* Presentation titles marked with an * indicates the
paper has been Peer Reviewed
Concurrent Session
1D
Critical
Systems Engineering Perspectives for the Development and Implementation of
Enterprise Health Management Solutions
Roger Vodicka,Defence
Science & Technology Organisation,AUSTRALIA
Autonomic
and Sense and Respond Logistics: Evidence from the USA and UK*
Ray Hingst, University Of Southern
Queensland, AUSTRALIA
Overview
of In-situ Environmental Monitoring and Corrosion Sensing Systems for Aircraft
Environmental Degradation Management
Steve Galea, Defence
Science & Technology Organisation, AUSTRALIA
Concurrent Session
1E
The
Minimum Flight Routine for Helicopter Rotor Track and Balance
Nick Lieven, University
of Bristol, UNITED KINGDOM
Rotorcraft
Weight and Center of Gravity Estimation
Nicole Apetre,
Technical Data Analysis Inc, USA
Use
of Artificial Neural Networks for Helicopter Load Monitoring*
Catherine Cheung, National Research Council Canada, CANADA
Concurrent Session 2D
Super
Hornet � F414 Engine Condition Monitoring System (ECMS)
Matthew Williams, TAE, AUSTRALIA
An
Alternative Approach for Setting Wear Debris Limits
Andrew Becker, Defence
Science & Technology Organisation, AUSTRALIA
Enhancing
Propulsion System Condition Monitoring for the RNZAF
Adrian Weller, NZDF,
NEW ZEALAND
Concurrent Session 2E
Implementation
of Structural Health Monitoring for the USMC CH-53E
Jason Thomas, NAVAIR, USA
Flight
Testing of Wireless Sensing Networks for Rotorcraft Structural Health and
Usage Management Systems*
Steven Arms, MicroStrain
�Inc, USA
Structural
Health Monitoring and Damage Detection of the Helicopter
Main Rotor Blades with the Structure Integrated
Sensors
Krzysztof Dragan, Air
Force Institute of Technology, POLAND
Concurrent Session 3D
Spin
Test Monitoring Using Blade Tip Timing Measurement
Wenyi Wang, Defence Science & Technology
Organisation, AUSTRALIA
Optimization
of PHM System for Electronic Assemblies Using Maintenance Aware Design Environment
Software*
Chris Stecki, PHM
Technology, AUSTRALIA
C-130J-30
In-Flight Propeller Balancing System
Brian Rebbechi, Defence
Science & Technology Organisation, AUSTRALIA
Concurrent Session 3E
Using
HUMS Data to Manage the Fatigue Life of Rotorcraft Critical Dynamic Components
David White, Avion Solutions, USA
Integrated
Software Platform for Diagnostics and Prognostics with Air Vehicle HUMS
Carl Byington, Impact Technologies,
USA
MRH 90 HUMS (this paper has been removed)
Ashley Tuck, QinetiQ,
AUSTRALIA
Concurrent Session 4D
KC-30A
SHMS Verification and Validation
Ashley Tuck, QinetiQ,
AUSTRALIA
Non-Destructive
Testing Techniques for Aerospace Applications
Alison Glover, Olympus
Australia, AUSTRALIA
Concurrent Session 4E
A
Systematic Approach to Bearing Health Monitoring
Chris Hickenbottom, Honeywell
Aerospace, AUSTRALIA
Evaluation
of Vibration Based Health Assessment and Diagnostic Techniques for Helicopter
Bearing Components
David Siegel & Jay Lee, US Army Research Lab / University of Cincinnati, USA
Concurrent Session 5D
Enabling
Condition Based Maintenance with Health and Usage Monitoring Systems
Scott Kilby, US AMSAA, USA
Terrain
Regime Identification and Classification for Condition Based Maintenance
Kait Hatton, US AMSAA, USA
The
Role of HUMS in the Evolving Generic Vehicle Architecture
Keith Mowbray, Dytecna Ltd, UNITED KINGDOM
Concurrent Session 5E
Joint
Time Frequency Vibration Diagnostics of Main and Engine Accessory Gearboxes
Carl Byington, Impact Technologies, LLC,
USA
Improved
Simulations of Faults in Gearboxes for Diagnostic and Prognostic Purposes
using a Reduced Finite Element Model of the Casing*
Nader Sawalhi, University
of New South Wales, AUSTRALIA
Detachable
Acoustic Electric Feedthrough for In Situ SHM Systems
Jeremy Skippen, Defence
Science & Technology Organisation, AUSTRALIA
Concurrent Session 6D
Next
Generation Data Acquisition Technologies for Aging Aircraft*
Niall Heffernan, ACRA
CONTROL, IRELAND
The
AUSAM System for Fatigue Crack Monitoring in a Wing Skin:A
Case Study
Cedric Rosalie, Defence
Science & Technology Organisation, AUSTRALIA
Slotted
Circular Microstrip Patch Antenna Application in Strain Based Structural Health
Monitoring*
Ali Daliri, RMIT University, AUSTRALIA
Concurrent Session 6E
Maneuver/Regime
Recognition Validation & Verification Using Visualization Technique
Suresh Moon, Air Vehicle Engineering,
L-3 Communications, USA
The Dutch Approach to Force Life Management (FLM)
Issues
Lex ten Have & Arjen Vollebregt, NLR, THE NETHERLANDS [Paper not available
at time of printing]
Replacing
Obsolete Equipment For Drivetrain Health Monitoring On RAN Sea King Helicopters
Paul Marsden, Defence Science &
Technology Organisation, AUSTRALIA