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A Small Disturbance Stability Analysis Method for Aircraft Power System Based on Generalized State Space Averaging

A state-space averaging and power system technology, applied in the direction of electrical digital data processing, special data processing applications, instruments, etc., can solve problems such as economic loss and stability damage

Inactive Publication Date: 2017-11-14
CIVIL AVIATION UNIV OF CHINA
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] With the B787, A380 and other multi-electric aircrafts put into use, more and more attention has been paid to the safe and stable operation of the aircraft power system. Once its stability is damaged, it will cause huge economic losses and catastrophic consequences.

Method used

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  • A Small Disturbance Stability Analysis Method for Aircraft Power System Based on Generalized State Space Averaging
  • A Small Disturbance Stability Analysis Method for Aircraft Power System Based on Generalized State Space Averaging
  • A Small Disturbance Stability Analysis Method for Aircraft Power System Based on Generalized State Space Averaging

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Embodiment

[0059] In this embodiment, based on a power system of a multi-electric aircraft, a generalized state-space average model is established and small-disturbance stability analysis is performed. figure 2 This is a schematic diagram of the power system structure of a multi-electric aircraft including specific links, assuming that the adjustment speed of the GCU is fast enough, so the alternator can be replaced by an AC 400Hz regulated AC power supply, and the electric actuation system can be replaced by a constant power load. The remaining components include: Transmission lines, transformer rectifiers, DC filter capacitors. R eq , L eq ,C eq Respectively, line and transformer equivalent resistance, reactance, capacitance.

[0060] 1) According to the simplified structure diagram of the multi-electric aircraft power system, convert the DC side circuit to the AC side, and get image 3 The single-line diagram of the AC-DC mixed power flow calculation of the aircraft power system ...

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Abstract

The invention relates to a small-disturbance stability analysis method for an aircraft power system based on generalized state space averaging. Based on the equivalent circuit of the generalized state space average modeling of the aircraft power system, the nonlinear differential equation of the aircraft power system is obtained; the state variables of the nonlinear differential equation are determined, and the generalized state space described by Fourier coefficients is obtained through Fourier decomposition Average model; according to the model, it is calculated and processed to judge the small disturbance stability of the aircraft power system. The effect of the invention is that the method realizes the small disturbance stability analysis under different dynamics of the aircraft power system, can realize the sensitivity analysis of the small disturbance stability, provides valuable suggestions for the design and improvement of the power system in the manufacture of large aircraft, and can be used by the crew at the same time Provide reliable aircraft electrical system operating information.

Description

technical field [0001] The present invention relates to a small-disturbance stability analysis method for an aircraft power system, in particular to a small-disturbance stability analysis method for an aircraft power system based on generalized state space averaging. Through state matrix analysis using Fourier coefficients as state variables, the Realize accurate small-disturbance stability determination of aircraft power system. Background technique [0002] In order to save energy, reduce costs and improve the performance of airborne systems, modern aircraft increasingly use electric energy to replace hydraulic and pneumatic energy on traditional aircraft, that is, replace the mechanical, hydraulic and pneumatically driven loads directly driven by the engine with electric drives load. The concept of "More Electric Aircraft" thus proposed has become the mainstream trend in the development of the aircraft industry. With the development and maturity of more electric aircraf...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F17/50
Inventor 杨占刚赵宏旭荆涛徐萌石旭东
Owner CIVIL AVIATION UNIV OF CHINA
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