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General airplane data recording unit

A technology for recording unit and aircraft data, applied in the directions of registration/indication, time register, registration/indication of vehicle operation, etc., can solve the problems of low integration, non-universal, simple communication interface, etc., and achieve the effect of high integration

Pending Publication Date: 2022-06-21
成都科洛威尔科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to provide a general-purpose aircraft data recording unit, which solves the shortcomings of the existing data recording unit, such as single type of information collection, low integration, simple communication interface and non-universal use, and is not suitable for small aircraft such as general aviation. question

Method used

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Comparison scheme
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Embodiment 1

[0079] A general-purpose aircraft data recording unit, comprising a MCU logic processing unit, the MCU logic processing unit is electrically connected with a data storage unit, a data export interface, an RS232 data recording interface, an angle displacement acquisition interface, a temperature acquisition interface, and a flap position recorder. unit, stall warning recording unit, elevator joystick force recording unit;

[0080] The electrical signal of the RS232 data recording interface is connected to the onboard RS232 communication bus, the electrical signal of the stall warning recording unit is connected to the speed warning detection system, and the electrical signal of the flap position recording unit is connected to the flap control board angle sensor, so The electric signal of the elevator joystick force recording unit is connected to the force sensor.

Embodiment 2

[0082] On the basis of Embodiment 1, the temperature acquisition interface is an 8-way J-type thermocouple temperature acquisition interface, and the electrical signal of the 8-way J-type thermocouple temperature acquisition interface is connected with an air intake box temperature sensor and a drive bearing end temperature sensor , Stator coil temperature sensor, stator end temperature sensor, positive heat sink temperature sensor, left magneto temperature sensor, right magneto temperature sensor, fuel temperature sensor.

Embodiment 3

[0084] On the basis of the above embodiment, the angular displacement acquisition interface is a 3-way angular displacement acquisition interface, and the electrical signals of the 3-way angular displacement acquisition interface are connected with an elevator deflection angle displacement sensor, a rudder deflection angle displacement sensor, and ailerons. Deflection angle displacement sensor.

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Abstract

The invention discloses a general aircraft data recording unit, belongs to the technical field of flight data recording, and aims to solve the problem that the existing data recording unit is not suitable for small aircrafts such as general aviation due to the defects of single type of acquired information, low integration level, simple communication interface and non-universality. The system comprises an MCU logic processing unit, and the MCU logic processing unit is electrically connected with a data storage unit, a data export interface, an RS232 data recording interface, an angle displacement acquisition interface, a temperature acquisition interface, a flap position recording unit, a stall alarm recording unit and an elevator joystick force recording unit. The RS232 data recording interface is electrically connected with an airborne RS232 communication bus, the stall alarm recording unit is electrically connected with a stall alarm detection system, the flap position recording unit records the position of a flap, and the elevator joystick force recording unit is electrically connected with a force sensor. The method is suitable for a general aircraft data recording unit.

Description

technical field [0001] The invention belongs to the technical field of flight data recording, in particular to a general aircraft data recording unit. Background technique [0002] The existing flight parameter recording system is an onboard electronic device used to record various system parameters on the aircraft, commonly known as "black box". The recorded flight parameters can be used for fault recording, ground maintenance, aircraft daily flight quality assessment, aircraft status analysis and flight. accident analysis. [0003] The existing data recording units generally have shortcomings such as single type of collected information, low integration, simple and uncommon communication interfaces, and are not suitable for small aircraft such as general aviation. With the development of the general aviation industry, general aircraft have the characteristics of large demand, flexible application, high integration, light weight and low cost. The development of data record...

Claims

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Application Information

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IPC IPC(8): G07C5/08
CPCG07C5/085
Inventor 文建钦梁春艳张小磊
Owner 成都科洛威尔科技有限公司
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