Engineering Data


 

General Applications ~ Nominal Chemical Composition & Typical Properties

Introduction

Tin Bronze and Leaded Tin Bronze

Red Brass and Semi-Red Brass

High-Leaded Tin Bronze

Silicon Bronze and Silicon Brass

Manganese Bronze

Aluminum Bronze

Aluminum Alloys

Zinc Aluminum Alloys

References


 

Introduction:

The following information is intended for reference only. The information has been assembled to assist you in making comparisons regarding the different alloys we work with at Bergstrom Foundry. It should not be used to make a particular determination without consulting an engineer and our Sales Staff. We have listed the most common alloys we pour on a daily or regular basis. If an alloy is not listed this does not mean, we do not / or have not, poured it in the past. Please feel free to forward any questions to our Sales Staff and we will try to answer them for you.

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Tin Bronze and Leaded Tin Bronze:

These are basically alloys of copper, tin and zinc. They are the true bronzes. Tin and zinc added to copper greatly increase its strength and hardness. Phosphorus and lead are also sometimes added to the tin bronzes: phosphorus to further increase hardness; lead to improve machinability. All of the Tin Bronzes and leaded tin bronzes are characterized by a good combination of physical properties and exceptional corrosion resistance. They are used in naval construction and are considered among the best valve and pump bronzes.

Alloy C90500/Ingot#210 Commonly referred to as Gunmetal is a good corrosion and wear resistant alloy used typically for Bearings, pump impellers, steam fittings, gears, piston rings, pump bodies, valve components.

Alloy C90700/Ingot#205 Phos. Gear Bronze excellent resistance to both wear and corrosion and is usually specified for use as special bearings, pump parts, gears and steam fittings.

Alloy C92200/Ingot#245 also known as Navy "M" is used for high quality valves, fittings and other pressure vessel applications operating at temperatures up to 550F (290C) is also used for gears, bearings and bushings.

Alloy C92600/Ingot#215 Strong general utility structural bronze for use under severe conditions, steam pressure castings, high pressure valves and pipe fittings, pump pistons, bolts, nuts, and gears.

Nominal Chemical Composition & Typical Properties

Common Name

Gunmetal

Phos. Bronze

Navy "M"

Gear Bronze

Ingot #

210

205

245

215

UNS No.

C90500

C90700

C92200

C92600

Formerly SAE

62

65

622

-

Federal

QQ-C-390

QQ-C-390

QQ-C-390

QQ-C-390

ASTM

B22

B427

B584

-

Typical Properties

Tensile Strength, psi

40,000

35,000

34,000

35,000

Yield Strength, psi

18,000

18,000

16,000

18,000

Elongation, % in 2"

25

10

22

10

Brinell Hardness (500kg load)

75

-

65

70

Machinability Rating (% of free cutting brass)

35

-

42

40

Nominal Chemical Composition

Copper

88%

89%

88%

87%

Tin

10%

11%

6%

10%

Lead

2%

1%

Zinc

2%

4%

2%

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Red Brass and Semi-Red Brass

The red brasses and semi-red brasses are the most widely used of all copper base casting alloys. These alloys offer an excellent combination of corrosion resistance, machinability, moderate strength, and foundry characteristics. In this group of alloys, tin and zinc are alloyed with copper to add strength. Lead is added to improve Machinability. Most red brasses and semi-red brasses are comparatively low in cost.

Alloy C83600/Ingot #115 is used for valves, pipe fittings, water pump and meter housings, impellers, small gears, high quality plumbing goods, statuary and plaques, and marine applications. These applications are possible due to the corrosion resistance, machinability, strength, bearing properties, color and excellent castability of the alloy.

Alloy C84400/Ingot #123 is used for general hardware fittings, ornamental castings, commercial plumbing fixtures, and certain low-pressure valves and fittings.

Nominal Chemical Composition & Typical Properties

Common Name

C83600

C84400

Ingot #

115

123

UNS No.

Leaded Red Brass

Leaded Semi Red Brass

Formerly SAE

40

Federal

QQ-C-390

QQ-C-39C

ASTM

B62

B271

Typical Properties

Tensile Strength, psi

30,000

29,000

Yield Strength, psi

14,000

13,000

Elongation, % in 2"

20

18

Brinell Hardness (500kg load)

60

55

Machinability Rating (% of free cutting brass)

84

90

Nominal Chemical Composition

Copper

85%

81%

Tin

5%

3%

Lead

5%

7%

Zinc

5%

9%

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High-Leaded Tin Bronze

These alloys are traditionally the bearing and bushing bronzes. The copper-tin forms the load-bearing matrix: the lead is present as well-distributed particles, which provide embeddability, lubrication under load, and ease of machining. By varying the relative proportions of tin and lead in high-leaded tin bronze, it is possible to design a family of alloys that can be used over a wide range of conditions. For example, the high-tin, low-lead alloys will tolerate high loads and high speeds while the higher lead alloys are usually used for high load and low-speed service. In applications where shaft alignment or shaft wear is a problem, the leaded tin bronzes are often the most satisfactory materials to use. They have the malleability to adapt to changing conditions; they will transfer heat sufficiently to run cool; and they will stand up for long periods of time without adequate lubrication.

Alloy C93200/Ingot#315 is the general-utility alloy of this family and finds use in general bearing and bushing applications.

Alloy C93700/Ingot#305 Because of its higher tin and lead contents, is suitable for bearings involving high speed and heavy pressures, as well as pump and impeller parts requiring corrosion resistance and strength.

Alloy C93800/Ingot#319 is also used for larger bearings, but for less demanding service involving only moderate pressures. The material is also commonly used for pump parts in acid mine waters.

Nominal Chemical Composition & Typical Properties

Anti Acid Metal

Common Name

Bearing Bronze

Bearing Bronze

(Plastic Bronze)

Ingot #

315

305

319

UNS No.

C93200

C93700

C93800

Formerly SAE

660

64

67

Federal

QQ-C-390

QQ-C-390

QQ-C-390

ASTM

B584

B22

B66

Typical Properties

Tensile Strength, psi

30,000

30,000

26,000

Yield Strength, psi

14,000

12,000

14,000

Elongation, % in 2"

15

15

12

Brinell Hardness (500kg load)

65

60

55

Machinability Rating (% of free cutting brass)

70

80

80

Nominal Chemical Composition

Copper

83%

80%

78%

Tin

7%

10%

7%

Lead

7%

10%

15%

Zinc

3%

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Silicon Bonze and Silicon Brass

These casting alloys are made by basically adding silicon to copper. They have generally excellent qualities; corrosion resistance equal to that of copper, and a wide range of desirable physical characteristics.

Alloy C87200/Ingot#500 (Silicon Bronze) Typical applications are pump and valve parts, impellers, bearings, gears, marine fittings, bells, statuary, and art casting.

Alloy C87500/Ingot#500 (Silicon Brass) applications include bearings, gears, impellers, valve stems, rocker arms, small boat propellers.

Nominal Chemical Composition & Typical Properties

Common Name

Silicon Brass

Silicon Bronze

Ingot #

500

500

UNS No.

C87500

C87200

Formerly SAE

Federal

QQ-C-39C

QQ-C-390

ASTM

B584

B584

Typical Properties

Tensile Strength, psi

60,000

45,000

Yield Strength, psi

24,000

18,000

Elongation, % in 2"

16

20

Brinell Hardness (500kg load)

115

80

Machinability Rating (% of free cutting brass)

50

40

Nominal Chemical Composition

Copper

82%

92%

Zinc

14%

4%

Silicon

4%

4%

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Manganese Bronze

Manganese Bronzes are the strongest of all copper-base alloys in the as cast condition. The term "manganese bronze" is inaccurate and somewhat confusing, since some alloys in this category actually contain very little manganese. For this reason, these alloys are more properly called high-strength yellow brasses. Manganese Bronze alloys find applications where relatively high strength is required in combination with exceptional corrosion resistance and moderate cost. Manganese Bronze is an alloy of copper and zinc to which aluminum, iron, manganese and sometimes nickel or tin have been added. Aluminum is the principal strengthening element and may be present from 0.75% to 7.5%.

Alloy C86500/Ingot#421 (Mag70) This alloy has somewhat better corrosion resistance than alloy C86200 & C86300 and is used for parts requiring strength and toughness. Typical applications include gears, valve stems, lever arms, liners, and marine fittings.

Alloy C86200/Ingot#423 (Mag90) Applications for this alloy include structural castings, heavy-duty bearings, hold down nuts, gears, etc.

Alloy C86300/Ingot#424 (Mag110) Extra heavy duty high strength alloy, typical uses for this alloy include slow speed heavy load bearings, gears, cams, screw down nuts, and hydraulic cylinder parts.

Nominal Chemical Composition & Typical Properties

Common Name

Mag 90

Mag 110

Mag 70

Ingot #

423

424

421

UNS No.

C86200

C86300

C86500

Formerly SAE

430A

430B

43

Federal

QQ-C-390

QQ-C-390

QQ-C-390

ASTM

B584

B584

B584

Typical Properties

Tensile Strength, psi

90,000

110,000

65,000

Yield Strength, psi

45,000

60,000

25,000

Elongation, % in 2"

20

18

30

Brinell Hardness (3000kg load)

180

225

100 (500kg load)

Machinability Rating (% of free cutting brass)

30

8

26

Nominal Chemical Composition

Copper

64%

63%

58%

Tin

0.5%

Zinc

26%

25%

39.5%

Iron

3%

3%

1%

Aluminum

4%

6%

1%

Manganese

3%

3%

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Aluminum Bronze

Aluminum bronze alloys offer high strength and, hardness, excellent corrosion resistance, good wearing qualities, good fatigue resistance, and are well suited for service at elevated temperatures. The properties of alloys within certain composition ranges can be improved further by heat treatment. The addition of aluminum, about 6% to 12%, and varying amounts of iron, nickel, manganese and/or silicon alloying additions provide a broad range of mechanical properties; from high ductility (as in the tin bronzes) to the high-strength levels of high-tensile manganese bronze. Aluminum bronzes are widely used in applications where good strength, hardness, ductility and corrosion resistance is required. Because of their unusual range of properties, aluminum bronzes are used for special engineering applications such as dies, valve seats, slides, worm gears, cams, screw-down nuts, and non-sparking safety tools.

Alloy C95400/Ingot#415 9C Typical uses include pump impellers, bearings, gears, worms, bushings, valve seats, non-sparking tools, valve and pump bodies. This alloy is not suitable for exposure to oxidizing acids.

Alloy C95500/Ingot#415 9D This alloy is used for corrosion resistant structural parts, bushings, gears, pickling hooks, agitators, pump parts, dies and wear parts, not suitable for use in strong oxidizing acids.

Alloy C95800/Ingot#415 Typical uses for this alloy include propeller blades and hubs for fresh and sea water service, structural applications, gears and worm wheels.

Nominal Chemical Composition & Typical Properties

Common Name

Alum. Bronze "C"

Alum Bronze "D"

Nickel Alum Bronze

Ingot #

415 9C

415 9D

415

UNS No.

C95400

C95500

C95800

Formerly SAE

Federal

QQ-C-390

QQ-C-390

QQ-C-390

ASTM

B148

B148

B148

Typical Properties

Tensile Strength, psi

85,000

100,000

95,000

Yield Strength, psi

35,000

44,000

38,000

Elongation, % in 2"

18

12

25

Brinell Hardness (500kg load)

170

195 (3000Kg)

159 (3000Kg)

Machinability Rating (%of free cutting brass)

20

20

20

Nominal Chemical Composition

Copper

85%

81%

81%

Iron

4%

4%

4%

Nickel

4%

5%

Aluminum

11%

11%

9%

Manganese

1%

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Aluminum Alloys

The applications for aluminum alloys are almost limitless. Choosing an Aluminum alloy for a particular application depends on many factors. Some considerations that should be taken into account are:

  1. Foundry characteristics for the casting process that will be used;
  2. Required mechanical and other properties for the service intended;
  3. Mechanical properties over the service life;
  4. Corrosion resistance for the application;
  5. Machinability, pressure tightness and finishability, if necessary;

Another consideration that should be taken into account is the finished cost of the part. The following among many other variables can directly affect the cost:

    1. The alloy chosen and the technical requirements of casting that alloy;
    2. Quantity of castings to be produced;
    3. Process used;
    4. Complexity of the shape of the part;
    5. The tooling used for producing the molds;
    6. Dimensional tolerances required;
    7. Inspection and quality standards required

Common Aluminum Alloys we pour at Bergstrom Foundry:

Typical Mechanical Properties

Tensile Strength

Yield Strength

Elongation

Hardness

psi

psi

% in 2"

(500 kg load)

319

27,000

18,000

2

70

319-T6

36,000

24,000

2

80

A356

23,000

12,000

6

70

A356-T6

40,000

30,000

6

75

357.0

25,000

13,000

5

-

357-T7

46,000

36,000

3

85

535

40,000

20,000

13

70

705

30,000

17,000

5

-

713

32,000

22,000

3

75

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Zinc Aluminum Alloys

In many instances the zinc-aluminum alloys offer major performance and cost benefits over cast iron, aluminum, and bronze, offering new opportunities to designers. Zinc Aluminum alloys offer tensile strengths competitive with cast iron (class 30) and superior to those of bronze, brass and aluminum. These alloys show superior hardness over bronze and aluminum, usually resulting in improved wear characteristics. ZA-12 and ZA-27 are extremely resistant to galling, and have natural lubricity. They are well suited for moderate to high load, slow speed bearing and bushing applications running below 200 degrees F. ZA-12 and ZA-27, as cast can handle repeated or cyclic stress levels up to approximately 15KPSI and 25KPSI respectively. Typical applications include; machine parts, fluid and pressure applications, electrical conduit fittings, transportation components, decorative applications.

Nominal Chemical Composition & Typical Properties

Common Name

ZA-12

ZA-27

ASTM

B-669-80

Typical Properties

As Cast (Sand)

As Cast (Sand)

Density (lb. cu/in)

0.218

0.181

Ultimate Tensile Strength (kpsi)

40 - 45

58 - 64

Yield Strength (kpsi), 0.2% offset

30 - 31

53 - 54

Elongation, % in 2"

1 - 3

3 - 6

Brinell Hardness (500kg load)

92 - 97

110 - 120

Shear Strength (kpsi)

36 - 38

41 - 43

Nominal Chemical Composition

Aluminum (wt. %)

10.5 - 11.5

25 - 28

Copper

0.5 - 1.25

2.0 - 2.5

Magnesium

0.015 - 0.030

0.01 - 0.02

Iron

<0.075

<0.10

Lead

<0.004

<0.004

Cadmium

<0.003

<0.003

Tin

<0.002

<0.002

Zinc

balance

balance

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References:

While information contained on this page is believed to be accurate, they are offered as suggestions only and no warranty or representation is intended.

 

    1. Casting Copper-Base Alloys, American Foundrymen's Society; Des Plaines, Illinois
    2. Lavingot, R. Lavin & Sons, Inc.; Chicago, Ill
    3. Colonial Metals Co., Columbia, PA.
    4. Guide to Copper Casting Alloys, Federated Metals; New York, N.Y.
    5. Brass & Bronze Casting Alloys, Federated Metals; New York, N.Y.
    6. Aluminum Casting Technology-2nd Edition, American Foundrymen's Society; Des Plaines, Illinois
    7. Zinc Casting Alloys, Kidd Creek Mines Ltd.,

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