Intelligent security and disinfection all-in-one machine

Abstract

The utility model discloses an intelligent security and disinfection all-in-one machine, which comprises a front shell assembly, a protective cover assembly, a rear shell assembly, a machine body assembly and an installation support assembly, the front shell assembly comprises a front panel, a front shell, a flame sensor assembly, a high-definition camera assembly, a light supplementing lamp assembly and a signal lamp assembly, and the flame sensor assembly, the high-definition camera assembly, the light supplementing lamp assembly and the signal lamp assembly are fixedly arranged on the front shell assembly. A 4G rear shell is arranged on the outer side face of the rear panel, a 4G antenna is installed on the 4G rear shell, the front shell assembly and the rear shell assembly are fixedly connected through four connecting columns penetrating through the inner side of the machine body assembly, a loudspeaker assembly is arranged on the lower end face of the machine body assembly, and the installation support assembly is arranged at the lower end of the machine body assembly. The flame sensor assembly, the high-definition camera assembly, the light supplementing lamp assembly, the signal lamp assembly and the installation support assembly are all electrically connected with the remote intelligent terminal. According to the utility model, the whole machine adopts a modular design, each component is independently assembled into a component and then is integrally assembled together, and the fire-fighting and security functions are simultaneously realized, the performance is stable, and the anti-interference performance is strong.

Description

Technical Field

[0001] The utility model relates to the technical field of security equipment, and in particular to an intelligent all-in-one security and fire protection machine. Background Art

[0002] Firefighting and security are two important issues that are closely related to the safety of people's lives and property. At present, in terms of the technical development of fire monitoring systems, indoor fire alarms are relatively mature. They are judged by light, smoke, temperature, etc., and then directly implement fire extinguishing measures such as power off, water spraying, etc. and alarm. However, security systems generally do not have fire alarm functions. To achieve firefighting and security, it is often necessary to build two independent systems, which increases the difficulty and efficiency of management, and also increases construction and maintenance costs. Utility Model Content

[0003] The purpose of the utility model is to provide an intelligent integrated fire protection and safety device, which combines the functions of fire protection and safety protection in one device through a modular design, so as to overcome the above-mentioned deficiencies existing in the prior art.

[0004] In order to achieve the above technical purpose, the technical solution of the utility model is implemented as follows:

[0005] An intelligent integrated safety and firefighting machine comprises a front shell assembly, a protective cover assembly, a rear shell assembly, a fuselage assembly and a mounting bracket assembly. The front shell assembly comprises a front panel, a front shell and a flame sensor assembly, a high-definition camera assembly, a fill light assembly and a signal light assembly fixedly arranged on the front shell assembly. The rear shell assembly comprises a rear panel. A 4G rear shell is arranged on the outer side of the rear panel. A 4G antenna is installed on the 4G rear shell. The front shell assembly and the rear shell assembly are fixedly connected by four connecting columns penetrating the inner side of the fuselage assembly. A speaker assembly is arranged on the lower end surface of the fuselage assembly. The mounting bracket assembly is arranged at the lower end of the fuselage assembly. The flame sensor assembly, the high-definition camera assembly, the fill light assembly, the signal light assembly and the mounting bracket assembly are all electrically connected to a remote intelligent terminal.

[0006] Furthermore, the flame sensor assembly includes a flame sensor embedded in the front panel and a flame sensor board fixed on the inner side of the front shell assembly, the high-definition camera assembly includes a high-definition camera embedded in the front panel and a camera main control board fixed on the inner side of the front shell assembly, and the fill light assembly includes an LED light embedded in the front panel and an LED light board fixed on the inner side of the front shell assembly.

[0007] Furthermore, the mounting bracket assembly includes an alloy bracket, one end of which is integrally provided with a mounting portion, and the other end of the alloy bracket is connected to the fuselage assembly via a multi-directional angle adjustment assembly.

[0008] Furthermore, a mounting groove for accommodating a speaker assembly is provided on the lower side surface of the body assembly near the front end. The speaker assembly includes a speaker and an interface cover. The upper end of the interface cover is provided with a receiving groove adapted to the speaker. A through hole is provided at the bottom of the receiving groove. A waterproof and sound-permeable membrane is provided between the speaker and the receiving groove. The interface cover is fixedly connected to the receiving groove.

[0009] Furthermore, waterproof rings are provided between the front shell assembly and the body assembly, between the rear shell assembly and the body assembly, and between the interface cover and the receiving groove.

[0010] Beneficial effects of the utility model: the whole machine of the utility model adopts modular design, each component is assembled into components separately, and then assembled together as a whole, and has fire protection and security functions at the same time, stable performance, and strong anti-interference ability. BRIEF DESCRIPTION OF THE DRAWINGS

[0011] Figure 1 It is a structural schematic diagram of the intelligent fire-fighting integrated machine in the embodiment of the utility model;

[0012] Figure 2 It is a schematic diagram of the structure of the intelligent fire-fighting integrated machine in the embodiment of the utility model after the body is removed;

[0013] Figure 3 It is a schematic diagram of the exploded structure of the front shell assembly in the embodiment of the utility model;

[0014] Figure 4 It is a schematic diagram of the connection structure between the mounting bracket assembly and the fuselage in the embodiment of the utility model;

[0015] Figure 5 It is a schematic diagram of the exploded structure of the speaker assembly in the embodiment of the utility model;

[0016] Figure 6 It is a structural schematic diagram of the function of the protective cover assembly and the fuselage assembly in the embodiment of the utility model;

[0017] Figure 7 It is a schematic diagram of the exploded structure of the rear shell assembly in the embodiment of the utility model;

[0018] Figure 8 It is a structural schematic diagram of the fuselage in the embodiment of the utility model.

[0019] As shown in the figure:

[0020] 1-Front panel; 2-Rear panel; 3-4G rear shell; 4-4G antenna; 5-Connecting column; 6-Flame sensor; 7-Flame sensor board; 8-HD camera; 9-Camera main control board; 10-LED light; 11-LED light board; 12-Alloy bracket; 13-Mounting part; 14-Multi-directional angle adjustment component; 15-Speaker; 16-Interface cover; 17-Through hole; 18-Waterproof and sound-permeable membrane; 19-Waterproof ring; 20-Signal light; 21-Mounting frame; 22-Interface board; 23-Waterproof connector; 24-Card interface; 25-Mounting cover; 26-Fixing screws; 27-Protective cover; 28-Body; 29-Waterproof ring screws; 30-Card slot. DETAILED DESCRIPTION

[0021] The technical solutions in the embodiments of the present invention are described clearly and completely below in conjunction with the accompanying drawings in the embodiments of the present invention.

[0022] like Figure 1-2 and Figure 7 As shown, according to an embodiment of the utility model, an intelligent fire protection integrated machine includes a front shell component, a protective cover component, a rear shell component, a fuselage component and a mounting bracket component. The front shell component includes a front panel 1, a front shell and a flame sensor component, a high-definition camera component, a fill light component and a signal light component fixedly arranged on the front shell component 1. The front panel 1 is made of sapphire glass and acrylic material, the back is silk-screened, and it is fixedly installed on the front shell with waterproof glue. The front shell is aluminum alloy. The rear shell component includes a rear panel 2. A 4G rear shell 3 is arranged on the outer side of the rear panel 2. A 4G antenna 4 is installed on the 4G rear shell. The front shell component and the rear shell component are fixedly connected by four connecting columns 5 that pass through the inner side of the fuselage component, as shown in FIG. Figure 8 As shown, a card slot 30 adapted to the connecting column 5 is provided on the inner side of the fuselage 28, and the card slot 30 facilitates the fixation between the fuselage 20 and the connecting column 5. A speaker assembly is provided on the lower end surface of the fuselage assembly, and a mounting bracket assembly is arranged at the lower end of the fuselage assembly. The flame sensor assembly, the high-definition camera assembly, the fill light assembly, the signal light assembly and the mounting bracket assembly are all electrically connected to the remote intelligent terminal.

[0023] like Figure 2 and 3 As shown, the flame sensor assembly includes a flame sensor 6 embedded in the front panel 1 and a flame sensor board 7 fixedly arranged on the inner side of the front shell assembly, the high-definition camera assembly includes a high-definition camera 8 embedded in the front panel 1 and a camera main control board 9 fixedly arranged on the inner side of the front shell assembly, and the fill light assembly includes an LED lamp 10 embedded in the front panel 1 and an LED light board 11 fixedly arranged on the inner side of the front shell assembly. The flame sensor board 7, the camera main control board 9 and the LED light board 11 are fixed on the front shell assembly through the mounting column and the mounting frame 21 provided on the front shell assembly.

[0024] like Figure 4 As shown, the mounting bracket assembly includes an alloy bracket 12, and a tail wire connector storage area 24 for accommodating the wiring is provided at the bottom of the alloy bracket 12. The wiring is electrically connected to the circuit components in the front shell assembly through a waterproof connector 23. A mounting portion 13 is integrally provided at one end of the alloy bracket 12. The mounting portion 13 is fixedly connected to the all-in-one machine by a mounting screw 13, and the other end is connected to the fuselage assembly through a multi-directional angle adjustment assembly 14.

[0025] like Figure 5 As shown, a mounting groove for accommodating a speaker assembly is provided on the lower side surface of the body assembly near the front end, and a card insertion interface 24 is provided in the mounting groove. The speaker assembly includes a speaker 15 and an interface cover 16. A receiving groove adapted to the speaker 15 is provided at the upper end of the interface cover 16. The speaker 15 and the interface cover 16 are connected via a mounting cover 25 provided on the speaker 15. A through hole 17 is provided at the bottom of the receiving groove. A waterproof and sound-permeable membrane 18 is provided between the speaker 15 and the receiving groove, and the interface cover 16 is fixedly connected to the receiving groove by fixing screws 26.

[0026] like Figure 5-6 As shown, waterproof rings 19 are provided between the front panel 1 and the body assembly, between the rear panel 2 and the body assembly, and between the interface cover 16 and the receiving groove.

[0027] The fuselage components are made of alloy structure, combined with protective cover components, which are rain and snow proof, heat-insulated and explosion-proof. The overall structure has a sealing effect, and dust is not easy to enter the fuselage 28. It can withstand high temperatures of 70 degrees and low temperatures of -40 degrees. After testing, the equipment is still in normal working condition after working for 2 hours in a high temperature of 70 degrees or a low temperature of -40 degrees. During normal use, the equipment is resistant to electrostatic discharge, radio frequency electromagnetic field radiation, radio frequency field induced conduction disturbance, electrical fast transient pulses, and surges, and has good practicality.

[0028] The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the protection scope of the present invention.

Claims

1. An intelligent fire-fighting integrated machine, characterized in that: The invention comprises a front shell component, a protective cover component, a rear shell component, a fuselage component and a mounting bracket component. The front shell component comprises a front panel (1), a front shell and a flame sensor component, a high-definition camera component, a fill light component and a signal light component fixedly arranged on the front shell component. The rear shell component comprises a rear panel (2). A 4G rear shell (3) is arranged on the outer side of the rear panel (2). A 4G antenna (4) is installed on the 4G rear shell. The front shell component and the rear shell component are fixedly connected via four connecting columns (5) penetrating the inner side of the fuselage component. A speaker component is arranged on the lower end surface of the fuselage component. The mounting bracket component is arranged at the lower end of the fuselage component. The flame sensor component, the high-definition camera component, the fill light component, the signal light component and the mounting bracket component are all electrically connected to a remote intelligent terminal.

2. The intelligent fire-fighting integrated machine according to claim 1, characterized in that: The flame sensor assembly comprises a flame sensor (6) embedded in the front panel (1) and a flame sensor board (7) fixedly arranged on the inner side of the front shell assembly; the high-definition camera assembly comprises a high-definition camera (8) embedded in the front panel (1) and a camera main control board (9) fixedly arranged on the inner side of the front shell assembly; and the fill light assembly comprises an LED light (10) embedded in the front panel (1) and an LED light board (11) fixedly arranged on the inner side of the front shell assembly.

3. The intelligent fire-fighting integrated machine according to claim 1, characterized in that: The mounting bracket assembly comprises an alloy bracket (12), one end of the alloy bracket (12) is integrally provided with a mounting portion (13), and the other end is connected to the fuselage assembly via a multi-directional angle adjustment assembly (14).

4. The intelligent fire-fighting integrated machine according to claim 1, characterized in that: A mounting groove for accommodating a speaker assembly is provided on the lower side surface of the body assembly near the front end. The speaker assembly comprises a speaker (15) and an interface cover (16). A receiving groove adapted to the speaker (15) is provided at the upper end of the interface cover (16). A through hole (17) is provided at the bottom of the receiving groove. A waterproof sound-permeable membrane (18) is provided between the speaker (15) and the receiving groove. The interface cover (16) is fixedly connected to the receiving groove.

5. The intelligent fire-fighting integrated machine according to any one of claims 1 to 4, characterized in that: Waterproof rings (19) are provided between the front shell component and the body component, between the rear shell component and the body component, and between the interface cover (16) and the accommodating groove.

Images