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Distributed atmosphere data system

An atmospheric data, distributed technology, applied in measurement devices, instruments, surveying and navigation, etc., can solve the problems of no-model application, difficult sensor selection, limited available space on the surface of the aircraft, etc., and achieves a reduction of 2 pieces of equipment. , the effect of reducing the total amount of the system and improving the degree of system integration

Inactive Publication Date: 2016-09-21
JIANGXI HONGDU AVIATION IND GRP
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  • Claims
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AI Technical Summary

Problems solved by technology

Air data sensors are basically arranged in areas where the flow field characteristics on the surface of the aircraft have little change, and the available space on the surface of the aircraft is limited, and they must be arranged separately from devices protruding from the surface of the aircraft such as antennas, which leads to a relatively large gap in the location selection of the sensors. difficulty
In order to reduce the number of air data probes protruding from the aircraft surface, a multi-functional probe sensor integrating static pressure measurement and airflow deflection angle measurement has appeared in the world, but there is no aircraft application in China at present

Method used

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Embodiment Construction

[0013] The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments. The following examples are only used to illustrate the present invention, and are not intended to limit the protection scope of the present invention.

[0014] figure 1 Shown, a kind of distributed air data system of the present invention, it comprises left and right multifunctional probe sensor 1,2, left and right L-shaped pressure sensor assembly 3,4, upper and lower attack angle sensor 5,6 , side slip angle sensor 7 and total temperature sensor 8;

[0015] The left and right multi-function probe sensors 1 and 2 respectively provide a set of total, static pressure and local angle of attack signals to the left and right L-shaped pressure sensor components 3 and 4 through the RS-422A interface, and send them to the flight control computer 9 respectively. Provide a set of dynamic and static pressure signals and two sets of angle-of-attack signal...

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Abstract

The invention discloses a distributed air data system, which includes left and right multifunctional probe sensors, left and right L-shaped pressure sensor components, up and down angle of attack sensors, sideslip angle sensors and a total temperature sensor; , the right multi-function probe sensor provides a set of total, static pressure and local angle of attack signals to the left and right L-shaped pressure sensor components, and provides dynamic and static pressure signals in the form of analog quantities and two sets of angle of attack to the flight control computer signal, the left and right multi-function probe sensors receive the slip angle signals from the left and right L-shaped pressure sensor components for parameter correction; the left and right L-shaped pressure sensor components receive the slip angle signals from the upper and lower angle-of-attack sensors Calculate the angle of attack from the pressure signal, collect the side-slip angle signal from the side-slip angle sensor, calculate various atmospheric parameters through voting and correction, and provide them to the airborne transponder, inertial navigation system, electromechanical management computer and Flight parameter collector. Compared with the independent sensor solution, the present invention can reduce two pieces of equipment, improve the system integration degree, and reduce the total amount of the system.

Description

technical field [0001] The invention relates to a distributed air data system in the field of aviation instruments and equipment, in particular to a distributed air data system using a multifunctional probe. Background technique [0002] The air data system is an extremely important system on an aircraft. It collects and provides atmospheric parameters such as airspeed, Mach number, barometric altitude, lift speed, angle of attack, and sideslip angle to the aircraft. The air data system is usually composed of sensors such as total static pressure sensor, angle of attack sensor, sideslip angle sensor and total temperature sensor, sensors and air data computer. Atmospheric data systems can be divided into centralized and distributed. The core of the centralized air data system is the air data computer, and the signals sensed by all sensors and receptors are sent to the air data computer for processing; , The sensor and the microprocessor are integrated together, and one devic...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01C23/00G01P13/02
CPCG01C23/00G01P13/025
Inventor 祝庆黄斌顾张亮秦波张晓姣邹林林周家初冯福来
Owner JIANGXI HONGDU AVIATION IND GRP
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