H-53E Super Stallion/Sea Dragon Auxiliary Power Plant Power Survey
Date Issued
May 1, 2004
Author(s)
Twomey, Patrick Joseph
Advisor(s)
Robert B. Richards
Additional Advisor(s)
Paul Solies
Ted Paludan
Abstract
This research has provided possible explanations to failures experienced in the P-7-2 Auxiliary Power Plant reduction gearbox as installed on the CH-53E Super Stallion and MH-53E Sea Dragon helicopters. Ground testing with the rotors static was conducted during two separate phases from March 1995 to December 1995. Reduction gearbox loading was measured, resulting in the identification of several detrimental over and transient loads. Loading reduction techniques are investigated, discussed, and/or evaluated for U.S. Navy and U.S. Marine Corps fleet introduction viability.
Disciplines
Degree
Master of Science
Major
Aviation Systems
Embargo Date
May 1, 2004
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Name
TwomeyPatrickJoseph.pdf
Size
902.18 KB
Format
Adobe PDF
Checksum (MD5)
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