SAE ARP 1558-2014 Interface Protection - Ground Equipment to Aircraft.pdf
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1、AEROSPACERECOMMENDED PRACTICEARP1558Issued 2014-10Interface Protection - Ground Equipment to AircraftRATIONALEThis ARP, superseding former AIR 1558A originally published in 1978, specifies both passive devices and current state of the art active detection systems that should be incorporated or consi
2、dered in GSE design in order to ensure aircraft protection against fuselage damage resulting from GSE interface. The change of document status from AIR to ARP is intended to take into account research findings on composite fuselage aircraft protection.TABLE OF CONTENTS1. SCOPE 31.1 Purpose. 31.2 Fie
3、ld of Application 32. REFERENCES 32.1 Applicable Documents 32.1.1 SAE Publications. 32.1.2 ANSI Publications . 32.1.3 ASTM Publications 32.1.4 ISO/IEC International Standards. 42.1.5 Other Documents 42.2 Definitions . 43. GENERAL . 53.1 Aluminum Alloy Aircraft Fuselages . 53.2 Composite Aircraft Fus
4、elages. 53.3 Operation 53.4 Docking Speed 54. PASSIVE DEVICES REQUIREMENTS 64.1 Application. 64.2 Characteristics 64.3 Contact Area . 64.4 Cylinder Thickness 64.5 Choice of Fender. 64.6 Cylinder Deterioration . 74.7 Method of Installation 74.8 Variety of Fenders. 74.8.1 “D” Type Fender 74.8.2 “O” Ty
5、pe Fender 74.9 Operators Training 74.9.1 “D II” Type Fenders. 104.9.2 Corner Fenders. 11_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
6、and suitability for any particular use, including any patent infringement arising therefrom, 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 an
7、d suggestions.Copyright 2014 SAE InternationalAll rights reserved. No part of this 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 PL
8、ACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada)Tel: +1 724-776-4970 (outside USA)Fax: 724-776-0790Email: CustomerServicesae.orgSAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedbackon this Technical Report, please visithttp:/www.sae.org/technical/standards/ARP15
9、58 SAE INTERNATIONAL ARP1558 Page 2 of 164.9.3 Padded Pivot Fenders. 124.9.4 Flat Fenders 124.10 Fender Material Characteristics 134.10.1 Load Deflection . 134.10.2 Hardness. 134.10.3 Examples of Shore “A” Readings 134.11 Advanced Fender Profiles. 144.11.1 Profiles Geometry . 144.11.2 Profiles Perfo
10、rmance. 145. ACTIVE SYSTEMS REQUIREMENTS. 155.1 Application. 155.2 Alerting Function . 155.3 Active Safety Function 165.4 Additional Safety Functions 166. NOTES 16FIGURE 1 Basic Fender Installation. 8FIGURE 2 Example of Correct Placement of Bumpers or Fenders . 9FIGURE 3 Type “D” Fender Installation
11、 (Dimensions approximate) 10FIGURE 4 Type “D II“ Fender Installation (Dimensions approximate). 10FIGURE 5 Corner Fenders (Dimensions approximate) 11FIGURE 6 Corner Fenders (Dimensions approximate) 11FIGURE 7 Protection Devices (Passenger Stairs, Commissary/Cabin Cleaning Trucks) . 12FIGURE 8 Bumper
12、- FWD Platform Assembly. 13FIGURE 9 Bumper contact area. 14FIGURE 10 Typical Performance Curve 14TABLE 1 Examples of Shore “A” Readings 13SAE INTERNATIONAL ARP1558 Page 3 of 161. SCOPE1.1 PurposeThis SAE Aerospace Recommended Practice (ARP) discusses damage to aircraft fuselages caused by ground equ
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