Simulation-Based Study on the Dynamics of Wing-Flap Actuating Hydraulic Circuit

Author:

Gronczewski Andrzej1

Affiliation:

1. Wroclaw University of Technology

Abstract

Modern air transportation systems prove to be of numerous advantages, but there is always a risk of an air accident. Air accidents occur for many and various reasons. The group of aircraft accidents due to engineering causes, includes events directly resulting from the malfunctioning of the hydraulic circuit that controls high-lift devices. In this paper presented is a mathematic model of dynamic behaviour of a wing flap system, which has been intended to enable simulation tests with account taken of operation-induced failures/damages. Major emphasis has been put on analyses of the simulation-tested dynamics of a flap-driving hydraulic circuit, with account taken of the following defects: changes in compressibility of hydraulic fluid, internal leakages in the hydraulic cylinder, external leaks of hydraulic fluid.

Publisher

Trans Tech Publications, Ltd.

Subject

Condensed Matter Physics,General Materials Science,Atomic and Molecular Physics, and Optics

Reference11 articles.

1. Błachnio J.: An investigation into damages/failures to aircraft while in operation. The problems of studying and operating aeronautical systems. Air Force Institute of Technology, Warszawa (1993).

2. Borowczyk H.: Non-logarithmic probabilistic rates of the object condition's uncertainty and the diagnostic symptoms' informativity. 6th IFAC Symposium, Beijing, China – Amsterdam, Elsevier 2007, pp.493-498.

3. Gronczewski A.: Statistical Approach to Flight Safety - Journal of Transdisciplinary System Science, Vol. 9, (2004).

4. Gronczewski A.: Modelling of Hydraulic System for Aircraft Wing Mechanics under Occurrence of Disturbances. Doctor's thesis. Air Force Institute of Technology, Warszawa (2007).

5. Gronczewski A. Błachnio J.: Modelling of dynamic behavior attributable to the two-output hydraulic system for driving mechanisms of aircraft wings. Research Works of Air Force Institute of Technology. No. 21, (2007).

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