49.030.01 紧固件综合 标准查询与下载

BS ISO 4580:2021 航天 内部驱动器 TORX PARALOBE 驱动器位 几何定义、测量和技术要求

What is ISO 4580 about? ISO 4580 specifies basic dimensions, characteristics and engineering requirements for TORX® PARALOBE® driver bits used with aerospace fasteners. ISO 4580 also includes basic driver bit configuration, inspection, torque test, and torque test procedure. Who is ISO 4580 for? ISO 4580 on basic dimensions, characteristics and engineering requirements for TORX® PARALOBE® driver bits in aerospace fasteners is applicable to: Aerospace fasteners manufacturers Mechanical engineers  TORX® PARALOBE® driver bits manufacturers Product designers Why should you use ISO 4580 ? TORX® PARALOBE® is a unique, proprietary drive system with full surface drive contact thus reducing stress at the bit/recess contact points. With this drive system, Acument reports that there is 20% greater bit torsional strength and 20% greater drive system strength than the TORX PLUS drive system, and 40% greater torque strength than the TORX drive system. ISO 4580 walks us through basic dimensions, characteristics and engineering requirements for TORX® PARALOBE® driver bits which as we have seen is superior to the other drive systems used in the market, and hence with the use of TORX® PARALOBE®, you will have an edge when it comes to torque strength and drive system strength. The use of ISO 4580:2021 helps to contribute to UN Sustainable Development Goal 9 which aims to ensure the building of resilient infrastructure, promoting inclusive and sustainable industrialization and fostering innovation.  

Aerospace. Drives, internal, TORX PARALOBE driver bit. Geometrical definition, gaging and technical requirements

BS ISO 4579:2021 航天 驱动器 内部 TORX PARALOBE 驱动器 几何定义、测量和技术要求

What is ISO 4579 about? ISO 4579 specifies basic dimensions, characteristics and engineering requirements for TORX® PARALOBE® recesses in aerospace fasteners. ISO 4579 also includes basic fastener recess configuration, recess inspection and fastener recess torque test. Who is ISO 4579 for? ISO 4579 on basic dimensions, characteristics and engineering requirements for TORX® PARALOBE® recesses in aerospace fasteners is applicable to: Aerospace fasteners manufacturers Mechanical engineers  TORX® PARALOBE® recesses manufacturers Product designers Why should you use ISO 4579? TORX® PARALOBE® is a unique, proprietary drive system with full surface drive contact thus reducing stress at the bit/recess contact points. With this drive system, Acument reports that there is 20% greater bit torsional strength and 20% greater drive system strength than the TORX PLUS drive system and 40% greater torque strength than the TORX drive system. ISO 4579 walks us through basic dimensions, characteristics and engineering requirements for TORX® PARALOBE® recesses which as we have seen is superior to the other drive systems used in the market, and hence with the use of TORX® PARALOBE® you will have an edge when it comes to torque strength and drive system strength.

Aerospace. Drives, internal, TORX PARALOBE drive. Geometrical definition, gaging and technical requirements

ISO 4580:2021 航空航天 TORX®PARALOBE®内螺纹驱动钻头 几何定义、测量和技术要求

This document specifies basic dimensions, characteristics and engineering requirements for TORX® PARALOBE®1) driver bits used with aerospace fasteners.

Aerospace - Drives, internal, TORX® PARALOBE® driver bit - Geometrical definition, gaging and technical requirements

ISO 4579:2021 航空航天 TORX®PARALOBE®内部驱动器 几何定义、测量和技术要求

This document specifies basic dimensions, characteristics and engineering requirements for TORX® PARALOBE®1) recesses in aerospace fasteners.

Aerospace - Drives, internal, TORX® PARALOBE® drive - Geometrical definition, gaging and technical requirements

FprEN 4853-2021 航空航天系列-外螺纹紧固件，100°沉头普通头，螺旋驱动凹槽-分类：1100 MPa（在环境温度下）/425°C

Aerospace series - Externally threaded fastener, 100° countersunk normal head, Spiral Drive Recess - Classification: 1100 MPa (at ambient temperature)/425 °C

21/30421021 DC BS ISO 4579 航空航天 驱动器 内部 TORX PARALOBE 驱动器 几何定义、测量和技术要求

BS ISO 4579. Aerospace. Drives, internal, TORX PARALOBE drive. Geometrical definition, gaging and technical requirements

21/30421024 DC BS ISO 4580 航空航天 内部驱动器 TORX PARALOBE 起子头 几何定义、测量和技术要求

BS ISO 4580. Aerospace. Internal drive, TORX PARALOBE, driver bit. Geometrical definition, gaging and technical requirements

BS 2SP 94:2019 航空航天系列 衬套（普通衬套和法兰衬套）、压接垫圈和止推垫圈、保油烧结青铜 规格

1   Scope This British Standard specifies material, dimensions, characteristics and identification of sintered bronze plain and flanged oil‑retaining bushes and oil‑retaining thrust washers for aircraft use. The bushes are charged with lubricating oil and have a normal oil content of from 25% − 30% by volume, within the size range from  3 / 16  in. (4.8 mm) to 2 1 / 2 in. (63.5 mm) nominal bore. NOTE 1 Owing to slight variations between products of different manufacturers, exact dimensions and limits for diameters are not given in this British Standard, as these dimensions are declared by respective manufacturers. Bushes supplied to this British Standard give correct bores when fitted in housings as specified. NOTE 2 The dimensional values depicted are in inch units and are to be regarded as the standard. Where metric mm equivalents are shown, they have been rounded. More accurate conversions should be based on the tables in BS 350, “Conversion factors and tables”.

Aerospace series. Bushes (plain and flanged), press-fit and thrust washers, oil‑retaining sintered bronze. Specification

19/30397937 DC BS EN 6117 航空航天系列 用鲸蜡醇润滑紧固件规范

BS EN 6117. Aerospace series. Specification for lubrication of fasteners with cetyl alcohol

DIN 65946:2017 航空航天系列 特定条件下螺栓和螺母摩擦系数的测定

Aerospace series - Determination of coefficients of friction of bolts and nuts under specific conditions; Text in German and English

KS W ISO 7403-2016 航空航天 花键传动装置 扳手配置 公制系列

Aerospace－Spline drives－Wrenching configuration－Metric series

KS W ISO 7403:2016 航空航天 花键传动 扳手结构 米制系列

Aerospace－Spline drives－Wrenching configuration－Metric series

SAE AS5864A-2015 闷头、24度锥形非扩口、液体连接、配件端的设计标准

FITTING END@ BULKHEAD@ 24��ONE@ FLARELESS@ FLUID CONNECTION@ DESIGN STANDARD

15/30328090 DC BS SP 94 AMD3 青铜挡油衬套和止推垫圈规范 飞机用

BS SP 94 AMD3. Specification for bronze oil-retaining bushes and thrust washers. For aircraft

SAE AS870E-2015 扳手配置，双六角（12 点）驱动，设计标准

WRENCHING CONFIGURATION, BI-HEXAGONAL (12 POINT) DRIVE, DESIGN STANDARD FOR

SAE AIR1551B-2014 扭矩拧紧公制螺钉紧固件

The purpose of this Aerospace Information Report (AIR) is to provide the aerospace propulsion industry with recommended assembly torque limits for threaded fasteners when a common torque value per fastener size is the objective. (The fasteners are based on the dimensional data in MA1518). It also provides a series of curves that show the effect of the coefficient of friction on the axial load produced in a fastener, when the recommended torques are applied.

Torque Tightening Metric Screw Threaded Fasteners

KS W 1553-2013 航天锛峂pline drives锛峂renching configuration锛峂etric系列

Aerospace－Spline drives－Wrenching configuration－Metric series

SAE AS5270-2013 采购规格中抗拉强度为220 ksi的行动加强型UNS N07718镍合金螺栓, 螺钉和螺柱

This procurement specification covers bolts, screws and studs made from a work-strengthened corrosion and heat resistant, age Hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS N07718. The following properties are covered: 220 ksi minimum ultimate tensile strength at room temperature 180 ksi minimum ultimate tensile strength at 900 °F 114 ksi tension to 11.4 ksi tension fatigue at room temperature

Bolts, Screws and Studs, Nickel Alloy, UNS N07718, Work-Strengthened, Tensile Strength 220 ksi, Procurement Specification

SAE J2277-2013 喷丸覆盖面的测定

This SAE Recommended Practice provides procedures some procedure for determining shot penning coverage and relating coverage to part exposure to the media stream.. Effectiveness of shot peening is directly dependent on coverage. Either incomplete or excessive coverage may be detrimental to fatigue strength and life.

Shot Peening Coverage Determination

SAE MA4360A-2013 公制扳手:非变形6和12点扁平螺母

This SAE Metric Aerospace Standard (MA) covers metric double end flare nut wrenches that are designed with the following requirements: a. Non-distorting usage; b. Possessing the strength, clearances, and internal wrenching design to be used on hydraulic tube fittings that conform to the requirements of SAE J 514; c. Transmitting torque to fittings without bearing on the apex of fitting wrenching points. Inclusion of dimensional data in this document is not intended to imply that all of the products described herein are stock production sizes. Consumers are requested to consult with manufacturers concerning lists of stock production sizes.

Metric Wrenches: 6 and 12 Point Flart Nut, Non-distorting