CN210721824U

Movatterモバイル変換

Info

Publication number: CN210721824U
Application number: CN201921622071.XU
Authority: CN
Inventors: 张自军; 石岩; 方庆山; 王磊; 张小虎
Original assignee: Bengbu And Energy Information Technology Co ltd
Current assignee: Bengbu And Energy Information Technology Co ltd
Priority date: 2019-09-27
Filing date: 2019-09-27
Publication date: 2020-06-09
Anticipated expiration: 2029-09-27

Abstract

The utility model discloses a vehicle-mounted power supply execution device for aircraft testing, which comprises an execution device body and a data acquisition end; the execution device body comprises a flat rectangular shell, a PCB circuit board arranged in the flat rectangular shell and a display screen arranged on the upper surface of the flat rectangular shell, wherein the left side and the right side of the flat rectangular shell are respectively provided with a semicircular lug extending outwards, and each semicircular lug is provided with a plurality of control keys; the upper side of the flat rectangular shell is provided with a plurality of control buttons, the upper side of the flat rectangular shell is also provided with an antenna slot, and one end of the antenna slot is provided with a telescopic antenna connected with the PCB; the lower surface of the flat rectangular shell is provided with a battery cavity, and a battery cover is arranged on the battery cavity. The utility model discloses an executor body and data acquisition end, the executor body is flat rectangle structure, can realize quick charge, is equipped with the display screen on the executor body, can be in real time with the communication of data acquisition end to the data feedback that will acquire is on the display screen.

Description

Vehicle-mounted power supply execution device for aircraft test

Technical Field

The utility model relates to an aircraft test technical field, especially an on-vehicle power supply final controlling element for aircraft test.

Background

Aircraft testing refers to the full testing of aircraft according to specified technical requirements and specific specified stacks. The main items of the test comprise a system test, a flight test and a comprehensive test. Only the tested aircraft can ensure the purposes of flight safety and risk control.

At present, the test of the aircraft is mainly performed through a test platform, the test platform is connected with the aircraft through a data line, when the aircraft is started, data of the aircraft are directly acquired, and because the test environment of the aircraft is greatly different from the real environment, equipment for testing the aircraft in the real environment and performing data interaction with the test platform in real time is needed.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to overcome prior art not enough, provide an on-vehicle power supply final controlling element for aircraft test, including final controlling element body and data acquisition end, the final controlling element body is flat rectangle structure, can realize quick charge, is equipped with the display screen on the final controlling element body, can be in real time with data acquisition end communication to the data feedback that will acquire is on the display screen.

The purpose of the utility model is realized through the following technical scheme:

Furthermore, an annular device convenient for being held by hand is arranged below the two semicircular lug plates of the execution device body.

Furthermore, the upper surface of the execution device body is also provided with a micro screen, and the micro screen is arranged at the upper right corner of the display screen.

Furthermore, the lower side surface of the execution device body is also provided with a plurality of data interfaces.

Furthermore, the data interface is a USB interface.

Further, the PCB circuit board comprises a processor, a wireless communication device, a data processing device and a memory; the processor is respectively communicated with the wireless communication device, the data processing device and the memory.

Further, the processor is interconnected with the data acquisition end through a wireless communication device.

The utility model has the advantages that:

the utility model comprises an execution device body and a data acquisition end, wherein the execution device body is of a flat rectangular structure, can realize quick charging, is provided with a display screen, can communicate with the data acquisition end in real time, and feeds back acquired data on the display screen; the utility model discloses still be equipped with the data interface, can realize that data passes each other with external device through the data interface.

Drawings

Fig. 1 is a schematic connection diagram of the present invention;

FIG. 2 is a schematic front view of the actuator body according to the present invention;

fig. 3 is a schematic view of the back structure of the actuator body according to the present invention;

in the figure, 10-an execution device body, 11-a display screen, 12-a semicircular lug, 13-a control key, 14-a ring device, 15-a battery cavity and 20-a data acquisition end.

Detailed Description

The technical solution of the present invention is described in further detail below with reference to the accompanying drawings, but the scope of the present invention is not limited to the following description.

Example 1:

The structural feature of final controlling element body has been elaborated in this embodiment, and final controllingelement body 10 is flat rectangle structure, and final controllingelement body 10 upper surface is equipped withdisplay screen 11, can show the data of gathering in real time throughdisplay screen 11, and the left and right sides of flat rectangle casing is equipped withsemi-circular auricle 12 of outside extension respectively, can pass through the operation ofsemi-circular auricle 12 control aircraft.

Example 2:

on the basis of embodiment 1, theannular device 14 convenient to grasp by hand is further arranged below the twosemicircular lug pieces 12 of theexecution device body 10, and the upper surface of theexecution device body 10 is further provided with a micro screen which is arranged at the upper right corner of the display screen.

Furthermore, a plurality of data interfaces are arranged on the lower side surface of theexecution device body 10.

Furthermore, the data interface is a USB interface.

The utility model comprises anexecution device body 10 and a data acquisition end 20, wherein theexecution device body 10 is of a flat rectangular structure, can realize quick charging, and is provided with adisplay screen 11 on theexecution device body 10, can communicate with the data acquisition end in real time, and feeds back acquired data to thedisplay screen 11; the utility model discloses still be equipped with the data interface, can realize that data passes each other with external device through the data interface.

The above-mentioned embodiments only express the specific embodiments of the present invention, and the description thereof is specific and detailed, but not construed as limiting the scope of the present invention. It should be noted that, for those skilled in the art, without departing from the spirit of the present invention, several variations and modifications can be made, which are within the scope of the present invention.

Claims

2. The vehicle-mounted power supply execution device for the aircraft test according to claim 1, wherein an annular device convenient for being held by hands is further arranged below the two semicircular lugs of the execution device body.

3. The vehicle-mounted power supply execution device for the aircraft test according to claim 1, wherein a micro screen is further arranged on the upper surface of the execution device body, and the micro screen is arranged at the upper right corner of the display screen.

4. The vehicle-mounted power supply execution device for the aircraft test as claimed in claim 1, wherein the lower side surface of the execution device body is further provided with a plurality of data plug interfaces.

5. The vehicle-mounted power supply execution device for the aircraft test according to claim 4, wherein the data socket is a USB interface.

6. The vehicle-mounted power supply execution device for aircraft testing according to claim 1, characterized in that the PCB circuit board comprises a processor, a wireless communication device, a data processing device and a memory; the processor is respectively communicated with the wireless communication device, the data processing device and the memory.

7. The vehicle-mounted power supply execution device for the aircraft test according to claim 1 or 6, wherein the processor is interconnected with the data acquisition end through a wireless communication device.