Study on a Low-Noise Current Collector and the Aerodynamics Using a Delta-Wing-Shaped Collector Head
In the low-noise current collector using a delta-wing-shaped collector head in which the aerodynamics becomes quite large, it is desired to develop an active control using a force actuator. This paper deals with the numerical calculations of aerodynamics generated by a delta-wing-shaped collector he...
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Published in | Transactions of the Japan Society of Mechanical Engineers Series C Vol. 63; no. 611; pp. 2278 - 2286 |
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Main Authors | , , , , |
Format | Journal Article |
Language | Japanese |
Published |
The Japan Society of Mechanical Engineers
1997
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Subjects | |
Online Access | Get full text |
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Summary: | In the low-noise current collector using a delta-wing-shaped collector head in which the aerodynamics becomes quite large, it is desired to develop an active control using a force actuator. This paper deals with the numerical calculations of aerodynamics generated by a delta-wing-shaped collector head and a pair of insulators. A variation lift was verified to generate clear in the experiment results of high-speed test train with a full size prototype current collector. The conclusions of this research using a new current collector are as follows;(1) In the simulation result of an active control generated the average lift at 160 N, it was verified that the contact strip has same characteristics of contact force at max. 70 N as the conventional one.(2) The variation lift of the collector head at 350 km/h is expected to be 80 N lower than that before improvement. |
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ISSN: | 0387-5024 1884-8354 |
DOI: | 10.1299/kikaic.63.2278 |