Influence of the Radial Clearance of a Squeeze Film Damper on the Vibratory Behavior of a Single Spool Gas Turbine Designed for Unmanned Aerial Vehicle Applications

<div>Three-dimensional illustration of the cross-section of the developed gas turbine: (a) bipartite mounting of the axial compressor and other inner components; (b) front or cold bearing; and (c) rear or hot bearing.</div>

Shock and Vibration

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Figure 2

Figure 2: Influence of the Radial Clearance of a Squeeze Film Damper on the Vibratory Behavior of a Single Spool Gas Turbine Designed for Unmanned Aerial Vehicle Applications 

Figure 2 | Influence of the Radial Clearance of a Squeeze Film Damper on the Vibratory Behavior of a Single Spool Gas Turbine Designed for Unmanned Aerial Vehicle Applications 