CN112414451A

CN112414451A - Airborne platform information acquisition device

Info

Publication number: CN112414451A
Application number: CN202011077444.7A
Authority: CN
Inventors: 许之琦
Original assignee: Xi'an Longzi Electronic Technology Co ltd
Current assignee: Xi'an Longzi Electronic Technology Co ltd
Priority date: 2020-10-10
Filing date: 2020-10-10
Publication date: 2021-02-26

Abstract

The invention provides an airborne platform information collector, which comprises a set top box, a bottom plate, a computer chip and a display, wherein a plurality of heat dissipation holes are formed in the left side surface, the right side surface and the upper surface of the set top box, the computer chip, a horizontal sensor, a signal receiver, a humidity sensor, a storage and a signal transmitter are connected through data lines, the computer chip, the signal receiver, the storage and the signal transmitter are all arranged in the set top box, and the horizontal sensor and the humidity sensor are arranged outside the set top box. Inside level sensor is used for detecting the balance of aircraft fuselage, and humidity transducer detects the humidity of air in the high altitude, and signal receiver can gather task systems such as radar, sonar, tacang and audio-video signal to can go out the information of gathering through signal transmitter transmission, the information that ground station accessible received platform information collector and gathered.

Description

Airborne platform information acquisition device

Technical Field

The invention relates to an airborne platform information collector, belonging to the field of mechanical equipment.

Background

The original Russian flight collector is low in collecting capacity, part of signals are collected on vibration signals of a vibration signal executing mechanism, and comprehensive collection of task systems such as radars, sonars and tacans and audio and video signals cannot be achieved, so that stored flight information in recording equipment is less, and a worker can not send signals to a ground station to feed back information detected during flight when analyzing the working state of an airplane according to the stored flight information and omit the stored flight information.

Therefore, there is a need for an onboard platform information collector.

Disclosure of Invention

Aiming at the defects in the prior art, the invention aims to provide an airborne platform information collector to solve the problems in the background technology.

In order to achieve the purpose, the invention is realized by the following technical scheme: the utility model provides a machine carries platform information collection station, includes STB, bottom plate, computer chip and display, the upper surface of STB is seted up flutedly, and the inside both sides face at the recess is installed to the handle, a plurality of louvres have been seted up to STB left and right sides face and upper surface, the front surface at the STB is installed to the bottom plate, the front surface of bottom plate is provided with the aviation plug, connect by the data line between computer chip, level sensor, signal receiver, humidity transducer, accumulator and the signal transmitter, computer chip, signal receiver, accumulator and signal transmitter all set up inside the STB, and level sensor and humidity transducer set up at the STB outsidely.

Furthermore, the bottom plate, the handle and the top box are connected through epoxy resin adhesives.

Further, the level sensor, the signal receiver and the humidity sensor are connected with a power supply through wires.

Furthermore, the top box, the bottom plate and the handle are made of carbon fiber composite materials.

Further, the output ends of the level sensor, the signal receiver and the humidity sensor are connected with the input end of the computer chip, the output end of the computer chip is connected with the input end of the display, the output end of the computer chip is connected with the input end of the storage in a two-way mode, and the output end of the computer chip is connected with the input end of the signal transmitter.

Furthermore, the aerial plug consists of an aerial plug socket at the output end of the computer and a power supply aerial plug socket.

Furthermore, when the airplane flies, the airplane body balance information of the airplane is collected through the horizontal sensor, the humidity information of the air in the air is collected through the humidity sensor, signals of task systems such as radar, sonar and tacon are collected through the signal receiver, the collected information is sent to the computer chip, the computer chip processes the received information and sends the information collected by the airborne platform information collector to the upper part of the display through the connection of the output end of the computer chip and the input end of the display so as to be watched by users, the computer chip can also send the collected information to the storage through the connection of the output end and the input end of the storage so as to be stored in the storage, so that the working personnel can analyze the working state of the airplane through the stored flying information, when the received information needs to be sent to the ground station, the computer chip sends the collected information to the signal transmitter through the connection of the output end of the computer chip and the input end of the signal transmitter, the signal transmitter converts the received information into a signal to be transmitted, and the ground station obtains the information collected by the airborne platform information collector by receiving the signal transmitted by the signal transmitter.

The invention has the beneficial effects that: according to the airborne platform information collector, the handle of the top box is convenient for taking and putting the collector, the internal horizontal sensor is used for detecting the balance of the airplane body, the humidity sensor is used for detecting the humidity of air in the high air, the signal receiver can collect task systems such as radar, sonar, tacon and the like and audio and video signals, the collected information can be transmitted out through the signal transmitter, and the ground station can receive the information collected by the platform information collector through the received signal.

Drawings

Other features, objects and advantages of the invention will become more apparent upon reading of the detailed description of non-limiting embodiments with reference to the following drawings:

FIG. 1 is a schematic structural diagram of an airborne platform information collector according to the present invention;

FIG. 2 is a schematic perspective view of an airborne platform information collector according to the present invention;

in the figure: 1-top box, 2-heat dissipation holes, 3-handle, 4-groove, 5-bottom plate, 6-aviation plug, 7-connection hole, 8-level sensor, 9-signal receiver, 10-humidity sensor, 11-computer chip, 12-display, 13-signal emitter, 14-storage and 15-ground station.

Detailed Description

In order to make the technical means, the creation characteristics, the achievement purposes and the effects of the invention easy to understand, the invention is further described with the specific embodiments.

Referring to fig. 1 and fig. 2, the present invention provides a technical solution: including STB 1, bottom plate 5, computer chip 11 and display 12, the upper surface of STB 1 is seted up flutedly 4, handle 3 is installed at the inside both sides face of recess 4, a plurality of louvres 2 have been seted up to 1 left and right sides face of STB and upper surface, bottom plate 5 installs the front surface at STB 1, the front surface of bottom plate 5 is provided with aviation plug 6, computer chip 11, level sensor 8, signal receiver 9, humidity transducer 10, connect by the data line between memory 14 and the signal transmitter (13), computer chip 11, signal receiver 9, memory 14 and signal transmitter 13 all set up inside STB 1, level sensor 8 and humidity transducer 10 set up in STB 1 outsidely.

The bottom plate 5, the handle 3 and the top box 1 are connected by epoxy resin adhesive, and the epoxy resin adhesive is convenient to cure, strong in adhesive force, low in contractibility, stable in chemical property and resistant to mildew. The process is simple, excessive pressure is not required to be applied, and the rubber gasket has good insulativity, chemical corrosion resistance and better oil resistance and solvent resistance.

The level sensor 8, the signal receiver 13, and the humidity sensor 10 are connected to a power source through electric wires.

The top box 1, the bottom plate 5 and the handle 3 are made of carbon-fiber composite materials, the carbon-fiber composite materials are high in density and strength which are 5 times that of steel, the specific gravity of the carbon-fiber composite materials is smaller than that of 1/5 of steel, the carbon-fiber composite materials have lighter weight, the carbon-fiber composite materials can bear high temperature above 2000 ℃, the thermal capacity of the carbon-fiber composite materials is small, the thermal shock resistance and the geothermal expansion coefficient of the carbon-fiber composite materials are excellent, and the corrosion resistance and the radiation performance of.

The output ends of the level sensor 8, the signal receiver 9 and the humidity sensor 10 are connected with the input end of a computer chip 11, the output end of the computer chip 11 is connected with the input end of a display 12, the output end of the computer chip 11 is bidirectionally connected with the input end of a storage 14, and the output end of the computer chip 11 is connected with the input end of a signal emitter 13.

The aerial plug 6 consists of an aerial plug socket at the output end of the computer and a power supply aerial plug socket.

As an embodiment of the present invention: the airplane is internally provided with a bolt, an internal thread is rolled in a connecting hole 7 of an airborne platform information collector, the airborne platform information collector is installed on the airplane through the thread matching connection between the bolt and the connecting hole 7, a power cord is inserted into a power supply aviation socket, a wire at the input end of a display on the airplane is inserted into a computer data output aviation socket, the airplane acquires the self body balance information of the airplane through a level sensor 8 when flying, acquires the humidity information of high-altitude air through a humidity sensor 10, acquires the signals of a task system such as radar, sonar, tacang and the like and audio and video through a signal receiver 9, then transmits the acquired information to a computer chip 11, the computer chip 11 processes the received information and then transmits the information acquired by the airborne platform information collector to the position above a display 12 through the connection between the output end of the computer chip and the input end of the display so as to be watched by a user, the computer chip 11 can also connect the collected information with the input end of the storage through the output end, and send the information to the storage 14 for storage, so that the working personnel can analyze the working state of the airplane through the stored flight information, when the received information needs to be sent to the ground station 15, the computer chip 11 connects the collected information with the input end of the signal transmitter through the output end of the computer chip, and sends the information to the signal transmitter 13, the signal transmitter 13 converts the received information into a signal for transmission, and the ground station 15 obtains the information collected by the airborne platform information collector through receiving the signal transmitted by the signal transmitter 13.

Although the present invention has been described with reference to a preferred embodiment, it should be understood that various changes, substitutions and alterations can be made herein without departing from the spirit and scope of the invention as defined by the appended claims.

Claims

1. The utility model provides an airborne platform information collector, includes top box (1), bottom plate (5), computer chip (11) and display (12), its characterized in that: the upper surface of STB (1) is seted up flutedly (4), and the inside both sides face in recess (4) is installed in handle (3), a plurality of louvres (2) have been seted up to STB (1) left and right sides face and upper surface, install the front surface at STB (1) bottom plate (5), the front surface of bottom plate (5) is provided with aviation plug (6), computer chip (11), level sensor (8), signal receiver (9), humidity transducer (10), connect by the data line between accumulator (14) and signal transmitter (13), computer chip (11), signal receiver (9), accumulator (14) and signal transmitter (13) all set up inside STB (1), and level sensor (8) and humidity transducer (10) set up in STB (1) outside.

2. The airborne platform information collector of claim 1, wherein: the bottom plate (5) and the handle (3) are connected with the top box (1) through epoxy resin adhesives.

3. The airborne platform information collector of claim 1, wherein: the level sensor (8), the signal receiver (9) and the humidity sensor (10) are connected with a power supply through electric wires.

4. The airborne platform information collector of claim 1, wherein: the top box (1), the bottom plate (5) and the handle (3) are made of carbon fiber composite materials.

5. The airborne platform information collector of claim 1, wherein: the output of level sensor (8), signal receiver (9) and humidity transducer (10) is connected with the input of computer chip (11), the output of computer chip (11) is connected with the input of display (12), the output of computer chip (11) and the input both way junction of accumulator (14), the output of computer chip (11) is connected with the input of signal transmitter (13).

6. The airborne platform information collector of claim 1, wherein: the aerial plug (6) consists of a computer output end aerial plug socket and a power supply aerial plug socket.

7. The airborne platform information collector of claim 1, wherein: when the airplane flies, the fuselage balance information of the airplane is collected through a horizontal sensor (8), the humidity information of air in the air is collected through a humidity sensor (10), the signals of a radar task system, a sonar task system, a Takang task system and audio and video are collected through a signal receiver (9), the collected information is sent to a computer chip (11), the computer chip (11) processes the received information and then sends the information collected by an airborne platform information collector to a position above a display (12) through the connection between the output end of the computer chip and the input end of the display so as to be watched by users, the computer chip (11) can also connect the collected information with the input end of a storage through the output end and send the information into the storage (14) for storage so that the working personnel can analyze the working state of the airplane through the stored flying information, when the received information needs to be sent to the ground station (15), the computer chip (11) is used for connecting the acquired information with the input end of the signal transmitter through the output end of the computer chip and sending the information into the signal transmitter (13), the signal transmitter (13) is used for converting the received information into a signal to be transmitted, and the ground station (15) is used for receiving the signal transmitted by the signal transmitter (13) to obtain the information acquired by the airborne platform information acquirer.