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ultimately enable major design and process changes
creating the opportunity for considerable cost savings for
the aerospace industry. Future structures could be
designed with fewer and smaller access panels and
maintenance times could be reduced.
This paper presents early stage results of the
demonstration snake-arm robot and outlines
expectations for future development. The paper
identifies critical design parameters for the snake-arm
and considers the tools and processes to be delivered
by the snake-arm.
REFERENCES
1. “Robot capability test and development of industrial
robot positioning system for the aerospace industry”,
Summers M., 2005 Transactions Journal of
Aerospace, p1108
2. "Snake-arm robots - a new tool for the aerospace
industry", Buckingham R. & Graham A., Aerofast
2003, Palais des Congrès, Montreal, Quebec,
Canada, September 2003
3. “Kinematics for Multi-Section Continuum Robots”,
Jones B. & Walker I.D., IEEE Transactions on
Robotics, Vol. 22, No. 1, February 2006, pp. 45-53.
4. "Snaking around in a nuclear jungle", Buckingham
R. & Graham A., Int. J. Industrial Robot, Vol. 32, No.
2, p120-127, 2005, ISSN 0143-991X
CONTACT
Rob Buckingham: OCRobotics, Unit 5, Abbey Wood
Business Park, Filton, Bristol BS34 7JU, UK;
rob@ocrobotics.com; www.ocrobotics.com
Comparative Vacuum Monitoring
CVMTM
Andrew Chilcott
Structural Monitoring Systems Ltd
Perth, Australia
Tel: +61 8 9204 4844, Fax: +61 8 9204 4866
a.chilcott@smsystems.com.au
www.smsystems.com.au
Outline
• What is CVMTM? / How does it work?
• Development background / early applications
• Application to Automotive industry
What is CVMTM ?
Vacuum
source
Flow meter or
Pressure switch
Sensor
How does it work?
Operating Modes
CVM
Continuous Periodic
Monitor Switch
More efficient Testing More efficient NDI
•Complex networks
•Real time monitoring •Automatic control •Less strip / rebuild
Development
• 1994 inventor, Ken Davey files CVM patent
• 2002 First installation on operating aircraft for US Navy (H53).
• 2004 CVM™adopted by Airbus for A380 full scale fatigue testing
• 2005 CVM™ trials – ADF Black Hawk; RN Sea King; RAF Nimrod, RAF
Harrier II.
• 2005 Airbus In-flight CVM™Joint Development Agreement
• 2005 License agreement with Boeing for CVM™use on commercial aircraft
• 2005 Pilot trial with PBR automotive brake manufacturer
• 2006 Completion of Boeing SPM program / Completion of DSTO trials –
(Australian military Director General )
• 2006 Development of low cost CV Switch for fatigue test automation
Military Aircraft
Airbus JDA
Boeing NDT SPM
•2006: CVM included in Standard Practice Manual
•2007: CVM as AMOC for several SB 737inspections
CV Switch
•Quality control testing
•Developmental testing
•Small Crack detected in real time
•Appropriate action automated
- test stopped
- alarm (light/sound) triggered
- signal sent
Quicker, More Accurate, Less labor intensive testing

　
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