CN213635303U

CN213635303U - Aircraft on-site state warning interaction device

Info

Publication number: CN213635303U
Application number: CN202023104074.XU
Authority: CN
Inventors: 陈俊逸
Original assignee: Individual
Current assignee: Individual
Priority date: 2020-12-22
Filing date: 2020-12-22
Publication date: 2021-07-06
Anticipated expiration: 2030-12-22

Abstract

The utility model discloses an aircraft on-site state warning interaction device, which comprises a base, universal wheels are fixedly connected at four right angles at the bottom of the base, a fixed frame is fixedly connected at the top of the base, a control box is fixedly connected at the top of the fixed frame at the bottom, a LED display control panel is fixedly connected at the front of the control box, a monitoring interaction camera is fixedly connected at the middle part of the bottom of the fixed frame, information notification can be changed at any time, when the aircraft state changes, the display information of an aircraft state display board only needs to be updated at a control end, the change of the display information can be completed within 1 second at the fastest, safety and high efficiency are realized, the information notification form is diversified, besides character information, optical information and sound voice broadcast can be provided by a warning lamp system, sound, light and electricity are combined, information bidirectional notification is realized, the technology of the Internet of, the manager can obtain the field situation through the carried camera and timely receive the feedback of the field personnel to form a closed loop.

Description

Aircraft on-site state warning interaction device

Technical Field

The utility model relates to an aircraft on-the-spot state warns interactive system technical field, specifically is an aircraft on-the-spot state warns interactive installation.

Background

In a traditional aircraft regular inspection maintenance site, a simple display board is generally used for prompting state information such as 'pressing' and 'electrifying' of an aircraft, so that damage to personnel, the aircraft and equipment caused by the actuation of the aircraft is avoided. The display board is generally made of metal or wood materials, the airplane state is notified by pasting or writing characters on the sticker, information is simple and cannot be updated in real time, and warning effects such as lamplight and voice are lacked, so that the information is easy to ignore.

The display board is used for displaying the state of the airplane and has the following defects:

1. the reported information cannot be changed in time. If the state of the airplane is changed, for example, the 'pressing' state is changed into the 'power-on' state, the 'pressing' display board needs to be removed and the 'power-on' display board needs to be replaced, and the time lag exists.

2. The information reporting form is single. The display board can only provide visual information, and the staff is carrying out certain work, neglects on-the-spot aircraft state easily, can't receive this information in time, has the potential safety hazard.

3. The notified information can be transmitted only in one direction. After the display board is used for reporting the state of the airplane, field personnel can only receive information in one direction, and managers cannot receive field feedback information in real time.

4. The field working scene lacks evidence obtaining and leaving ways, and is not beneficial to the analysis and improvement of the working scene.

5. The image data beyond the visible distance can not be provided, and the field management monitoring means is delayed.

SUMMERY OF THE UTILITY MODEL

Technical problem to be solved

Not enough to prior art, the utility model provides an aircraft site state warns mutual device has solved the problem that the background art provided.

(II) technical scheme

The utility model provides a following technical scheme: the utility model provides an aircraft on-site condition warns mutual device, includes the base, the equal fixedly connected with universal wheel in four right angles departments of base bottom, the fixed frame of base top fixedly connected with, the top fixedly connected with control box of the fixed frame of end, the positive fixedly connected with LED display control board of control box, the bottom middle part fixedly connected with control mutual camera of fixed frame, fixed frame left side fixedly connected with wiFi control module, the left side fixedly connected with 12V lithium battery module at base top, the top fixedly connected with public address loudspeaker and two warning stroboscopic lamps of control box.

Preferably, the 12V lithium battery module is respectively and electrically connected with the LED display control panel, the WiFi control module and the monitoring interaction camera.

Preferably, the WiFi control module is electrically connected with the two warning strobe lights and the loudspeaker respectively.

Preferably, the LED display control panel comprises a first LED lamp panel, a second LED lamp panel, a third LED lamp panel and a fourth LED lamp panel, and the first LED lamp panel, the second LED lamp panel, the third LED lamp panel and the fourth LED lamp panel are all electrically connected with the WiFi control module.

Preferably, the model of the WiFi control module is DL-KGEBJ/2H.

(III) advantageous effects

Compared with the prior art, the utility model provides an aircraft site state warns mutual device possesses following beneficial effect:

1. the information report can be changed at any time, when the state of the airplane changes, the display information of the airplane state display board only needs to be updated at the control end, the change of the display information can be finished within 1 second at the fastest speed, and the method is safe and efficient.

2. The information reporting mode is diversified, besides character information, optical information can be provided through the warning lamp system, sound information can be provided through sound voice broadcasting, and sound, light and electricity are combined.

3. The information reporting is interactive in two directions, and by using the technology of the Internet of things, managers can obtain the field situation through the carried camera and timely receive the feedback of the field personnel to form a closed loop.

4. And providing an image background and a mobile investigation monitoring image, and providing image data for the analysis and optimization of a working scene.

5. The remote 360-degree interaction image is provided through the Internet of things technology, the field remote control function is realized, and the field maintenance management efficiency is improved.

Drawings

FIG. 1 is a schematic view of the present invention;

FIG. 2 is a schematic view of the present invention;

fig. 3 is a circuit diagram of the present invention.

In the figure: 1 base, 2 universal wheels, 3 fixed frames, 4 warning stroboscopic lamps, 5 public address loudspeaker, 6LED display control panel, 7 mutual cameras of control, 8wiFi control module, 912V lithium cell module, 10 control box.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Referring to fig. 1-3, an aircraft on-site warning interaction device comprises a base 1, universal wheels 2 are fixedly connected to four right-angle corners of the bottom of the base 1, the universal wheels 2 are arranged to facilitate carrying and moving of the device, a fixed frame 3 is fixedly connected to the top of the base 1, a control box 10 is fixedly connected to the top of the fixed frame 3, and the control box 10 uses a DL-KGBJ8/2H internet-of-things intelligent controller and can control a sub-circuit switch through a network; the method comprises the following steps of installing a TL-IPC43AN-4 camera, monitoring the field condition and remote interaction in real time, fixedly connecting an LED display control panel 6 to the front side of a control box 10, fixedly connecting a monitoring interaction camera 7 to the middle of the bottom of a fixed frame 3, fixedly connecting a WiFi control module 8 to the left side of the fixed frame 3, fixedly connecting a 12V lithium battery module 9 to the left side of the top of a base 1, supplying power to a system power supply by adopting a safe low-voltage 12V lithium battery, wherein the maximum current of the whole circuit is 10A, and partial leads are self-contained circuits of; the trouble of job site power consumption safety and tow line power supply is avoided, and the top fixedly connected with public address loudspeaker 5 and two warning stroboscopic lamps 4 of control box 10, foretell connection can adopt welding or bolt installation one of them or two kinds.

As shown in fig. 2 and fig. 3, the 12V lithium battery module 9 is electrically connected to the LED display control board 6, the WiFi control module 8 and the monitoring interactive camera 7 respectively. WiFi control module 8 is connected with two warning stroboscopic lamps 4 and public address loudspeaker 5 electricity respectively, public address loudspeaker 5 passes through the control of stereo set controller, it possesses the recording to change public address loudspeaker 5 like this, the broadcast, the function of talkbacking, the penetrating power can be overcome more strongly on-the-spot circular telegram, noise such as suppressing is to the interference of key broadcast information content, when there is the early warning condition, public address loudspeaker 5 can send the tip information, this moment, two warning stroboscopic lamps 4 are switched into red by the orange, and light scintillation, be used for reminding the on-the-spot personnel like this. The LED display control panel 6 comprises a first LED lamp panel, a second LED lamp panel, a third LED lamp panel and a fourth LED lamp panel, the first LED lamp panel, the second LED lamp panel, the third LED lamp panel and the fourth LED lamp panel are electrically connected with the WiFi control module 8, the first LED lamp panel, the second LED lamp panel, the third LED lamp panel and the fourth LED lamp panel are P10LED display boards, highlight P10LED display boards are used for reporting character information, each LED display board can be independently controlled and changed in content, the first LED lamp panel, the second LED lamp panel, the third LED lamp panel and the fourth LED lamp panel are in two states, one state is a work reminding state, and the same information content is displayed. Each LED panel can be controlled individually, for example, to display "press" and "power on" simultaneously, while the other state is off, with text display.

Specifically, the model of the WiFi control module 8 is DL-KGEBJ/2H.

It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides an aircraft on-site condition warns mutual device, includes base (1), four equal fixedly connected with universal wheels (2) of right angle department of base (1) bottom, the fixed frame of base (1) top fixedly connected with (3), its characterized in that: the utility model discloses a portable electronic device, including base (1), top fixedly connected with control box (10) of fixed frame (3), the positive fixedly connected with LED display control panel (6) of control box (10), the mutual camera (7) of bottom middle part fixedly connected with control of fixed frame (3), fixed frame (3) left side fixedly connected with wiFi control module (8), the left side fixedly connected with 12V lithium cell module (9) at base (1) top, the top fixedly connected with public address loudspeaker (5) and two warning stroboscopic lamps (4) of control box (10).

2. An aircraft field status alert interaction device as claimed in claim 1, wherein: the 12V lithium battery module (9) is electrically connected with the LED display control panel (6), the WiFi control module (8) and the monitoring interaction camera (7) respectively.

3. An aircraft field status alert interaction device as claimed in claim 1, wherein: WiFi control module (8) are connected with two warning stroboscopic lamp (4) and public address loudspeaker (5) electricity respectively.

4. An aircraft field status alert interaction device as claimed in claim 1, wherein: the LED display control panel (6) comprises a first LED lamp panel, a second LED lamp panel, a third LED lamp panel and a fourth LED lamp panel, and the first LED lamp panel, the second LED lamp panel, the third LED lamp panel and the fourth LED lamp panel are all electrically connected with the WiFi control module (8).

5. An aircraft field status alert interaction device as claimed in claim 1, wherein: the model of the WiFi control module (8) is DL-KGEBJ/2H.