An Investigation of Electrodeposited Alloys for Protection of Steel Aircraft Parts

Item

Title
An Investigation of Electrodeposited Alloys for Protection of Steel Aircraft Parts
Date
1953
Index Abstract
Not Available
Photo Quality
Undetermined
Report Number
AF TR 5692 Supplement 4
Creator
Tripler, Arch B.
Fuller, Glen
Faust, Charles L.
Corporate Author
Battelle Memorial Institute
Extent
64
PB Number
PB097655S4
NTRL Accession Number
AD018113
Identifier
AD0018113
Access Rights
Unknown
Distribution Classification
1
DTIC Record Exists
Yes
Distribution Change Authority Correspondence
AFWAL LTR
Distribution Conflict
Fix
Abstract
Exploratory research was conducted to determine substitutes for Zn and Cd coatings for steel parts of aircraft. Since the coatings had to provide sacrificial (cathodic) protection for SAE 4130 steel and be capable of being electrodeposited, the search was limited to alloys of Cd or Zn and pure Mn and its alloys. Test panels with pure Mn, Mn-Zn and its alloys. Test panels with pure Mn, Mn-Zn-alloy, and Zn-Sn-alloy coatings were exposed concurrently with panels having standard coating of Zn, Cd, and chromated Zn. Cumulative results are tabulated for exposures from 60 to 302 days and from 12 and 20 mo. The pure- Mn and Mn-Zn coating were inferior to the Zn and Cd standards. The Zn-Sn-alloy coatings of 0.3-mil thickness and greater protected the underlying steel as well as the Zn and Cd standards.
Report Availability
Not available via Contrails
Date Issued
1953-07
Index In
PB/AD Index
Type
report