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 theref
2、rom, 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 ma
3、y 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.orgAS8057 AEROSPACESTANDARDIssued 2008-07 Minimum Design and Performance of Airplane Galley Insert Equipment, Electrical/Pressurized RATIONALEGalley Insert Equipment (GAIN) is electrical equipment, used in conjunction wit
5、h aircraft food service. GAIN (e.g., beverage maker, oven) is not an integral part of the galley and is removable from the galley without tools or with the use of simple tools. The design and operation of GAIN has a significant impact on cabin service, cabin safety and workload of the crew members.
6、Most types of GAIN have significant electrical power consumption, are connected to the aircraft potable water system, and are controlled by electronic devices. This AS specifies criteria to assure safe GAIN design and function.FOREWORDThis SAE Aerospace Standard (AS) and the SAE AS8056 “Minimum Desi
7、gn and Performance of Airplane Galley In-Flight Carts, Containers, and Associated Components” establish minimum design and performance requirements for galley insert equipment. The content of both standards is harmonized. SAE is an international not-for-profit organization, formed to advance the art
8、 and science of aviation and aviation electronic systems for the benefit of the public. Since SAE is not an official agency of the U.S. government, its recommendations may not be regarded as statements of official government policy unless so enunciated by the U.S. government organization or agency h
9、aving statutory jurisdiction over any matters to which the recommendations relate. SAE AS8057 - 2 -TABLE OF CONTENTS 1. SCOPE 51.1 General . 51.2 Purpose. 51.3 Mandating and Recommendation Phrases. 52. REFERENCES 62.1 Applicable Documents 62.1.1 SAE Publications. 62.1.2 ASTM Publications 62.1.3 Code
10、 of Federal Regulations (CFR) and other FAA Publications 62.1.4 U.S. Government Publications 72.1.5 U.S. Food and Drug Administration (FDA) Publication. 72.1.6 National Sanitation Foundation (NSF) Publications . 72.1.7 American Welding Society (AWS) Publications 72.1.8 National Aeronautics and Space
11、 Administration (NASA) Publications. 72.1.9 RTCA Publications 72.1.10 ISO Publications 82.2 Definitions . 83. REQUIREMENTS . 103.1 Introduction . 103.2 General . 113.2.1 Materials and Materials Control 113.2.2 General Construction 133.2.3 Construction for Waste Enclosures (e.g., Trash Compactor). 14
12、3.2.4 Injury Hazard. 153.2.5 Interface Clearances. 153.2.6 Sanitary Construction 153.2.7 Identification 153.2.8 Continued Airworthiness. 163.3 Structural. 163.3.1 General . 163.3.2 Design Load Factors. 163.3.3 Local Attachment Factor . 163.3.4 Material Strength Properties and Material Variability .
13、163.3.5 Retention of Items of Mass . 173.3.6 Weight and Center of Gravity 183.3.7 Doors and Hinges . 193.3.8 Adjacent Equipment Loads. 193.3.9 Floor Loads . 193.3.10 Trash Compactor Design Criteria . 193.4 Electrical 193.4.1 Power 193.4.2 Protection against Electrical Failure or Overcurrent . 193.4.
14、3 Electrical Installation . 193.4.4 Dielectric Requirements 203.4.5 Grounding and Bonding 213.4.6 Motors . 213.4.7 Microwave Ovens 213.4.8 Electro-Magnetic Interference (EMI). 213.4.9 Control Elements. 223.5 Thermal Protection/Overheat 22SAE AS8057 - 3 -3.6 Wet Equipment Design Requirement . 233.6.1
15、 General . 233.6.2 Wet Equipment Connected with the Airplane Potable Water System 233.6.3 Low Water Sensing. 233.6.4 Self Venting/Self Draining . 233.6.5 Pressure Vessels 243.6.6 Pressure Limits . 243.6.7 Water Taps/Faucets 253.7 Equipment Ventilation/Exhaust Air 253.8 Maximum Temperature Design Req
16、uirements. 253.9 Fire Properties of Materials. 253.9.1 Flammability 253.9.2 Heat Release and Smoke Density 263.10 Fire Containment. 263.11 Placards 263.11.1 Placards for Design Limitations 263.11.2 Placards for Weight. 263.11.3 Placards for Fire Safety 263.11.4 Placards for Loose Equipment/Loose Com
17、ponents/Associated Components. 263.12 Acoustics Noise generated by the Equipment. 273.13 Ovens 273.14 Interchangeability / Installation/Removal/Replacement 273.15 Software 273.16 Electronic Hardware 273.17 Environmental Design Requirements . 273.18 Power Quality Constant and Wide Frequency Equipment
18、 (AC) 303.18.1 Power Consumption 303.18.2 Maximum Current Demand / Inrush Current. 303.18.3 Load Switching Transients 313.18.4 Input Capacitance . 323.19 Safety Analysis 324. QUALIFICATION AND ACCEPTANCE 324.1 General . 324.2 Qualification 324.2.1 Structural. 324.2.2 Electrical 344.2.3 Wet Equipment
19、 344.2.4 Pressure Vessels 344.2.5 External Temperatures . 344.2.6 Fire Properties. 354.2.7 Fire Containment. 354.2.8 Acoustics - Noise generated by the equipment 354.2.9 Software and Electronic Hardware . 354.2.10 Environmental Test Conditions. 354.2.11 Power Quality Constant and Wide Frequency Equi
20、pment (AC) 354.2.12 Maximum Current Demand / Inrush Current. 364.2.13 Load Switching Transients 374.2.14 Input Capacitance . 374.2.15 Safety Analysis 374.3 Acceptance Test . 385. DATA REQUIREMENTS 395.1 Interface Control Document 395.2 Qualification Documentation. 40SAE AS8057 - 4 -6. COMPLIANCE MAT
21、RIX 417. NOTES 43APPENDIX A ADDITIONAL VERIFICATION REQUIREMENTS 44FIGURE 1 TYPICAL GAIN DIRECTIONS RELATIVE TO AIRPLANE. 17FIGURE 2 MAXIMUM INRUSH CURRENT FOR AC EQUIPMENT WITH MOTOR CONTROLLERS. 31FIGURE 3 LIMITS FOR THE GENERATION OF SPIKE VOLTAGE TRANSIENT . 31TABLE 1 APPLICABLE REQUIREMENTS 11T
22、ABLE 2 ENVIRONMENTAL DESIGN REQUIREMENTS 28TABLE 3 DESIGN LOAD FACTORS . 33TABLE 4 ABUSE LOADS. 33TABLE 5 INRUSH CURRENT TEST CONDITIONS FOR CONSTANT FREQUENCY EQUIPMENT 36TABLE 6 INRUSH CURRENT TEST CONDITIONS FOR AC EQUIPMENT 37SAE AS8057 - 5 -1. SCOPE 1.1 General This SAE Aerospace Standard (AS)
23、establishes minimum design and performance requirements for galley insert equipment with an electrical and/or pressure system, as well as associated components intended for installation in galleys and other areas (e.g., bars) of transport category airplanes.1.2 Purpose 1.2.1 This standard applies to
24、 the following equipment intended for installation in galleys and other areas (e.g., bars) within transport category airplanes, such as but not limited to the following: a. Ovens (e.g., convection, steam, induction, microwave, bun warmer, plate warmer) b. Beverage makers (e.g., coffee makers, coffee
25、 warmers, water heaters, espresso makers) c. Beverage cups and jugs (so-called hot cups and jugs) d. Self contained refrigeration equipment (e.g., refrigerators, freezers, wine chillers, water coolers, air chillers) e. Trash compactors f. Rail assemblies g. Associated components, such as oven racks
26、and trays, beverage servers1.2.2 This standard does not: a. Address equipment covered in AS8056 “Minimum Design and Performance of Airplane Galley In-Flight Carts, Containers, and Associated Components”. b. Fully address design details that provide extended service life and continued airworthiness,
27、since these are a function of: (1) total galley and food/beverage system design, (2) human factors engineering desired by individual operators, (3) techniques of care in servicing, and (4) maintenance philosophy. However, references to these considerations are included as appropriate. c. Fully addre
28、ss requirements that are covered by national aviation regulations, pertinent U.S. Public Health regulations and/or design details, which should be covered by galley operator/airplane manufacturer specifications for the subject equipment.d. Fully address requirements for equipment utilizing hydraulic
29、 systems (e.g., Trash compactors). 1.2.3 When the term “equipment” is used in this standard, it refers to all of the items identified in the Purpose (1.2) unless specifically identified otherwise. 1.3 Mandating and Recommendation Phrases a. “Shall” The word “shall” indicates a mandatory criterion. b
30、. “Should” The word “should” indicates a criterion for which an alternative, including non-compliance, may be applied if it is documented and justified. SAE AS8057 - 6 -2. REFERENCES 2.1 Applicable Documents The following publications form a part of this document to the extent specified herein. The
31、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 text of this document takes precedence. Nothing in this
32、 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 Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.o
33、rg.AMS-STD-401 Sandwich Constructions and Core Materials; General Test Methods AMS2175 Castings, Classification and Inspection ofARP4761 Guidelines and Methods for Conducting the Safety Assessment Process on Civil Airborne Systems and EquipmentAS8056 Minimum Design and Performance of Airplane Galley
34、 In-Flight Carts, Containers, and Associated ComponentsAS39029 Contacts, Electrical Connector, General Specification For AS50881 Wiring Aerospace Vehicle CAESAR 3-D Anthropometric Database 2.1.2 ASTM Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohoc
35、ken, PA 19428-2959, Tel: 610-832-9585, www.astm.org.ASTM C 273 Standard Test Methods for Shear Properties of Sandwich Core Materials ASTM C 393 Standard Test Method for Flexural Properties of Sandwich Construction ASTM D 1781 Standard Test Method for Climbing Drum Peel for Adhesives 2.1.3 Code of Fe
36、deral Regulations (CFR) and other FAA Publications Available from US Government Printing Office, Superintendent of Documents, Mail Stop SSOP, Washington, DC 20402-9325.AC 25-17 Transport Airplane Cabin Interiors Crashworthiness Handbook AC 25.856-1 Thermal/Acoustic Insulation Flame Propagation Test
37、Method 14 CFR Part 1 Definitions and Abbreviations 14 CFR Part 25 Airworthiness Standards: Transport Category Airplanes SAE AS8057 - 7 -21 CFR Part 1240 Control of Communicable Diseases 21 CFR Part 1250 Interstate Conveyance Sanitation HF-STD-001 The Human Factors Design Standard 2.1.4 U.S. Governme
38、nt Publications Available from DODSSP, Subscription Services Desk, Building 4D, 700 Robbins Avenue, Philadelphia, PA 19111-5094, http:/assist.daps.dla.mil/quicksearch/.MIL-STD-889 Dissimilar Metals 2.1.5 U.S. Food and Drug Administration (FDA) Publication Available at http:/www.fda.gov/ora/inspect_r
39、ef/igs/icsfatt.html .Attachment 3 to Guide to Inspections of Interstate Carriers and Support Facilities 2.1.6 National Sanitation Foundation (NSF) Publications Available from NSF International, P.O. Box 130140, 789 N. Dixboro Road, Ann Arbor, MI 48113-0140, Tel: 734-769-8010, Toll Free (USA): 800-NS
40、F-MARK, www.nsf.org.NSF/ANSI 51 Food Equipment Materials 2.1.7 American Welding Society (AWS) Publications Available from American Welding Society, 550 NW LeJeune Road, Miami, FL 33126, Tel: 1-800-443-9353, www.aws.org.AWS D17.1 Specification for Fusion Welding for Aerospace Applications 2.1.8 Natio
41、nal Aeronautics and Space Administration (NASA) Publications Available from Man-Systems Integration Standard Office, NASA Johnson Space Center, Mail Code SF3, 2101 NASA Road One, Houston, TX 77058-3591, http:/msis.jsc.nasa.gov/.NASA-STD-3000 Man-Systems Integration Standards 2.1.9 RTCA Publications
42、Available from Radio Technical Commission for Aeronautics Inc., 1828 L Street, NW, Suite 805, Washington, DC 20036-5133, Tel: 202-833-9339, www.rtca.org.RTCA DO-160 Environmental Conditions and Test Procedures for Airborne Equipment RTCA DO-178 Software Considerations in Airborne Systems and Equipme
43、nt Certification RTCA DO-248 Final Report for Clarification of DO-178B “Software Considerations in Airborne Systems and Equipment Certification” RTCA DO-254 Design Assurance Guidance for Airborne Electronic Hardware SAE AS8057 - 8 -2.1.10 ISO Publications Available from International Organization fo
44、r Standardization, 1, rue de Varembe, Case postale 56, CH-1211 Geneva 20, Switzerland, Tel: +41-22-749-01-11, www.iso.org.ISO 3744 Acoustics-Determination of sound power levels of noise sources using sound pressure Engineering method in an essentially free field over a reflecting plane ISO 3745 Acou
45、stics-Determination of sound power levels of noise sources using sound pressure Precision methods for anechoic and hemi-anechoic rooms 2.2 Definitions ACCEPTANCE TEST: A test conducted to verify that the operational and safety performance of each production unit conforms to its design and published
46、technical data.ANALYSIS: Verification by technical/mathematical evaluation using mathematical representations (i.e., models, simulation, and algorithms), charts, graphs, drawings and representative test data. An example means of analysis could be a bit comparison of the actual outputs of the equipme
47、nt to be qualified with the expected outputs, given a specific set of inputs. ASSOCIATED COMPONENTS: Defined as both of the following: 1. Items, such as oven racks and trays, as well as beverage servers, that are stowed in or connected with galley insert equipment, but are not part of the equipment
48、part number. 2. Items that need to meet 14 CFR 25 requirements to be included as part of an airplane type design. BEVERAGE CUP: Cup placed at the galley worktop, and with an electrical connector to a galley receptacle, designed to heat water (similar to household electric kettle). BEVERAGE JUG: Cont
49、ainer with integrated heating element, and with an electrical connector to a galley receptacle, designed to hold hot beverages. CLOSED SYSTEM: (a) Galley insert equipment for which check valves or similar devices isolate the equipment potable water plumbing from the airplane potable water system or the ambient environment. (b) Self contained refrigeration equipment with a vapor cycle. CONFIGURATION: Relative arrangement of parts. T
