High Speed Pneumatic Theory and Technology Volume I Servo System
This book covers the author’s research achievements and the latest advances in high-speed pneumatic control theory and applied technologies. It presents the basic theory and highlights pioneering technologies resulting from research and development effort
- PDF / 14,307,047 Bytes
- 370 Pages / 453.544 x 683.151 pts Page_size
- 28 Downloads / 184 Views
High Speed Pneumatic Theory and Technology Volume I Servo System
High Speed Pneumatic Theory and Technology Volume I
Yaobao Yin
High Speed Pneumatic Theory and Technology Volume I Servo System
123
Yaobao Yin School of Mechanical Engineering Tongji University Shanghai, China
ISBN 978-981-13-5985-9 ISBN 978-981-13-5986-6 https://doi.org/10.1007/978-981-13-5986-6
(eBook)
Jointly published with Shanghai Scientific and Technical Publishers, Shanghai, China The print edition is not for sale in China Mainland. Customers from China Mainland please order the print book from: Shanghai Scientific and Technical Publishers. Library of Congress Control Number: 2018966830 © Springer Nature Singapore Pte Ltd. and Shanghai Scientific and Technical Publishers 2019 This work is subject to copyright. All rights are reserved by the Publisher, whether the whole or part of the material is concerned, specifically the rights of translation, reprinting, reuse of illustrations, recitation, broadcasting, reproduction on microfilms or in any other physical way, and transmission or information storage and retrieval, electronic adaptation, computer software, or by similar or dissimilar methodology now known or hereafter developed. The use of general descriptive names, registered names, trademarks, service marks, etc. in this publication does not imply, even in the absence of a specific statement, that such names are exempt from the relevant protective laws and regulations and therefore free for general use. The publisher, the authors and the editors are safe to assume that the advice and information in this book are believed to be true and accurate at the date of publication. Neither the publisher nor the authors or the editors give a warranty, express or implied, with respect to the material contained herein or for any errors or omissions that may have been made. The publisher remains neutral with regard to jurisdictional claims in published maps and institutional affiliations. This Springer imprint is published by the registered company Springer Nature Singapore Pte Ltd. The registered company address is: 152 Beach Road, #21-01/04 Gateway East, Singapore 189721, Singapore
Preface
Pneumatic servo control originated from the gas servo system of missile and rocket attitude control before and after World War II. In the past 60 years, in order to develop space in Europe and America, cold air or hot gas has been used as working medium for rocket attitude control and thrust vector control of aircraft. The attitude control of China’s Long March series launch vehicles uses cylinder gas source to drive pneumatic turbine and hydraulic pump to generate hydraulic energy. The thrust vector control of missiles and large launch vehicles uses integrated gas turbine pump electro-hydraulic integrated energy device. Because high-temperature, high-pressure, high-speed hot gas and ultra-high-pressure cold gas technology can be used in weapon systems, at present, countries have implemented strict control and blockade on aerospace high-speed pneumatic control t
Data Loading...
