CN217719931U - Small multi-link measurement and control station for medium and long distance unmanned aerial vehicle - Google Patents
Small multi-link measurement and control station for medium and long distance unmanned aerial vehicle Download PDFInfo
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- CN217719931U CN217719931U CN202221964724.4U CN202221964724U CN217719931U CN 217719931 U CN217719931 U CN 217719931U CN 202221964724 U CN202221964724 U CN 202221964724U CN 217719931 U CN217719931 U CN 217719931U
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Abstract
The utility model discloses a small multi-link measurement and control station of a medium-long distance unmanned aerial vehicle, belonging to the technical field of communication measurement and control; the measurement and control station comprises a shelter body, a push rod type lifting mechanism, an antenna seat, a directional antenna combination, an operation box, a working cabin door, a power distribution cabinet, a folding type boarding ladder, an omnidirectional antenna, a link equipment cabinet and the like. The utility model discloses a methods such as scientific planning, rational arrangement make limited space obtain the utilization of maximum efficiency, both installed multilink equipment, accord with small-size shelter installation national standard requirement again, realized that well long-range unmanned aerial vehicle multilink observes and controls the miniaturization of station.
Description
Technical Field
The utility model relates to communication observes and controls technical field, in particular to station is observed and controled to the small-size multilink of well long-range unmanned aerial vehicle.
Background
In the field of communication measurement and control, antennas capable of forming high gain and scanning beams mainly have the following structural forms, and have certain defects in performance although having various characteristics.
Along with the development of the technology, the application field of the unmanned aerial vehicle is more and more extensive, and meanwhile, the requirement on the measurement and control technology of the unmanned aerial vehicle is higher and higher, and medium-long distance, multilink, miniaturization and the like become development trends. At present, miniaturization of a multi-link measurement and control station of a medium-long distance unmanned aerial vehicle is rarely achieved. Because the flight distance of the medium-long distance unmanned aerial vehicle is long, long-distance measurement and control can be realized only by adopting a high-gain directional antenna. Directional antennas must rely on antenna mounts with self-tracking and tend to be bulky. Furthermore, multiple links require multiple devices, requiring more space, which is in conflict with miniaturization.
SUMMERY OF THE UTILITY MODEL
To the problem that exists among the above-mentioned background art, the utility model provides a station is observed and controled to the small-size multilink of well long-range unmanned aerial vehicle. The measurement and control station can be used for installing a plurality of sets of link equipment and can meet the installation requirements of a small standard shelter.
In order to realize the purpose, the utility model discloses the technical scheme who takes does:
a small-size multilink of medium-long range unmanned aerial vehicle observes and controls station, includes:
the square cabin body is I-shaped, the left side wall and the right side wall are inwards concave and narrowed, and the exposed part of the square cabin bottom plate becomes a mounting platform for mounting the lifting mechanism, the antenna seat and the directional antenna combination; the cabin body of the shelter is divided into a front cabin and a rear cabin; the installation interface of the shelter body of the shelter adopts a standard CAF20 small-sized shelter mechanical interface
The push rod type lifting mechanisms are provided with two sets and are respectively arranged at the left and right outer side mounting platforms of the shelter body of the shelter; the lifting and unfolding of the utility model are outward under the working state; when the device is not in working state, the device descends to the inner side for collection;
an antenna pedestal: two sets of directional antenna assemblies are arranged and are respectively arranged at the tops of the left lifting mechanism and the right lifting mechanism; the antenna pedestal comprises a servo system, an azimuth mechanism and a pitching mechanism; the servo system can enable the antenna to automatically track the target; wherein, the rotation range of the azimuth mechanism is 0-360 degrees, the rotation range of the pitching mechanism is 0-180 degrees, and the combined rotation range of the azimuth and the pitching covers all airspaces.
Two sets of directional antenna combinations are arranged and respectively positioned on corresponding antenna bases, the lifting mechanism drives the lifting and the lowering, and the antenna bases drive the direction and the pitching; the two sets of directional antennas work independently without mutual influence;
two sets of operation boxes are arranged and respectively control the corresponding directional antenna combination and the lifting mechanism; the two operation boxes are respectively positioned on the outer wall surfaces of the left side and the right side;
the working cabin door is arranged on the front side of the shelter body of the shelter and is used for entering the front cabin;
the front cabin is provided with a link equipment cabinet, the link equipment cabinet is a standard 19-inch equipment cabinet, and the height of the link equipment cabinet is 20U; equipment including a transceiving combination, an intelligent distribution box, an industrial personal computer, a switch, a Beidou positioning and orienting instrument and an integrated display is arranged on a link equipment cabinet, and the equipment in the link equipment cabinet is a standard 19-inch plug box, so that the link equipment cabinet is convenient to disassemble and assemble; the equipment in the link equipment cabinet can complete the functions of remote control, remote measurement, tracking and real-time transmission and recording of video information of the remote unmanned aerial vehicle;
the power distribution cabinet is positioned in the rear cabin and used for supplying power to the transceiving combination; the outer walls of the two sides of the rear cabin are respectively provided with a power distribution cabinet operation door and a power distribution cabinet maintenance door which are used for operating and maintaining power distribution cabinet equipment;
the foldable boarding ladder is arranged on the back of the shelter body of the shelter; when being stored, the movable support can be tightly attached to the cabin wall, so that the space is not occupied, and people can climb the cabin top for use when needed;
the omnidirectional antenna is fixed at the top of the shelter body of the shelter through the lodging mechanism, the omnidirectional antenna is tightly attached to the top of the shelter body of the shelter in a collection state, and the omnidirectional antenna is perpendicular to the top of the shelter body of the shelter in a working state.
Furthermore, the installation interface adopts a standard CAF20 small-sized shelter mechanical interface and is installed at each angular position of the outer walls of the left side and the right side of the shelter body.
The utility model adopts the beneficial effect that above-mentioned technical scheme produced lies in:
1. the utility model discloses a methods such as scientific planning, rational arrangement make limited space obtain the utilization of maximum efficiency, both installed many sets of link equipment, accord with small-size shelter installation national standard requirement again, realized that well long-range unmanned aerial vehicle multilink observes and controls the miniaturization of station.
2. The operation box of the utility model can operate the lifting mechanism and the antenna without entering the cabin; the setting is reasonable, and the operation is convenient.
3. The utility model discloses the main part is the I-shaped cabin body, is equipped with the small-size shelter mechanical interface of CAF20 that accords with national standard, can install on the platform is carried to the standard. The device is mounted in a limited space, and the requirement on miniaturization is met.
Drawings
Fig. 1 is a schematic diagram of a partially expanded structure according to an embodiment of the present invention.
Fig. 2 is a schematic diagram of the angle rotation range of the fully extended antenna pedestal according to an embodiment of the present invention.
Fig. 3 is a partially expanded side schematic view of an embodiment of the invention.
Fig. 4 is a schematic front structural view of the embodiment of the present invention.
Fig. 5 is a schematic diagram of the angle rotation range of the partially unfolded antenna according to the embodiment of the present invention.
Fig. 6 is a first structural diagram of the embodiment of the present invention in a storage state.
Fig. 7 is a second structural schematic diagram of the embodiment of the present invention in the storage state.
In the figure: 1. the device comprises a directional antenna combination, 2 omni-directional antennas, 3 and 10 antenna bases, 4 and 9 lifting mechanisms, 5 signal transfer boxes, 6 and 8 operation boxes, 7 and 12 Beidou antennas, 13 overhead air conditioners, 14 power distribution cabinets, 15 link equipment cabinets, 16 power distribution cabinet doors, 17 folding type boarding ladders, 18 work cabin doors.
Detailed Description
The present invention will be further described with reference to the accompanying drawings and the detailed description.
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings of the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art that other drawings can be obtained according to these drawings without inventive labor.
A small-size multilink of long-range unmanned aerial vehicle observes and controls station in well, includes:
the square cabin body is I-shaped, the left side wall and the right side wall are inwards concave and narrowed, and the exposed part of the square cabin bottom plate becomes a mounting platform for mounting the lifting mechanism, the antenna seat and the directional antenna combination; the cabin body of the shelter is divided into a front cabin and a rear cabin; the installation interface of the shelter body of the shelter adopts a standard CAF20 small-sized shelter mechanical interface
The push rod type lifting mechanisms are provided with two sets and are respectively arranged at the left and right outer side mounting platforms of the shelter body of the shelter; the lifting and unfolding of the utility model are outward under the working state; in a non-working state, the collection is carried out by descending towards the inner side;
an antenna pedestal: two sets of directional antenna assemblies are arranged and are respectively arranged at the tops of the left lifting mechanism and the right lifting mechanism and used for mounting the directional antenna assemblies; the antenna pedestal comprises a servo system, an azimuth mechanism and a pitching mechanism; the servo system can enable the antenna to automatically track the target; wherein, the rotation range of the azimuth mechanism is 0-360 degrees, the rotation range of the pitching mechanism is 0-180 degrees, and the rotation range of the combination of azimuth and pitching covers all airspaces.
Two sets of directional antenna combinations are arranged, are respectively positioned on corresponding antenna bases, are driven to lift up and fall back by a lifting mechanism, and are driven to move in direction and pitch by the antenna bases; the two sets of directional antennas work independently without mutual influence;
two sets of operation boxes are arranged and respectively control the corresponding directional antenna combination and the lifting mechanism; the two operation boxes are respectively positioned on the outer wall surfaces of the left side and the right side;
the working cabin door is arranged on the front side of the shelter body of the shelter and is used for entering the front cabin;
the front cabin is provided with a link equipment cabinet, the link equipment cabinet is a standard 19-inch equipment cabinet, and the height of the link equipment cabinet is 20U; the equipment comprising a transceiving combination, an intelligent distribution box, an industrial personal computer, a switch, a Beidou positioning and orienting instrument and an integrated display is arranged on the link equipment cabinet, and the equipment in the link equipment cabinet is a standard 19-inch plug-in box, so that the link equipment cabinet is convenient to disassemble and assemble; the equipment in the link equipment cabinet can complete the functions of remote control, remote measurement, tracking and real-time transmission and recording of video information of the medium-long distance unmanned aerial vehicle;
the power distribution cabinet is positioned in the rear cabin and used for supplying power to the transceiving combination; the outer walls of the two sides of the rear cabin are respectively provided with a power distribution cabinet operation door and a power distribution cabinet maintenance door which are used for operating and maintaining power distribution cabinet equipment;
the folding boarding ladder is arranged on the back of the shelter body of the shelter; when being stored, the movable support can be tightly attached to the cabin wall, so that the space is not occupied, and people can climb the cabin top for use when needed;
the omnidirectional antenna is fixed at the top of the shelter body of the shelter through the lodging mechanism, the omnidirectional antenna is tightly attached to the top of the shelter body of the shelter in a collection state, and the omnidirectional antenna is perpendicular to the top of the shelter body of the shelter in a working state.
Furthermore, the installation interface adopts a standard CAF20 small-sized shelter mechanical interface and is arranged at each angular position of the outer walls of the left side and the right side of the shelter body.
The following is a more specific example:
referring to fig. 1 to 7, the shelter installation interface of the present embodiment adopts a standard CAF20 small-sized shelter mechanical interface, and the shelter body is i-shaped: the left side wall and the right side wall are narrowed inwards, and the exposed part of the shelter bottom plate becomes a mounting platform for mounting the lifting mechanism, the antenna pedestal and the directional antenna combination. The cabin body is divided into a front cabin and a rear cabin, so that the equipment can be mounted by fully utilizing the limited space, and the miniaturization requirement can be met;
the platform is equipped with the pusher-type lifting gear on both sides of cabin, its outside rises and expandes while working; when not in work, the utility model descends to the inner side for collection;
two sets of antenna bases are arranged at the top of the lifting mechanism and used for installing the directional antenna combination. The antenna mount includes a servo system, an azimuth mechanism, and a pitch mechanism. The servo system can make the antenna automatically track the target. The rotation range of the azimuth mechanism is 0-360 degrees, the rotation range of the pitching mechanism is 0-180 degrees, and the rotation range of the combination of azimuth and pitching can cover all airspaces.
Each set of antenna pedestal is provided with a directional antenna combination, and the lifting mechanism drives the jacking and the back-falling; the two sets of directional antennas work independently without mutual influence.
The two operation boxes are respectively positioned on the outer wall surfaces of the left side and the right side of the shelter, and are used for controlling the corresponding directional antenna combination and the lifting mechanism, so that the antenna lifting mechanism can be operated outside the shelter.
The working cabin door is arranged on the front side of the shelter body of the shelter and is used for entering the front cabin;
the front compartment houses a link equipment cabinet, which is a standard 19 inch equipment cabinet, height 20U. The cabinet is equipped with equipment such as receiving and dispatching combination, intelligent power distribution box, industrial computer, switch, big dipper location direction finder, integration display, and all equipment are 19 inch standard plug-in boxes on the cabinet, easy dismounting. The equipment in the cabinet can complete the functions of remote control, remote measurement, tracking and real-time transmission and recording of video information of the unmanned aerial vehicle;
the power distribution cabinet is positioned in the rear cabin, is provided with a UPS and a battery box and is used for supplying power to the equipment cabinet; for convenient operation, install intelligent power distribution box on front deck cabin equipment rack. The outer walls of the two sides of the rear cabin are respectively provided with a power distribution cabinet operation door and a power distribution cabinet maintenance door which are used for operating and maintaining power distribution cabinet equipment;
the back of the shelter is provided with a folding type climbing ladder which is normally tightly attached to the shelter wall for storage, and can be opened for people to climb the top of the shelter for use when in need.
The omnidirectional antenna is fixed at the top of the shelter body of the shelter through the lodging mechanism, the omnidirectional antenna is tightly attached to the top of the shelter body of the shelter in a collection state, and the omnidirectional antenna is vertical to the top of the shelter body of the shelter in a working state;
to sum up, the utility model discloses a small-size multilink observes and controls station can provide a plurality of communication link and has realized the miniaturization for long-range unmanned aerial vehicle in.
The appearance of the shelter of the measurement and control station adopts an original I-shaped structure, and the installation interface adopts a small shelter CAF20 mechanical interface which accords with the national standard. The limited space installation equipment is fully utilized, and the requirements of miniaturization and vehicle-carrying platform installation are met. Two independent push rod type lifting mechanisms, a high-gain directional antenna combination and an antenna seat are respectively arranged on the mounting platforms on the two sides outside the cabin body, the lifting mechanisms are lifted outwards when the lifting mechanisms are unfolded, and the lifting mechanisms are lowered inwards when the lifting mechanisms are stored. The antenna can rotate in 0-180 degrees in pitch and 0-360 degrees in azimuth after being unfolded, and the working range covers all airspaces. The two sets of lifting mechanisms and the antenna can work simultaneously and respectively and can also work independently without mutual influence. The cabin top is provided with a Beidou antenna, an overhead air conditioner, an omnidirectional antenna and a lodging mechanism, and the lodging mechanism can rotate by 0-90 degrees. The lodging mechanism is erected during working and is laid down during storage. The lifting/lodging mechanism operation boxes are arranged on the two sides outside the cabin door, so that the lifting mechanism and the antenna can be unfolded or collected without entering the cabin. And a link equipment cabinet and a power supply cabinet are arranged in the shelter. The front of the shelter is provided with a working cabin door, and the chain equipment cabinet can be operated by opening the working cabin door; the power cabinet is in the rear cabin, and switch board operation door and switch board maintenance door have been opened respectively to cabin body both sides wall rear portion, opens the door and can operate and maintain switch board equipment. The cabin top is provided with an omnidirectional antenna, a lodging mechanism, a Beidou antenna, an overhead air conditioner and other equipment. When the lifting mechanism is in work, the lifting mechanism is lifted through the lifting mechanism operation box, the antenna is unfolded, and the cabin door is opened to operate the link equipment. After the work is finished, the cabin door is closed, and the antenna is collected to the spaces on the two sides of the cabin body for transferring.
The present invention has been explained by using specific embodiments, and the explanation of the above embodiments is only used to help understand the method and the core idea of the present invention; meanwhile, for a person skilled in the art, according to the idea of the present invention, there may be changes in the specific embodiments and the application range, and in summary, the content of the present specification should not be construed as a limitation to the present invention.
Claims (2)
1. The utility model provides a small-size multilink of medium and long-range unmanned aerial vehicle observes and controls station which characterized in that includes:
the square cabin body is I-shaped, the left side wall and the right side wall are inwards concave and narrowed, and the exposed part of the square cabin bottom plate becomes a mounting platform for mounting the lifting mechanism, the antenna pedestal and the directional antenna combination; the cabin body of the shelter is divided into a front cabin and a rear cabin; the installation interface of the shelter body of the shelter adopts a standard CAF20 small shelter mechanical interface;
the push rod type lifting mechanisms are provided with two sets and are respectively arranged at the left and right outer side mounting platforms of the shelter body of the shelter; the lifting and unfolding of the utility model are outward under the working state; in a non-working state, the collection is carried out by descending towards the inner side;
an antenna pedestal: two sets of directional antenna assemblies are arranged and are respectively arranged at the tops of the left lifting mechanism and the right lifting mechanism; the antenna pedestal comprises a servo system, an azimuth mechanism and a pitching mechanism; the servo system is used for tracking the target; wherein, the rotation range of the azimuth mechanism is 0-360 degrees, the rotation range of the pitching mechanism is 0-180 degrees, and the rotation range of the combination of azimuth and pitching covers all airspaces;
two sets of directional antenna combinations are arranged, are respectively positioned on corresponding antenna bases, are driven to lift up and fall back by a lifting mechanism, and are driven to move in direction and pitch by the antenna bases; the two sets of directional antennas are combined to work independently and do not influence each other;
two sets of operation boxes are arranged and respectively control the corresponding directional antenna combination and the lifting mechanism; the two operation boxes are respectively positioned on the outer wall surfaces of the left side and the right side;
the working cabin door is arranged on the front side of the shelter body of the shelter and is used for entering the front cabin;
the front cabin is provided with a link equipment cabinet, the link equipment cabinet is a standard 19-inch equipment cabinet, and the height of the link equipment cabinet is 20U; the equipment comprising a transceiving combination, an intelligent distribution box, an industrial personal computer, a switch, a Beidou positioning and orienting instrument and an integrated display is arranged on the link equipment cabinet, and the equipment in the link equipment cabinet is a standard 19-inch plug-in box, so that the link equipment cabinet is convenient to disassemble and assemble; the equipment in the link equipment cabinet can complete the functions of remote control, remote measurement, tracking and real-time transmission and recording of video information of the remote unmanned aerial vehicle;
the power distribution cabinet is positioned in the rear cabin and used for supplying power to the transceiving combination; the outer walls of the two sides of the rear cabin are respectively provided with a power distribution cabinet operation door and a power distribution cabinet maintenance door for operating and maintaining power distribution cabinet equipment;
the folding boarding ladder is arranged on the back of the shelter body of the shelter; when in storage, the folding type cabin can be tightly attached to the cabin wall, so that the space is not occupied, and people can climb the cabin top for use when needed;
the omnidirectional antenna is fixed at the top of the shelter body of the shelter through the lodging mechanism, the omnidirectional antenna is tightly attached to the top of the shelter body of the shelter in a collection state, and the omnidirectional antenna is perpendicular to the top of the shelter body of the shelter in a working state.
2. The small-scale multilink measurement and control station of the medium-long-range unmanned aerial vehicle as claimed in claim 1, wherein the installation interface is a standard CAF20 small-scale shelter mechanical interface, and is installed at each angular position of the outer walls of the left and right sides of the shelter body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221964724.4U CN217719931U (en) | 2022-07-28 | 2022-07-28 | Small multi-link measurement and control station for medium and long distance unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221964724.4U CN217719931U (en) | 2022-07-28 | 2022-07-28 | Small multi-link measurement and control station for medium and long distance unmanned aerial vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN217719931U true CN217719931U (en) | 2022-11-01 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221964724.4U Active CN217719931U (en) | 2022-07-28 | 2022-07-28 | Small multi-link measurement and control station for medium and long distance unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217719931U (en) |
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2022
- 2022-07-28 CN CN202221964724.4U patent/CN217719931U/en active Active
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