Tethered airship for monitoring
Technical Field
The utility model relates to the field of suspension balloons, in particular to the technical field of tethered airship, and specifically relates to a tethered airship for monitoring.
Background
The conventional tethered airship consists of an anchored, a floating airship, a tethered system, a communication system and a photoelectric monitoring system, and can carry various task loads and can be deployed in 2 hours at maximum due to the modular design of the system. However, if the strength of the connection between the anchoring vehicle and the capsule is insufficient, the connection may break when strong wind or other external forces are encountered, resulting in the airship being out of control or falling off directly from the mooring device, which may pose a serious threat to the safety of the airship and may cause the airship to be damaged or lost.
On the basis of causing task interruption, the completion effect of the task is affected, and potential safety hazards can be formed to ground personnel and equipment.
Disclosure of Invention
In view of the above-mentioned drawbacks of the prior art, an object of the present utility model is to provide a tethered airship for monitoring, which is used to solve the difficulties of the prior art.
To achieve the above and other related objects, the present utility model provides a tethered airship for monitoring, comprising:
A anchoring vehicle 1, the anchoring vehicle 1 being provided on the ground and loaded with a mooring structure to which a mooring unit is mounted;
The airship 2 is arranged above the anchoring vehicle 1, and the airship 2 is also integrally provided with an equipment carrying unit;
the mooring car 1 and the airship 2 are connected by mooring rope units.
According to a preferred aspect, the mooring structure comprises:
a mooring tower 3, wherein the mooring tower 3 is arranged at the highest position of the anchoring vehicle 1;
The mooring box bodies 4 are provided with a pair of mooring box bodies 4 which are symmetrically arranged at two sides of the trailer position of the anchoring parking 1 respectively;
And the semi-hanging support legs 5 are erected below the front end and the rear end of the mooring box body 4, and the mooring box body 4 is supported and arranged on the ground.
According to the preferred scheme, embedded mounting grooves are formed below the front end and the rear end of the mooring box body 4 and correspond to the semi-hanging support legs 5.
According to a preferred aspect, the mooring cable unit comprises:
a connecting steel 6, said connecting steel 6 being horizontally disposed between a pair of said tethered boxes 4;
A cable 7, wherein one end of the cable 7 is connected to the bottom of the airship 2, and the other end of the cable 7 is connected to the connecting steel 6;
the hanging frame 8 is vertically arranged on the connecting steel 6, and a hook for connecting a hanging rope 9 at the bottom of the airship 2 is arranged at the top of the hanging frame 8.
According to a preferred embodiment, through holes for the connecting cables 7 are preset in the connecting steel 6.
According to a preferred embodiment, the hanger 8 is mounted on the end of the connecting steel 6 remote from the head of the anchor parking 1, and the fore-and-aft distance can be adjusted according to the position of the airship 2.
According to a preferred embodiment, the cables 7 are arranged in a plurality along the nose to tail of the airship 2.
According to a preferred aspect, the device-mounting unit includes:
A nacelle 10 mounted on the lower bottom of the airship 2, the connection to the bottom plate being made by peripherally arranged steel brackets 11;
A mission cabin 12, wherein the mission cabin 12 is installed between the nacelle 10 and the tail wing of the airship 2, and a cavity for accommodating equipment required by a corresponding mission is formed inside the mission cabin.
According to a preferred scheme, each hanging steel bracket 11 is provided with two groups of hanging steels, the tops of the two groups of hanging steels are overlapped, and the bottoms of the two groups of hanging steels are separated.
According to a preferred embodiment, the pod 10 is an optoelectronic pod.
According to a preferred solution, the bottom of the airship 2 is also detachably equipped with a gas valve 13 and a safety valve 14, and the top of the nacelle 10 is connected below the gas valve 13 and the safety valve 14.
The utility model achieves the effect of stabilizing the airship by connecting the anchoring and parking device and the airship through the mooring rope unit, and in addition, the air valve and the safety valve are arranged at the bottom of the airship to provide stable buoyancy for the airship, ensure safety and provide stable support for the equipment carrying unit, improve the adaptability of the mooring airship to the environment and be widely applied to emergency events.
Preferred embodiments for carrying out the present utility model will be described in more detail below with reference to the attached drawings so that the features and advantages of the present utility model can be easily understood.
Drawings
FIG. 1 is a schematic perspective view of the present utility model;
FIG. 2 is an enlarged schematic view showing a three-dimensional structure of the anchoring parking according to the present utility model;
FIG. 3 is an enlarged schematic view showing a three-dimensional structure of the airship according to the utility model;
Description of the reference numerals
1. Anchoring and parking, 2, an airship, 3, a mooring tower, 4, a mooring box body, 5, semi-hanging support legs, 6, connecting steel, 7, and a cable;
8. The device comprises a hanging frame, 9 hanging ropes, 10 hanging cabins, 11 hanging steel brackets, 12 task cabins, 13 air valves, 14 safety valves.
Detailed Description
In order to make the objects, technical solutions and advantages of the technical solutions of the present utility model more clear, the technical solutions of the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings of specific embodiments of the present utility model. Like reference numerals in the drawings denote like parts. It should be noted that the described embodiments are some, but not all embodiments of the present utility model. All other embodiments, which can be made by a person skilled in the art without creative efforts, based on the described embodiments of the present utility model fall within the protection scope of the present utility model.
Possible embodiments within the scope of the utility model may have fewer components, have other components not shown in the drawings, different components, differently arranged components or differently connected components, etc. than the examples shown in the drawings. Furthermore, two or more of the elements in the figures may be implemented in a single element or a single element shown in the figures may be implemented as multiple separate elements.
Unless defined otherwise, technical or scientific terms used herein should be given the ordinary meaning as understood by one of ordinary skill in the art to which this utility model belongs. The terms "first," "second," and the like in the description and in the claims, are not used for any order, quantity, or importance, but are used for distinguishing between different elements. Likewise, the terms "a" or "an" and the like do not necessarily denote a limitation of quantity. The word "comprising" or "comprises", and the like, means that elements or items preceding the word are included in the element or item listed after the word and equivalents thereof, but does not exclude other elements or items. The terms "connected" or "connected," and the like, are not limited to physical or mechanical connections, but may include electrical connections, whether direct or indirect. "upper", "lower", "left", "right", etc. are used merely to indicate relative positional relationships, which may also be changed when the absolute position of the object to be described is changed.
The utility model provides a tethered airship for monitoring, which is used for structural design of the tethered airship, and the tethered airship is not limited by the types of a base station, a patrol car, a satellite and the like, but is particularly suitable for emergency rescue, anti-terrorism monitoring, communication interruption, meteorological monitoring and the like.
In general, the tethered airship for monitoring provided by the utility model mainly comprises a anchoring vehicle 1, an airship 2 and a mooring rope unit. Therein, reference may be made to fig. 1, which shows the arrangement of a mooring car 1, an airship 2, a mooring line unit.
In order to achieve the purpose of stabilizing the airship connection structure, the device solves the problems that in the background art, a conventional tethered airship consists of an anchored parking system, a floating airship, a tethered system, a communication system and a photoelectric monitoring system, and due to the modularized design of the system, various task loads can be carried, and the device can be deployed in 2 hours at the highest speed. However, if the connection strength between the anchoring vehicle and the capsule is insufficient, the connection part may be broken when strong wind or other external forces are encountered, so that the airship is out of control or directly falls off from the mooring device, which may cause serious threat to the safety of the airship and damage or loss of the airship, and on the basis of causing task interruption, the completion effect of the task is affected, and potential safety hazards to ground personnel and equipment may be formed.
As shown in fig. 1, the anchoring vehicle 1 is disposed on the ground, the anchoring vehicle 1 is loaded with a mooring structure with a mooring unit, the airship 2 is disposed above the anchoring vehicle 1, and an equipment loading unit is integrally mounted, in this embodiment, in order to achieve structural stability between the two, the two are fastened by the mooring cable unit before the airship 2 is not flown.
As described above, the mooring structure includes a pair of mooring boxes 4 symmetrically installed at the trailer position of the anchoring vehicle 1, on both sides of the trailer, respectively, a space for accommodating installation equipment is formed inside, and the mooring tower 3 is disposed at the highest position of the anchoring vehicle 1, in order to ensure that the mooring boxes 4 and the mooring tower 3 on the trailer of the anchoring vehicle 1 are not affected to move or the like uncontrollably when the airship 2 works after the anchoring vehicle 1 is stably stopped, semi-hanging legs 5 are installed under the front and rear ends of the mooring boxes 4, the mooring boxes 4 are supported on the ground by the semi-hanging legs 5, and when the semi-hanging legs 6 are not needed, the hanging legs 6 are retracted under the action of hydraulic pressure or air cylinders, and in addition, embedded installation grooves are provided under the front and rear ends of the mooring boxes 4 corresponding to the semi-hanging legs 5, so that the influence on the mooring boxes 4 is not increased.
The mooring rope unit has the connection function between the corresponding mooring structure and the airship 2, on one hand, a connecting steel 6 is horizontally arranged between a pair of mooring boxes 4, through holes for ropes 7 used for being connected with the airship 2 are preset in the connecting steel 6, one end of each rope 7 is connected to the bottom of the airship 2, the other end of each rope 7 is connected to the connecting steel 6 when the airship 2 is in use, and the airship 2 is enabled to be stably connected with the airship 2 due to the fact that the structure of the airship 2 is large, and a plurality of ropes 7 are arranged along the head to the tail of the airship 2;
on the other hand, the hanger 8 is arranged at one end of the connecting steel 6 far away from the head of the anchor parking 1, the hanger 8 is vertically arranged, and as the top of the hanger 8 is provided with a hook for connecting the hanging rope 9 at the bottom of the airship 2, the hanger 8 can adjust the front and back distance in the connecting steel 6 according to the position of the airship 2 during use so as to adapt to the requirements of different airship 2 structures.
On the basis, an equipment carrying unit is also arranged below the airship 2, a nacelle 10 is arranged at the bottom of the airship 2, a connection to a bottom plate is formed through surrounding steel hanging brackets 11, the nacelle 10 is used for carrying auxiliary equipment and systems required by the airship, such as a power supply system, a communication system, a control system and the like, each steel hanging bracket 11 is provided with two groups of hanging steels, the tops of the two groups of hanging steels coincide, the bottoms are separated to ensure that the equipment and the systems can be stably carried in the flying process, a task cabin 12 is arranged between the nacelle 10 and a tail wing of the airship 2, a cavity for accommodating equipment required by corresponding tasks is formed inside, and various task modules such as emergency signal coverage, ocean wide area monitoring, urban safety maintenance monitoring, forest fire prevention monitoring, emergency lighting, signal interruption and the like can be quickly adapted.
Preferably, the pod 10 adopts a photoelectric pod, and the photoelectric pod integrates multiple functions of target detection, identification, tracking and the like, so that the photoelectric pod is more suitable for emergency scenes.
As shown in fig. 1, the bottom of the airship 2 is also detachably provided with an air valve 13 and a safety valve 14, and the top of the nacelle 10 is connected below the air valve 13 and the safety valve 14, which is beneficial to further improving the stability of the airship 2 and is suitable for more scenes.
The above embodiments are merely illustrative of the principles of the present utility model and its effectiveness, and are not intended to limit the utility model. Modifications and variations may be made to the above-described embodiments by those skilled in the art without departing from the spirit and scope of the utility model. Accordingly, it is intended that all equivalent modifications and variations of the utility model be covered by the claims, which are within the ordinary skill of the art, be within the spirit and scope of the present disclosure.