SIST EN 3141:2001

Aerospace series - Rivets, solid, universal head, in heat resisting nickel base alloy NI-P11, cadmium plated, inch based series

This standard specifies the characteristics of solid rivets, with universal head, in heat resisting nickel base alloy NI-P11, cadmium plated, inch based series, for maximum operating temperature 235 °C.

Luft- und Raumfahrt - Vollniete, mit Universalkopf, aus hochwarmfester Nickelbasislegierung NI-P11, verkadmet, Zoll-Reihe

Diese Norm legt die Eigenschaften von Vollnieten, mit Universalkopf, aus hochwarmfester Nickelbasislegierung NI-P11, verkadmet, Zoll-Reihe, zur Verwendung bei Temperaturen bis 235 °C, fest.

Série aérospatiale - Rivets ordinaires, a tete ronde aplatie, en alliage résistant a chaud a base de nickel NI-P11, cadmiés, série base inches

La présente norme spécifie les caractéristiques des rivets ordinaires, à tête ronde aplatie, en alliage résistant à chaud à base de nickel NI-P11, cadmiés, série base inches, pour température maximale d'utilisation 235 °C.

Aerospace series - Rivets, solid, universal head, in heat resisting nickel base alloy NI-P11, cadmium plated, inch based series

General Information

• Status: Published
• Publication Date: 31-Dec-2000
• ICS: 49.030.60 - Rivets
• Technical Committee: SS SPL - Technical Board for the general field
• Current Stage: 6060 - National Implementation/Publication (Adopted Project)
• Start Date: 01-Jan-2001
• Due Date: 01-Jan-2001
• Completion Date: 01-Jan-2001
• Ref Project: EN 3141:1996 - Aerospace series - Rivets, solid, universal head, in heat resisting nickel base alloy NI-P11, cadmium plated, inch based series

Overview

SIST EN 3141:2001 is a European standard under the Aerospace series published by CEN, defining the specifications for solid universal head rivets made from heat-resisting nickel base alloy NI-P11. These rivets are cadmium plated and designed as inch-based series components. The standard targets rivet applications in environments with maximum operating temperatures up to 235 °C. Its focus on heat-resistant materials ensures reliable performance in demanding aerospace conditions where temperature resilience and mechanical strength are critical.

Key Topics

• Material Specification: Rivets are composed of nickel base alloy NI-P11, known for excellent heat resistance, suitable for aerospace components exposed to elevated temperatures.
• Surface Treatment: Cadmium plating provides corrosion protection and enhances rivet durability, extending lifecycle and maintaining joint integrity in harsh operational environments.
• Rivet Design: Universal head shape facilitates ease of installation and ensures secure fastening under mechanical loads.
• Dimensional Standards: Inch-based sizing conforms to aerospace industry requirements for compatibility and interoperability across components and assemblies.
• Temperature Rating: Rated for use up to 235 °C, addressing operational demands in aerospace engine and airframe applications.

Applications

EN 3141 rivets are widely used in aerospace manufacturing and maintenance where high-temperature resistance, structural reliability, and corrosion protection are necessary. Typical applications include:

• Aircraft Airframes: Fastening fuselage and structural assemblies exposed to thermal stresses.
• Engine Components: Securing parts subjected to elevated operational temperatures.
• Spacecraft Structures: Providing dependable mechanical joints withstanding extreme conditions.
• High-Temperature Industrial Equipment: Extending use beyond aerospace for heat-resistant fastening needs.

Manufacturers and engineers rely on the standard to ensure that rivets meet stringent quality and performance criteria critical for safety and durability in aerospace environments.

Related Standards

For comprehensive aerospace fabrication and quality assurance, EN 3141 complements other standards such as:

• EN 22164 – Aluminium alloy solid rivets for aerospace applications.
• EN 2553 – Heat-resisting steel rivets.
• ISO 13918 – Specification for rivets and similar fastening systems.
• AS 2195 – Aerospace specifications on solid rivets, often referenced in global aerospace industries.

Employing EN 3141 rivets alongside compatible materials and installation standards ensures cohesive compliance with aerospace industry best practices, contributing to safer and more efficient aircraft design and maintenance.

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Keywords: EN 3141, aerospace rivets, nickel alloy NI-P11, heat-resistant rivets, cadmium plated rivets, universal head rivets, high-temperature fasteners, aerospace standards, inch-based rivets.

Standards Content (Sample)

SLOVENSKI STANDARD
01-januar-2001
Aerospace series - Rivets, solid, universal head, in heat resisting nickel base alloy
NI-P11, cadmium plated, inch based series
Aerospace series - Rivets, solid, universal head, in heat resisting nickel base alloy NI-
P11, cadmium plated, inch based series
Luft- und Raumfahrt - Vollniete, mit Universalkopf, aus hochwarmfester
Nickelbasislegierung NI-P11, verkadmet, Zoll-Reihe
Série aérospatiale - Rivets ordinaires, a tete ronde aplatie, en alliage résistant a chaud a
base de nickel NI-P11, cadmiés, série base inches
Ta slovenski standard je istoveten z: EN 3141:1996
ICS:
49.030.60 Kovice Rivets
2003-01.Slovensk
...