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FEATURE

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 |

M A R C H

2 0 1 6

4 3

9

of similar material within a vacuum chamber. The process

deposits material at a higher rate than DMLS, but the fin-

ished shape is not as fine. Material for EBAM parts that are

vacuum heat treated is predominantly Ti-6Al-4V (Fig. 3).

Binder jet process (BJP)

involves spraying a liquid bind-

er onto a bed of powder at ambient temperature. The con-

glomeration of the binder and powder is solidified using a

very low heat source equivalent to a heat lamp. Each layer

is printed in a manner similar to a printer depositing ink on

paper. The printed part is lowered after each layer solidifies

until the component is complete (Fig. 4). This method has

the lowest manufacturing cost of all additive processes—as

much as 10 times less expensive. However, vacuum heat

treating of BJP parts is more complicated.

VACUUM HEAT TREATING AM PARTS

AM is rapidly developing due to the demand for near-

net shape parts with geometries that are impossible to ma-

chine. Because AM parts require very little material removal

during downstream processing, it is imperative that finished

parts do not have any decarburization or contaminated

surfaces from subsequent thermal processing. Therefore, a

crucial piece of equipment in the additive manufacturing in-

dustry is a well-maintained vacuum furnace, which operates

totally devoid of oxygen, is equippedwith diffusion pumps to

achieve deep vacuum levels, and has very precise tempera-

ture control (Fig. 5).

One of the most important factors for successful inert

vacuum heat treatment of AM parts is a leak-free furnace.

Therefore, a leak rate of less than five microns per hour is

imperative regardless of the chamber size. The furnace must

also be thoroughly baked out at a minimum temperature

of 2400°F prior to an AM furnace cycle. Overall temperature

uniformity is critical for successful thermal processing of any

parts, especially printedparts. For example, BJP components

function as a type of thermocouple sensor. A BJP workpiece

that does not reach or exceed a

±

2°F temperature range ex-

hibits a lack of temperature control in the form of excessive

shrinkage or growth. Therefore, when sintering tempera-

tures (around 2500°F) preclude attaching thermocouples to

the workpiece, a Type S sensor must be strategically located

within inches of the workpiece (Fig. 6). There is tremendous

potential for scrap without precise temperature control.

Solar Atmospheres has processed AM parts of many

shapes and sizes. The DMLS method generally requires

Fig. 2 —

Decorative part for the yacht “Hollow Ribbons” made

using DMLS.

Fig. 3 —

EBAM is used to deposit titaniumwire on a titanium

base.

Fig. 4 —

BJP-printed engine blades and other titanium alloy test

pieces.