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Out of Area Experiences With the RB199 in TorontoThe Turbo Union RB 199 engine was developed during the late 1960's / early 1970's to meet a specification requirement aimed at defense of the Western European NATO alliance countries against the (then) perceived threat. During the latter part of the 1980's Tornado aircraft were delivered to the Royal Saudi Air Force and, supplemented by deployed units from the Royal Air Force, were engaged in an operational role during 1990 / 1991. Aircraft operations in the Saudi Arabia climates and natural environment created problems with engine life, hitherto not encountered in the European area of operation, nor during many RAF overseas deployments, including North America. These problems, mainly concerned with turbine blade contamination from airborne sand, were alleviated by the introduction of unique engine maintenance management techniques and eliminated by design changes.
Document ID
19950013238
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
M G Down
(Rolls-Royce (United Kingdom) London, United Kingdom)
M J Williams
(Rolls-Royce (United Kingdom) London, United Kingdom)
Date Acquired
August 16, 2013
Publication Date
November 1, 1994
Publication Information
Publication: Erosion, Corrosion and Foreign Object Damage Effects in Gas Turbines
Publisher: North Atlantic Treaty Organization
ISBN: 9283600053
Subject Category
Aircraft Propulsion and Power
Report/Patent Number
AGARD-CP-558
Meeting Information
Meeting: Propulsion and Energetics Panel (PEP) Symposium
Location: Rotterdam
Country: NL
Start Date: April 25, 1994
End Date: April 28, 1994
Sponsors: North Atlantic Treaty Organization
Accession Number
95N19654
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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