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iTSSe

TSS

A D V A N C E D M A T E R I A L S & P R O C E S S E S | F E B R U A R Y 2 0 1 6

4 0

iTSSe

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10

CASE STUDY

MAGNESIUM REPAIR ON LIGHTWEIGHT

AEROSPACE COMPONENTS

REASON TO CONSIDER SURFACING

Magnesium components feature unique structural

strength combined with lightweight attributes. However,

these components are difficult to repair due to a heat-sensitive

corrosion reaction. “Magnesium alloys have been developed

that have good mechanical properties, low densities, can be

cast into complex shapes, and also feature good machining

characteristics. These characteristics make them ideal for

use in weight-critical applications, especially in helicopters,”

Fig. 1 —

Micrograph shows commercially pure aluminum applied

via high pressure cold spray.

Fig. 2 —

Hydraulic pump pad in the as-sprayed condition shows

the AA4047 coating. Courtesy of Applied Research Laboratory, Penn

State.

Fig. 3 —

Hydraulic pump pad after final machining of cold spray

repair. Transmission is fully assembled and resting in the engine test

stand. Courtesy of Applied Research Laboratory, Penn State.

Fig. 4 —

Aluminum repair on magnesium sump. Courtesy of ASB

Industries.

*Excerpt fromTimEden’s contribution to “High Pressure Cold Spray: Prin-

ciples and Applications,” a new book from ASM to be published in May.

explains Tim Eden, head of the Materials Processing Division,

Penn State Applied Research Laboratory.* “A disadvantage of

magnesium alloys is that they have a very high anodic index,

which means they are electrochemically active and very sus-

ceptible to galvanic corrosion when coupled to another metal.

Care must be taken to apply coatings that isolate the magne-

sium alloys from other metals and to create an environmental

barrier to prevent corrosion. Once the coating is damaged, cor-

rosion is initiated and quickly propagates.”