 through the camera fixing frame, a boss is arranged on the inner side of a front mounting plate 15, and the camera lens is in compression fit with the front mounting plate 15 through the camera 1.
The lighting module comprises two lighting lamps, each lighting lamp comprises a lamp shade 7, lamp bead radiating fins 9, lamp beads 10 and a headlamp lens, the upper ends and the lower ends of the lamp bead radiating fins 9 are fixedly connected with the side faces, opposite to the heating panel 6, of the upper heating panel 4 respectively, the lamp beads 10 are in compression fit with the lamp shade 7 through the lamp bead radiating fins 9, a boss is arranged in the middle of the front mounting plate 15, and the headlamp lens is fixedly installed with the front mounting plate 15 through glue.
The top parts of the two side plates 5 are respectively provided with a connecting boss, the connecting boss is provided with a cavity structure for mounting the electronic plug-in 2, and a screw mounting hole is arranged in the connecting boss so as to be quickly connected with the unmanned aerial vehicle through a mounting screw; and completing the electrical connection of the pod to the drone.
The distance detection module includes distancer 8, lid behind distancer lens and the distancer, the boss at upper heating panel 4 middle part is equipped with the screw hole, fix distancer 8 on upper heating panel 4 through the bolt, cover behind the distancer is fixed on upper heating panel 4 through the bolt, preceding mounting panel 5 middle part is equipped with the screw hole, cover is fixed in the front on mounting panel 5 behind the distancer through the screw, preceding mounting panel 15 inboard is equipped with the boss, the distancer lens carries out compressed tightly through distancer 8 and preceding mounting panel 15 and cooperates.
The laser aiming module comprises a diode, a laser fixing piece and a laser lens, wherein a heat dissipation block 19 for increasing the surface area of the diode is arranged in the middle of the upper heat dissipation plate 4, a screw mounting hole and a diode mounting hole are formed in the rear part of the upper heat dissipation plate 4, the diode is arranged in the diode mounting hole of the upper heat dissipation plate 4, the laser fixing piece is fixed on the heat dissipation block 19 in the middle of the upper heat dissipation plate 4 by using a screw, and meanwhile, the mounting and fixing of the diode are realized; the laser lens is in compression fit with the boss on the inner side of the front mounting plate 15 through the middle part of the upper heat dissipation plate 4.
The data processing module 20 is installed on the lower heat dissipation plate 6, and the data processing module 20 is used for function configuration and control of each module; the data processing module 20 can receive the unmanned aerial vehicle control signal, and the signal processing unit of the data processing module 20 configures and controls the working parameters of the laser aiming module, the distance detection module, the illumination module and the camera module.
The shell includes first radiator fan 11 and two second radiator fan 3, and first radiator fan 11 installs on lower heating panel 6, is provided with the ventilation export that is used for first radiator fan 11 to exhaust on the lower heating panel 6, and two second radiator fan 3 respectively fixed mounting are in two lamp shades 7 one side near back mounting panel 16, and back mounting panel 16 is provided with two ventilation intakes, and the air intake of second radiator fan 3 is located two ventilation intakes respectively.
Each ventilation inlet is provided with a plurality of inclined baffles, the height of one end, close to the second cooling fan 3, of each inclined baffle is higher than that of one end, and the height of one end, far away from the second cooling fan 3, of each inclined baffle.
The rotary driving piece is a steering engine 14, connecting shafts 17 are fixedly mounted on the side faces, away from each other, of the two side plates 5, bearings 18 are fixedly mounted in the middle of the two connecting shafts 17, outer rings of the two bearings 18 are fixedly connected with the mounting frame 12, a rotating shaft of the steering engine 14 is fixedly connected with one of the connecting shafts 17, and the steering engine 14 is fixedly connected with the mounting frame 12 through screws.
Bosses are arranged at the tops of the left fixing disk and the right fixing disk, and screw mounting holes are arranged in the bosses, so that the multifunctional nacelle and the unmanned aerial vehicle can be quickly connected through mounting screws; the top of the right fixing disc is provided with a cavity for installing an electronic plug-in 2 to complete the electrical connection of the multifunctional nacelle and the unmanned aerial vehicle.
The maximum rotation angle of the housing is 90 °.
And the radiating block 19 is used for increasing the radiating area of the diode in the laser aiming module, and both the radiating block 19 and the diode are fixedly arranged on the upper side surface of the upper radiating plate 4.
Through the installation set up lighting module in the shell, camera module, laser aim module and distance detection module, and lighting module's direction of illumination, camera module's video image acquisition direction, laser aim direction and distance detection module's direction of measurement is the same, when the calamity takes place, after unmanned aerial vehicle goes up the installation nacelle, arrive the scene of accident overhead for the very first time, carry out long-time patrolling to calamity accident area through camera module, pass back scene of a scene image in real time, also can be through distance detection module measurement distance, provide the basis for the scene of a fire commander decision-making, also can confirm the concrete position of operation target through laser aim module simultaneously, guarantee fire control unmanned aerial vehicle real-time operation's accuracy and high efficiency.
The technical scheme of the utility model is not limited to the restriction of above-mentioned specific embodiment, all according to the utility model discloses a technical scheme makes technical deformation, all falls into within the protection scope of the utility model.
Claims (8)
1. A nacelle for a multi-functional unmanned aerial vehicle, comprising:
a mounting frame;
a housing; both ends of the shell can be rotatably arranged on the mounting rack;
the camera module is used for acquiring video images;
a lighting module;
the laser aiming module is used for aiming the working target by laser;
the distance detection module is used for measuring the distance between the target object and the unmanned aerial vehicle; the camera module and the distance detection module are both arranged in the shell, and the illumination direction of the illumination module, the video image acquisition direction of the camera module, the aiming direction of the laser aiming module and the measurement direction of the distance detection module are all the same;
the rotary driving piece is used for driving the shell to rotate; the rotation action end of the rotation driving piece acts on the shell; when the nacelle is installed on unmanned aerial vehicle, mounting bracket and unmanned aerial vehicle fixed connection, camera module, laser aim module, distance detection module and rotation driving piece all with unmanned aerial vehicle electrical connection.
2. The pod for the multifunctional unmanned aerial vehicle as claimed in claim 1, wherein the housing comprises an upper heat dissipation plate, a lower heat dissipation plate, two side plates, a front mounting plate and a rear mounting plate, the front mounting plate is provided with a camera opening, a lighting opening, a laser opening and a distance measuring opening, two arc-shaped mounting concave platforms are arranged on opposite sides of the upper heat dissipation plate and the lower heat dissipation plate, upper and lower ends of two lighting lamp covers of the lighting module are respectively in pressing contact with the mounting concave platforms of the upper heat dissipation plate and the lower heat dissipation plate, the laser aiming module, the distance detection module and the camera module are respectively and fixedly mounted on opposite sides of the upper heat dissipation plate and the lower heat dissipation plate, and the two side plates are rotatably mounted on the mounting frame.
3. The pod for the multifunctional unmanned aerial vehicle as claimed in claim 2, wherein the housing comprises a first cooling fan and two second cooling fans, the first cooling fan is mounted on the lower cooling plate, the lower cooling plate is provided with a ventilation outlet for the first cooling fan to exhaust air, the two second cooling fans are respectively and fixedly mounted on one sides of the two lamp shades close to the rear mounting plate, the rear mounting plate is provided with two ventilation inlets, and the air inlets of the second cooling fans are respectively located at the two ventilation inlets.
4. The pod for a multi-functional unmanned aerial vehicle of claim 3, wherein each ventilation inlet is fitted with a plurality of inclined baffles, the height of each inclined baffle at an end near the second heat dissipating fan being higher than the height of each inclined baffle at an end away from the second heat dissipating fan.
5. The pod for the multifunctional unmanned aerial vehicle as claimed in claim 2, wherein the rotary driving member is a steering engine, the side surfaces of the two side plates which are deviated from each other are fixedly provided with connecting shafts, the middle parts of the two connecting shafts are fixedly provided with bearings, the outer rings of the two bearings are fixedly connected with the mounting frame, the rotating shaft of the steering engine is fixedly connected with one of the connecting shafts, and the steering engine is fixedly arranged in the mounting frame.
6. The pod for a multipurpose unmanned aerial vehicle according to any one of claims 1 to 5, wherein a maximum rotation angle of the housing is 90 °.
7. The pod for the multi-functional unmanned aerial vehicle of claim 6, further comprising a heat sink for increasing a heat dissipation area of the diode in the laser sighting module, wherein the heat sink and the diode are fixedly mounted on an upper side surface of the upper heat sink.
8. The pod for the multifunctional unmanned aerial vehicle of claim 1, further comprising a data processing module, wherein the data processing module is mounted on the lower heat dissipation plate, the data processing module is used for functional configuration and control of the laser aiming module, the distance detection module, the illumination module and the camera module, and the data processing module is in communication connection with the unmanned aerial vehicle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120926367.1U CN214729736U (en) | 2021-04-30 | 2021-04-30 | Multi-functional for unmanned aerial vehicle nacelle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120926367.1U CN214729736U (en) | 2021-04-30 | 2021-04-30 | Multi-functional for unmanned aerial vehicle nacelle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214729736U true CN214729736U (en) | 2021-11-16 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120926367.1U Active CN214729736U (en) | 2021-04-30 | 2021-04-30 | Multi-functional for unmanned aerial vehicle nacelle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214729736U (en) |
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2021
- 2021-04-30 CN CN202120926367.1U patent/CN214729736U/en active Active
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Address after: No. 1666 Oucheng North Road, Qingbaijiang District, Chengdu City, Sichuan Province, 610300, Building 28, Annex 1 Patentee after: Sichuan Guofei Innovation Aviation Technology Co.,Ltd. Address before: 618300 1, building 16, No. 2, Section 1, Guangzhou road, Guanghan City, Deyang City, Sichuan Province Patentee before: Sichuan zhongtianhai Innovation Technology Co.,Ltd. |