GB/T 13536-2018 English PDF

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GB/T 13536-2018: Connectors for aircraft ground electrical supplies
Status: Valid

GB/T 13536: Historical versions

Standard ID	USD	BUY PDF	Lead-Days	Standard Title (Description)	Status
GB/T 13536-2018	299	Add to Cart	3 days	Connectors for aircraft ground electrical supplies	Valid
GB/T 13536-1992	839	Add to Cart	4 days	Connectors for ground electeical supplies	Obsolete

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Basic data

Standard ID: GB/T 13536-2018 (GB/T13536-2018)
Description (Translated English): Connectors for aircraft ground electrical supplies
Sector / Industry: National Standard (Recommended)
Classification of Chinese Standard: L23
Classification of International Standard: 31.220.10
Word Count Estimation: 15,140
Date of Issue: 2018-02-06
Date of Implementation: 2018-02-06
Older Standard (superseded by this standard): GB/T 13536-1992
Quoted Standard: ISO 7137
Adopted Standard: ISO 461-1-2003��MOD; ISO 461-2-1985, MOD
Regulation (derived from): National Standard Notice No. 2 of 2018
Issuing agency(ies): State Administration for Market Regulation, China National Standardization Administration
Summary: This standard specifies the design requirements, performance requirements, test methods and dimensions of connectors for aircraft ground power connectors (hereinafter referred to as connectors). This standard applies to aircraft ground power connectors.

GB/T 13536-2018: Connectors for aircraft ground electrical supplies

---This is a DRAFT version for illustration, not a final translation. Full copy of true-PDF in English version (including equations, symbols, images, flow-chart, tables, and figures etc.) will be manually/carefully translated upon your order.
Connectors for aircraft ground electrical supplies ICS 31.220.10 L23 National Standards of People's Republic of China Replacing GB/T 13536-1992 Aircraft ground power connector (ISO 461-1.2003, Aircraft-Connectorsforgroundelectrical supplies-Part 1.design,performanceandtestrequirements; ISO 461-2.1985, Aircraft-Connectorsforgroundelectrical supplies-Part 2.dimensions,MOD) Published on.2018-02-06 2018-02-06 Implementation General Administration of Quality Supervision, Inspection and Quarantine of the People's Republic of China China National Standardization Administration released Directory Preface III 1 Scope 1 2 Normative references 1 3 Terms and Definitions 1 4 Design and Performance Requirements 1 4.1 General 1 4.2 Polarity and Phase Sequence 2 4.3 Current rating 2 4.4 Control Jack Contacts 2 4.5 Voltage Rating 2 4.6 Replacement of plug contacts 2 5 Inspection and Test 2 5.1 Check 2 5.2 Test 2 5.3 Test Method 3 6 Product Identification and Ordering Procedures 5 6.1 Product Identification 5 6.2 Packing 5 6.3 Ordering 5 7 Size 6 7.1 Scope and Use 6 7.2 Size 6

Foreword

This standard was drafted in accordance with the rules given in GB/T 1.1-2009. This standard supersedes GB/T 13536-1992 Aircraft ground power connector, which is a major change from GB/T 13536-1992 as follows. --- Deleted the original Chapter 3 "plane ground power connector" term, added 3.1 "fixed aircraft connector" and 3.2 "terrestrial power supply Free Connector terminology; --- Deleted the original 4.1 basic type, 4.2 end connection type, 4.3 product model, 4.4 rated voltage, rated current and contact even number; --- Remove the original Chapter 5 technical requirements, according to ISO 461-1.2003 increase Chapter 4 design and performance requirements; --- Delete the original Chapter 6 test methods, Chapter 7 inspection rules, according to ISO 461-1.2003 increase Chapter 5 inspections and tests; --- Delete the original Chapter 8 signs, packaging, transportation, storage, according to ISO 461-1.2003 increase Chapter 6 product identification and ordering procedures; --- Delete the original Chapter 9 Quality Assurance Period. This standard uses the redrafted law to modify the use of ISO 461-1.2003 "plane ground power connector Part 1. Design, performance and "Test Requirements" and ISO 461-2.1985 "Aircraft Terrestrial Power Connectors Part 2. Dimensions". Compared with ISO 461-1.2003 and ISO 461-2.1985, the structure is adjusted as follows. --- Replace "5.3.1.1 Types 1, 2, and 3" in ISO 461-1.2003 with "5.3.1.1 Test Procedures" and "5.3.1.2 Types 1, 2, and 3". "5.3.1.2 Type 4" was changed to "5.3.1.3 Type 4". --- Adjusted Chapter 1 of ISO 461-2.1985 to 7.1, Chapter 4 adjusted to 7.2, deleted Chapters 2 and 3. This standard also made the following editorial changes. ---4.1.5 increase "Note. 105 °C for ambient temperature heating rise"; --- Added "ISO 7137" (source of the figure) to ISO 9001-1.2003 5.3.7 before Figure 8-5 and Figure 8-6. This standard was proposed by China Aviation Industry Corporation. This standard is under the jurisdiction of the National Aircraft Standardization Technical Committee (SAC/TC435). This standard was drafted by. Shenyang Xinghua Aviation Electrical Appliance Co., Ltd., Anhui Zhiyi Technology Consulting Co., Ltd., China Aviation Comprehensive Technology Institute of Technology, Chinese People's Liberation Army station in one of the seventeen military representative office. The main drafters of this standard are. Ma Fei, Wang Hongxia, Yang Yusong, Jin Huijie, Sun Haihang, Yu Huimin, and Dong Derong. The previous versions of the standards replaced by this standard are. --- GB/T 13536-1992. Aircraft ground power connector

1 Scope

This standard specifies the design requirements, performance requirements, test methods and connectors for aircraft ground power connectors (hereinafter referred to as connectors). size. This standard applies to aircraft ground power connectors.

2 Normative references

The following documents are indispensable for the application of this document. For dated references, only dated versions apply to this article Pieces. For undated references, the latest version (including all amendments) applies to this document. ISO 7137 Aircraft Airborne Equipment Environmental Conditions and Test Methods (Aircraft-Environmentalconditionsandtest) Proceduresforairborneequipment)

3 Terms and Definitions

The following terms and definitions apply to this document. 3.1 Aircraft fixed connector (socket) aircraftfixed connector (receptacle) The connector mounted on the aircraft receives an external power supply to the aircraft via a ground power free connector. 3.2 Ground Power Free Connector (Plug) groundsupplyfreeconnector(plug) The connector installed on the external ground power cable mates with the fixed connector of the aircraft to supply power to the aircraft.

4 Design and Performance Requirements

4.1 General 4.1.1 Structure The plug structure should be firm, with a certain degree of mechanical strength, able to withstand mechanical vibration and wear during use, and ensure safe operation. No sharp edges. 4.1.2 Antifungal The materials used for sockets and plugs should be mildewproof. 4.1.3 Metallic Materials The metal used should be corrosion-resistant or corrosion-resistant. 4.1.4 Incompatible materials When incompatible materials are used in direct contact, they shall be protected against electrolytic corrosion. ......

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