AIR FORCE MIL-HDBK-1760 A-2004 AIRCRAFT STORE ELECTRICAL INTERCONNECTION SYSTEM《飞机 备用电器联网系统》.pdf
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1、 METRIC MIL-HDBK-1760A 10 March 2004 Superseding: MIL-HDBK-1760 15 February 2000 DEPARTMENT OF DEFENSE HANDBOOK AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM This handbook is for guidance only. Do not cite this document as a requirement. AMSC: N/A AREA SESS DISTRIBUTION STATEMENT A. Approved for
2、public release; distribution is unlimited. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-HDBK-1760A ii FOREWORD 1. This handbook was developed by a team including members from the three U.S. military services, the UK MOD, the SAE AS-1B committe
3、e, and contractors. It includes information previously published in document ASD-TR-87-5028 with certain elements of ASD-TR-91-5009. Some of this information was also published in DEF-STAN-00-69 (Part II), which is written around MIL-STD-1760B. This revision of this handbook is written around MIL-ST
4、D-1760D and assumes that the reader is also reading 1760D. 2. This handbook provides information on the implementation of a standardized electrical interconnection system, as defined by MIL-STD-1760, into both current and future aircraft and stores. It provides guidance on design considerations and
5、options for including the standard interface capability at the aircrafts store stations and for providing a common electrical interface on carriage stores and mission stores. As a handbook, it cannot be invoked as a requirement in a contract. 3. Trends in weapon system designs (aircraft and stores)
6、caused concern over the general proliferation of aircraft-to-store electrical interfacing requirements and the resulting high cost to achieve interoperability between aircraft and stores. The intent of MIL-STD-1760 is to reduce the aircraft/store electrical integration problem by specifying a standa
7、rd electrical interface between aircraft and stores. The standard electrical interface is based on recognized trends in store management systems which use serial digital data transmission for control, monitor and release of stores. In general, the handbook provides the following: a. An overview of M
8、IL-STD-1760 requirements, exclusions and future growth provisions. b. Detail design considerations applicable to the Aircraft Station Interface (ASI), Mission Store Interface (MSI), Carriage Store Interface (CSI) and the Carriage Store Station Interface (CSSI), with application guidelines. c. Aircra
9、ft/Store Physical Design Considerations. d. A commentary on the purpose of each requirement in MIL-STD-1760. e. A summary of changes between the various revisions of MIL-STD-1760. 4. Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in improving t
10、his document should be addressed to: ASC/ENOI, 2530 Loop Road West, Wright-Patterson AFB, OH 45433-7101, or e-mailed to: James.Byrdwpafb.af.mil. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-HDBK-1760A iiiCONTENTS (Abbreviated - limited to 2 di
11、git paragraph numbers) PARAGRAPH PAGE 1. SCOPE1 1.1 Purpose.1 1.2 Background. 1 1.3 Limitations. 2 2. APPLICABLE DOCUMENTS 3 2.1 General. 3 2.2 Government documents3 2.3 Other Government documents, drawings, and publications. 4 2.4 Non-Government standards and other publications5 2.5 MIL-STD-1760.5
12、3. DEFINITION OF TERMS AND ACRONYMS 6 3.1 Definition and use of terms. 6 3.2 Acronyms and Abbreviations. .9 4. GENERAL .16 4.1 Scope of the standard. 16 4.2 MIL-STD-1760 interface definitions.19 4.3 MIL-STD-1760 interface elements. .20 4.4 MIL-STD-1760 classes23 4.5 Summary of requirements.23 4.6 Pu
13、rpose, goals and projected benefits of MIL-STD-1760. 29 4.7 The MIL-STD-1760 application process33 5. SYSTEM DESIGN.36 5.1 General. 36 5.2 Aircraft design considerations.36 5.3 Store design considerations47 5.4 System safety features51 5.5 Interface design/documentation process. .73 5.6 Future trend
14、s and considerations77 6. DIGITAL DATA BUS INTERFACE79 6.1 Overview of data bus application to AEIS. 79 6.2 Data communications and system control. .84 6.3 Network reconfiguration. .86 6.4 Data bus interface EMI considerations. 88 6.5 Architectural considerations94 6.6 Data bus topology issues. .99
15、6.7 Mission store issues107 7. DISCRETES113 7.1 Release consent. 113 7.2 Interlock interface127 7.3 Address interface. .135 8. HIGH BANDWIDTH INTERFACES.149 8.1 General. 149 8.2 Detailed discussion on HB requirements. .154 Provided by IHSNot for ResaleNo reproduction or networking permitted without
16、license from IHS-,-,-MIL-HDBK-1760A iv PARAGRAPH PAGE 8.3 Cable selection for HB interfaces175 8.4 HB Type A signal path linear distortion. 175 8.5 HB Type A signal path system-level performance budget. .188 8.6 Video signal path system-level performance. .199 8.7 Requirements for GPS RF Signals. 20
17、4 9. LOW BANDWIDTH (LB)210 9.1 LB characteristics210 9.2 Aircraft design requirements. 211 9.3 Mission store low bandwidth interface. .214 9.4 Grounding requirements. 216 9.5 Differential signal transmission. 216 9.6 Electromagnetic considerations. .217 9.7 Analog network BIT.220 9.8 Insertion gain.
18、221 9.9 Equalization requirements.221 9.10 Noise. 221 10. POWER AND STRUCTURE GROUND INTERFACES 223 10.1 Power source rating. .223 10.2 Power return circuits interference issues. .224 10.3 Phase sequence. 226 10.4 Shielding. 228 10.5 Aircraft power control and power characteristics at the ASI228 10.
19、6 Carriage store power control and distribution. 237 10.7 Mission Store power control and power characteristics at the MSI.240 10.8 Store power return interfaces246 10.9 Operational power interfaces. .246 10.10 Circuit protection. 247 10.11 Structure ground. 252 10.12 270 VDC254 11. RESERVED FUNCTIO
20、N 270 VDC 260 12. RESERVED FUNCTION FIBER OPTICS 261 12.1 Characteristics of fiber optics261 12.2 Strategy for implementation of fiber optics261 12.3 Proposed interface. .261 13. ELECTROMAGNETIC COMPATIBILITY 263 13.1 Reason for lack of EMC requirements. .263 13.2 EMC requirements that were in Revis
21、ion B.263 14. CONNECTORS, WIRING AND UMBILICALS 268 14.1 Aircraft station interface connectors271 14.2 Mission store interface. .283 14.3 Carriage store interface (CSI). 290 14.4 Carriage store station interface (CSSI). 290 14.5 Umbilicals and buffers.290 14.6 Low bandwidth cable characteristics.300
22、 14.7 LB connectors. 300 14.8 Use of existing audio wiring in LB installation. 301 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-HDBK-1760A vPARAGRAPH PAGE 15. COMMENTARY ON THE REQUIREMENTS OF MIL-STD-1760D.302 15.1 Scope. .302 15.2 Applicable
23、 documents. 302 15.3 Definitions. 303 15.4 General requirements. 305 15.5 Detailed requirements. 311 15.6 NOTES359 16. CARRIAGE STORES362 17. LOGICAL DEFINITION .363 17.1 Scope. .363 17.2 Applicable documents. 364 17.3 Definitions. 364 17.4 Requirements364 17.5 Table B-XXXI.548 18. COMPATIBILITY BET
24、WEEN VERSIONS OF MIL-STD-1760 550 19. CHANGES BETWEEN MIL-STD-1760 AND MIL-STD-1760A551 19.1 MIL-STD-1760 First Issue. 551 19.2 MIL-STD-1760 Notice 1. .551 19.3 MIL-STD-1760 Notice 2. .551 19.4 MIL-STD-1760A. .551 20. CHANGES BETWEEN MIL-STD-1760A AND MIL-STD-1760B .552 20.1 MIL-STD-1760A Notice 1.
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