ARINC-628P4B-1999.pdf
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1、CABIN EQUIPMENT INTERFACES PART 4B CABIN MANAGEMENT AND ENTERTAINMENT SYSTEM CABIN DISTRIBUTION SYSTEM - STAR WIRING ARINC SPECIFICATION 628P4B PUBLISHED: JUNE 18, 1999 AN AA DOCUMENT Prepared by AIRLINES ELECTRONIC ENGINEERING COMMITTEE Published by AERONAUTICAL RADIO, INC. 2551 RIVA ROAD, ANNAPOLI
2、S, MARYLAND 21401 Copyright 1999 by AERONAUTICAL RADIO, INC. 2551 Riva Road Annapolis, Maryland 21401-7465 USA ARINC SPECIFICATION 628P4B CABIN EQUIPMENT INTERFACES PART 4B CABIN MANAGEMENT AND ENTERTAINMENT SYSTEM CABIN DISTRIBUTION SYSTEM STAR WIRING Published: June 18, 1999 Prepared by the Airlin
3、es Electronic Engineering Committee Characteristic 628P4BAdopted by the Airlines Electronic Engineering Committee:October 28, 1998 Characteristic 628P4BAdopted by the Industry:April 23, 1999 -,-,- FOREWORD Activities of AERONAUTICAL RADIO, INC. (ARINC) and the Purpose of ARINC Reports and Specificat
4、ions Aeronautical Radio, Inc. is a corporation in which the United States scheduled airlines are the principal stockholders. Other stockholders include a variety of other air transport companies, aircraft manufacturers and non-U.S. airlines. Activities of ARINC include the operation of an extensive
5、system of domestic and overseas aeronautical land radio stations, the fulfillment of systems requirements to accomplish ground and airborne compatibility, the allocation and assignment of frequencies to meet those needs, the coordination incident to standard airborne compatibility, the allocation an
6、d assignment of frequencies to meet those needs, the coordination incident to standard airborne communications and electronics systems and the exchange of technical information. ARINC sponsors the Airlines Electronic Engineering Committee (AEEC), composed of airline technical personnel. The AEEC for
7、mulates standards for electronic equipment and systems for the airlines. The establishment of Equipment Characteristics is a principal function of this Committee. It is desirable to reference certain general ARINC Specifications or Report which are applicable to more than one type of equipment. Thes
8、e general Specifications and Reports may be considered as supplementary to the Equipment Characteristics in which they are referenced. They are intended to set forth the desires of the airlines pertaining to components and general design, construction and test criteria, in order to insure satisfacto
9、ry operation and the necessary interchangeability in airline service. The release of a Specification or Equipment Characteristics should not be construed to obligate ARINC or any airline insofar as the purchase of any components or equipment is concerned. An ARINC Report ( Specification or Character
10、istic) has a twofold purpose, which is: (1)To indicate to the prospective manufacturers of airline electronic equipment the considered opinion of the airline technical people, coordinated on an industry basis, concerning requisites of new equipment, and (2)To channel new equipment designs in a direc
11、tion which can result in the maximum possible standardization of those physical and electrical characteristics which influence interchangeability of equipment without seriously hampering engineering initiative. ii -,-,- ARINC SPECIFICATION 628 PART 4B TABLE OF CONTENTS ITEMSUBJECTPAGE iii 1.0INTRODU
12、CTION1 1.1Purpose of this Document1 1.2Related Documents1 1.3Cabin Distribution system Description 2 1.3.1Seat Related Network2 1.3.2Overhead Network2 1.3.2.1Overhead Video Network2 1.3.2.2Cabin Management Network2 1.3.2.3Telecom Network2 1.3.3Cabin Electronics Compartment2 1.3.4Remote Control Cente
13、r2 1.3.5Electronics-Avionics Bay2 2.0SEAT AND OVERHEAD RELATED NETWORK3 2.1Introduction3 2.2Unit Specifications3 2.2.1Cabin Electronics Compartment (CEC)3 2.2.2Area Distribution Panel (ADP)3 2.2.2.1Mechanical Interface3 2.2.2.2Electrical Interface3 2.2.2.2.1Connectors and Pin Arrangement3 2.2.2.2.2P
14、ower Requirements3 2.2.3FDI (Floor Disconnect Interface)3 2.2.3.1Mechanical Interface3 2.2.3.2Electrical Interface3 2.2.3.2.1Connectors and Pin Arrangement3 2.2.3.2.2Power Requirements3 2.2.4Seat Electronics Box (SEB)3 2.2.4.1Mechanical Interface4 2.2.4.2Electrical interface4 2.2.4.2.1Connectors and
15、 Pin Arrangement4 2.2.4.2.2Power Requirements4 2.3Wiring Specification4 2.3.1Wiring Between CEC and ADP4 2.3.2Wiring Between ADP and FDI4 2.3.3Wiring Between FDI and SEB4 3.0OVERHEAD VIDEO NETWORK5 3.1Introduction5 3.2Unit Specification5 3.2.1Cabin Electronics Compartment5 3.2.1.1Mechanical Interfac
16、e5 3.2.1.2Electrical Interface5 3.2.2Tapping Unit5 3.2.2.1Mechanical Interface5 3.2.2.2Electrical Interface5 3.3Wiring Specification5 3.3.1Wiring Between CEC and TU5 3.3.2Wiring Between TU and TU5 3.3.3Wiring Between TU and Display Unit5 4.0CABIN MANAGEMENT NETWORK6 5.0BULKHEAD TELECOM NETWORK7 6.0C
17、ABIN ELECTRONICS COMPARTMENT (CEC)8 6.1Introduction8 6.2Wiring Specification8 6.2.1Wiring Between CEC and Aircraft8 6.2.2Wiring Between CEC and ADP8 6.2.3Wiring Between CEC and CTU8 6.2.4Wiring Between CEC and PFIS8 6.2.5Wiring Between CEC and RCC8 6.2.6Wiring Between CEC and Cabin Overhead Network8
18、 -,-,- ARINC SPECIFICATION 628 PART 4B TABLE OF CONTENTS ITEMSUBJECTPAGE iv 7.0WIRING AND EQUIPMENT IDENTIFICATION9 8.0DATA REQUIREMENTS10 ATTACHMENTS 1Cabin Distribution System11 2Seat Related network12 3Overhead Video Network23 4Cabin Management Network29 5Bulkhead Telephone network30 6Cabin Elect
19、ronics Compartment31 APPENDIX ALIST OF ACRONYMS39 BWIRING DIAGRAM SYMBOLS40 -,-,- ARINC SPECIFICATION 628 PART 4B Page 1 1.0 INTRODUCTION 1.1 Purpose of this Document ARINC Specification 628 part 4B defines Star-wired architecture and aircraft infrastructure for the proper use and interface of vario
20、us cabin related IFE equipment. Compliance with ARINC Specification 628 allows each respective system to operate in concert when integrated with other relevant cabin type equipment. ARINC Specification 628 Part 4B defines standards for the aircraft IFE Cabin Distribution System (CDS) wiring, connect
21、ors, power, identification codes, space envelopes and mounting principles. The 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 o
22、n the interfaces and installation of cabin equipment aboard the aircraft. Functional improvements are capable of being performed through the addition or enhancement of modules without modification on the aircraft. The CDS should be designed for maximum requirements but scaleable to all commercial ai
23、rcraft types. A generic configuration of cabin subsystems interconnection is shown in Part 1 and Part 2, “Cabin Equipment Interfaces Block Diagram”. The block diagram also includes connection with other avionics that contribute to the operation of the cabin. 1.2 Related Documents This document is in
24、tended to be used in conjunction with ARINC Specification 628, “Cabin Equipment 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 interfa
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