Optimization Of Pressure Vessel Using A Composite Material. DEEPAK THOMAS. 1, COLIN JOHNSON2, SARATH KRISHNA3,N.SIVASELVA KUMAR 4 Department of Aeronautical Engineering Park College Of Technology. ![]() Recent advances in lightweight, filament-wound composite pressure vessel technology NTRS Full-Text: [PDF Size: 4.7 MB] Author and Affiliation: Lark, R. (NASA Lewis Research Center, Cleveland, OH, United States) Abstract: A review of recent advances is presented for lightweight, high performance composite pressure vessel technology that covers the areas of design concepts, fabrication procedures, applications, and performance of vessels subjected to single cycle burst and cyclic fatigue loading. Filament wound fiber/epoxy composite vessels were made from S glass, graphite, and Kevlar 49 fibers and were equipped with both structural and nonstructural liners. Pressure vessels structural efficiencies were attained which represented weight savings, using different liners, of 40 to 60 percent over all titanium pressure vessels. Significant findings in each area are summarized. ![]() Publication Date: Sep 22, 1977 Document ID. (Acquired Nov 18, 1995) Accession Number: 77N33265 Subject Category: COMPOSITE MATERIALS Report/Patent Number: NASA-TM-73699, E-9239 Document Type: Conference Paper Publisher Information: United States Meeting Information: 1977 Energy Conf.; 18-23 Sep. Microsoft excel mac for free. 1977; Houston, TX; United States Meeting Sponsor: ASME Financial Sponsor: NASA; United States Organization Source: NASA Lewis Research Center; Cleveland, OH, United States Description: 34p; In English Distribution Limits: Unclassified; Publicly available; Unlimited Rights: No Copyright NASA Terms: FILAMENT WINDING; PRESSURE VESSEL DESIGN; PRESSURE VESSELS; TECHNOLOGY UTILIZATION; COMPOSITE WRAPPING; CYCLIC LOADS; LOADS (FORCES); METAL FIBERS; PERFORMANCE TESTS Imprint And Other Notes: Presented at the 1977 Energy Conf., Houston, Tex., 18-23 Sep. 1977; sponsored by ASME.
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