SAE AIR 6364-2017 Test Facility Shakedown and Commissioning.pdf
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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 ther
2、efrom, 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 2017 SAE International All rights reserved. No part of this
3、publication 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: +1 724-776-49
4、70 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org SAE values your input. To provide feedback on this Technical Report, please visit http:/standards.sae.org/AIR6364 AEROSPACE INFORMATION REPORT AIR6364 Issued 2017-11 Test Facility Shakedown and Commis
5、sioning RATIONALE This SAE Aerospace Information Report (AIR) is intended to provide guidance and recommendations to future or existing users of turbofan, turbojet, and turboshaft/turboprop gas turbine engine test facilities regarding commissioning readiness of new, modified, or re-located facilitie
6、s. TABLE OF CONTENTS 1. SCOPE 3 2. REFERENCES 3 2.1 Applicable Documents 3 2.1.1 SAE Publications . 3 2.1.2 Other Publications . 4 2.2 Definitions/Acronyms 4 3. PHASE 1 OFF SITE (FACTORY) EQUIPMENT COMMISSIONING CHECKS 5 3.1 Introduction . 5 3.2 Mechanical 6 3.3 Electrical 6 3.4 Software 7 4. PHASE
7、2 ON SITE STATIC EQUIPMENT COMMISSIONING CHECKS (NO ENGINE RUNNING) . 8 4.1 Introduction . 8 4.2 Handling and Hoisting Systems 9 4.3 Thrust Stand 9 4.4 Engine Test Adapters 9 4.5 Fuel System, including the Inhibiting Oil System (if installed) 9 4.6 Hydraulic System (Loading System, Pressure Power Pa
8、ck ) . 9 4.7 Lubrication System (Engine and/or Drive Line Equipment) 10 4.8 Air Start System 10 4.9 Electrical Start System 10 4.10 Water System (TS/TP Applications) . 10 4.11 Drive Line (TS/TP Applications) 10 4.12 Instrumentation . 11 4.13 Control System 11 4.14 CCTV and Intercom 11 4.15 DAS . 11
9、SAE INTERNATIONAL AIR6364 Page 2 of 13 5. PHASE 3 ON SITE DYNAMIC EQUIPMENT CHECKS (INCLUDES ENGINE RUNNING) 11 5.1 General 11 5.2 Dynamic Commissioning. 12 5.3 Documentation and training 13 6. NOTES 13 6.1 Revision Indicator 13 SAE INTERNATIONAL AIR6364 Page 3 of 13 1. SCOPE The paper discusses in
10、general terms the activities required to be undertaken or demonstrated during the establishment of the facility such as: the assessment checks prior to forwarding to the end users site for embodiment into the facility system the establishment of the facility such as trial installations of hardware,
11、functionality checking of lifting transportation and access systems, centerline pull checks, pressure testing of fuel and air start systems, flushing of wet systems and electrical continuity checking. the commissioning of the facility such as instrumentation calibrations, engine starts, engine runni
12、ng, assessment of command and control system, assessment of DAS system, aerodynamic and acoustic surveys. The paper will concentrate on the main engineering engine related aspects of the facility and will not necessarily contain information on the construction validation activities such as HVAC, ele
13、ctrical, facility fire system, waste water etc. Risk analysis may be performed during the design phase whose results could lead to pay particular attention to some specific equipment / functionalities during the commissioning phase. If identified, these risks should be translated to specific tests a
14、nd integrated into the validation plan, either at the factory or on site or both. If the test cell is designed to test several engine types, the acceptance process should validate upon which engine the test cell will be commissioned these discussions should take place at the early stage of the desig
15、n process if not during the bidding phase. Moreover, an agreement between the Contractor and the Customer may have to be reached in order to clearly define how the scaling will be demonstrated in the case of the available engine types for commissioning are not representative of the full capacity upo
16、n which the facility is designed (e.g. the requirements are assessed based on future engine types). It is particularly relevant to air flow and acoustic levels and tones where effects arent only linear. Correlation activities are outside the scope of this document. Document is primary intended for t
17、ypical overhaul (MRO) test cells. Development/Production facilities may include additional and specific equipment that requires dedicated shakedown and commissioning processes and procedures issued directly from the OEMs. Outdoor test cell specifics are not covered by this document. 2. REFERENCES 2.
18、1 Applicable Documents The following publications form a part of this document to the extent specified herein. The latest issue of SAE publications shall apply. The applicable issue of other publications shall be the issue in effect on the date of the purchase order. In the event of conflict between
19、 the text of this document and references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained. 2.1.1 SAE Publications Available from SAE International, 400 Commonwealth D
20、rive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or +1 724-776-4970 (outside USA), www.sae.org. AIR4827 Physical Modeling Techniques for Jet Engine Test Cell Aerodynamics AIR4869 Design Considerations for Enclosed Turbofan/Turbojet Engine Test Cells AIR4951 Test Cell Thrust
21、 Measurement AIR4989 Design Considerations for Enclosed Turboshaft Engine Test Cells AIR5026 Test Cell Instrumentation SAE INTERNATIONAL AIR6364 Page 4 of 13 AIR5295 Design Considerations for Enclosed Turboprop Engine Test Cells ARP741 Turbofan and Turbojet Gas Turbine Engine Test Cell Correlation A
22、RP4755 Turboshaft/Turboprop Gas Turbine Engine Test Cell Correlation ARP5435 APU Gas Turbine Engine Test Cell Correlation ARP5758 Trend Analysis for Maintaining Correlation of Gas Turbine Engine Test Cells ARP5759 Acoustical Considerations for Engine Test Cells ARP6028 Configuration Control for Main
23、taining Correlation of Gas Turbine Engine Test Cells ARP6068 Gas Turbine Engine Test Facility Vibration Measurement 2.1.2 Other Publications “Measurement Uncertainty: Methods and Applications“, 4th Edition, Dieck, Ronald H.; ISA The International Society of Automation, 2007, ISBN-13: 978-55617-915-0
24、. 2.2 Definitions/Acronyms The following list defines certain terms and phrases used in this document: ACOUSTIC TONE: Sound pressure at a constant frequency that can vary in amplitude. In the area of aero engine testing, the apparition of a tone in the exhaust section could be potentially problemati
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