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Airplane gravity center automatic regulation system and regulating method

A technology of automatic adjustment and adjustment method, applied in aircraft parts, special data processing applications, instruments, etc., can solve problems such as large fluctuations in the position of the center of gravity of the aircraft, and achieve strong anti-interference ability and improve reliability.

Inactive Publication Date: 2017-09-01
XIAN AERONAUTICAL POLYTECHNIC INST
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AI Technical Summary

Problems solved by technology

[0003] The purpose of the present invention is to provide an automatic adjustment system for the center of gravity of an aircraft, which solves the problem of large fluctuations in the position of the center of gravity of the aircraft during the flight of the aircraft in the prior art

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  • Airplane gravity center automatic regulation system and regulating method
  • Airplane gravity center automatic regulation system and regulating method
  • Airplane gravity center automatic regulation system and regulating method

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Embodiment Construction

[0041] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0042] According to the actual modification plan and the requirements of technical indicators and functions, and absorbing the experience in the Y7200B military counterweight system, through analysis and calculation, it is finally determined that the system is composed of the central display control subsystem and the antifreeze balance subsystem. The system hardware structure diagram is as follows figure 1 shown.

[0043] An aircraft center of gravity automatic adjustment system of the present invention includes a central display control subsystem 1 and an antifreeze trim subsystem 2 connected to the central display control subsystem. The central display control subsystem 1 is the core part of the entire system, and the central display control subsystem System 1 includes a control cabinet 3 installed in the aircraft cabin and a center of gravi...

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Abstract

The invention discloses an airplane gravity center automatic regulation system, which comprises a center display control sub system and an antifreezing solution balancing sub system connected with the center display control sub system, wherein the center display control sub system comprises a control cabinet arranged in an airplane passenger cabin and a gravity center display touch screen arranged in a cab; an integral work station, a PLC (programmable logic controller) and an AD (analog-to-digital) conversion module are arranged in the control cabinet; the output end of the PLC is connected with the AD conversion module and is then connected with the integral work station. The invention also discloses a regulation method of the airplane gravity center automatic regulation system. The problem of large airplane gravity center position change range in the airplane flying process in the prior art is solved.

Description

technical field [0001] The invention belongs to the technical field of center-of-gravity adjustment in aircraft type test flight, and in particular relates to an automatic center-of-gravity adjustment system of an aircraft. The invention also relates to an adjustment method of the automatic center-of-gravity adjustment system of an aircraft. Background technique [0002] During the flight of the aircraft, the position of the center of gravity of the aircraft (especially the longitudinal center of gravity) directly affects the maneuverability and stability of the aircraft. Since the two have their own important functions, and their requirements on the center of gravity position are exactly opposite, the position of the center of gravity of the aircraft must be in an appropriate and small range of change. During the flight, the center of gravity of the aircraft often deviates from the safe range due to many factors such as aircraft attitude changes, fuel consumption, external ...

Claims

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Application Information

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IPC IPC(8): G06F17/50B64F5/00
CPCB64F5/00G06F30/15
Inventor 王瑜瑜刘少军叶婷晁林王植
Owner XIAN AERONAUTICAL POLYTECHNIC INST
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