Study on high speed traction drive CVT for aircraft power generation (Analysis of ratio-changing response)-Reference-Cited by-同舟云学术

Study on high speed traction drive CVT for aircraft power generation (Analysis of ratio-changing response)

Published:2018 Issue:861 Volume:84 Page:17-00472-17-00472
ISSN:2187-9761
Container-title:Transactions of the JSME (in Japanese)
language:en
Short-container-title:

Author:

MATSUDA Kippei¹,TANAKA Kenichiro¹,IMAI Hideyuki¹,GOI Tatsuhiko¹,SATO Yasukazu²,TANAKA Hirohisa²

Affiliation:

1. Kawasaki Heavy Industries, Ltd.

2. Yokohama National University

Publisher

Japan Society of Mechanical Engineers

Link

https://www.jstage.jst.go.jp/article/transjsme/84/861/84_17-00472/_pdf

Reference4 articles.

1. Goi, T., Tanaka, H., Nakashima, K. and Watanabe, K., Study on Stability of High Speed Traction Drive CVT for Aircraft Generator, Journal of the Japan Society for Aeronautical and Space Sciences, Vol.58, No.678 (2010), pp. 203-209 (in Japanese).

2. Matsuda, K., Goi, T., Tanaka, K., Imai, H., Tanaka, H. and Sato, Y., Study on high speed traction drive CVT for aircraft power generation - Gyroscopic effect of the thrust ball bearing on the CVT - , Journal of Advanced Mechanical Design, Systems, and Manufacturing, Vol.11, No.6 (2017), Paper No. 17-00390.

3. Miyata, S. and Liu, D., Study of the control mechanism of a half-toroidal CVT during load transmission, Journal of Advanced Mechanical Design, Systems, and Manufacturing, Vol.1, No.3 (2007), pp. 346-357.

4. Tanaka, H. and Eguchi, M., Speed ratio control of a half-toroidal traction drive CVT, Transactions of the Japan Society of Mechanical Engineers, Series C, Vol.57, No.543 (1991), pp. 3682-3685 (in Japanese).

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