Meteorological early warning machine

Abstract

The utility model discloses a meteorological early warning machine which comprises a machine shell assembly, a control assembly and a receiving assembly. The machine shell assembly comprises a machine body, a first shell and a second shell, the control assembly comprises a substrate and a plurality of connectors arranged on the substrate, and the connectors are communicated with the machine body for communication connection; the receiving assembly is arranged at the end, away from the connector, of the machine body and used for receiving weather information, the second shell is used for covering the control assembly, the first shell covers the second shell, and a broadcasting device is arranged on the substrate. According to the utility model, the connector is arranged in the machine body to realize communication connection, the receiving assembly receives control signals and broadcasts meteorological information in real time through the broadcaster, and meanwhile, the second shell covers the control assembly to protect the control assembly. The traditional mode that a listener turns on a television or switches a radio to a corresponding broadcast channel or frequency to obtain disaster information is replaced, the information obtaining efficiency is improved, and response time is provided for responding to changing weather.

Description

Technical Field

[0001] The utility model relates to the technical field of disaster reduction warning systems, and particularly relates to a meteorological warning aircraft. Background Art

[0002] Weather forecasting or meteorological forecasting is to predict the state of the earth's atmosphere at a certain location in the future using modern scientific and technological means. Since prehistoric times, humans have started to predict the weather to arrange their work and life accordingly (such as agricultural production, military operations, etc.). Today's weather forecasting mainly uses a large amount of data collection (temperature, humidity, wind direction and speed, air pressure, etc.), and then uses the understanding of atmospheric processes (meteorology) to determine future air changes.

[0003] Currently, in the face of severe meteorological disasters, disaster forecasting departments can use advanced technical means to predict the possible upcoming disaster information within a certain period of time. People mainly obtain meteorological information through television stations and traditional emergency radio systems. When public emergency information (such as meteorological disaster warning information) is released, listeners must turn on the TV or radio and switch to the corresponding radio channel or frequency to possibly receive relevant warning information.

[0004] However, it takes a certain amount of time for listeners to turn on the TV or radio and switch to the corresponding radio channel or frequency to obtain disaster information, which is likely to delay the best opportunity to handle emergencies and may cause certain losses. Content of the Utility Model

[0005] Based on this, the purpose of the utility model is to provide a meteorological warning aircraft, aiming to solve the problem that it takes a certain amount of time for listeners to turn on the TV or radio and switch to the corresponding radio channel or frequency to obtain disaster information, which is likely to delay the best opportunity to handle emergencies and may cause certain losses.

[0006] To achieve the above purpose, the utility model is realized through the following technical solutions: a meteorological warning aircraft, the meteorological warning aircraft includes:

[0007] A housing assembly, including a body, a first outer shell and a second outer shell provided on the body;

[0008] A control assembly, including a substrate and a plurality of connectors provided on the substrate, the connectors being connected to the body for communication connection;

[0009] A receiving assembly, provided at one end of the body away from the connectors for receiving meteorological information;

[0010] Wherein, the second outer shell is used to cover the control assembly, the first outer shell covers the second outer shell, and a broadcaster is further provided on the substrate.

[0011] In summary, a weather warning aircraft proposed according to the present utility model realizes communication connection by providing connectors inside the aircraft body, and then receives control signals through a receiving component and broadcasts weather information in real time through a broadcaster. At the same time, a second outer shell is used to cover the control component to protect the control component. Specifically, the housing assembly includes an aircraft body, a first outer shell and a second outer shell provided on the aircraft body. The control component includes a substrate and a plurality of connectors provided on the substrate. The connectors communicate with the aircraft body to supply power to the control component and establish a communication connection. At the same time, weather information is received in real time through a receiving component provided at the front end of the aircraft body, and is broadcast in real time through a broadcaster provided on the substrate. It replaces the traditional way for listeners to turn on the TV or radio and switch to the corresponding broadcast channel or frequency to obtain disaster information, improves the information acquisition efficiency, and provides reaction time for dealing with changing weather.

[0012] According to one aspect of the above technical solution, the aircraft body is recessed with a receiving cavity for accommodating the control component, and the end face of the receiving cavity is lower than the end face of the aircraft body.

[0013] According to one aspect of the above technical solution, a plurality of connection holes are symmetrically provided on the end face of the receiving cavity for connecting the second outer shell.

[0014] According to one aspect of the above technical solution, the height of the second outer shell is equal to the height difference between the end face of the receiving cavity and the end face of the aircraft body.

[0015] According to one aspect of the above technical solution, a first notch and a second notch are provided on the side of the aircraft body. The first notch communicates with the connector, and a switch member is provided in the second notch.

[0016] According to one aspect of the above technical solution, the second notch communicates with the receiving cavity for inserting a memory card.

[0017] According to one aspect of the above technical solution, the receiving component includes an infrared receiver and a wiring connecting the infrared receiver and the substrate. The infrared receiver is embedded in the aircraft body.

[0018] According to one aspect of the above technical solution, a wiring groove is further provided between the receiving cavity and the infrared receiver.

[0019] According to one aspect of the above technical solution, a backing plate is provided on one side of the aircraft body away from the first housing.

[0020] Additional aspects and advantages of the present utility model will be given in part in the following description, will become apparent in part from the following description, or will be understood through the practice of the present utility model. Description of the Drawings

[0021] The above and / or additional aspects and advantages of the present utility model will become obvious and easy to understand from the description of the embodiments in conjunction with the following drawings, where:

[0022] Figure 1 is a schematic structural diagram of a meteorological early warning aircraft in an embodiment of the present utility model;

[0023] Figure 2 is an assembly schematic diagram of a receiving component and a fuselage;

[0024] Figure 3 is an assembly schematic diagram of a control component and a fuselage;

[0025] Figure 4 is a schematic structural diagram of the fuselage.

[0026] Explanation of the symbols of the components in the drawings:

[0027] Housing assembly 100, fuselage 110, accommodation cavity 111, connection hole 112, wire routing groove 113, first notch portion 114, second notch portion 115, first outer shell 120, second outer shell 130, control component 200, substrate 210, connector 220, storage member 230, broadcaster 240, receiving component 300, infrared receiver 310, wiring 320, switch member 400, backing plate 500. Detailed implementation manners

[0028] In order to make the objectives, features and advantages of the present utility model more obvious and understandable, the following detailed description of the specific implementation manners of the present utility model is given in conjunction with the drawings. Several embodiments of the present utility model are shown in the drawings. However, the present utility model can be implemented in many different forms and is not limited to the embodiments described herein. On the contrary, the purpose of providing these embodiments is to make the disclosure of the present utility model more thorough and comprehensive.

[0029] It should be noted that when an element is referred to as being "fixedly provided on" another element, it can be directly on the other element or there may also be an intermediate element. When an element is considered to be "connected" to another element, it can be directly connected to the other element or there may be an intermediate element at the same time. The terms "vertical", "horizontal", "left", "right", "upper", "lower" and similar expressions used herein are only for the purpose of illustration and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be construed as a limitation of the present utility model.

[0030] In the present utility model, unless otherwise clearly defined and limited, terms such as "installation", "connection", "linkage", "fixation" should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediate medium, and it can be the communication inside two components. For those of ordinary skill in the art, the specific meanings of the above terms in the present utility model can be understood according to specific circumstances. The term "and / or" used herein includes any and all combinations of one or more of the related listed items.

[0031] Please refer to Figures 1 - 4 , which shows a schematic structural diagram of a meteorological early warning aircraft provided in an embodiment of the present utility model. The meteorological early warning aircraft includes a housing assembly 100, a control assembly 200 and a receiving assembly 300 provided on the housing assembly 100, wherein:

[0032] In order to support the control assembly 200 and the receiving assembly 300, the housing assembly 100 includes a body 110 for installing the control assembly 200 and the receiving assembly 300, and a first outer shell 120 and a second outer shell 130 provided on the body 110. Since the body 110 is recessed downward to form a receiving cavity 111 for receiving the control assembly 200, the second outer shell 130 is used to cover the receiving cavity 111 to protect the control assembly 200 provided in the receiving cavity 111. The first outer shell 120 is used to seal the end face of the body 110, which not only plays a sealing role but also has an aesthetic function, and a logo or pattern can also be set on the end face of the first outer shell 120.

[0033] Furthermore, in order to use the second outer shell 130 to cover the control assembly 200 to protect the control assembly 200, the end face of the receiving cavity 111 is set lower than the end face of the body 110. At the same time, a plurality of connection holes 112 are symmetrically provided on the end face of the receiving cavity 111 for connecting the second housing, so as to cover the cavity end face of the receiving cavity 111. And in order to avoid affecting the installation of the first housing, the height of the second housing is equal to the height difference between the cavity of the receiving cavity 111 and the end face of the body 110, so that when the second housing is installed on the cavity end face of the receiving cavity 111, the end face of the second housing is flush with the end face of the body 110. Furthermore, when the first housing is installed, it will not be unable to be installed on the end face of the body 110 due to the protrusion of the second housing.

[0034] Furthermore, the body 110 in this embodiment is funnel-shaped with an isosceles trapezoid cross-section. A first notch 114 and a second notch are provided on its side. Both the first notch 114 and the second notch 115 communicate with the accommodation cavity 111 for connecting the control component 200. A switch 400 is also provided at the second notch. By toggling the switch 400, the start and stop of the weather warning device can be controlled. To facilitate toggling the switch 400, it is provided on the top end face of the second notch 115. The listener only needs to place the hand in the second notch 115 to touch the switch 400, thus facilitating toggling the switch 400. It should be emphasized that the size of the second notch 115 is slightly larger than the finger size to facilitate quickly touching the toggle and connecting to the control component 200.

[0035] To achieve the control function, a control component 200 is provided at the bottom of the accommodation cavity 111. The control component 200 includes a substrate 210 and a plurality of connectors 220 provided on the substrate 210. The substrate 210 is connected to the bottom of the accommodation cavity 111 through fasteners. The body 110 communicates with the above connectors 220 at the first notch 114. The above connectors 220 can be used to connect to power supply, or a home network, or a display screen, etc. to achieve multi-functional media. Furthermore, a broadcaster 240 is also provided on the substrate 210 for real-time broadcasting of the current weather. A storage 230 is also provided on the substrate 210, and the storage 230 communicates with the second notch 115 of the body 110 for inserting a memory card. In addition, a backing plate 500 is provided at the bottom of the body 110.

[0036] To achieve the control function of the weather warning device, a receiving component 300 is also provided at one end of the body 110 away from the accommodation cavity 111. The receiving component 300 includes an infrared receiver 310 and a wiring 320 connecting the infrared receiver 310 and the substrate 210. The infrared receiver 310 is embedded in the front end of the body 110. A wiring groove 113 is also provided between the accommodation cavity 111 and the infrared receiver 310 for placing the wiring 320. The infrared receiver 310 receives the control signal from an external infrared transmitter to control the broadcast frequency, sound volume, etc. of the weather warning device. Then, the obtained weather information is broadcast through the broadcaster 240, replacing the traditional way that the listener turns on the TV or radio and switches to the corresponding broadcast channel or frequency to obtain disaster information, improving the information acquisition efficiency and providing a reaction time for coping with changing weather.

[0037] In summary, a weather early warning aircraft proposed according to the present utility model realizes communication connection by providing connectors inside the aircraft body, and then receives control signals through a receiving component and broadcasts weather information in real time through a broadcaster. At the same time, a second outer shell is used to cover the control component to protect the control component. Specifically, the housing assembly includes an aircraft body, a first outer shell and a second outer shell provided on the aircraft body. The control component includes a substrate and a plurality of connectors provided on the substrate. The connectors are connected to the aircraft body to supply power to the control component and establish a communication connection. At the same time, weather information is received in real time through a receiving component provided at the front end of the aircraft body and broadcast in real time through a broadcaster provided on the substrate. It replaces the traditional way that listeners turn on the TV or radio and switch to the corresponding radio channel or frequency to obtain disaster information, improves the information acquisition efficiency, and provides reaction time for coping with changing weather.

[0038] In the description of this specification, the description with reference to terms such as "one embodiment", "some embodiments", "example", "specific example", or "some examples" means that the specific features, structures, materials, or characteristics described in connection with the embodiment or example are included in at least one embodiment or example of the present utility model. In this specification, the schematic representations of the above terms do not necessarily refer to the same embodiment or example. Moreover, the specific features, structures, materials, or characteristics described can be combined in a suitable manner in any one or more embodiments or examples.

[0039] The above-described embodiments only represent several implementation manners of the present utility model, and the description thereof is relatively specific and detailed, but it cannot be understood as a limitation on the patent scope of the present utility model. It should be noted that for those of ordinary skill in the art, without departing from the concept of the present utility model, several modifications and improvements can still be made, and these all belong to the protection scope of the present utility model. Therefore, the protection scope of the patent of the present utility model shall be subject to the appended claims.

Claims

1. A meteorological early warning aircraft, characterized in that, The meteorological early warning aircraft includes: A housing assembly, including a fuselage, a first outer shell and a second outer shell provided on the fuselage; A control assembly, including a substrate and a plurality of connectors provided on the substrate, the connectors communicating with the fuselage for communication connection; A receiving assembly, provided at one end of the fuselage away from the connectors for receiving meteorological information; Wherein, the second outer shell is used to cover the control assembly, the first outer shell covers the second outer shell, and a broadcaster is further provided on the substrate.

2. The meteorological early warning aircraft according to claim 1, wherein The fuselage is recessed with a receiving cavity for accommodating the control assembly, and the end face of the receiving cavity is lower than the end face of the fuselage.

3. The meteorological early warning aircraft according to claim 2, characterized in that, A plurality of connecting holes are symmetrically provided on the end face of the receiving cavity for connecting the second outer shell.

4. The weather warning aircraft according to claim 3, characterized in that, The height of the second outer shell is equal to the height difference between the end face of the receiving cavity and the end face of the fuselage.

5. The weather warning aircraft according to claim 1, wherein A first notch and a second notch are provided on the side of the fuselage, the first notch communicates with the connectors, and a switch is provided in the second notch.

6. The weather warning aircraft according to claim 5, wherein, The second notch communicates with the receiving cavity for inserting a memory card.

7. The weather warning aircraft according to claim 1, wherein The receiving assembly includes an infrared receiver and a wiring connecting the infrared receiver and the substrate, and the infrared receiver is embedded in the fuselage.

8. The meteorological early warning aircraft according to claim 7, characterized in that, A wiring groove is further provided between the receiving cavity and the infrared receiver.

9. The meteorological early warning aircraft according to claim 1, wherein A backing plate is provided on the side of the fuselage away from the first housing.

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