UNLIMITED FREE ACCESS TO THE WORLD'S BEST IDEAS

close
Already an Engineering360 user? Log in.

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

Customize Your Engineering360 Experience

close
Privacy Policy

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

NEN-EN 2133

Aerospace series - Cadmium plating of steels with specified tensile strength1 ≤ 450 MPa, copper, copper alloys and nickel alloys

active, Most Current
Organization: NEN
Publication Date: 1 December 2020
Status: active
Page Count: 24
ICS Code (Coatings and related processes used in aerospace industry): 49.040
scope:

This document specifies the electrolytic cadmium plating of parts and fasteners in steel of tensile strength UTS ≤ 1 450 MPa, copper, copper alloys and nickel alloys, whose temperature in service does not exceed 235 °C.

Document History

NEN-EN 2133
December 1, 2020
Aerospace series - Cadmium plating of steels with specified tensile strength1 ≤ 450 MPa, copper, copper alloys and nickel alloys
This document specifies the electrolytic cadmium plating of parts and fasteners in steel of tensile strength UTS ≤ 1 450 MPa, copper, copper alloys and nickel alloys, whose temperature in service...
October 1, 2010
Aerospace series - Cadmium plating of steels with specified tensile strength ≤ 1450 MPa, copper, copper alloys and nickel alloys
This European standard specifies the electrolytic cadmium plating of parts in steel of tensile strength Rm (max.) ≤ 1450 MPa, copper, copper alloys and nickel alloys, whose temperature in service...
November 1, 1997
Aerospace series - Cadmium plating of steels with specified tensile strength ≤ 1450 MPa, copper, copper alloys and nickel alloys
Specifies the electrolytic cadmium plating of parts in steels of tensile strength Rm(max.) ≤ 1450 MPa, copper, copper alloys and nickel alloys, the temperature in service of which does not exceed...

References

Advertisement