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Magneto-Rheological (MR) Damper for Landing Gear System

TLDR
In this article, the authors focused on modeling of a MR damper for landing gear system and analysis of semi-active controller to attenuate dynamic load and landing impact, and developed a PID controller to reduce the acceleration of the system.
Abstract
Depending on the different sink speeds, angles of attack and masses; aircraft landing gears could face a wide range of impact conditions which may possibly cause structural damage or failure. Thus, in hard landing scenarios, the landing gear must absorb sufficient energy in order to minimize dynamic stress on the aircraft airframe. Semi-active control systems are the recent potential solutions to overcome these limitations. Among semi-active control strategies, those based on smart fluids such as magneto-rheological (MR) fluids have received recent attraction as their rheological properties can be continuously controlled using magnetic or electric field and they are not sensitive to the contaminants and the temperature variation and also require lower powers. This thesis focuses on modeling of a MR damper for landing gear system and analysis of semi-active controller to attenuate dynamic load and landing impact. First, passive landing gear of a Navy aircraft is modeled and the forces associated with the shock strut are formulated. The passive shock strut is then integrated with a MR valve to design MR shock strut. Here, MR shock strut is integrated with the landing gear system modeled as the 2DOF system and governing equations of motion are derived in order to simulate the dynamics of the system under different impact conditions. Subsequently the inverse model of the MR shock strut relating MR yield stress to the MR shock strut force and strut velocity is formulated. Using the developed governing equations and inverse model, a PID controller is formulated to reduce the acceleration of the system. Controlled performance of the simulated MR landing gear system is demonstrated and compared with that of passive system

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MAGNETO-RHEOLOGICAL (MR) DAMPER FOR
LANDING GEAR SYSTEM
Mahboubeh Khani
A Thesis
in
the Department
of
Mechanical and Industrial Engineering
Presented in Partial Fulfillment of
the
Requirements
for the Degree of Master of Applied Science (Mechanical Engineering) at
Concordia University
Montreal, Quebec, Canada
June 2010
© Mahboubeh Khani, 2010

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ABSTRACT
Magneto-Rheological (MR) Damper for Landing Gear System
Mahboubeh Khani
Depending on the different sink speeds, angles of attack and masses; aircraft
landing gears could face a wide range of impact conditions which may possibly cause
structural damage or failure. Thus, in hard landing scenarios, the landing gear must
absorb sufficient energy in order to minimize dynamic stress on the aircraft airframe.
Semi-active control systems are the recent potential solutions to overcome these
limitations. Among semi-active control strategies, those based on smart fluids such as
magneto-rheological (MR) fluids have received recent attraction as their rheological
properties can be continuously controlled using magnetic or electric field and they are not
sensitive to the contaminants and the temperature variation and also require lower
powers.
This thesis focuses on modeling of a MR damper for landing gear system and
analysis of semi-active controller to attenuate dynamic load and landing impact. First,
passive landing gear of a Navy aircraft is modeled and the forces associated with the
shock strut are formulated. The passive shock strut is then integrated with a MR valve to
design MR shock strut.
Ill

Here, MR shock strut is integrated with the landing gear system modeled as the
2DOF system and governing equations of motion are derived in order to simulate the
dynamics of the system under different impact conditions. Subsequently the inverse
model of the MR shock strut relating MR yield stress to the MR shock strut force and
strut velocity is formulated. Using the developed governing equations and inverse model,
a PID controller is formulated to reduce the acceleration of the system. Controlled
performance of the simulated MR landing gear system is demonstrated and compared
with that of passive system.
IV

ACKNOWLEDGMENTS
First, I would like to pay my great appreciation to my supervisors, Dr. Ion Stiharu and Dr.
Ramin Sedaghati for their endless amount of moral support and encouragement along
with their practical opinions throughout the thesis work.
The financial support by Mechanical and Industrial Engineering Department of
Concordia University is acknowledged.
I also would like to extend my thanks to my colleagues, MR. Arash Firoozrai and MR.
Amin Changizi, for their collaborations.
Finally, I would like to dedicate this thesis to my beloved husband, Majid Fekri, my
parents, Masi Hassan zadeh and Eino Khani and my sisters, Marzi, Leila and Zara Khani
who have always been there for me throughout my life with their love, support, advice
and encouragement.
V

Citations
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Journal ArticleDOI

Preliminary experimental evaluation of a novel loudspeaker featuring magnetorheological fluid surround absorber

TL;DR: In this article, a magnetorheological fluid (MRF) based surround device for a loudspeaker system was proposed to predict the change of shear yield stress, which can be easily manipulated at a different sound source by applying a magnetic field.
Dissertation

Robust Semi-active Control of Aircraft Landing Gear System Equipped with Magnetorheological Dampers

TL;DR: In this article, a semi-active magnetorheological (MR) suspension system was developed for a three degree-of-freedom (3 DOF) aircraft model considering a tri-cycle landing gear configuration, and two different controller approaches, namely, the Linear Quadratic Regulator (LQR) and the H∞ control are adopted.
Journal Article

Conceptual Design of Single-Acting Oleo-Pneumatic Shock Absorber in Landing Gear with Combined Method

TL;DR: In this paper, the authors studied the relationship arising from oil and gas liquids in the case of practical modes of isotherms during taxi and poly trophic during landing and the results of the extracted relations using numerical methods compared with practical results showed that not only the force on the aircraft body but also the vibrations on it have been significantly reduced and improved system performance.

An electric control for an electrohydraulic active control aircraft landing gear

I. Ross, +1 more
TL;DR: In this paper, an electronic controller for an electrohydraulic active control aircraft landing gear was developed and drop tests of a modified gear from a 2722 Kg (6000 lbm) class of airplane were conducted to illustrate controller performance.
References
More filters
Journal ArticleDOI

Induced Fibration of Suspensions

TL;DR: In this article, the authors describe some of the phenomena found to have their origin in electrically induced fibration of small particles in fluid liquid suspension, including the induced shear resistances found in layers of the fluid when bounded by potentialized electrode surfaces.

Phenomenological Model of a Magnetorheological Damper

TL;DR: In this article, a new model for controllable fluid dampers is proposed that can effectively portray the behavior of a typical magnetorheological damper and compared with experimental results for a prototype damper indicates that the model is accurate over a wide range of operating conditions.
MonographDOI

Aircraft landing gear design principles and practices

TL;DR: In this paper, the authors provide a link in landing gear technology from historical practices to modern design trends, also considering the necessary airfield interface with gear design, and lead students and engineers from the initial concepts of landing gear design through to the final detail design.
Journal ArticleDOI

Dynamic mechanical studies of electrorheological materials: Moderate frequencies

D. R. Gamota, +1 more
- 01 Apr 1991 - 
TL;DR: In this paper, an ER material composed of alumino-silicate particles in paraffin oil is studied for its response to sinusoidally oscillating shear strains at frequencies in the range of 10-50/s.
Journal ArticleDOI

Nondimensional analysis of semi-active electrorheological and magnetorheological dampers using approximate parallel plate models

TL;DR: In this article, the authors developed nonlinear quasi-steady electrorheological and magnetorheological damper models using an idealized Bingham plastic shear flow mechanism, where damping forces are developed in an annular bypass via Couette (shear mode), Poiseuille (flow mode) flow, or combined Couette and Poiseiulle flow (mixed mode).