A STUDY ON A TRANSDUCER-STEPPED TYPE SOLID HORN SYSTEM FOR FLEXURAL MODE ULTRASONIC HIGH POWER TRANSDUCER WITH ONE DIMENSIONAL CONSTRUCTION

Author(s):  
Yuji Watanabe ◽  
Yoneo Tsuda ◽  
Eiji Mori
2020 ◽  
Vol 2020 (12) ◽  
Author(s):  
V.Y. Rodyakin ◽  
◽  
V.M. Pikunov ◽  
V.N. Aksenov ◽  
◽  
...  

We present the results of a comparative theoretical analysis of the electron beam bunching in a single-stage klystron amplifier using analytical models, a one-dimensional disk program, and a two-dimensional program. Data on the influence of various one-dimensional and two-dimensional nonlinear effects on the efficiency of electron beam bunching at different values of the space charge parameter and the modulation amplitude are presented. The limits of applicability of analytical and one-dimensional numerical models for electron beam bunching analysis in high-power klystron amplifiers are found.


2021 ◽  
Vol 41 (2) ◽  
pp. 1270-1279 ◽  
Author(s):  
Beecher H. Watson ◽  
Michael J. Brova ◽  
Mark Fanton ◽  
Richard J. Meyer ◽  
Gary L. Messing
Keyword(s):  

2017 ◽  
Vol 129 (42) ◽  
pp. 13120-13125 ◽  
Author(s):  
Yifan Xu ◽  
Peining Chen ◽  
Jing Zhang ◽  
Songlin Xie ◽  
Fang Wan ◽  
...  

1976 ◽  
Vol 60 (3) ◽  
pp. 734-740 ◽  
Author(s):  
S. E. Auyer ◽  
W. A. Miller
Keyword(s):  

1975 ◽  
Vol 58 (S1) ◽  
pp. S81-S81
Author(s):  
W. A. Miller ◽  
S. E. Auyer
Keyword(s):  

Author(s):  
Chris Freeman ◽  
Arthur L. Rowe

An engine experiment has been carried out to investigate Fan Stability and response to ambient wind conditions during static high power running of a modern large turbofan engine. This paper describes the experiment and the conclusions. Intermittently the inlet would separate and drive the fan into stall from which it did not recover when the inlet cleared up: on high working lines one inlet separation could stall the fan; on lower working lines the inlet separation / fan flow / bypass duct pressure would develop a divergent 10Hz oscillation which could eventually stall the fan. The interaction of the stalled fan with the turbine and mixed nozzle would then raise the fan running line above the stall dropout level thus locking the fan into stall even when the inlet cleared up. A one dimensional dynamic model of the engine was created that would exhibit similar behaviour to the engine when a delay was introduced between the inlet loss and fan face loss. The engine never showed steady operation with the inlet separated.


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