DocumentCode
2408312
Title
Fly-by-light aircraft system cable plants
Author
Weaver, Thomas L.
Author_Institution
McDonnell Douglas Corp., St. Louis, MO, USA
Volume
2
fYear
1997
fDate
26-30 Oct 1997
Firstpage
7.3
Abstract
A program was completed with joint industry and government funding to apply fiber optics to aircraft. The technology offers many potential benefits. Among them are increased electromagnetic interference immunity and the possibility of reduced weight, increased reliability, and enlarged capability by redesigning architectures to use the bandwidth of fiber optics. Those benefits can be realized if fiber optics meets the requirements of aircraft networks. The Fly-by-Light Advanced System Hardware (FLASH) program expanded on previous cable plant efforts by building components based on a cohesive aircraft cable plant system concept. The concept was rooted in not just optical performance, but also cost, manufacturing installation, maintenance, and support. To do that, the FLASH team evaluated requirements, delineated use conditions, designed, built, and tested fiber optic components, for transport aircraft, tactical aircraft, and helicopters. In addition, the FLASH team developed installation and test methods, and support equipment for aircraft optical cable plants. The results of the effort are reported here
Keywords
aircraft control; aircraft instrumentation; interference suppression; optical cables; optical fibre couplers; AVMAC connector; FLASH; FLOAT; cost; electromagnetic interference immunity; fiber optics; fly-by-light aircraft; helicopters; maintenance; manufacturing installation; optical performance; tactical aircraft; transport aircraft; Aerospace industry; Aircraft manufacture; Bandwidth; Buildings; Electromagnetic interference; Government; Hardware; Optical fiber cables; Optical fibers; Telecommunication network reliability;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference, 1997. 16th DASC., AIAA/IEEE
Conference_Location
Irvine, CA
Print_ISBN
0-7803-4150-3
Type
conf
DOI
10.1109/DASC.1997.637237
Filename
637237
Link To Document