ASD-STAN PREN 3716-001-1997 Aerospace Series Connector Single-Way with Triaxial Interface for Transmission of Digital Data Part 001 Technical Specification (Edition P 1)《航空航天系列 数字数.pdf
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1、 STD-AECMA PREN 37Lb-OOL-ENGL 1797 D LU123LL 0033227 782 AECMA STANDARD prEN 37 1 6-00 1 NORME AECMA Edition P 1 AECMA NORM May 1997 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES (AECMA) Gulledelle 94 - 8-1200 BRUXELLES - Tel. (32) 2 775 81 10 - Fax. (32) 2 775 81 11 ICs : 49.060 Edi
2、tion approved for publication 1997-05-30 Descriptors : C2 Chairman Comments should be sent within six months after the date of publication to Gulledelle 94 AECMA Mr Pezzetta 8-1 200 BRUXELLES ENGLISH VERSION Aerospace series Connector, single-way, with triaxial interface, for transmission of digital
3、 data Part O01 : Technical specification Srie arospatiale Luft- und Raumfahrt Connecteur, monovoie, Steckverbinder, triaxial avec interface triaxial, pour transmission de donnes numriques Partie O01 : Spcification technique fr digitale Datenbertragung in einer Richtung Teil O01 : Technische Lieferbe
4、dingungen This “Aerospace Series” Prestandard has been drawn up under the responsibility of AECMA (The European Association of Aerospace Industries). It is published on green paper for the needs of AECMA-Members. It has been technically approved by the experts of the concerned Technical Committee fo
5、llowing comment by the Member countries. Subsequent to the publication of this Prestandard, the technical content shall not be changed to an extent that interchangeability is affected, physically or functionally, without re-identification of the standard. After examination and signature of the AECMA
6、 Standard Checking Centre INPSI and formal agreement of the Official Services of the Member countries it will be submitted as a draft European Standard to CEN (European Committee for Standardization) for formal vote. STD-AECMA PREN 373b-003-ENGL 3777 I LOL2333 0033230 4T4 I Page 2 prEN 3716-001 : 19
7、97 I Contents list 1 2 3 4 5 6 7 8 9 10 11 Scope Normative references Definitions Description Design Definition drawings and masses Tests Quality assurance Designation and marking Packaging Packing 12 Storage Page 3 3 4 4 4 4 9 14 17 18 18 18 STD-AECMA PREN 374b-1-ENGL L777 3032331 0033233 330 H Pag
8、e 3 prEN 3716-001 : 1997 1 Scope This standard applies to single-way connectors with triaxial interfaces used in the transmission of digital data, with the two-core shielded cables in accordance with EN 3375-003, EN 3375-004 and EN 3375-005. This standard defines the general characteristics of conne
9、ctors with screw couplings usable up to a frequency of 5 MHz. It specifies the conditions of qualification, acceptance and quality assurance. It defines the test programmes and groups. Temperature class : - 65OC to 150C 2 Normative references This European Standard incorporates by dated or undated r
10、eference provisions from other publications. These normative references are cited at the appropriate places in the text and the publications are listed hereafter. For dated references, subsequent amendments to or revisions of any of these publications apply to this European Standard only when incorp
11、orated in it by amendment or revision. For undated references the latest edition of the publication referred to applies. EN2591 * EN 3042 EN 3155-001 EN 3375-003 EN 3375-004 EN 3375-005 MIL-A-8243D MIL-C-87936 M I L-H -5 606 E MIL-L-7808H MIL-L-23699C MIL-STD-454 MI L-T-56 24L FED-STD-H28 Aerospace
12、series - Elements of electrical and optical connection - Test methods - General Aerospace series - Quality assurance - EN aerospace products - Qualification procedure Aerospace series - Electrical contacts used in elements of connection - Part O01 : Technical specification 1) Aerospace series - Cabl
13、es, electrical, for signal data transmissions - Part 003 : Cable, bifilar, double-braid - Product standard 2) Aerospace series - Cables, electrical, for signal data transmissions - Part 004 : Cable, bifilar, singie-braid - Product standard 2) Aerospace series - Cables, electrical, for signal data tr
14、ansmissions - Part 005 : Cable, bifilar, double-braid, high immunity - Product standard 2) Anti-icing and deicing-defrosting fluids 3) Cleaning compounds, aircraft exterior surfaces, water diluable 3) Hydraulic fluid, petroleum base, aircraft, missile and ordnance 3) Lubricating oil aircraft turbine
15、 engine, synthetic base, NATO code number 0-1 48 3) Lubricating oil, aircraft turbine engine, synthetic base 3) Electronic equipment, standard general requirements for 3) Turbine fuel, aviation, grades JP-4, JP-5 and JP-5/JP-8 ST 3) Screw thread standards for federal services 3) * Including ail its
16、parts quoted 1) Published as AECMA Prestandard at the date of publication of this standard 2) In preparation at the date of publication of this standard 3) Published by : Department of Defense (DOD), the Pentagon, Washington D.C. 20301 USA. STD*AECMA PREN 373b-OO3-ENGL 3797 1012311 0033232 277 M Pag
17、e 4 prEN 371 6-001 : 1997 3 Definitions For the purposes of this standard, the definitions given in EN 2591 and EN 31 55-001 apply. 4 Description The triaxial connectors are the solder or crimp contact type, with mechanical end stop. The coupling system is the screw type ; at the end of coupling the
18、 housings are mechanically stopped. 4.1 Receptacle Fixing is by nut, anti-vibration washer and gasket seal. 4.2 Plug The knurled coupling ring mounted permanently on the plug allows the connectors to be coupled and decoupled. 4.3 Materials and surface treatment When dissimilar metals are in close co
19、ntact, adequate protection against corrosion shall be used to ensure that the electro-chemical potential difference does not exceed 0,25 V. 4.3.1 Housing Copper alloy, tin plated. 4.3.2 Contact Copper alloy, gold-plated over an appropriate undercoat. 4.3.3 Insert The materials used shall have electr
20、ical and mechanical characteristics compatible with the required use. 4.3.4 Ferrule Material identical to that used for housing. 5 Design The insert is not removable. It is retained mechanically in the housing. The fronts of the inserts are designed to guarantee the seal when the connectors are mate
21、d. 6 Definition drawings and masses The general definition drawings and masses of the receptacles, plugs and flight caps are given in the product standards. STD.AECMA PREN 37Lb-001-ENGL 1997 m LOL23Ll 0033233 Ln3 m 1,55 * 0.70 I I I Page 5 prEN 3716-001 : 1997 End of pin contact 6.1 Receptacle matin
22、g dimensions 6.1.1 With socket contact See figures 1 and 2. Dimensions and tolerances are in millimetres. 2,28 * 0.60 I 8,80 min. I - - I Point of contact with a flat-ended pin # 1,850 2 0,005 I U *I5 - Il.40 I I -.- , I I 11.35 min. - I Figure 1 0,254 min. I I End of socket contact 0,450 max. 1: 1
23、I Reference plane 0 4 compatible with intermediate pin Figure 2 Page 6 prEN 3716-001 : 1997 0,254 min. I I 6.1.2 With pin contact See figure 3. Dimensions and tolerances are in millimetres. End of insulator Point of contact with flat-ended oin general appearance. Final examination : no loosening of
24、parts, no cracking, no wear affecting the function, no part detached. As per 6 and product standard Test applicable to central and intermediate contacts. Measurement points on the cable as close as possible to the contacts, depending on the configuration of the test assemblies. Cable type : EN 3375-
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