SAE AIR 6197-2011 Site Selection Considerations for New Re-Located Gas Turbine Engine Test Facilities《重新装载新燃气涡轮发动机试验设施的现场选择考虑因素》.pdf
《SAE AIR 6197-2011 Site Selection Considerations for New Re-Located Gas Turbine Engine Test Facilities《重新装载新燃气涡轮发动机试验设施的现场选择考虑因素》.pdf》由会员分享,可在线阅读,更多相关《SAE AIR 6197-2011 Site Selection Considerations for New Re-Located Gas Turbine Engine Test Facilities《重新装载新燃气涡轮发动机试验设施的现场选择考虑因素》.pdf(12页珍藏版)》请在麦多课文档分享上搜索。
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 2017 SAE International All rights reserved. No part of this p
3、ublication 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: +1 724-776-497
4、0 (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/AIR6197 AEROSPACE INFORMATION REPORT AIR6197 Issued 2011-11 Reaffirmed 2017-06 Site Selection C
5、onsiderations for New Re-Located Gas Turbine Engine Test Facilities RATIONALE AIR6197 has been reaffirmed to comply with the SAE Five-Year Review policy. 1. PURPOSE AND SCOPE This document discusses, in broad and general terms, the effects of various natural and man-made influences on the design, co
6、nstruction, equipping, operation and long term supportability of gas turbine engine test facilities. It will assist existing or future operators of gas turbine engine test facilities in making informed decisions regarding the siting, design, construction or long term support of their facilities. Thi
7、s document is intended to aid operators in understanding the basic terms and concerns regarding gas turbine engine test facility site selection. It is not intended that this document be an exhaustive design guide such that any operator or contractor could accomplish the task of gas turbine test faci
8、lity site selection independently and without further specialist advice or assistance. To this end it is suggested that this document be read in in conjunction with other SAE International specialist ARP and AIR documents and in association with other industry experts from the OEMs, test facility sp
9、ecialist design houses, architects with specialised knowledge or independent consultants (SMEs) within the field. TABLE OF CONTENTS 1. PURPOSE AND SCOPE 1 2. APPLICABLE DOCUMENTS AND REFERENCES . 3 2.1 SAE Publications . 3 2.2 ISO Publications 3 3. DEFINITIONS . 3 4. GEOGRAPHICAL AND GROUND CONDITIO
10、NS 4 4.1 Altitude 4 4.2 Terrain . 5 4.3 Ground Conditions 5 4.4 Seismic Activity . 5 5. WEATHER CONDITIONS 6 5.1 Wind 6 5.2 High Temperatures . 6 5.3 Low Temperatures 7 5.4 High Humidity/Fog . 7 5.5 Salt Fog . 7 5.6 Airborne Dust and Sand 8 5.7 Snow . 8 5.8 Rain . 8 5.9 Electrical Storms . 8 6. NATU
11、RAL CONDITIONS 9 6.1 Forest 9 6.2 Insects . 9 7. MAN MADE CONSIDERATIONS . 9 7.1 Location . 9 7.2 Infrastructure . 10 7.3 Availability of Site Services . 10 7.4 Brown Field or Contaminated Sites 10 7.5 Planning Permission . 10 8. EFFECTS OF GAS TURBINE ENGINE TEST FACILITIES ON SURROUNDING AREAS. 10
12、 8.1 Construction Effects 10 8.2 Acoustic Impact . 11 8.3 Infrasound . 11 8.4 Vibration 11 8.5 Emissions 12 8.6 Long Term Contamination and Disposals . 12 _ SAE INTERNATIONAL AIR6197 2 of 122. APPLICABLE DOCUMENTS AND REFERENCES The following publications form a part of this document to the extent s
13、pecified herein. The latest issue of SAE publications shall apply. The applicable issue of the other publications shall be the issue in effect on the date of the purchase order. In the event of conflict between the text of this document and references cited herein, the text of this document takes pr
14、ecedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained. 2.1 SAE Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (
15、outside USA), www.sae.org. AIR4869 Design Considerations for Enclosed Turbofan/Turbojet Engine Test Cells AIR4989 Design considerations for Enclosed Turboshaft Engine Test Cells 2.2 ISO Publications Available from International Organization for Standardization, 1, rue de Varembe, Case postale 56, CH
16、-1211 Geneva 20, Switzerland, Tel: +41-22-749-01-11, www.iso.org. ISO7196 Acoustics Frequency-Weighting Characteristic for Infrasound Measurement. 3. DEFINITIONS AIR: Aerospace information report ARP: Aerospace recommended practice CBR: California bearing ratio. Penetration test for evaluation of th
17、e mechanical strength of road subgrades and basecourses. Correlation: The comparison of gas turbine engine performance parameters measured on a common engine tested in two test facilities, where one facility is the reference. DAS: Data acquisition system. DBG: scale for the measurement of very low f
18、requency noise. EMI: Electro magnetic interference. FOD: Foreign object damage (to engine). GSE: Ground support equipment. HGI: Hot gas ingestion. HVAC: Heating ventilation and air conditioning. ISA: International standard atmospheres. ISO: International standards organisation. IT: Information techn
19、ology. _ SAE INTERNATIONAL AIR6197 3 of 12MAX: Maximum MRO: Maintenance repair and overhaul. OEM: Original Equipment Manufacturer of respective Gas Turbine Engine RFI: Radio Frequency Interference SLS: Sea level static. SME: Subject matter expert. Test Facility: An area in which a gas turbine engine
20、 is operated. UV: Ultra violet. %: Percentage : Less than C: Degree celsius. 4. GEOGRAPHICAL AND GROUND CONDITIONS 4.1 Altitude Definition of altitude Elevation above Mean Sea Level (MSL) Where possible gas turbine engine test facilities should be located close to sea level, this is due to the fact
21、that as altitude increases the properties of air change. This change in air properties has the effect of decreasing the developed thrust of engines due to a decrease in air density and a reduction in oxygen levels. Although Performance Engineers attempt to correct all gas turbine engine testing data
22、 back to International Standards Atmosphere (ISA) day conditions (15 C) at Sea Level Static (SLS 1013mbar) these corrections and extrapolations can cause difficulties in achieving a successful correlation with a master test facility that is closer to sea level. These difficulties would be increased
23、in regions where large temperature or humidity variations from the master test facility location produce additional variables. This inherent level of measurement uncertainty at the time of the correlation could potentially cause errors in the final pass off data for each subsequent engine tested. To
24、 avoid this uncertainty a significant amount of engineering time and effort can be spent by the engine OEM developing analytical engine performance models to recreate and understand the altitude effects, however, these models are expensive to produce and validate and unless created perfectly could h
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