High Temp Metals 800-500-2141

ALLOY 49 TECHNICAL DATA


Type Analysis | Description | Applications | Corrosion Resistance
Physical Properties | Magnetic Properties | Heat Treatment | Workability | Typical Mechanical Properties

Type Analysis

Element

Min

Max

Carbon

--

0.02

Nickel

--

48.0

Iron

Balance

Silicon

--

0.35

Manganese

--

0.50

Description

High Permeability "49" alloy is a 48% nickel-iron alloy which has a saturation flux density of approximately 15,000 gausses after hydrogen annealing. Hysteresis loss is very low in either DC or AC circuits in which the frequency is less than 400 cycles per second.
Following a low temperature hydrogen anneal at 1300/1400°F (704/760°C), alloy 49 exhibits constant permeability characteristics. Its initial permeability is approximately 500 gausses.


Application

High permeability "49" alloy has been used in laminated cores for instrument transformers, magnetic shields and cores for certain electronic and communications devices in which extremely high permeability at low magnetizing forces greatly increases the efficiency and effectiveness of the equipment. Because of its high permeability, it has also been used in solenoid cores in light, sensitive relays that must operate and respond to weak currents that induce low magnetizing forces.


Corrosion Resistance

High Permeability "49" alloy resists weather and moisture corrosion to a moderate extent.


Physical Properties


Specific gravity..........................................8.18                             Electrical resistivity
Density                                                                                            ohm c/mf................................ 290
   lb/cu in............................................... 0.295                                 microhm-mm.......................... 480
   kg/cu m............................................... 8249                            Temperature coefficient of electrical
Thermal conductivity                                                                   resistivity
   Btu-in/ft²/hr/°F........................................ 90                                  per °F(0/930°F)...................0.002
   W/m-K.................................................... 13                                  per  °C(-17.8/499°C)........ 0.0036
Mean coefficient of thermal expansion                                        Melting point
   x 10(-6)/°F(77/400°F)............................ 4.6                                 °F.......................................... 2600
   x 10(-6)/°C(25/204°C)............................ 8.3                                 °C......................................... 1427
Curie temperature                                                                          Specific heat
    °F................................................... 840/930                                  Btu/lb-°F.............................. 0.12
    °C................................................... 449/499                                  kJ/kg-K................................ 0.50

Magnetic Properties

DC Magnetic Properties
Determined according to ASTM-A-596

Properties

Bar

Strip

0.014"

0.025 to 0.125"

Initial Permeability B100
Maximum Permeability
Residual Magnetism, Gausses
Coercive Force,
Oersteds from 10,000 Gausses
Saturation Inductance from
H-100 Oersted, Gausses

6,500
75,000
9,000

0.04/0.07

15,000

12,000
150,000
9,000

0.04/0.07

15,000

8,000
90,000
9,000

0.04/0.07

15,000

Temperature Variation of Permeability
Expressed in % of value of 77°F (25°C). AC and DC magnetic properties of lamination strip 0.006" and 0.014" thick

Temperature

Permeability at
1000 Gausses

Maximum
Permeability

°F

°C

-94
212

-70
100

75/90
120/130

90/95
100/105


Heat Treatment

Strain Relieving Anneal
To relief all strains and restore the alloy to a soft condition suitable for drawing, spinning, forming, bending and similar operations, anneal for not more than 1 hour at 1450/1600°F .
Since high-nickel, high permeability alloys readily absorb carbon, sulfur, oxygen and other contaminants from combustion furnace gasses, in-process annealing should be done in a hydrogen or inert gas atmosphere.

Standard Hydrogen Anneal
For maximum softness and optimum magnetic and electrical properties, High Permeability "49" alloy should be annealed in an oxygen-free, dry hydrogen atmosphere with a dew point below -40°F (-40°C) for 2 to 4 hours at 2150°F (1177°C), followed by a furnace cool at a rate of 100/200°F (38/93°C) per hour down to 800°F (427°C) and at any rate thereafter.
Oil, grease, lacquer and any other contaminants must be removed before annealing. During hydrogen annealing, the individual parts should be separated by a surface insulation media or an inert insulating powder, such as magnesium or aluminum oxide.


Workability

Machinability
If components are to machined in volume from bar stock, High Permeability "49"-FM, a free-machining grade, is recommended. The standard grade , High Permeability "49" alloy, machines somewhat like the austenitic stainless alloys. It develops gummy chips but does not work harden as rapidly as the stainless alloys. Sulfur-bearing cutting compounds are highly detrimental to the final magnetic properties. Animal lard oil should be used in drilling and machining operations which must be performed at low speeds. Work hardened bars offer the best machining characteristics. Parts should be degreased and cleaned as soon as possible.
Suggested speeds for machining alloy 49 are contained in the following chart:

High Speed Tool*

Turning
and Forming

Tool Width

Cut-Off
Tool

1/16"

SFM
FEED

65
.0010

1/8"

SFM
FEED

67
.0012

1/4"

SFM
FEED

69
.0016

Form Tool

1/2"

SFM
FEED

67
.0012

1"

SFM
FEED

63
.0010

1-1/2"

SFM
FEED

63
.0009

Drilling

Drill
Diameter

3/8"

SFM
FEED

43
.0030

3/4"

SFM
FEED

45
.0036

Reaming

Under 1/2"

SFM
FEED

57
.0030

Over 1/2"

SFM
FEED

57
.0045

Threading

T.P.I

3-7½
8-15

SFM
SFM

8
10

Over 16

SFM

15

Tapping

T.P.I

3-7½
8-15
16-24
Over 25

SFM
SFM
SFM
SFM

6
7
11
15

Turning

Single Point
and Box Tools

High Speed Tools

SFM
FEED

60-65
.0029-.0043

Carbide Tools

SFM
FEED

160-215
.025-.008

* When using carbide tools, surface speed feet/minute (sfm) can be increased between 2 to 3 times over the high-speed tool suggestions. Feeds can be increased between 50 and 100%.
Figures used for all metal removal operations reported are average. On certain work, the nature of the part may require adjustment of the speeds and feeds. Each job has to be developed for best production results with optimum tool life. Speeds or feeds should be increased or decreased in small steps.

Cold forming
For best blanking characteristics, strip should be ordered in the cold rolled condition at Rockwell B90 minimum. For best forming characteristics, strip should be ordered as cold rolled and annealed for forming. Best drawing characteristics are obtained when ordered as annealed, deep drawing quality.

Forging
The recommended forging temperature is 2150°F (1177°C).

Welding
Alloy 49 is readily blazed, welded and soft or hard soldered by employing the usual practices used on ferrous alloys.


Typical Mechanical Properties

Bar

Tensile
Strength

Yield
Strength

Proportional
Limit

%
Elongation

%
Reduction
in Area

Modulus of Elasticity

Hardness
Rb

Izod
Impact

ksi

MPa

ksi

MPa

ksi

MPa

in tension

in torsion

ft-lbs

J

psi x 10(6)

MPa x 10(3)

psi x 10(6)

MPa x 10(3)

---------------------------------------------As Cold Drawn-------------------------------------------------

95

655

80

552

35

241

25

62

24.0

166

7.8

54

98

93/99

126/134

-----------------------------As Hydrogen Annealed at 2150°F(1177°C)-------------------------------

70

483

22

152

12

83

45

68

22.5

155

7.5

52

62

93/98

126/133

-----------------------------After Process Annealed at 1600°F(871°C)---------------------------------

75

517

23

154

13

90

43

65

22.0

152

7.6

52

75

95

129

Strip

Tensile Strength

%
Elongation

Modulus of Elasticity
(in tension)

Hardness
Rockwell B

--------------------------Cold Rolled------------------------------

130

896

5

24.0

166

100

-------------Forming and DeepDraw Quality------------------

80

552

32

24.0

166

68

Effect of Heat Treating Temperature on Typical Mechanical Properties
Strip 0.060" (1.52 mm) thick heat treated for 2 hours at indicated temperature

Temperature

Yield Strength
2% Offset

Tensile Strength

%
Elongation in 2"

°F

°C

ksi

MPa

ksi

MPa

1450
1600
1750

788
871
954

37
34
27

255
234
186

79
75
71

545
517
490

30
31
32

Invar 49 - Current Inventory Stock

ALLOY 49 TECHNICAL DATA


Type Analysis | Description | Applications | Corrosion Resistance
Physical Properties | Magnetic Properties | Heat Treatment | Workability | Typical Mechanical Properties

Type Analysis

Element

Min

Max

Carbon

--

0.02

Nickel

--

48.0

Iron

Balance

Silicon

--

0.35

Manganese

--

0.50

Description

High Permeability "49" alloy is a 48% nickel-iron alloy which has a saturation flux density of approximately 15,000 gausses after hydrogen annealing. Hysteresis loss is very low in either DC or AC circuits in which the frequency is less than 400 cycles per second.
Following a low temperature hydrogen anneal at 1300/1400°F (704/760°C), alloy 49 exhibits constant permeability characteristics. Its initial permeability is approximately 500 gausses.


Application

High permeability "49" alloy has been used in laminated cores for instrument transformers, magnetic shields and cores for certain electronic and communications devices in which extremely high permeability at low magnetizing forces greatly increases the efficiency and effectiveness of the equipment. Because of its high permeability, it has also been used in solenoid cores in light, sensitive relays that must operate and respond to weak currents that induce low magnetizing forces.


Corrosion Resistance

High Permeability "49" alloy resists weather and moisture corrosion to a moderate extent.


Physical Properties

Specific gravity..........................................8.18                             Electrical resistivity
Density                                                                                            ohm c/mf................................ 290
   lb/cu in............................................... 0.295                                 microhm-mm.......................... 480
   kg/cu m............................................... 8249                            Temperature coefficient of electrical
Thermal conductivity                                                                   resistivity
   Btu-in/ft²/hr/°F........................................ 90                                  per °F(0/930°F)...................0.002
   W/m-K.................................................... 13                                  per  °C(-17.8/499°C)........ 0.0036
Mean coefficient of thermal expansion                                        Melting point
   x 10(-6)/°F(77/400°F)............................ 4.6                                 °F.......................................... 2600
   x 10(-6)/°C(25/204°C)............................ 8.3                                 °C......................................... 1427
Curie temperature                                                                          Specific heat
    °F................................................... 840/930                                  Btu/lb-°F.............................. 0.12
    °C................................................... 449/499                                  kJ/kg-K................................ 0.50

Magnetic Properties

DC Magnetic Properties
Determined according to ASTM-A-596

Properties

Bar

Strip

0.014"

0.025 to 0.125"

Initial Permeability B100
Maximum Permeability
Residual Magnetism, Gausses
Coercive Force,
Oersteds from 10,000 Gausses
Saturation Inductance from
H-100 Oersted, Gausses

6,500
75,000
9,000

0.04/0.07

15,000

12,000
150,000
9,000

0.04/0.07

15,000

8,000
90,000
9,000

0.04/0.07

15,000

Temperature Variation of Permeability
Expressed in % of value of 77°F (25°C). AC and DC magnetic properties of lamination strip 0.006" and 0.014" thick

Temperature

Permeability at
1000 Gausses

Maximum
Permeability

°F

°C

-94
212

-70
100

75/90
120/130

90/95
100/105


Heat Treatment

Strain Relieving Anneal
To relief all strains and restore the alloy to a soft condition suitable for drawing, spinning, forming, bending and similar operations, anneal for not more than 1 hour at 1450/1600°F .
Since high-nickel, high permeability alloys readily absorb carbon, sulfur, oxygen and other contaminants from combustion furnace gasses, in-process annealing should be done in a hydrogen or inert gas atmosphere.

Standard Hydrogen Anneal
For maximum softness and optimum magnetic and electrical properties, High Permeability "49" alloy should be annealed in an oxygen-free, dry hydrogen atmosphere with a dew point below -40°F (-40°C) for 2 to 4 hours at 2150°F (1177°C), followed by a furnace cool at a rate of 100/200°F (38/93°C) per hour down to 800°F (427°C) and at any rate thereafter.
Oil, grease, lacquer and any other contaminants must be removed before annealing. During hydrogen annealing, the individual parts should be separated by a surface insulation media or an inert insulating powder, such as magnesium or aluminum oxide.


Workability

Machinability
If components are to machined in volume from bar stock, High Permeability "49"-FM, a free-machining grade, is recommended. The standard grade , High Permeability "49" alloy, machines somewhat like the austenitic stainless alloys. It develops gummy chips but does not work harden as rapidly as the stainless alloys. Sulfur-bearing cutting compounds are highly detrimental to the final magnetic properties. Animal lard oil should be used in drilling and machining operations which must be performed at low speeds. Work hardened bars offer the best machining characteristics. Parts should be degreased and cleaned as soon as possible.
Suggested speeds for machining alloy 49 are contained in the following chart:

High Speed Tool*

Turning
and Forming

Tool Width

Cut-Off
Tool

1/16"

SFM
FEED

65
.0010

1/8"

SFM
FEED

67
.0012

1/4"

SFM
FEED

69
.0016

Form Tool

1/2"

SFM
FEED

67
.0012

1"

SFM
FEED

63
.0010

1-1/2"

SFM
FEED

63
.0009

Drilling

Drill
Diameter

3/8"

SFM
FEED

43
.0030

3/4"

SFM
FEED

45
.0036

Reaming

Under 1/2"

SFM
FEED

57
.0030

Over 1/2"

SFM
FEED

57
.0045

Threading

T.P.I

3-7½
8-15

SFM
SFM

8
10

Over 16

SFM

15

Tapping

T.P.I

3-7½
8-15
16-24
Over 25

SFM
SFM
SFM
SFM

6
7
11
15

Turning

Single Point
and Box Tools

High Speed Tools

SFM
FEED

60-65
.0029-.0043

Carbide Tools

SFM
FEED

160-215
.025-.008

* When using carbide tools, surface speed feet/minute (sfm) can be increased between 2 to 3 times over the high-speed tool suggestions. Feeds can be increased between 50 and 100%.
Figures used for all metal removal operations reported are average. On certain work, the nature of the part may require adjustment of the speeds and feeds. Each job has to be developed for best production results with optimum tool life. Speeds or feeds should be increased or decreased in small steps.

Cold forming
For best blanking characteristics, strip should be ordered in the cold rolled condition at Rockwell B90 minimum. For best forming characteristics, strip should be ordered as cold rolled and annealed for forming. Best drawing characteristics are obtained when ordered as annealed, deep drawing quality.

Forging
The recommended forging temperature is 2150°F (1177°C).

Welding
Alloy 49 is readily blazed, welded and soft or hard soldered by employing the usual practices used on ferrous alloys.


Typical Mechanical Properties

Bar

Tensile
Strength

Yield
Strength

Proportional
Limit

%
Elongation

%
Reduction
in Area

Modulus of Elasticity

Hardness
Rb

Izod
Impact

ksi

MPa

ksi

MPa

ksi

MPa

in tension

in torsion

ft-lbs

J

psi x 10(6)

MPa x 10(3)

psi x 10(6)

MPa x 10(3)

---------------------------------------------As Cold Drawn-------------------------------------------------

95

655

80

552

35

241

25

62

24.0

166

7.8

54

98

93/99

126/134

-----------------------------As Hydrogen Annealed at 2150°F(1177°C)-------------------------------

70

483

22

152

12

83

45

68

22.5

155

7.5

52

62

93/98

126/133

-----------------------------After Process Annealed at 1600°F(871°C)---------------------------------

75

517

23

154

13

90

43

65

22.0

152

7.6

52

75

95

129

Strip

Tensile Strength

%
Elongation

Modulus of Elasticity
(in tension)

Hardness
Rockwell B

--------------------------Cold Rolled------------------------------

130

896

5

24.0

166

100

-------------Forming and DeepDraw Quality------------------

80

552

32

24.0

166

68

Effect of Heat Treating Temperature on Typical Mechanical Properties
Strip 0.060" (1.52 mm) thick heat treated for 2 hours at indicated temperature

Temperature

Yield Strength
2% Offset

Tensile Strength

%
Elongation in 2"

°F

°C

ksi

MPa

ksi

MPa

1450
1600
1750

788
871
954

37
34
27

255
234
186

79
75
71

545
517
490

30
31
32

Invar 49 - Current Inventory Stock