Conceptual Design of a Pressure Vessel |
Author(s): |
| Mr .Kasuba Sainath , Sreyas Institute of Engineering and Technology; Mr. Kacham Nithin, Sreyas Institute of Engineering and Technology; Mr. A. Yuva Kiran Reddy, Sreyas Institute of Engineering and Technology; Mr. G. Sumit, Sreyas Institute of Engineering and Technology; Dr Suresh Akella, Sreyas Institute of Engineering and Technology |
Keywords: |
| Pressurised Air Vessel, Thickness, Cooling, Compressible Liquids, High Pressure, Hemispherical Ends, Design Procedure |
Abstract |
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This discusses the result of the work done in development of a pressure vessel. It is a part of the Aero Space application project going on, and aims at the development of a pressurised air vessel for the purpose of cooling in aero space vehicles. Pressurised Air Vessels are used for storage of gases and compressible liquids at high pressure for a large variety of applications. Ex: Fire extinguishers, air bottles and fuel bottles for catering aerospace propulsion system and seeker cooling system etc. It consists of a shell with a thickness depending upon the material and it also varies with the material stored in it and the pressures acting on it at different temperatures. The design of an air vessel project aims at the development of a design procedure for developing a capsule (cylinder with hemispherical ends). |
Other Details |
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Paper ID: RTIMEP002 Published in: Conference 7 : RTIME-2k16 Publication Date: 01/05/2016 Page(s): 7-12 |
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