ARINC 628P4A-3-2005 CABIN EQUIPMENT INTERFACES PART 4A CABIN MANAGEMENT AND ENTERTAINMENT SYSTEM CABIN DISTRIBUTION SYSTEM DAISY CHAIN《船舱接口部分4A管理和娱乐系统分布环1999包括附录1 2 和 3》.pdf

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1、 AN DOCUMENT Prepared by AIRLINES ELECTRONIC ENGINEERING COMMITTEE Published by AERONAUTICAL RADIO, INC. 2551 RIVA ROAD, ANNAPOLIS, MARYLAND 21401 CABIN EQUIPMENT INTERFACES PART 4A CABIN MANAGEMENT AND ENTERTAINMENT SYSTEM CABIN DISTRIBUTION SYSTEM DAISY CHAIN ARINC SPECIFICATION 628P4A-3 PUBLISHED

2、: February 28, 2005 This document is based on material submitted by various participants during the drafting process. Neither AEEC nor ARINC has made any determination whether these materials could be subject to valid claims of patent, copyright or other proprietary rights by third parties, and no r

3、epresentation or warranty, express or implied, is made in this regard. Any use of or reliance on this document shall constitute an acceptance thereof “as is” and be subject to this disclaimer. 2005 BY AERONAUTICAL RADIO, INC. 2551 RIVA ROAD ANNAPOLIS, MARYLAND 21401-7465 USA Prepared by the Airlines

4、 Electronic Engineering Committee Specification 628P4 Adopted by the Airlines Electronic Engineering Committee October 26, 1998 Summary of Document Supplements Supplement Adoption Date Published Specification 628P4A-1 October 16, 2002 November 11, 2002 Specification 628P4A-2 October 14, 2003 Februar

5、y 23, 2004 Specification 628P4A-3 October 26, 2004 February 28, 2005 A description of the changes introduced by each supplement is included on Goldenrod paper at the end of this document. ARINC SPECIFICATION 628P4A-3 CABIN EQUIPMENT INTERFACES PART 4A CABIN MANAGEMENT AND ENTERTAINMENT SYSTEM CABIN

6、DISTRIBUTION SYSTEM DAISY CHAIN Published: February 28, 2005ii FOREWORD Aeronautical Radio, Inc., the AEEC, and ARINC Standards Aeronautical Radio, Inc. (ARINC) was incorporated in 1929 by four fledgling airlines in the United States as a privately-owned company dedicated to serving the communicatio

7、ns needs of the air transport industry. Today, the major U.S. airlines remain the Companys principal shareholders. Other shareholders include a number of non-U.S. airlines and other aircraft operators. ARINC sponsors aviation industry committees and participates in related industry activities that b

8、enefit aviation at large by providing technical leadership and guidance and frequency management. These activities directly support airline goals: promote safety, efficiency, regularity, and cost-effectiveness in aircraft operations. The Airlines Electronic Engineering Committee (AEEC) is an interna

9、tional body of airline technical professionals that leads the development of technical standards for airborne electronic equipment-including avionics and in-flight entertainment equipment-used in commercial, military, and business aviation. The AEEC establishes consensus-based, voluntary form, fit,

10、function, and interface standards that are published by ARINC and are known as ARINC Standards. The use of ARINC Standards results in substantial benefits to airlines by allowing avionics interchangeability and commonality and reducing avionics cost by promoting competition. There are three classes

11、of ARINC Standards: a) ARINC Characteristics Define the form, fit, function, and interfaces of avionics and other airline electronic equipment. ARINC Characteristics indicate to prospective manufacturers of airline electronic equipment the considered and coordinated opinion of the airline technical

12、community concerning the requisites of new equipment including standardized physical and electrical characteristics to foster interchangeability and competition. b) ARINC Specifications Are principally used to define either the physical packaging or mounting of avionics equipment, data communication

13、 standards, or a high-level computer language. c) ARINC Reports Provide guidelines or general information found by the airlines to be good practices, often related to avionics maintenance and support. The release of an ARINC Standard does not obligate any airline or ARINC to purchase equipment so de

14、scribed, nor does it establish or indicate recognition or the existence of an operational requirement for such equipment, nor does it constitute endorsement of any manufacturers product designed or built to meet the ARINC Standard. In order to facilitate the continuous product improvement of this AR

15、INC Standard, two items are included in the back of this volume: An Errata Report solicits any corrections to the text or diagrams in this ARINC Standard. An ARINC IA Project Initiation/Modification (APIM) form solicits any recommendations for addition of substantive material to this volume which wo

16、uld be the subject of a new Supplement. ARINC SPECIFICATION 628 PART 4A TABLE OF CONTENTS iii 1.0 INTRODUCTION .1 1.1 Purpose of this Document .1 1.2 Related Documents .1 1.3 Cabin Distribution System Description 4 1.3.1 Seat Related Network .4 1.3.1.1 General.4 1.3.1.2 Fiber Optic Network5 1.3.1.3

17、In-Seat Power Network 5 1.3.2 Overhead Network 5 1.3.2.1 Overhead Video Network .5 1.3.2.2 Cabin Management Network6 1.3.3 Cabin Electronics Compartment .6 1.3.4 Remote Control Center .6 1.3.5 Electronics/Avionics Bay.6 1.4 Cable Assembly Letters/Legend6 2.0 SEAT RELATED NETWORK 8 2.1 Introduction8

18、2.2 Unit Specification.8 2.2.1 Passenger Entertainment System Controller8 2.2.1.1 Mechanical Interface 9 2.2.1.2 Electrical Interface9 2.2.1.2.1 Pin Arrangement 9 2.2.2 Area Distribution Box (ADB)9 2.2.2.1 Mechanical Interface 9 2.2.2.2 Electrical Interface9 2.2.2.2.1 Connectors 9 2.2.2.2.2 Pin Arra

19、ngement9 2.2.2.2.3 Power Requirements .10 2.2.3 Floor Disconnect Interface (FDI).10 2.2.3.1 Mechanical Interface 10 2.2.3.2 Electrical Interface10 2.2.3.2.1 Connectors 10 2.2.3.2.2 Pin Arrangement11 2.2.3.2.3 Power Requirements .11 2.2.4 Seat Electronic Box.11 2.2.4.1 Mechanical Interface 11 2.2.4.2

20、 Electrical Interface11 ARINC SPECIFICATION 628 PART 4A TABLE OF CONTENTS iv 2.3 Wiring Specification .11 2.3.1 Wiring between ADB and ADB11 2.3.2 Wiring between ADB and FDI .11 2.3.3 Wiring between FDI and SEB .11 2.3.4 Wiring between SEB and SEB11 2.3.5 Wiring between PESC and Aircraft .12 2.3.6 W

21、iring between PESC and CEC.12 2.3.7 Wiring between PESC and ARU.12 2.3.8 Wiring between PESC and CPMU12 2.3.9 Wiring between ADB and CEC .12 2.3.10 Wiring between ADB and Zone Service Controller .12 2.3.11 Wiring between PESC and CTU .12 2.3.12 Wiring between CEC and CTU .12 3.0 OVERHEAD VIDEO NETWO

22、RK .13 3.1 Introduction13 3.2 Unit Specification.13 3.2.1 Cabin Electronics Compartment (CEC) 13 3.2.1.1 Mechanical Interface 13 3.2.1.2 Electrical Interface13 3.2.2 Tapping Unit13 3.2.2.1 Mechanical Interface 13 3.2.2.2 Electrical Interface13 3.3 Wiring Specification .14 3.3.1 Wiring between TU and

23、 CEC14 3.3.2 Wiring between TU and TU.14 3.3.3 Wiring between TU and Display Unit 14 4.0 CABIN MANAGEMENT NETWORK15 4.1 Introduction15 4.2 Unit Specification.15 4.2.1 Cabin & Passenger Management Unit15 4.2.1.1 Mechanical Interface 15 4.2.1.2 Electrical Interface15 4.2.1.2.1 Connector 16 4.2.1.2.2 P

24、in Arrangement16 4.2.2 CPMS Equipment16 4.2.2.1 Mechanical Interface 16 ARINC SPECIFICATION 628 PART 4A TABLE OF CONTENTS v 4.2.2.2 Electrical Interface16 4.2.3 Tapping Connector .16 4.2.3.1 Mechanical Interface 16 4.2.3.2 Electrical Interface16 4.2.4 Link Connector16 4.2.4.1 Mechanical Interface.16

25、 4.2.4.2 Electrical Interface 16 4.2.5 Termination Connector .16 4.2.5.1 Mechanical Interface.17 4.2.5.2 Electrical Interface 17 4.3 Wiring Specification .17 4.3.1 Wiring between CPMU and Aircraft 17 4.3.2 Wiring between CPMU and Tapping Connector .17 4.3.3 Wiring between Tapping Connector and Tappi

26、ng Connector .17 4.3.4 Wiring between Tapping Connector and Any CPMS Unit.17 4.3.5 Wiring between CPMU and PESC17 4.3.6 Wiring between CPMU and SATCOM SDU17 5.0 BULKHEAD TELECOM NETWORK18 6.0 CABIN ELECTRONICS COMPARTMENT 19 6.1 Introduction19 6.2 Wiring Specification .19 6.2.1 Wiring between CEC an

27、d Aircraft .19 6.2.2 Wiring between CEC and PESC.19 6.2.3 Wiring between CEC and PFIS.19 6.2.4 Wiring between CEC and CPMS Tapping Connector.19 6.2.5 Wiring between CEC and Tapping Unit 19 6.2.6 Wiring between CEC and ADB .19 6.2.7 Wiring between CEC and RCC20 7.0 WIRING AND EQUIPMENT IDENTIFICATION

28、.21 7.1 Equipment Designators .21 7.2 Wire and Wire Bundle Assembly Designators.21 7.3 Wiring and Wire Bundle Marking Requirements21 7.3.1 Wire and Cable Identification 21 7.3.2 Mate-With and Wire Bundle Identification Sleeves .22 ARINC SPECIFICATION 628 PART 4A TABLE OF CONTENTS vi 7.3.3 Marking Qu

29、ality .23 8.0 TECHNICAL DATA24 8.1 Installed Electrical Equipment24 8.2 Electrical Diagrams and Schematics .24 8.2.1 System Schematics 24 8.2.2 Wiring Diagram .24 8.3 Associated Equipment and Wire List Data 25 8.3.1 Electrical and Electronic Equipment List.25 8.3.2 Wire List 25 8.3.3 Wire Hook-Up Li

30、st.25 8.4 Wire Bundle Assembly and Installation Drawings .26 8.4.1 Wire Assembly Fabrication Drawings .26 8.4.2 Wire Bundle Installation Drawings 26 9.0 FIBER OPTIC NETWORK.27 9.1 Introduction27 9.2 Fiber Network Topology.27 9.2.1 CEC-ADB Fibers27 9.3 Fiber Optic Link Characteristics.27 9.3.1 Optica

31、l Fiber Physical Parameters27 9.4 Fiber Optic Connectors28 9.4.1 Fiber Connector Type .28 9.4.2 Fiber Connector Configurations 28 9.4.3 Connector Insertion Loss 28 9.4.4 Connector Force .28 9.4.5 Intermateability/Interoperability .28 9.5 Fiber Cable Assemblies.28 9.5.1 Fiber Cable Attenuation 29 9.5

32、.1.1 Overall Link Attenuation .29 9.5.2 Temperature Ranges 29 9.5.3 Vibration29 9.6 Launch Conditions.29 9.6.1 Intent .29 9.6.2 Procedure for LED Based System 29 9.6.2.1 Test Equipment Requirements.30 9.6.2.1.1 Launch Condition Simulator (see 9.6.2.2.1) 30 9.6.2.1.2 Optical Power Detector30 ARINC SP

33、ECIFICATION 628 PART 4A TABLE OF CONTENTS vii 9.6.2.2 Launch System Configuration .30 9.6.2.2.1 Launch Condition Simulator 30 10.0 IN-SEAT POWER NETWORK.31 10.1 Introduction31 10.1.1 Current Harmonics31 10.2 Unit Specification.31 10.2.1 Master Control Unit .31 10.2.1.1 Power Supply .32 10.2.1.2 Circ

34、uit Breaker32 10.2.1.3 Ground Fault Interrupt (GFI).34 10.2.1.4 Power Management .34 10.2.1.5 System Cut-off and Reset 35 10.2.1.6 Connected Device Power Availability.35 10.2.1.7 Seat Control Data.35 10.2.1.8 Configuration Data .35 10.2.1.9 Mechanical Interface 37 10.2.1.10 Electrical Interface37 10

35、.2.1.11 BITE .37 10.2.2 Power Floor Disconnect37 10.2.2.1 Mechanical Interface 38 10.2.2.2 Electrical Interface38 10.2.3 Seat Interface Box 38 10.2.3.1 Mechanical Interface 38 10.2.3.2 Electrical Interface38 10.2.4 Control Data for Seats 38 ATTACHMENTS 1 Block Diagram for Cabin Distribution Network.

36、44 2 Seat Related Network45 3 Overhead Video Network.70 4 Cabin Management Network .78 5 Bulkhead Telecom Network.91 6 Cabin Electronics Compartment92 7 Cable Characteristics.99 8 Data Requirements107 ARINC SPECIFICATION 628 PART 4A TABLE OF CONTENTS viii 9 Technical Data.109 10 Fiber Optic Intermat

37、eability and Interoperability Provisions.113 11 In-Seat Power Network Diagrams .116 APPENDICES A List of Acronyms 127 B Link Margin Analysis Instructions 131 C Wiring Diagram Symbols .132 D Optional Slide Latch Assemblies .133 ARINC Standard Errata Report ARINC IA Project Initiation/Modification (AP

38、IM) ARINC SPECIFICATION 628 PART 4A - Page 1 1.0 INTRODUCTION 1.1 Purpose of this Document ARINC Specification 628 defines general architectural philosophy and aircraft infrastructure for the proper use and interface of various cabin related IFE equipment. Consistency with ARINC Specification 628 al

39、lows each respective system to operate in concert when integrated with other relevant cabin equipment. ARINC Specification 628 Part 4A defines standards for the aircraft IFE Cabin Distribution System (CDS) wiring, connectors, power, identification codes, space envelopes and mounting principles. The

40、equipment itself is not a subject of this specification because it may be unique to the system manufacturer and/or marketplace-driven. Design guidelines are included for informational purposes as these guidelines impact the interfaces and installation of cabin equipment aboard the aircraft. Function

41、al improvements are capable of being performed through the addition or enhancement of modules without modification on the aircraft. The CDS should be designed to support an airplane configuration, but scaleable to all commercial aircraft types. A generic configuration of cabin subsystems interconnec

42、tion is shown in Part 1 and Part 2, “Cabin Equipment Interfaces Block Diagram.” The block diagram also includes connection with avionics that contribute to the operation of the cabin. 1.2 Related Documents This document is intended to be used in conjunction with ARINC Specification 628, “Cabin Equip

43、ment Interfaces, Parts 1, 2, 3 and 5, Cabin Management and Entertainment System.” Part 1 defines the interfaces between cabin management and entertainment systems and selected peripheral equipment. Part 2 defines the interfaces of the seat-mounted equipment. Part 3 defines the electrical interface b

44、etween the CDS and the aircraft. Part 5 will define the in-seat wiring installation practices. The latest revisions of the following documents are pertinent to the design of equipment intended to meet this standard. AC 43.13, Acceptable Methods, Techniques, and Practices-Aircraft Inspection and Repa

45、ir ARINC Specification 413: Guidance for Aircraft Electrical Power Utilization & Transient Protection ARINC Specification 485: Cabin Equipment Protocol, Part 1 Head End Equipment (proposed) ARINC Characteristic 535: Lightweight Headset and Boom Microphone ARINC Specification 600: Air Transport Avion

46、ics Equipment Interfaces ARINC Report 604: Guidance for Design and Built-in Test Equipment (BITE) ARINC SPECIFICATION 628 PART 4A - Page 2 1.0 INTRODUCTION ARINC Report 606: Guidance for Electrostatic Sensitive Device Utilization and Protection ARINC Report 607: Design Guidance for Avionics Equipmen

47、t ARINC Report 609: Design Guidance for Aircraft Electrical Power ARINC Report 624: Design Guidance for Onboard Maintenance System (OMS) ARINC Specification 626: Standard ATLAS for Modular Test ARINC Specification 628: Cabin Equipment Interfaces (CEI) Part 1, Cabin Management and Entertainment Syste

48、m - Peripherals ARINC Specification 628: Cabin Equipment Interfaces (CEI) Part 2, Cabin Management and Entertainment System - Seat Interfaces ARINC Specification 628: Cabin Equipment Interfaces (CEI) Part 3, Cabin Management and Entertainment System - In-Flight Entertainment ARINC Specification 628:

49、 Cabin Equipment Interfaces (CEI) Part 4B, Cabin Management and Entertainment System - Cabin Distribution System (CDS) - Star Wiring ARINC Specification 628: Cabin Equipment Interfaces (CEI) Part 5, Cabin Management and Entertainment System - In-Seat Wiring Installation Practices ARINC Specification 628: Cabin Equipment Interfaces (CEI) Part 6, Fiber Optic Cable Assembly General ARINC Specification 628: Cabin Equipment Interfaces (CEI) Part 7, Cabin Equipment Cooling General Specification ARINC Characteristic 741: Aviation Sa