1、_ SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising there
2、from, is the sole responsibility of the user.” SAE reviews each technical report at least every five years at which time it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions.Copyright 2013 SAE International All rights reserved. No part of this pu
3、blication may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: +1 724-776-4970
4、 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/ARP355BAEROSPACERECOMMENDED PRACTICEARP355 REV. BIssued 1946-09 Revised 2004-02 Sta
5、bilized 2013-12 Superseding ARP355A Terminology of Dual and Coaxial Counter-Rotating Propellers RATIONALEThis document has been determined to contain basic and stable technology which is not dynamic in nature. This standard has been stabilized. STABILIZED NOTICE This document has been declared “Stab
6、ilized“ by the SAE E-25 General Standards for Aerospace and Propulsion Systems Committee and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability of technical requirements. Newer technology may exist. Copyright SAE Int
7、ernational Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-1. SCOPE: This document provides definitions pertaining to dual and coaxial counter-rotating propellers. 2. Dual Rotation Propellers or Dual Rotation Propeller Shafts -
8、 The concentric arrangement in which each component of the propeller rotates in an opposite direction at the same speed because of a fixed gear ratio between shafts. 3. Coaxial Propellers and Coaxial Propeller Shafts - The concentric arrangement in which each component of the propeller rotates in an
9、 opposite direction wherein the speed of each component can vary independently because no fixed gear ratio is incorporated between the shafts. 4. Counter Rotating Propellers and Propeller Shafts - The airplane arrangement in which shafts and propellers rotate in opposite directions but in which the
10、shafts are not concentric. 5. Inboard Component - The component of a dual rotation or coaxial propeller which is mounted on the inboard shaft. (Nearest to power source) 6. Outboard Component - The component of a dual rotation or coaxial propeller which is mounted on the outboard shaft. (Farthest fro
11、m power source) 7. Designation of Number of Blades - The number of blades of a dual rotation or coaxial propeller shall be designated as the total number in both components. PREPARED UNDER THE JURISDICTION OF SAE COMMITTEE E-25, GENERAL STANDARDS FOR AEROSPACE & PROPULSION SYSTEMS SAE INTERNATIONAL ARP355B Page 1 of 1_Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
