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Lessons Learned - Altitude Exhausters

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:47:10Z
date available2017-09-04T18:47:10Z
date copyright07/08/1993
date issued1993
identifier otherAMZCQCAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsessionid=3826AF679D40527318548F1EFDEC014A/handle/yse/228373
description abstractDescription of Driving Event:
Exhausters were running to provide simulation of altitude conditions in a combustor rig when the mishap occurred. The equipment operators were short-handed and, as a result, a certain amount of confusion existed. A valve at the discharge end of the exhausters was inadvertently closed. The reduced flow caused the inlet pressure to rise because a continuous quantity of air was being supplied to the exhauster inlet from the compressors in the system. As a result, the pressure at the exhauster inlet increased to almost atmospheric. The exhausters then became compressors and generated a discharge pressure level high enough to rupture the inverted, dished head of the exhauster header located 50 feet downstream. The inverted, dished head was 8 feet in diameter and 3/8 inches thick located 16 inches underneath the floor level. A hole about 30 feet in diameter was blown in the roof of the building located 35 feet above the floor level. A large number of windows were broken and the reinforced concrete floor in the vicinity of the rupture was destroyed.
languageEnglish
titleNASA-LLIS-0238num
titleLessons Learned - Altitude Exhaustersen
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1993
contenttypefulltext
subject keywordsFacilities
subject keywordsIndustrial Operations
subject keywordsPressure Vessels


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