CN217496548U - Shell structure and formation unmanned aerial vehicle - Google Patents
Shell structure and formation unmanned aerial vehicle Download PDFInfo
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- CN217496548U CN217496548U CN202221232235.XU CN202221232235U CN217496548U CN 217496548 U CN217496548 U CN 217496548U CN 202221232235 U CN202221232235 U CN 202221232235U CN 217496548 U CN217496548 U CN 217496548U
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Abstract
The utility model discloses a shell structure and formation unmanned aerial vehicle, the formation unmanned aerial vehicle includes shell structure, and shell structure includes upper cover, fuselage center, lower cover and front end housing, and upper cover and lower cover are connected with fuselage center respectively, form a first installation cavity for installing electronic module between the three; the front end cover is connected with the middle frame of the machine body, and a second mounting cavity for mounting the sensor is formed by the front end cover and the middle frame of the machine body; the utility model provides a shell structure and formation unmanned aerial vehicle have easy dismounting's characteristics, through installing upper cover, lower cover and front end housing respectively to the fuselage center can accomplish shell structure's installation, easy dismounting to the shell structure after the equipment is accomplished forms the first installation cavity that is used for installing electronic module and is used for installing the second installation cavity of sensor, and each installation cavity is independent each other, reduces the interference problem between each electronic module and the sensor.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to a shell structure and formation unmanned aerial vehicle.
Background
With the rapid development of economy, the unmanned aerial vehicle for civil use is rapidly developed, the civil unmanned aerial vehicle as one type of the unmanned aerial vehicle is widely applied to the fields of aerial photography of some photography enthusiasts in our lives, and some defects and shortcomings still exist in the using process of some existing intelligent unmanned aerial vehicles. Traditional intelligent unmanned aerial vehicle does not have a convenient structure of dismantlement of installation at the in-process that uses to sensor and electronic module are all installed in the casing, make to take place easily and disturb between sensor and the electronic module, thereby influence signal transmission quality, can influence unmanned aerial vehicle's flight safety even when serious.
SUMMERY OF THE UTILITY MODEL
The utility model discloses the technical problem that will solve is: the utility model provides a make things convenient for shell structure and formation unmanned aerial vehicle of dismouting.
In order to solve the technical problem, the utility model discloses a technical scheme be: a shell structure comprises an upper cover, a machine body middle frame, a lower cover and a front end cover, wherein the upper cover and the lower cover are respectively connected with the machine body middle frame, and a first mounting cavity for mounting an electronic module is formed among the upper cover, the machine body middle frame, the lower cover and the front end cover; the front end cover is connected with the middle frame of the machine body, and a second installation cavity for installing the sensor is formed by the front end cover and the middle frame of the machine body.
Further, the front end cover is provided with a fixing portion, and the sensor is mounted on the fixing portion.
Furthermore, the lower cover is made of semitransparent materials.
Further, the sensor is TOF, light stream, camera, bluetooth or keeps away barrier module.
Furthermore, the middle frame of the machine body is provided with a ventilation notch communicated with the inner side of the middle frame.
Furthermore, the fuselage center is equipped with the horn that extends to its outside, the horn is used for installing rotor motor, the horn with fuselage center junction is equipped with the ventilation breach.
Furthermore, the lower cover is provided with a ventilation gap corresponding to the ventilation gap.
Furthermore, the front end cover is provided with a positioning bulge, and the middle frame of the machine body is provided with a positioning slot connected with the positioning bulge.
Furthermore, the electronic module can be one or more of a lamp panel, an MCU central control board, an IMU inertial navigation board and a battery.
In order to solve the technical problem, the utility model also provides a formation unmanned aerial vehicle, including above-mentioned shell structure.
The beneficial effects of the utility model reside in that: the utility model provides a shell structure and formation unmanned aerial vehicle have easy dismounting's characteristics, through installing upper cover, lower cover and front end housing respectively to the fuselage center can accomplish shell structure's installation, easy dismounting to the shell structure after the equipment is accomplished forms the first installation cavity that is used for installing electronic module and is used for installing the second installation cavity of sensor, and each installation cavity is independent each other, reduces the interference problem between each electronic module and the sensor.
Drawings
Fig. 1 is an exploded view of a housing structure according to a first embodiment of the present invention;
fig. 2 is a schematic structural diagram of a lower shell assembly of a shell structure according to a first embodiment of the present invention.
Description of reference numerals:
1. an upper cover; 2. a fuselage middle frame; 21. a horn; 22. a ventilation gap; 3. a front end cover; 31. a fixed part; 32. positioning the projection; 4. a lower cover; 41. a ventilation gap; 5. a sensor.
Detailed Description
In order to explain the technical contents, the objects and the effects of the present invention in detail, the following description is made with reference to the accompanying drawings in combination with the embodiments.
Referring to fig. 1 to 2, a housing structure includes an upper cover 1, a middle frame 2, a lower cover 4 and a front end cover 3, where the upper cover 1 and the lower cover 4 are respectively connected to the middle frame 2, and a first mounting cavity for mounting an electronic module is formed therebetween; the front end cover 3 is connected with the lower cover 4 and the machine body middle frame 2, and a second installation cavity for installing the sensor 5 is formed by the front end cover, the lower cover and the machine body middle frame.
From the above description, the beneficial effects of the present invention are: the installation of shell structure can be accomplished to fuselage center 2 through installing upper cover 1, lower cover 4 and front end housing 3 respectively, easy dismounting to the shell structure after the equipment is accomplished forms the first installation cavity that is used for installing electronic module and is used for installing sensor 5's second installation cavity, has reduced the signal interference between electronic module and the sensor 5, has ensured signal transmission's quality.
Further, the front end cap 3 is provided with a fixing portion 31, and the sensor 5 is mounted on the fixing portion 31.
As can be seen from the above description, the fixing portion 31 facilitates fixing the sensor 5, and ensures the stability of the operation of the sensor 5.
Further, the lower cover 4 is made of a semitransparent material.
As can be seen from the above description, the material of the lower cover 4 can be set according to the actual application requirement.
Further, the sensor 5 is a TOF module, an optical flow module, a camera, a bluetooth module or an obstacle avoidance module.
As can be seen from the above description, the sensor 5 can be selected according to the actual application requirements.
Further, the middle frame 2 of the body is provided with a ventilation notch 22 communicated with the inner side of the middle frame.
As can be seen from the above description, the ventilation notch 22 facilitates the external air to enter and exit the housing structure, and facilitates heat dissipation.
Further, fuselage center 2 is equipped with the horn 21 that extends to its outside, horn 21 is used for installing the rotor motor, horn 21 with fuselage center 2 junction is equipped with ventilation breach 22.
As can be seen from the above description, the position of the ventilation notch 22 can be set according to the actual application requirement.
Further, the lower cover 4 is provided with a ventilation gap 41 corresponding to the ventilation gap 22.
As can be seen from the above description, the ventilation notch 41 corresponding to the ventilation notch 22 is provided in the lower cover 4, which is beneficial to further improving the heat dissipation performance.
Furthermore, the front end cover 3 is provided with a positioning protrusion 32, and the middle frame 2 of the machine body is provided with a positioning slot connected with the positioning protrusion 32.
As can be seen from the above description, the positioning protrusions 32 are connected with the positioning slots in a matching manner, so that the front end cover 3 is connected with the middle frame 2 of the body.
Furthermore, the electronic module can be one or more of a lamp panel, an MCU central control board, an IMU inertial navigation board and a battery.
In order to solve the technical problem, the utility model also provides a formation unmanned aerial vehicle, including above-mentioned shell structure.
Example one
Referring to fig. 1 and fig. 2, a first embodiment of the present invention is: an unmanned plane for formation comprises a shell structure, wherein the shell structure comprises an upper cover 1, a middle frame 2 of a machine body and a lower shell assembly, the lower shell assembly comprises a lower cover 4 and a front end cover 3, the upper cover 1 and the lower cover 4 are respectively connected with the middle frame 2 of the machine body, and a first installation cavity for installing an electronic module is formed among the upper cover 1, the lower cover 4 and the middle frame 2 of the machine body; the front end cover 3 is connected with the middle frame 2 of the machine body, and a second mounting cavity for mounting a sensor 5 is formed by the front end cover and the middle frame; specifically, the upper cover 1, the lower cover 4 and the front end cover 3 are installed in the body middle frame 2 in a screw connection mode, a bolt connection mode or a buckle connection mode, and the specific installation mode can be set according to actual application requirements, which is not repeated herein.
Preferably, the front end cover 3 is provided with a fixing portion 31, the sensor 5 is mounted on the fixing portion 31, and the fixing portion 31 is convenient for fixing the sensor 5, so as to ensure the stability of the operation of the sensor 5; specifically, the fixing portion 31 is an installation groove formed in the front end cover 3; more specifically, the front end housing 3 is provided with a positioning protrusion 32, and the body middle frame 2 is provided with a positioning slot connected with the positioning protrusion 32, so that the front end housing 3 is connected with the body middle frame 2.
In this embodiment, the material of lower cover 4 is translucent material, so, the homogeneous light of being convenient for, the material of front end housing 3 is the plastic material, and it is specifically can be according to actual application demand to be right the material of lower cover 4 and front end housing 3 sets up.
Optionally, the sensor 5 is one or more Of a TOF (Time Of Flight), an optical flow, a camera, bluetooth or an obstacle avoidance module, and the electronic module may be one or more Of a lamp panel, an MCU center control panel, an IMU inertial navigation panel and a battery; the sensor 5 and the electronic module may be specifically selected and matched according to actual application requirements.
Preferably, the middle frame 2 of the airframe is provided with a ventilation notch 22 communicated with the inner side of the middle frame, the ventilation notch 22 is convenient for external air to enter and exit the shell structure, and is convenient for heat dissipation, specifically, in this embodiment, the middle frame 2 of the airframe is provided with a horn 21 extending to the outer side of the middle frame, the horn 21 is used for installing a rotor motor, and the ventilation notch 22 is arranged at the joint of the horn 21 and the middle frame 2 of the airframe; in detail, the lower cover 4 is provided with a ventilation notch 41 corresponding to the ventilation notch 22, so that further improvement of heat dissipation performance is facilitated.
To sum up, the shell structure and the formation unmanned aerial vehicle provided by the utility model have the characteristics of convenient assembly and disassembly, the installation of the shell structure can be completed by respectively installing the upper cover, the lower cover and the front end cover to the middle frame of the body, the assembly and disassembly are convenient, and the assembled shell structure forms a first installation cavity for installing the electronic module and a second installation cavity for installing the sensor, the installation cavities are independent from each other, and the interference problem between the electronic modules and the sensor is reduced; the ventilation notch and the ventilation opening are arranged to facilitate the external air to enter and exit the shell structure, so that the heat dissipation is facilitated.
The above mentioned is only the embodiment of the present invention, and not the limitation of the patent scope of the present invention, all the equivalent transformations made by the contents of the specification and the drawings, or the direct or indirect application in the related technical field, are included in the patent protection scope of the present invention.
Claims (10)
1. A shell structure is characterized by comprising an upper cover, a machine body middle frame, a lower cover and a front end cover, wherein the upper cover and the lower cover are respectively connected with the machine body middle frame, and a first mounting cavity for mounting an electronic module is formed among the upper cover, the lower cover and the machine body middle frame; the front end cover is connected with the middle frame of the machine body, and a second installation cavity for installing the sensor is formed by the front end cover and the middle frame of the machine body.
2. The housing structure according to claim 1, wherein the front end cap is provided with a fixing portion to which the sensor is mounted.
3. The housing structure of claim 1, wherein the lower cover is made of a translucent material.
4. The housing structure according to claim 1, characterized in that the sensor is a TOF, optical flow, camera, bluetooth or obstacle avoidance module.
5. The enclosure structure of claim 1, wherein the fuselage center defines a vent opening in communication with an interior side thereof.
6. The enclosure structure of claim 5, wherein the fuselage center frame is provided with a horn extending outwardly therefrom, the horn being configured to mount a rotor motor, the ventilation gap being provided at a junction of the horn and the fuselage center frame.
7. The housing structure according to claim 5, characterized in that the lower cover is provided with ventilation slits corresponding to the ventilation notches.
8. The shell structure as claimed in claim 1, wherein the front end cover is provided with a positioning protrusion, and the middle frame of the body is provided with a positioning slot connected with the positioning protrusion.
9. The housing structure of claim 1, wherein the electronic module is one or more of a lamp panel, an MCU center control board, an IMU inertial navigation board, and a battery.
10. A formation drone, characterized in that it comprises a housing structure according to any one of claims 1 to 9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221232235.XU CN217496548U (en) | 2022-05-20 | 2022-05-20 | Shell structure and formation unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221232235.XU CN217496548U (en) | 2022-05-20 | 2022-05-20 | Shell structure and formation unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217496548U true CN217496548U (en) | 2022-09-27 |
Family
ID=83353265
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221232235.XU Active CN217496548U (en) | 2022-05-20 | 2022-05-20 | Shell structure and formation unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217496548U (en) |
-
2022
- 2022-05-20 CN CN202221232235.XU patent/CN217496548U/en active Active
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