CN209767536U - Aircraft communication device based on mobile communication technology and aircraft with same - Google Patents
Aircraft communication device based on mobile communication technology and aircraft with same Download PDFInfo
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- CN209767536U CN209767536U CN201920729998.7U CN201920729998U CN209767536U CN 209767536 U CN209767536 U CN 209767536U CN 201920729998 U CN201920729998 U CN 201920729998U CN 209767536 U CN209767536 U CN 209767536U
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Abstract
The utility model discloses an aircraft communication device and aircraft that has it based on mobile communication technique, aircraft communication device includes: the box body is internally limited with an accommodating cavity and is provided with a through hole and a plurality of jacks communicated with the accommodating cavity; the communication module is arranged in the accommodating cavity and can receive mobile communication signals, and is provided with an antenna plug-in module corresponding to the through hole and a plug-in module corresponding to the socket; the communication antenna comprises a first antenna segment and a second antenna segment, one end of the first antenna segment penetrates through the through hole and is detachably connected with the antenna plug-in module, and one end of the second antenna segment is pivotally connected with the other end of the first antenna segment. This aircraft communication device based on mobile communication technique can make aircraft and ground station real-time communication, has simple structure, and easy dismounting is convenient for store and transport, advantages such as outward appearance is pleasing to the eye.
Description
Technical Field
the utility model belongs to the technical field of the communication, concretely relates to aircraft communication device based on mobile communication technology and aircraft based on mobile communication technology's aircraft that has this aircraft.
Background
All control of the aircraft flying in the air need to be controlled through the ground or other means, the flight mode is limited to a network in a certain space area, and ultra-long-distance control cannot be achieved, so that the unmanned aerial vehicle is out of range after flying out of the control range, the condition of loss of connection occurs, and the use of the aircraft is limited.
the communication device is a device which can connect two or more devices to communicate with each other by using a signal transmission technology and can protect a built-in communication electronic element, and the devices establish communication with the outside through the communication electronic element. The existing communication device is usually provided with a fixedly connected communication antenna, and particularly for the communication device for the aircraft, the communication antenna cannot be quickly disassembled, only external force damage can be implemented, and resources are wasted. Moreover, the main body of the communication device is not easy to disassemble, and requires a special tool and a trained operator to operate, which is complicated. When actual storage and transport communication box, because communication antenna and communication box body fixed connection lead to unable quick adjustment communication antenna to the state of accomodating, communication antenna not only occupation space is big, is scraped or extrudeed by other objects on every side easily moreover, has increased communication device's defective rate.
SUMMERY OF THE UTILITY MODEL
The utility model discloses aim at solving one of the technical problem that exists among the prior art at least.
Therefore, the utility model provides an aircraft communication device based on mobile communication technology, this aircraft communication device based on mobile communication technology convenient to use, the assembly is simple, is convenient for store and carry, installs this aircraft communication device on the aircraft, can realize the control to the aircraft super remote distance.
According to the utility model discloses aircraft communication device based on mobile communication technique of first aspect embodiment includes: the box body is internally limited with an accommodating cavity and is provided with a through hole and a plurality of jacks communicated with the accommodating cavity; the communication module is arranged in the accommodating cavity and can receive mobile communication signals, and is provided with an antenna plug-in module corresponding to the through hole and a plug-in module corresponding to the socket; the communication antenna comprises a first antenna segment and a second antenna segment, one end of the first antenna segment penetrates through the through hole and is detachably connected with the antenna plug-in module, and one end of the second antenna segment is pivotally connected with the other end of the first antenna segment.
According to the utility model discloses aircraft communication device based on mobile communication technique is injectd in the box body and is held the chamber, is being equipped with communication module holding the intracavity, and communication antenna can peg graft with communication module through establishing the through-hole on the box body. The communication antenna comprises a first antenna segment and a second antenna segment, when the aircraft communication device based on the mobile communication technology needs to be stored and transported, only one end of the second antenna segment needs to be rotated around the other end of the first antenna segment, so that the second antenna segment can be adjusted to be in a storage state, pressure loss in the storage and transportation processes is prevented, and the communication strength can be improved in the adjustment process. This aircraft communication device based on mobile communication technique has simple structure, convenient to detach and installation, improves advantages such as convenience and security of storage and transport.
According to the utility model discloses an embodiment, the box body includes: the shell is formed into a box shape with one open end, the through hole is formed in the shell along the thickness direction of one side wall of the shell, and the socket is formed in the shell along the thickness direction of the other side wall of the shell; a bottom cover removably connected to the housing and cooperating with the housing to define the receiving cavity.
According to the utility model discloses an embodiment, communication module is equipped with the mounting hole that link up along its thickness direction, the bottom along its thickness direction be equipped with the counter sink that the mounting hole corresponds, aircraft communication device based on mobile communication technique still includes: and one end of the connecting piece sequentially penetrates through the counter bore and the mounting hole and then is detachably connected with the shell.
According to an embodiment of the invention, the connecting member is formed as a screw or a bolt.
According to the utility model discloses an embodiment, aircraft communication device based on mobile communication technique still include: the flexible piece, flexible piece detachably locates the counter sink and with the other end of connecting piece ends.
According to the utility model discloses an embodiment, aircraft communication device based on mobile communication technique still include: the positioning part is arranged on one side of the bottom cover facing to the direction of the shell, the positioning part is formed into a plurality of bulges protruding towards the direction of the shell, and the bulges are stopped against the communication module to fix the communication module.
According to an embodiment of the present invention, the first antenna segment comprises: one end of the first segment body is formed into a contact part, the contact part penetrates through the through hole to be detachably connected with the antenna plug-in module, and the contact part is in threaded connection with the through hole; and one end of the second section body is detachably connected with the other end of the first section body, and the other end of the second section body is pivotally connected with one end of the second antenna section.
According to the utility model discloses an embodiment, the first section body with second section body threaded connection.
According to the utility model discloses an embodiment, the second antenna section for first antenna section is movable between primary importance and second place, the second antenna section for first antenna section is located during primary importance, the axis of first antenna section with the axis of second antenna section is located same straight line, the second antenna section for first antenna section is located during the second place, the axis of first antenna section with the axis of second antenna section is perpendicular.
According to the utility model discloses an embodiment, the grafting module includes: the UART plug-in module can be respectively in communication connection with the aircraft and the communication module; and the SIM card inserting module can install or detach the SIM card.
According to the utility model discloses an embodiment, the grafting module still includes: and the Ethernet plug-in module is used for connecting the Ethernet equipment externally connected with the aircraft with the communication module.
according to the utility model discloses an embodiment, aircraft communication device based on mobile communication technique still include: and the USB host plug-in module is used for upgrading the firmware of the communication module.
according to the utility model discloses an embodiment, communication module is the PCBA board.
according to the utility model discloses an embodiment is equipped with the storage tank on the aircraft for place aircraft communication device, fix aircraft communication device on the aircraft through fixing device.
According to the utility model discloses an embodiment, communication module still is equipped with the reset key for to aircraft communication device resume factory setting.
The aircraft according to the second aspect of the present invention comprises the mobile communication technology-based aircraft communication device according to any one of the above.
additional aspects and advantages of the invention will be set forth in part in the description which follows and, in part, will be obvious from the description, or may be learned by practice of the invention.
drawings
the above and/or additional aspects and advantages of the present invention will become apparent and readily appreciated from the following description of the embodiments, taken in conjunction with the accompanying drawings of which:
Fig. 1 is a schematic structural diagram of an aircraft communication device based on mobile communication technology according to an embodiment of the present invention;
FIG. 2 is an exploded view of FIG. 1;
Fig. 3 is a schematic structural diagram of a second antenna segment of the aircraft communication device based on mobile communication technology at a second position according to an embodiment of the present invention;
FIG. 4 is a top view of FIG. 3;
FIG. 5 is a bottom view of FIG. 3;
FIG. 6 is a rear view of FIG. 3;
Fig. 7 is a left side view of fig. 3.
reference numerals:
An aircraft communication device 100 based on mobile communication technology;
a case 10; a through hole 11; a socket 12; a housing 13; a bottom cover 14; a counterbore 15;
A communication module 20; a mounting hole 21;
A communication antenna 30; a first antenna segment 31; a second antenna segment 32; a first segment 33; a second segment 34; a first position 35; a second position 36;
A flexible member 40; and a positioning part 50.
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 only for the purpose of 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 "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", "axial", "radial", "circumferential", and the like, indicate the orientation or positional relationship indicated based on 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, 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 otherwise specified.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
The aircraft communication device 100 based on the mobile communication technology according to the embodiment of the present invention is described in detail below with reference to the drawings.
As shown in fig. 1 to 7, an aircraft communication device 100 based on mobile communication technology according to an embodiment of the present invention includes: a box body 10, a communication module 20 and a communication antenna 30.
Specifically, a containing cavity is defined in the box body 10, the box body 10 is provided with a through hole 11 communicated with the containing cavity and a plurality of sockets 12, the communication module 20 is arranged in the containing cavity and can receive mobile communication signals, the communication module 20 is provided with an antenna plug-in module corresponding to the through hole 11 and a plug-in module corresponding to the sockets 12, the communication antenna 30 comprises a first antenna segment 31 and a second antenna segment 32, one end of the first antenna segment 31 passes through the through hole 11 to be detachably connected with the antenna plug-in module, and one end of the second antenna segment 32 is pivotally connected with the other end of the first antenna segment 31.
In other words, according to the utility model discloses an aircraft communication device 100 based on mobile communication technique mainly comprises box body 10, communication module 20 and communication antenna 30, has limited in box body 10 and has held the chamber, can be equipped with communication module 20 holding the intracavity, and box body 10 is equipped with and holds the through-hole 11 and a plurality of socket 12 of chamber intercommunication, and socket 12 can be SIM draw-in groove and input port and/or output port. The communication module 20 is provided with a plug-in module corresponding to the socket 12, through which the SIM card can be plugged in and out and a communication connection with other devices can be established. The communication module 20 is provided with an antenna plug-in module corresponding to the through hole 11, the communication antenna 30 comprises a first antenna segment 31 and a second antenna segment 32, one end of the first antenna segment 31 passes through the through hole 11 to be detachably connected with the antenna plug-in module, connection between the communication module 20 and the first antenna segment can be achieved, and the antenna plug-in module further has the advantages of convenience in installation and disassembly and the like. One end of the second antenna segment 32 is pivotally connected to the other end of the first antenna segment 31, that is, the second antenna segment 32 can move around the other end of the first antenna segment 31, which not only enhances the signal strength, but also facilitates storage and transportation.
Therefore, according to the utility model discloses an aircraft communication device 100 based on mobile communication technique adopts box body 10, communication module 20 and communication antenna 30 combine together, it holds the chamber to inject in the box body 10, be equipped with communication module 20 holding the intracavity, be equipped with through-hole 11 and a plurality of socket 12 on box body 10, communication antenna 30 includes first antenna section 31 and second antenna section 32, the one end of first antenna section 31 passes through-hole 11 and can dismantle with communication module 20 and link to each other, the one end of second antenna section 32 and the other end pivotally of first antenna section 31 can link to each other, this aircraft communication device 100 based on mobile communication technique not only can strengthen communication device's signal intensity through setting up communication antenna 30, and adopt the structure that communication antenna 30 is pivotable, have and be convenient for storage and transportation, advantages such as convenient to dismantle and install.
According to the utility model discloses an embodiment, box body 10 includes casing 13 and bottom 14, and casing 13 forms the box-like that one end is open, and casing 13 is equipped with through-hole 11 along one of them side wall thickness direction, and casing 13 is equipped with socket 12 along its another side wall thickness direction, and open department can be located to bottom 14, and bottom 14 links to each other with casing 13 detachably and prescribes a limit to with casing 13 and holds the chamber, can open and close bottom 14 and casing 13 fast, and the operation of being convenient for improves the installation effectiveness.
Alternatively, the through hole 11 and the socket 12 may be located on two adjacent side walls, and the box 10 may be formed as a rectangular box-shaped body, or may be formed as a structure with other shapes, specifically configured as required.
Furthermore, the communication module 20 is provided with a mounting hole 21 penetrating through the communication module in the thickness direction, the bottom cover 14 is provided with a counter bore 15 corresponding to the mounting hole 21 in the thickness direction, and one end of the counter bore 15 facing the communication module 20 can be stopped against the lower end face of the communication module 20 by the counter bore 15, so that the bottom cover 14 and the communication module 20 can be arranged at intervals, and the communication module 20 can be positioned to a certain extent. The aircraft communication device 100 based on the mobile communication technology further comprises a connecting piece, one end of the connecting piece penetrates through the counter bore 15 and the mounting hole 21 in sequence and then is detachably connected with the shell 13, and the bottom cover 14, the communication module 20 and the shell 13 can be locked through the connecting piece.
Optionally, the connecting piece is formed into screw or screw, has advantages such as extensive, the low price, reduction in production cost.
As shown in fig. 2, further, the aircraft communication device 100 based on the mobile communication technology further includes a flexible member 40, the flexible member 40 is detachably disposed in the counter bore 15 and abuts against the other end of the connector, and after the bottom cover 14, the communication module 20 and the housing 13 are completely fixed by using the connector, the flexible member 40 can be placed in the counter bore 15 to fill the counter bore 15, so that the appearance of the aircraft communication device 100 based on the mobile communication technology is more beautiful, and the bottom cover 14 can be prevented from being scratched. Wherein the flexible member 40 may be formed as a rubber cork.
Preferably, a recess is provided at the periphery of the counter bore 15, from which recess the rubber cork can be removed when the aircraft communication device 100 based on mobile communication technology is to be disassembled.
In some embodiments of the present invention, the aircraft communication device 100 based on mobile communication technology further includes a positioning portion 50, the positioning portion 50 is disposed on one side of the bottom cover 14 facing to the direction of the housing 13, the positioning portion 50 is formed as a plurality of protrusions protruding towards the direction of the housing 13, and the protrusions can stop against the communication module 20 to fix the communication module 20.
Alternatively, the positioning portion 50 may be formed as a raised ridge, the positioning portion 50 has a groove, and at least a portion of the lower end surface of the communication module 20 can extend into the groove to prevent damage during positioning.
It should be noted that the positioning portion 50 and the bottom cover 14 may be integrally formed.
as shown in fig. 2, according to an embodiment of the present invention, the first antenna segment 31 includes a first segment 33 and a second segment 34, one end of the first segment 33 is formed as a contact portion, the contact portion passes through the through hole 11 and is detachably connected to the antenna plug-in module, the contact portion is connected to the through hole 11 by screw threads, one end of the second segment 34 is detachably connected to the other end of the first segment 33, and the other end of the second segment 34 is pivotably connected to one end of the second antenna segment 32. That is, when mounting, the contact portion may be detachably connected to the communication module 20 through the through hole 11, the second segment 34 may be detachably connected to the first segment 33, the other end of the second segment 34 may be movably connected to the second antenna segment 32, and when the communication antenna 30 needs to be rotated for storage, storage or transportation, the second antenna segment 32 may be moved around the other end of the second segment 34.
alternatively, the second antenna segment 32 may be formed as a cylinder, one end of the second antenna segment 32 may be pivotally connected to the other end of the second segment 34, and the radial dimension of the other end of the second antenna segment 32 is smaller than the radial dimension of the one end of the second antenna segment 32.
The first segment 33 and the second segment 34 may be respectively formed as a cylindrical member, and a radial dimension of the first segment 33 may be smaller than a radial dimension of the second segment 34. The periphery of the second segment 34 is provided with a texture structure which is coaxial with the second segment 34 and increases friction, so that the locking degree between the first antenna segment 31 and the box body 10 is improved conveniently, and the first antenna segment 31 is prevented from falling off.
Further, the first section 33 and the second section 34 are connected by screw threads, so that the installation and the disassembly are convenient, and the operation is convenient.
As shown in fig. 1 and 3, in some embodiments of the present invention, the second antenna segment 32 is movable between a first position 35 and a second position 36 relative to the first antenna segment 31, when the second antenna segment 32 is located at the first position 35 relative to the first antenna segment 31, the axis of the first antenna segment 31 and the axis of the second antenna segment 32 are located on the same straight line, and when the second antenna segment 32 is located at the second position 36 relative to the first antenna segment 31, the axis of the first antenna segment 31 and the axis of the second antenna segment 32 are perpendicular, that is, can rotate approximately 0 ° to 90 °, so as to adjust the direction of the antenna and enhance the signal.
The utility model discloses an among some embodiments, the grafting module includes UART grafting module and SIM card grafting module, and UART grafting module can be respectively with aircraft and communication module communication connection, and SIM card grafting module can install or dismantle the SIM card. In specific implementation, the aircraft is connected to the communication module 20 through a power data line, when the SIM card plug-in module is plugged into the SIM, the aircraft is connected to the communication module by using the UART plug-in module, and the UART plug-in module can control the voltage to be 5V. The communication module 20 receives the mobile communication signal, utilizes the mobile communication technology to enable the aircraft to communicate with the ground station in real time, and enables the self state information and other data of the aircraft to interact with the ground station in real time, so that the ground station can monitor the state of the aircraft and the control of the ground station on the aircraft at an ultra-long distance, and the aircraft can complete flight tasks and flight safety.
It should be noted that when the SIM card is removed from the SIM card plug-in module, the communication device may lose its communication capability immediately.
Optionally, the plug-in module further comprises: and the Ethernet plug-in module is used for connecting the Ethernet equipment externally connected with the aircraft with the communication module 20. That is to say, the ethernet plug-in module can satisfy the communication access of the ethernet device externally connected to the aircraft, and the ethernet device is connected to the communication module 20 through the ethernet plug-in module, so as to ensure that the ethernet device and the flight control data exchange data with the ground station through the communication device.
By adopting the Ethernet plug-in module, the problem of large-capacity data stream transmission is solved, the data transmission speed can be accelerated, and different flight requirements and different environmental conditions can be adapted. For example, the ethernet device is a video image acquisition unit, the large-capacity data is video image data, the video image acquisition unit is connected to the ethernet plug-in module on the communication module, so that data exchange between the video image data and the ground station through the communication module 20 can be realized, the video image data is displayed on the video image playing device connected to the ground station, and the ground can monitor the video image shot by the aircraft.
According to the utility model discloses an embodiment, aircraft communication device based on mobile communication technique still includes USB host grafting module, and USB host grafting module can carry out firmware upgrading to communication module 20.
in some embodiments of the present invention, communication module 20 is further provided with a reset key (not shown in the figure), which facilitates the factory reset of the aircraft communication device.
According to an embodiment of the present invention, the communication module 20 may be a PCBA board.
It should be noted that the antenna patch module may be formed as a jack provided on the PCBA board.
According to the present invention, a containing groove (not shown) can be disposed on the aircraft for placing the aircraft communication device 100 based on the mobile communication technology, and the aircraft communication device 100 based on the mobile communication technology can be fixed on the aircraft by the fixing device (not shown).
It should be noted that, the mobile communication technology in the embodiment of the present invention may be a fourth generation mobile communication technology, the SIM card may be a SIM card for receiving 4G signals, and the mobile communication technology is not limited to the 4G communication technology, and is also applicable to the mobile communication technology updated later, and only needs to update the corresponding firmware/software.
The following describes in detail the assembly process and assembly features of the aircraft communication device 100 based on mobile communication technology according to an embodiment of the present invention.
First, the lower cover 14, the communication module 20 and the housing 13 are put in place from bottom to top, and the positions of the counter bore 15 on the lower cover 14, the mounting hole 21 on the communication module 20 and the positioning hole (not shown in the figure) on the housing 13 correspond, at which time the positioning part 50 is arranged opposite to the communication module 20; then, one end of the connecting piece sequentially extends into the counter bore 13, the mounting hole 21 and the positioning hole to be detachably connected, the lower cover 14, the communication module 20 and the shell 13 are locked, and at the moment, the upper end of the positioning part 50 is abutted against at least one part of the lower end face of the communication module 20, so that the communication module 20 is positioned; finally, the second segment 34 is detachably connected with the first segment 33, and the first segment is detachably connected with the antenna plug-in module of the communication module 20 through the through hole 11, so that the whole aircraft communication device 100 based on the mobile communication technology is assembled.
When the work, the storage and the transportation are needed, the second antenna section 32 can be made to be movable between a first position 35 and a second position 36 relative to the first antenna section 31, and when the second antenna section 32 is located at the first position 35 relative to the first antenna section 31, the axis of the first antenna section 31 and the axis of the second antenna section 32 are located on the same straight line, and the normal work can be carried out; when the second antenna segment 32 is located at the second position 36 relative to the first antenna segment 31, the axis of the first antenna segment 31 is perpendicular to the axis of the second antenna segment 32, and the second antenna segment 32 can be stored at the side of the box body 10, so that the communication antenna 30 is prevented from occupying too large space during storage and transportation, and risks such as article buckling are reduced.
In summary, according to the utility model discloses an aircraft communication device 100 based on mobile communication technology adopts the device that box body 10, communication module 20 and communication antenna 30 combined together, not only can realize being convenient for install and dismantle, still has the advantage such as be convenient for accomodate and transport, the outward appearance is pleasing to the eye.
according to the utility model discloses the aircraft includes the aircraft communication device 100 based on mobile communication technology according to above-mentioned embodiment, because according to the utility model discloses aircraft communication device 100 based on mobile communication technology of above-mentioned embodiment has above-mentioned technological effect, consequently, according to the utility model discloses the aircraft of embodiment also has corresponding technological effect, is not only convenient for installation and dismantlement promptly, and the appearance is pleasing to the eye moreover.
In the description herein, references to the description of the term "one embodiment," "some embodiments," "an illustrative embodiment," "an example," "a specific example," or "some examples" or the like 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 present invention. In this specification, the schematic representations of the terms used above do not necessarily 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.
While embodiments of the present invention have been shown and described, it will be understood by those of ordinary skill in the art that: various changes, modifications, substitutions and alterations can be made to the embodiments without departing from the principles and spirit of the invention, the scope of which is defined by the claims and their equivalents.
Claims (16)
1. An aircraft communication device based on mobile communication technology, comprising:
The box body is internally limited with an accommodating cavity and is provided with a through hole and a plurality of jacks communicated with the accommodating cavity;
The communication module is arranged in the accommodating cavity and can receive mobile communication signals, and is provided with an antenna plug-in module corresponding to the through hole and a plug-in module corresponding to the socket;
The communication antenna comprises a first antenna segment and a second antenna segment, one end of the first antenna segment penetrates through the through hole and is detachably connected with the antenna plug-in module, and one end of the second antenna segment is pivotally connected with the other end of the first antenna segment.
2. The mobile communication technology-based aircraft communication device according to claim 1, wherein the cartridge comprises:
The shell is formed into a box shape with one open end, the through hole is formed in the shell along the thickness direction of one side wall of the shell, and the socket is formed in the shell along the thickness direction of the other side wall of the shell;
A bottom cover removably connected to the housing and cooperating with the housing to define the receiving cavity.
3. The mobile communication technology-based aircraft communication device according to claim 2, wherein the communication module is provided with a mounting hole penetrating in a thickness direction thereof, the bottom cover is provided with a counter-bore corresponding to the mounting hole in the thickness direction thereof, and the mobile communication technology-based aircraft communication device further comprises:
and one end of the connecting piece sequentially penetrates through the counter bore and the mounting hole and then is detachably connected with the shell.
4. Aircraft communication device based on mobile communication technology according to claim 3, characterized in that the connection is formed as a screw or a bolt.
5. The mobile communication technology-based aircraft communication device according to claim 3, further comprising:
The flexible piece, flexible piece detachably locates the counter sink and with the other end of connecting piece ends.
6. The mobile communication technology-based aircraft communication device according to claim 2, further comprising:
The positioning part is arranged on one side of the bottom cover facing to the direction of the shell, the positioning part is formed into a plurality of bulges protruding towards the direction of the shell, and the bulges are stopped against the communication module to fix the communication module.
7. The mobile communication technology-based aircraft communication device according to claim 1, wherein the first antenna segment comprises:
One end of the first segment body is formed into a contact part, the contact part penetrates through the through hole to be detachably connected with the antenna plug-in module, and the contact part is in threaded connection with the through hole;
and one end of the second section body is detachably connected with the other end of the first section body, and the other end of the second section body is pivotally connected with one end of the second antenna section.
8. the mobile communication technology-based aircraft communication device according to claim 7, wherein the first segment is screwed to the second segment.
9. a mobile communications technology-based aircraft communication device according to any one of claims 1 to 8, wherein the second antenna segment is movable relative to the first antenna segment between a first position and a second position, the axis of the first antenna segment and the axis of the second antenna segment being collinear when the second antenna segment is in the first position relative to the first antenna segment, the axis of the first antenna segment and the axis of the second antenna segment being perpendicular when the second antenna segment is in the second position relative to the first antenna segment.
10. An aircraft communication device based on mobile communication technology according to any one of claims 1 to 8, characterised in that the plug-in module comprises:
the UART plug-in module can be respectively in communication connection with the aircraft and the communication module;
And the SIM card inserting module is used for installing or detaching the SIM card.
11. The mobile communication technology-based aircraft communication device according to claim 10, wherein the plug-in module further comprises:
And the Ethernet plug-in module is used for connecting the Ethernet equipment externally connected with the aircraft with the communication module.
12. A mobile communication technology-based aircraft communication device according to any one of claims 1-8, further comprising:
And the USB host plug-in module can be used for upgrading the firmware of the communication module.
13. A mobile communications technology based aircraft communication device according to any of claims 1 to 8, wherein the communication module is a PCBA board.
14. The aircraft communication device based on mobile communication technology as claimed in claim 1, wherein the aircraft is provided with a containing slot for placing the aircraft communication device, and the aircraft communication device is fixed on the aircraft by the fixing device.
15. the aircraft communication device based on mobile communication technology of claim 1, wherein the communication module is further provided with a reset key for restoring factory settings of the aircraft communication device.
16. An aircraft, characterized in that it comprises a mobile communication technology based aircraft communication device according to any of claims 1-15.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920729998.7U CN209767536U (en) | 2019-05-21 | 2019-05-21 | Aircraft communication device based on mobile communication technology and aircraft with same |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920729998.7U CN209767536U (en) | 2019-05-21 | 2019-05-21 | Aircraft communication device based on mobile communication technology and aircraft with same |
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| CN209767536U true CN209767536U (en) | 2019-12-10 |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111584996A (en) * | 2020-06-09 | 2020-08-25 | 哈尔滨农撷科技有限公司 | 5G antenna and preparation process thereof |
| WO2023077677A1 (en) * | 2021-11-05 | 2023-05-11 | 深圳市大疆创新科技有限公司 | Communication device, platform system, electrical connection assembly, and connection unit |
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2019
- 2019-05-21 CN CN201920729998.7U patent/CN209767536U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111584996A (en) * | 2020-06-09 | 2020-08-25 | 哈尔滨农撷科技有限公司 | 5G antenna and preparation process thereof |
| CN111584996B (en) * | 2020-06-09 | 2021-04-16 | 南京华脉科技股份有限公司 | 5G antenna and preparation process thereof |
| WO2023077677A1 (en) * | 2021-11-05 | 2023-05-11 | 深圳市大疆创新科技有限公司 | Communication device, platform system, electrical connection assembly, and connection unit |
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