SAE ARP 1836B-2008 Aircraft Cargo Conveyor - Battery Powered《电池驱动的航空货运设备》.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 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 reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2008 SAE International All rights reserved. No part of this publication m
3、ay 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: 724-776-4970 (outside USA)
4、 Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.orgARP1836B AEROSPACERECOMMENDEDPRACTICEIssued 1985-07 Revised 2008-10 Superseding ARP1836A Aircraft Cargo Conveyor - Battery Powered RATIONALEDimensional and technological changes since 1985 warrants a revision of ARP18
5、36. Changes to newer generation aircraft characteristics and ground servicing interfaces affects the need for a revision as well. 1. SCOPE This SAE Aerospace Recommended Practice (ARP) outlines the functional and design requirements for a battery powered, self-propelled belt conveyor for handling ba
6、ggage and cargo at aircraft bulk cargo holds. Additional considerations and requirements may legally apply in other countries. As an example, for operation in Europe (E.U. and E.F.T.A.), the applicable EN standards shall be complied with. 2. APPLICABLE DOCUMENTS The following publications form a par
7、t 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 the text of this document and references cited herein, the
8、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 SAE Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA
9、 and Canada) or 724-776-4970 (outside USA), www.sae.org.ARP1247 General Requirements for Aerospace Ground Support Equipment, Motorized and Nonmotorized ARP1328 Aircraft Ground Support Equipment - Wind Stability Determination AIR1375 Minimum Safety Requirements for Special Purpose Airline Ground Supp
10、ort Equipment AIR1558 Interface Protective Devices - Ground Equipment to Aircraft ARP1816 Charger for Battery Powered Ground Support Equipment ARP1817 Battery Industrial, Lead-Acid Type, for Use in Electric Powered Ground Support Equipment ARP1838 Pictograms for Ground Support Equipment ARP1892 Elec
11、trical Connectors for Use In Battery Powered Ground Support Equipment SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/ARP1836BCopyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or netw
12、orking permitted without license from IHS-,-,-SAE ARP1836B - 2 -2.2 AHM Publications Available from International Air Transport Association, 800 Place Victoria, PO Box 113, Montreal - H4Z 1M1, Quebec - Canada; Phone +1 514 874 0202; www.iata.org.AHM 918 Basic Requirements for Battery-Powered Ground
13、Support Equipment AHM 925 Functional Specification for Self-Propelled Conveyor Belt Loader 2.3 EN Standards (mandatory in E.U. and E.F.T.A. countries) Available from Comite Europeen de Normalisation (CEN), rue de Stassart 36, B-1050 Brussels, Belgium www.cen.eu/cennorm.EN 1915-1 Aircraft Ground Supp
14、ort Equipment General Requirements - Part 1: Basic Safety Requirements EN 12312-3 Aircraft Ground Support Equipment Specific Requirements - Part 3: Conveyor Belt Vehicles 3. DESIGN REQUIREMENTS Design, systems, hardware, and material used in the manufacture of the conveyor must meet automotive stand
15、ards and good industry practices. The loader shall be designed for easy access to those areas that require frequent checks for servicing.3.1 Physical Characteristics 3.1.1 Overall dimensions of the aircraft cargo conveyor shall be within 347 in (8.81 m) long and 88 in (2.03 m) wide. The vehicle shal
16、l have a minimum front to rear wheelbase of 110 in (2.8 m). Overall height should be kept as low as possible consistent with good operation, safety, and ground clearance. 3.1.2 The loader must be capable of servicing all commercial aircraft cargo compartments. This requires a range of travel of the
17、forward end of the conveyor of a minimum of 38 in (0.97 m), from the ground in the conveyor full down position, to a minimum of 170 in (3.8 m) in the full up position. The rear end of the conveyor must maintain 20 in (0.51 m) to 24 in (0.58 m) through the entire height range of the forward end and e
18、xtend to a minimum height of 50 in (1.27 m). 3.1.3 The turning radius as measured from the outside corner of the vehicle shall not be greater than 25 ft (7.6 m). 3.1.4 The following characteristics shall be met under normal operating conditions and loads: a. Approach angle: 16 degrees (0.28 rad) min
19、imum b. Ramp breakover angle: 10 degrees (0.18 rad) minimum c. Departure angle: 10 degrees (0.18 rad) minimum 3.1.5 The conveying belt shall be 24 in (0.61 m) wide. Usable conveyor bed width shall be a minimum of 30 in (0.81 m) with guides and a maximum of 40 in (1.02 m) overall. 3.1.6 The belt conv
20、eyor shall have tire tread suitable for outdoor use and all performance requirements as specified in this document. 3.1.7 The minimum ground clearance shall be at least 5 in (0.13 m). Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permit
21、ted without license from IHS-,-,-SAE ARP1836B - 3 -3.1.8 The loader chassis shall have rub rails on both sides for protection against damage. 3.1.9 To minimize aircraft damage the forward end of the conveyor support structure shall be protected with a type of rubber bumper. 3.1.9.1 First Bumper Alte
22、rnative Bumper does not extend across the front of the conveyor bed, but is mounted to the support structure on either side of the conveyor bed, reducing finger pinching hazard. 3.1.9.2 Second Bumper Alternative Bumper is full width, 5 in (0.13 m) ID x 7 in (0.18 m) OD (minimums). CAUTION: The gap w
23、idth between the bumper support and belt at the front of the conveyor should be chosen with great care. If too small, the risk of getting fingers caught exists. If too large, packages can get stuck or fall through the gap. 3.1.10 The operators control area shall have adequate room to safely and effi
24、ciently operate the loader. Recommended dimensions to accomplish this are shown in Figure 1 and Table 1. TABLE 1 - OPERATOR STATION INTERIOR DIMENSIONS TABLE 1A - DIMENSIONS A THROUGH N Dimension Inches Centimeters DescriptionA 18.0 min 22.0 max 45.72 min 55.88 max Seat width B 15.0 min 38.1 min Sea
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