Recently Downloaded: Paper ID: ART20203027, Total 1958 Articles Downloaded Today
Unbalance Response Analysis of Twin Spool Aero-Gas Turbine EngineMegha Mohan, Shruthi Raj, Disa Jaison Abstract: Twin spool Aero-gas turbine engine is rotating equipment having two rotors called low pressure (LP) Spool and high pressure (HP) Spool. The rotors are mainly assembly of axial flow compressor and axial turbine connected by shaft. The rotors are designed to rotate at wide range of rotational speeds to meet operational requirement. During this regime of speeds, rotor mechanical behavior is very critical in terms of its vibratory behavior. The vibratory behavior of rotor is analyzed by specialized technique called Rotor dynamics. In brief, rotor dynamics computes critical unbalance response of rotor. Keywords: Twin spool, whirling, rotordynamics, steady state response Country: India, Subject Area: Aerospace Engineering Pages: 1681 - 1686 Edition: Volume 8 Issue 5, May 2019 How to Cite this Article? Megha Mohan, Shruthi Raj, Disa Jaison, "Unbalance Response Analysis of Twin Spool Aero-Gas Turbine Engine", International Journal of Science and Research (IJSR), https://www.ijsr.net/archive/v8i5/show_abstract.php?id=ART20198171, Volume 8 Issue 5, May 2019, 1681 - 1686 Download PDF![]() |
Viewed 67 times.
Downloaded 27 times.