AECMA PREN 4176-1999 Aerospace Series Lockbolts 100 Degree Countersunk Normal Head or Protruding Head Tension- Sheartype Close Tolerance in Titanium Alloy TI-P64001 Anodized or wit.pdf
《AECMA PREN 4176-1999 Aerospace Series Lockbolts 100 Degree Countersunk Normal Head or Protruding Head Tension- Sheartype Close Tolerance in Titanium Alloy TI-P64001 Anodized or wit.pdf》由会员分享,可在线阅读,更多相关《AECMA PREN 4176-1999 Aerospace Series Lockbolts 100 Degree Countersunk Normal Head or Protruding Head Tension- Sheartype Close Tolerance in Titanium Alloy TI-P64001 Anodized or wit.pdf(17页珍藏版)》请在麦多课文档分享上搜索。
1、STDaAECflA PREN 417b-ENGL 1999 1012311 0017360 781 AECMA STANDARD prEN 4176 NORME AECMA Edition P I AECMA NORM Decem ber 1999 PUBLISHED BY ME EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES (AECMA) Gulledelle 94 - 8-1200 BRUXELLES - Tel. (+32) 2 775 81 10 - Fax. (+32) 2 775 81 11 ICs: 49.030.60 Descrip
2、tors: aircraft industry, aircraft equipment, rivet, titanium alloy, quality assurance, specification, characteristic, inspection, test ENGLISH VERSION Aerospace series Lockbolts, 100“ countersunk normal head or protruding head, tension- / sheartype, close tolerance, in titanium alloy TLP64001, anodi
3、zed or with aluminium pigmented coating Collars in titanium TLP99002 or aluminium alloy 2024 Metric series Technical specification Srie arospatiale Rivets bague sertie, tte fraise 100“ normale ou tte cylindrique, traction ou cisaillement, tolrance serre, en alliage de titane TLP64001, anodiss ou ave
4、c revtement alumino-organique Bagues en titane TLP99002 ou en alliage daluminium 2024 Srie mtrique Spcification technique Luft- und Raumfahrt Paniete, mit 100“ normalem Senkkopf oder Universalkopf, Zug- Schertyp, aus Titanlegierung TLP64001, anodisiert oder mit Aluminium pigmentierter Beschichtung R
5、inge aus Titan TLP99002 oder Aluminiumlegierung 2024 Metrische Reihe Technische Lieferbedingung 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.
6、It has been technically approved by the experts of the concerned Technical Committee following 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 of functionally,
7、without re-identification of the standard. After examination and signature of the AECMA Standard Checking Centre (NPS) and formal agreement of the Official Services of fhe Member countries if will be submitted as a draft European Standard to CEN (European Committee for Standardiza tion) for formal v
8、ote. Nota -Extra copies can be SUpplied by B.N.A.E. - Technopolis 54 - 199, rue Jean-Jacques Rousseau - 92138 ISSY-LES-MOULINEAUX CEDEX Edition approved for publication 1999-12-31 C3 Chairman I Comments should be sent within six months after the date of publication to AECMA Gulledelle 94 6-1 200 BRU
9、XELLES Mr Visconti Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 2 STD.AECflA PREN 4L7b-ENGL 1999 = LOL23LL 00L73bL bLB prEN 41 76: 1999 Content
10、s Scope . 3 Normative references . . 3 Terms and definitions . 4 Quality assurance 5 Requirements . 5 Delivery . 9 . Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license
11、 from IHS-,-,-STDmAECMA PREN 417h-ENGL li999 W 1012311 0037362 554 Page 3 prEN 41 76: 1999 1 Scope This specification specifies the characteristics, qualification and acceptance requirements for tension- I sheartype 100“ countersunk normal head or protruding head close tolerance lockbolts in titaniu
12、m alloy TLP64001 , anodized or with aluminium pigmented coating and collars in titanium TI-P99002 or aluminium alloy 2024, metric series, for use as pemanent attachment fasteners in shear applications. It is applicable whenever referenced. EN 3042 EN 4172 EN 4173 EN 4174 EN 4175 EN 4401 EN 4402 B46.
13、1: 1995 MIL-STD-105E NASMI 31 2 NAS 527: 1962 NAS 1413:1997 2 Normative references Pins and Collars, Swage Locking 4) Aerospace series - Quality assurance - EN aerospace products - Qualification procedure Aerospace series - Lockbolts, protruding head, sheartype, close tolerance, in titanium alloy TI
14、-P64001, anodized, metric series - Classification: 1 100 MPa (at ambient temperature) I 31 5 “C 1) Aerospace series - Lockbolts, 100“ countersunk normal head, sheartype, close tolerance, in titanium alloy TI-P64001 , anodized or aluminium coated, metric series - Classification: 1 100 MPa (at ambient
15、 temperature) i 315 “C 1) Aerospace series - Collars, swage locking, sheartype, in aluminium alloy 2024, anodized or chromated, metric series 1) Aerospace series - Collars, flanged swage locking, sheartype, in titanium TI-P02, metric series 1) Aerospace series - Lockbolts, protruding head, sheartype
16、, close tolerance, in titanium alloy TLP64001 , with aluminium pigmented coating, metric series - Classification: 1 100 MPa (at ambient temperature) / 315 “C 1) Aerospace series - Lockbolts, 100“ countersunk normal head, sheartype, close tolerance, in titanium alloy TI-P64001, with aluminium pigment
17、ed coating, metric series - Classification: I I O0 MPa (at ambient temperature) I 31 5 “C 1) Surface Texture (Surface Roughness, Waviness, and Lay) 2) Sampling Procedures and Tables for Inspection by Attributes 3) Fastener Test Methods 4) Inspection Procedure for Flush Fasteners 4) 1) Published as A
18、ECMA Prestandard at the date of publication of this standard 2) Published by: American Society of Mechanical Engineers (ASME), 3, Park Avenue, New York, NY 10017, USA 3) Published by: Department of Defense (DOD), the Pentagon, Washington, DC 20301, USA 4) Published by: Aerospace Industries Associati
19、on of America, Inc. (AIA), 1250 Eye Street, NW; Suite 1100, Washington, DC 20005, USA Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-_ STD*AECMA PREN
20、Ii37b-ENGL 3999 - 30323Ll 0037363 490 Page 4 prEN 4176: 1999 3 Terms and definitions For the purposes of this standard, the following terms and definitions apply. 3.1 inspection lot shall consist of finished parts which are of the same part number, fabricated by the same process, that are treated to
21、gether in one furnace lot from the same heat of material and submitted for manufacturers inspection of the same time 3.2 crack a clear crystalline break passing through the grain boundary without inclusion of foreign elements 3.3 seam open surface defect 3.4 surface defect caused by folding over met
22、al fins or sharp corners and then compressing them into the surface lap 3.5 nick surface defect caused by the sharp edge of a cutting element 3.6 gouge surface defect caused by a scraft 3.7 inclusions non-metallic particles originating from the material manufacturing process. These particles may be
23、isolated or arranged in strings. 3.8 sampling plan a plan according to which one or more samples are taken in order to obtain information and possibly to reach a decision 3.9 acceptable quality level AQL a quality level which in a sampling plan corresponds to a specified but relatively high probabil
24、ity of acceptance It is the maximum per cent defective (or the maximum number of defects per hundred units) that, for purposes of sampling inspection can be considered satisfactory as a process average. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under l
- 1.请仔细阅读文档,确保文档完整性,对于不预览、不比对内容而直接下载带来的问题本站不予受理。
- 2.下载的文档,不会出现我们的网址水印。
- 3、该文档所得收入(下载+内容+预览)归上传者、原创作者;如果您是本文档原作者,请点此认领!既往收益都归您。
本资源只提供5页预览,全部文档请下载后查看!喜欢就下载吧,查找使用更方便
5000 积分 0人已下载
下载 | 加入VIP,交流精品资源 |
- 配套讲稿:
如PPT文件的首页显示word图标,表示该PPT已包含配套word讲稿。双击word图标可打开word文档。
- 特殊限制:
部分文档作品中含有的国旗、国徽等图片,仅作为作品整体效果示例展示,禁止商用。设计者仅对作品中独创性部分享有著作权。
- 关 键 词:
- AECMAPREN41761999AEROSPACESERIESLOCKBOLTS100DEGREECOUNTERSUNKNORMALHEADORPROTRUDINGHEADTENSIONSHEARTYPECLOSETOLERANCEINTITANIUMALLOYTIP64001ANODIZEDORWITPDF

链接地址:http://www.mydoc123.com/p-421147.html