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1、AEROSPACE STANDARD MA2001 (ISO 6771) REV. B Issued1981-07 Revised1993-06 Reaffirmed2007-08 Aerospace Fluid Systems and Components - Pressure and Temperature Classifications FOREWORD Aerospace fluid systems and components are generally designed and marked for a specific fluid pressure and temperature
2、 type. The operating pressures listed are selected from ISO 2944 as far as practical. 1.SCOPE AND FIELD OF APPLICATION: This document establishes the temperature types and pressure classes that are commonly used in aerospace fluid systems. 2.REFERENCES: 2.1U.S. Government Publications: Available fro
3、m DODSSP, Subscription Services Desk, Building 4D, 700 Robbins Avenue, Philadelphia, PA 19111-5094. ISO 2944 Fluid Power Systems and Components-Nominal Pressures RATIONALE This document has been reaffirmed to comply with the SAE 5-Year Review policy. SAE Technical Standards Board Rules provide that:
4、 “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 therefrom, is the sole responsibility of the user.” SAE
5、reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2007 SAE International All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or t
6、ransmitted, 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: 724-776-4970 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SA
7、E WEB ADDRESS: http:/www.sae.org Copyright SAE International Provided by IHS under license with SAELicensee=Defense Supply Ctr/5913977001 Not for Resale, 12/04/2007 19:01:19 MSTNo reproduction or networking permitted without license from IHS -,-,- SAE MA2001 Revision B - 2 - 3.TEMPERATURE CLASSIFICA
8、TIONS: System operating temperature ranges shall be classified as follows (see Table 1): TABLE 1 - Temperature Type (C) 4.NOMINAL PRESSURE CLASSIFICATIONS: Nominal pressures shall be classified as follows (see Table 2): TABLE 2 - Nominal Pressure Classes kPa (bar) PREPARED BY SAE COMMITTEE G-3, AERO
9、SPACE COUPLINGS, FITTINGS, HOSE, AND TUBING ASSEMBLIES Copyright SAE International Provided by IHS under license with SAELicensee=Defense Supply Ctr/5913977001 Not for Resale, 12/04/2007 19:01:19 MSTNo reproduction or networking permitted without license from IHS -,-,- SAE MA2001 Revision B - 3 - AP
10、PENDIX A ISO/DIS 6771 AEROSPACE SYSTEM PRESSURES AND TEMPERATURES A.1ASSIGNMENT: At the fifth meeting of ISO/TC 20/SC 10 in Paris in October 1976, the U.S. agreed to prepare a standard for fluid system pressures and temperatures. A.2BACKGROUND: Initially, the proposal was discussed under a proposed
11、specification for fittings (SC 10 - N.53, N.93). In accordance with SC 10 resolution No. 33, the subject proposal was then drafted as a separate document (SC 10 - N.203) because of its applicability to other areas. Revision A changed the nominal pressure classes 10 000 and 20 000 kPa to 10 500 and 2
12、1 000 kPa respectively. The 10 000 and 20 000 kPa classes follow the ISO 2944 Renard Series for nominal pressures but would require redesign and changes to the currently used 1500 and 3000 psi hydraulic system components if they were to be used in metric systems. Revision A limits the changes to the
13、 fittings of the 1500 and 3000 psi components, and will avoid changes to wall thicknesses, bore dimensions, etc., allowing such components to be used in metric systems. Revision B revises classes C and F similar to B and D of Revision A. It also adds 14 000, 35 000 and 56 000 kPa classes, accomodati
14、ng through 8000 psi operating and all combinations for return pressures at a 1:2 ratio. A.3ACCEPTED STANDARDS, NATIONAL, INTERNATIONAL: The temperature ranges are fairly common to European and U.S. aircraft fluid systems specifications. The pressure ranges proposed in the referenced documents are se
15、lected from ISO 2944, pr EN2245 (AECMA) and MIL-H-5540 (U.S.). Copyright SAE International Provided by IHS under license with SAELicensee=Defense Supply Ctr/5913977001 Not for Resale, 12/04/2007 19:01:19 MSTNo reproduction or networking permitted without license from IHS -,-,- SAE MA2001 Revision B
16、- 4 - TABLE 1A A.4APPROVAL STATUS: The N.203 proposal was accepted by SC 10 at the 1977 Berlin meeting with changes as shown in N.261. The countries represented at the meeting: France, Germany, UK, USA. The N.261 document was coordinated in TC20 as DIS 6771, which resulted in disapprovals from Czech
17、oslovakia and the USSR. Comments were received from Germany F. R. All suggested changes were discussed by ISO/TC20 /SC10. The agreed on changes are shown in this specification. This metric Aerospace Standard is the equivalent of ISO 6771. ISO 6771 was published in 1981. Copyright SAE International Provided by IHS under license with SAELicensee=Defense Supply Ctr/5913977001 Not for Resale, 12/04/2007 19:01:19 MSTNo reproduction or networking permitted without license from IHS -,-,-