Rapidly solidified or mechanically alloyed powder in these alloys is consolidated into billets ranging in size from
approximately 45 kg (100 lb) to as large as 1360 kg (3000 lb) through the use of several consolidation techniques, such as
vacuum hot pressing and hot isostatic pressing. In this billet form, high-strength prealloyed P/M alloys can usually be
fabricated directly into forgings or, with other working techniques, such as rolling or extrusion, into bar or plate stock for
forging. As with aluminum-lithium alloys, the aluminum alloys produced using prealloyed P/M techniques are
considerably more expensive than the commercially used I/M 7xxx alloys. Therefore, high-definition and precision, net
shape forgings that reduce required metal input and subsequent machining are likely to be the most cost-effective forging
methods. Several of these alloys have found limited commercial application in forgings for aerospace applications that
require their unique property combinations.
Corrosion-Resistant Prealloyed P/M Aluminum Alloy Forgings. Alloy IN9052 (Table 4) is an intermediate-
strength prealloyed aluminum alloy with mechanical properties similar to those of I/M alloy 5083 but with superior
corrosion resistance. This alloy is forged at relatively low temperatures (<370 °C, or 700 °F), and its flow stress and
deformation characteristics are also similar to those of alloy 5083. As with the high-strength P/M aluminum alloys,
IN9052 is consolidated into billets and then into extruded stock prior to forging. The cost of this material suggests that
high-definition and/or precision forgings will be the most cost-effective forging type.
Elevated-Temperature Prealloyed P/M Aluminum Alloy Forgings. Several rapid-solidification techniques,
including atomization, melt spinning, and planar casting, have been used to develop a class of prealloyed aluminum alloys
with significantly improved elevated-temperature properties over those of existing wrought I/M aluminum alloys such as
2219 and 2618 and cast aluminum alloys such as A201. The nominal compositions of several of these alloys are listed in
Table 4. These alloys are being developed to provide enhanced properties in forgings in the range of 205 to 345 °C (400
to 650 °F), a temperature level that exceeds the useful capability of existing aluminum alloys, and to be competitive on a
density-compensated basis with some titanium alloys.
By virtue of their elevated-temperature capabilities, these alloys have been found to be difficult to fabricate into forgings,
displaying flow stresses up to twice that of alloy 7075 (Fig. 1). Recommended forging temperatures for these alloys have
not been completely established, but the alloys are typically forged at temperatures below 370 °C (700 °F) in order to
maintain their unique microstructural features. All of these elevated-temperature aluminum alloys are not heat treatable
and develop their mechanical properties through dispersion strengthening, intermetallic compounds, and/or work
hardening.
The working history of these alloys has also been shown to be a critical element in their suitability for fabrication. For
example, several alloys are not forgeable in the consolidated-billet form, but must be given primary working through
extrusion or other techniques. However, the forging process developmental work conducted to date has demonstrated that
these alloys can be successfully fabricated into sophisticated closed-die and annular forging shapes, including high-
definition and precision forgings. As with all expensive advanced aluminum alloy materials, these forgings may be the
most cost effective through the implementation of material and machining conservation.
Aluminum-Base Discontinuous Metal-Matrix Composites
An emerging advanced aluminum materials concept is the addition of ceramic particles, or whiskers, to aluminum-base
alloys through the use of either ingot-melting or casting and/or P/M techniques, creating a new class of materials termed
discontinuous metal-matrix composites. In these materials systems, the reinforcing material (for example, silicon carbide,
boron carbide, or boron nitride) is not continuous, but consists of discrete particles within the aluminum alloy matrix.
Unlike continuous metal-matrix composites, discontinuous metal matrix composites have been found to be workable by
all existing metalworking techniques, including forging. Addition of the reinforcement to the parent aluminum alloy
matrix, typically in volume percentages from 10 to 40%, modifies the properties of the alloy significantly. Typically,
compared to the matrix alloy and temper, such additions significantly increase the elastic and dynamic moduli, increase
strength, reduce ductility and fracture toughness, increase abrasion resistance, increase elevated-temperature properties,
and do not significantly affect corrosion resistance. Table 5 lists several of the developmental discontinuous metal-matrix
composite materials that are being evaluated in forgings. None of these materials yet has significant commercial
application; however, alloy and forging process development continues.
Table 5 Aluminum-base discontinuous metal-matrix composite materials
Producer
Type Matrix
Reinforcement
(a)
Reinforcement
loading,