• 热门标签

当前位置: 主页 > 航空资料 > 国外资料 >

时间:2010-08-15 08:53来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

Loma del Bosque 115, Leon, Gto. Mexico 37150
Phone: +52 477 441 42 00 Fax: +52 477 441 42 09, OFS-18@osa.org
Special Session
30th Anniversary of FOG
Invited talks:
Dr. HC Lefevre
iXCore S.A.S., France
" Reciprocity and Serendipity: the Early Development of FOG Architecture and Signal Processing"
Dr. Bill Burns
Photonics Inc., USA
"The Impact of Component Development on the Evolution of the Fiber Optic Gyroscope"
Prof. Shaoul Ezekiel
Afilician MIT, USA
"Optical Gyroscope Options: Principles and Challenges"
Dr Sudhakar Divakaruni and Dr Glen Sanders
Honeywell International, USA
“Fiber Optic Gyros – A Compelling Choice For High Precision Applications”
Dr Kalyan Ganesan et al.
KVH Industries, USA
"Advances in Open-loop FOG Sensors"
Dr George Pavlath
Northrop Grumman Corp., USA
"Fiber Optic Gyros, the Vision Realized"
Prof. Kazuo Hotate et al.
University of Tokyo, Japan
"Applications and Technical Progress of Fiber Optic Gyros in Japan"
Dr E.J. Friebele
Naval Research Laboratory, USA
"Development of Radiation Hard Fiber for IFOGs"
Dr. Liming Wang and Dr. Thomas Monte
KVH Industries, USA
"All Fiber Replaced Optical Cladding Phase Modulator for FOG applications and beyond"
Dr Steve Sanders and Dr Steve Smith
Honeywell International and Charles Stark Draper Laboratories, USA
"Volume production of Nav-grade, Depolarized Fiber Gyros"
Drs. J. Honthaas, T. Buret, Y. Paturel, T. Gaiffe
IXSea, France
"High performance FOG : one design, still no limit !?"
Drs. M. J. F. Digonnet, S. Blin, V. Dangui, Y. K. Kim G. S. Kino
Edward L. Ginzton laboratory, Stanford University, USA
"Sensitivity and stability of an air-core fiber-optic gyroscope"
Drs. T. Buret, J. Honthaas, D. Ramecourt, E. Willemenot, T. Gaiffe
IXSea, France
"FOG technology opens the way for the 21st century space gyros"
OFS-18 Secretariat, Centro de Investigaciones en Optica (CIO)
Loma del Bosque 115, Leon, Gto. Mexico 37150
Phone: +52 477 441 42 00 Fax: +52 477 441 42 09, OFS-18@osa.org
Special Workshop (Monday session)
Structural Health Monitoring (SHM)
SHM Tutorial by:
Prof. John Newhook
Dalhousie University, Canada
SHM Workshop Invited Talks:
Prof. Farhad Ansari
Univ. Illinois at Chicago, USA
“The Use of FOS in Civil Applications: A Retrospective”
Prof. Aftab Mufti
U. Mannitona, Canada
ISIS Canada
“Optical Fiber Sensors and Civionics”
Dr. Wolgang Habel
BAM, Germany
“Reliability Aspects of Fiber Sensors for SHM Applications”
Dr. Jinping Ou
Harbin Institute of Technology, China
“FO Bridge Monitoring Activities in China”
Prof. Chung Yue Wang
National Central University, Taiwan
“Structural Health Monitoring Activities in Taiwan”
Dr. Jose Manual Menendez
AIRBUS, Spain
“SHM using Fiber Sensors in Aerospace Applications”
Vol. 5
May Issue
Year 2004
Publication for the
Peening, Blasting and
Vibratory Finishing
Industries
www.mfn.li
The MFN
Trainer Column:
Peening in the Age of
Damage Tolerance
page 34
The Shot
Peening Process:
Developing Prediction
page 32-33
One of the World's Largest Shot Peening Machines at Airbus
4th Asian
Shot Peening
Workshop
8-10th Nov 2004
page 15
SCIENCE UPDATE:
Fatigue Response of
the Various Titanium
Alloy Classes to
Shot Peening
page 38-40
Separate Print: Vol. 5
May Issue
Year 2004
"One of the World's Largest Shot
Peening Machines installed at Airbus"
Peening
Airbus Innovation for A 380: Laser-
Beam Welding
A major challenge in aircraft design is
saving weight and therefore reducing
fuel consumption and airline operating
costs. Airbus, an EADS joint company
with BAE SYSTEMS, has developed a
number of new technologies, i.e. new
materials, new structural designs and
new manufacturing processes in order
to meet these challenges. These innovations
and new technologies will
be incorporated in the A 380 family,
which is the Airbus flagship for the
21st century.
Integral structures for aircraft fuselage
today consist of aluminium sheets and
stringers, whereby innumerable rivets
are needed as joints. However, Airbus
has recently used laser-beam welded
structures instead of rivets for A 318
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:航空翻译14(195)