TWM610574U - Ground platform for flight vehicle - Google Patents

Abstract

A ground platform matched with a flying vehicle is suitable for connecting a plurality of wires, and includes a base, an actuating platform arranged on the base, and a sensing unit. The actuating platform includes a body capable of rotating with a longitudinally extending axis of rotation relative to the base, and a plurality of connecting parts arranged on the body and suitable for inserting the wires. The sensing unit includes a first sensor suitable for being arranged on the flight vehicle, a second sensor arranged on the actuation platform and connected to the first sensor, and at least one information Connected to one of the first sensor and the second sensor, and used to control the operating platform according to a difference signal of the direction information sensed by the first sensor and the second sensor The main body rotates with respect to the controller of the base.

Description

Ground platform for flying vehicles

The new model relates to an auxiliary flight vehicle equipment, in particular to a ground platform matched with the flight vehicle.

In addition to the purpose of carrying people, flying vehicles, such as inflatable spacecraft, helium balloons, etc., which are easy to be positioned at specific positions in the air for a long time, are often raised to a certain height after connecting wires to provide communication base stations and fixed points. Lighting, advertising and other functions.

However, even if this kind of flying vehicle is relatively conducive to floating at a specific position in the air, it is still difficult to guarantee that there is a small range of movement due to the indeterminate airflow in the air, or it rotates on a vertical axis. At this time, if it is on the flying vehicle Wires such as cables for lighting, communication wires, and even fixing ropes for positioning are connected, and many different wires may be entangled with each other. When the wires are entangled with each other, it may affect the subsequent rewinding and cause damage to the wire, or may fall off from the connector, and then shake in a large area near the ground, causing danger to the surroundings. It is necessary to propose a corresponding improvement plan.

Therefore, the purpose of the present invention is to provide a ground platform for a matching flying vehicle that ensures that the wires connected to the flying vehicle will not be entangled with each other.

Therefore, the ground platform of the present invention is suitable for connecting multiple wires with one end for connecting to the flying vehicle, and includes a base suitable for positioning on the ground and an actuator set on the base. Station, and a sensor control unit.

The actuating platform includes a body capable of rotating with a longitudinally extending axis of rotation relative to the base, and a plurality of connecting parts arranged on the body and suitable for inserting the wires.

The sensing unit includes a first sensor suitable for being arranged on the flight vehicle, a second sensor arranged on the actuation platform and connected to the first sensor, and at least one information Connected to one of the first sensor and the second sensor, and used to control the operating platform according to a difference signal of the direction information sensed by the first sensor and the second sensor The main body rotates with respect to the controller of the base.

The effect of the present invention is that when the vehicle flying in the air has a deflection or rotation, the mutual comparison of the direction information of the first sensor and the second sensor can generate a correlation between the two directions. The difference signal of the difference, through the rotation of the body of the actuating table, can maintain the arrangement rules between the wires in response to the difference in direction, thereby avoiding the wires from being entangled with each other.

Refer to FIG. 1, which is an embodiment of a ground platform for a new type of flying vehicle. It is suitable for connecting a plurality of wires 92 with one end for connecting to the flying vehicle 91, and includes a base 1 suitable for positioning on the ground. , An actuating platform 2 arranged on the base 1, a sensor unit 3, and an information link to the operation interface 4 of the sensor unit 3. In this embodiment, three wires 92 are connected between the flying vehicle 91 and this embodiment. The flying vehicle 91 is an inflatable airship, but the connected wires 92 are The number, specific type, and form of the flight vehicle 91 are not limited to this.

Referring to FIGS. 1 and 2, the base 1 specifically needs to be stably fixed on the ground and sufficient to cope with the slight shaking that may occur after connecting the wires 92. The actuating platform 2 includes a main body 21 that can rotate relative to the base 1 with a longitudinally extending axis of rotation, and three connecting portions 22 arranged on the main body 21 and suitable for inserting the wires 92 respectively. Wherein, the main body 21 is preferably pivotally connected to the base 1 by a longitudinally extending pivot 19 so as to achieve the purpose of rotating relative to the base 1. In order to wait for the different types and quantities of the wires 92, the connecting parts 22 are in response to the connection needs. In addition to the number corresponding to the number of the wires 92 used, the shapes are such as wire sockets, network cable holes, and even It is the buckle of the fixed rope, which is possible to implement. In addition, the base 1 is not only firmly installed on the ground, but also can be integrated on a large movable carrier such as a truck and a trailer to increase application flexibility.

The sensing unit 3 includes a first sensor 31 suitable for being arranged on the flight vehicle 91, and a second sensor arranged on the actuation platform 2 and connected to the first sensor 31 for information 32, and at least one piece of information is connected to one of the first sensor 31 and the second sensor 32, and is used according to the direction information sensed by the first sensor 31 and the second sensor 32 A difference signal of the controller 33 controls the rotation of the main body 21 of the actuation table 2 relative to the base 1. Wherein, the first sensor 31 and the second sensor 32 are both selected from a compass, a global positioning system (GPS, Global Positioning System), or a satellite navigation system (GNSS, Global Navigation Satellite System). In addition, since the controller 33 mainly determines whether the direction between the flying vehicle 91 and the base 1 is based on the difference in direction sensing information between the first sensor 31 and the second sensor 32 There are deviations, so whether it is connected to the first sensor 31 or the second sensor 32, basically the same function can be achieved, so it can be freely selected according to the configuration environment or the convenience of implementation.

The operating interface 4 is connected to the sensing control unit 3 by a wireless connection mechanism, and can directly control the rotation of the main body 21 of the actuation table 2 relative to the base 1, thereby forming compensation for the automatic operation of the sensing control unit 3 Mechanism, or it can be directly controlled manually in response to a temporary emergency.

Referring to FIGS. 3 and 4 at the same time, when the flying vehicle 91 actually carries the required equipment and connects the three wires 92 to fly up, if the airflow or other factors turn slightly, the first sensor 31 will sense If the direction information of the flying vehicle 91 is deflected, it will be different from the direction information of the actuator 2 sensed by the second sensor 32 to generate a difference signal 300. At this time, the controller 33 receives the difference signal 300, and in order to maintain the directional information between the flight vehicle 91 and the actuation platform 2 in the initial state after flying, it controls the main body 21 of the actuation platform 2 to be relative to each other. When the base 1 rotates, after the main body 21 rotates, the relative position of the flying vehicle 91 and the actuating platform 2 will be maintained at the initial state of just ascending, that is, when the wires 92 are properly arranged, so It is indeed possible to prevent the wires 92 from being entangled with each other during the flight of the flight vehicle 91.

To sum up, in this embodiment of the ground platform of the present invention with a flying vehicle, as long as the flying vehicle 91 is deflected relative to the actuating platform 2, the difference in direction information can be sensed by the sensing unit 3 Accordingly, the main body 21 of the actuating platform 2 is controlled to rotate relative to the base 1, so that the relative positions of the wires 92 in a proper arrangement are maintained between the flying vehicle 91 and the actuating platform 2, so as to avoid the wires 92 92 entangled with each other. Therefore, it can indeed achieve the purpose of cost-new type.

However, the above are only examples of the present model, and should not be used to limit the scope of implementation of the present model, all simple equivalent changes and modifications made in accordance with the patent scope of the present model application and the contents of the patent specification still belong to This new patent covers the scope.

1: pedestal 19: pivot 2: Acting table 21: body 22: Connection part 3: Sensing control unit 300: Difference signal 31: The first sensor 32: second sensor 33: Controller 4: Operation interface 91: Flight Vehicle 92: Wire

The other features and effects of the present invention will be clearly presented in the embodiments with reference to the drawings, among which: Figure 1 is a schematic diagram illustrating an embodiment of the ground platform of the present invention with a flying vehicle; Figure 2 is a top view illustrating a base and an actuating table of the embodiment; Figure 3 is a block diagram illustrating a sensing unit of the embodiment and the operation of the sensing unit; and Fig. 4 is a schematic diagram, which, in conjunction with Fig. 3, illustrates the effect of this embodiment in avoiding entanglement of multiple connected wires.

1: pedestal

19: pivot

2: Acting table

21: body

22: Connection part

3: Sensing control unit

31: The first sensor

32: second sensor

33: Controller

4: Operation interface

91: Flight Vehicle

92: Wire

Claims (4)

A ground platform matched with a flying vehicle, suitable for connecting multiple wires with one end for connecting to the flying vehicle, and includes: A base, suitable for positioning on the ground; An actuating table is set on the base, and includes a body capable of rotating relative to the base with a longitudinally extending axis of rotation, and a plurality of connections provided on the body and suitable for plugging the wires Department; and A sensing unit, including a first sensor suitable for being arranged on the flight vehicle, a second sensor arranged on the actuation platform and connected to the first sensor, and at least one The information is connected to one of the first sensor and the second sensor, and is used to control the actuator according to a difference signal of the direction information sensed by the first sensor and the second sensor The main body rotates relative to the base controller. As described in claim 1, the ground platform matched with the flying vehicle further includes a control interface connected to the sensing control unit to directly control the rotation of the body of the actuation platform relative to the base. The ground platform matched with a flying vehicle according to claim 2, wherein the control interface and the sensing control unit are wirelessly connected. The ground platform matched with a flying vehicle according to any one of claims 1 to 3, wherein the first sensor and the second sensor of the sensing and control unit are both selected from a compass and a global positioning system , Or satellite navigation system.

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