MOQ:	1PCS
Price:	Negotiations
Standard Packaging:	Standard Export Wooden Pallet
Delivery Period:	10~20days
Payment Method:	T/T, L/C
Supply Capacity:	10000pcs /per month

Details Information

Product Description

Detail Information

Place of Origin

CHINA

Brand Name

JIMA

Certification

ISO9001-2008,SGS,ROHS.

Model Number

ALP

Application:

Airplane Cylinder Head And Piston

Name:

OEM 2618A Forged Aluminum Metal Parts For Airplane Cylinder Head And Piston,Metal Parts,Forging Parts

Standard:

JIS, DIN, BS, ASTM, SAE.

Alloy:

AL2618A

Sample:

Can Be Customized

Surface Treatment:

Anodizing,Plating,Satin,Painting,Powder Coating,Anodized Etc

Process:

Forging

Mold:

Can Be Customized

Highlight:

2618A Forged Aluminum Metal Parts

OEM Forged Aluminum Metal Parts

Airplane Cylinder Head Forging Metal Parts

Product Description

OEM 2618A Forged Aluminum Airplane Cylinder Head, Piston hub Auto Aluminum Parts, Forged Aluminum parts

Product Description

Material	Aluminum Alloy 2618A
Process	Forging+CNC+Heat Treatment
Surface Treatment	Transparent ;Color Anodized;Hard Anodizing;Powder Coating; Sandblasting, Laser Carving, Silk Screening; Nickel-Plated, Chrome, Galvanized, Silver/Gold Plating; Black Oxide Coating; Polishing; etc...
Manufacture Ability	Depends on The Complexity Of Different Products And Quantities
Experience	Aluminum Machining Service for 12 Years
Packaging	Standard Export Wooden Pallets Another Request According to Your Need
MOQ	1pcs
Sample	Can be Customized
Mold	Can be Customized
Lead Time	Mold for 15-20 Days Process for 15-20 Days
OEM	Can be Customized

Chemical Composition of 2618A

Alloy

Others

Each

Total

2618A

0.15-0.25

0.9-1.4

1.8-2.7

0.25

1.2~1.8

0.8~1.4

0.15

0.2

0.05

0.15

Rest

Properties	Metric	Imperial
Density	2.76g/cm³	0.0997 lb/in³
Melting point	549 - 638°C	1020 - 1180°F

Mechanical Properties

Properties	Metric	Tensile
Tensile Strength	372 MPa	54000 psi
Tensile Strength, Ultimate	441 Mpa	64000 psi
Shear Strength	262 Mpa	38000 psi
Fatigue Strength (completely reversed stress; RR Moore machine/specimen)	124 Mpa	18000 psi
			Elastic Modulus (AA; Typical; Average of tension and compression)	74.5 Gpa	10800 ksi
				74.5 Gpa	10800 ksi	Poisson's ratio	0.33	0.33
Elongation at Break	10% at -28.0 °C	10% -18.4 °F
	14% at 149 °C	14% at 300 °F
	50% at 260 °C	50% at 500 °F

Thermal Properties

Thermal Properties	Metric	Imperial
Thermal Conductivity	146 W/m-K	1010 BTU-in/hr-ft²-°F
Specific Heat Capacity	0.875 J/g-°C	0.209 BTU/lb-°F

Room Temperature Tensile Properties of 2618A Aluminum Alloy Forgings in T61 State
Type	Specs/mm	Direction	Tension strength R_m/MPa	Prescribed plastic elongation strength R_p0.2/MPa	Elongation A (%)
Die forgings	Thickness≤100		400	310	4
Die forgings	Thickness≤100		380	290	4
Flat forging	≤50	Portrait	400	325	7
		Long transverse	380	290	5
		Short transverse	360	290	4
	51-76	Portrait	400	315	7
		Long transverse	380	290	5
		Short transverse	360	290	4
	77--100	Portrait	385	310	7
		Long transverse	365	275	5
		Short transverse	350	270	4
Rolling ring	Thickness≤63	Tangential direction	380	285	6
Rolling ring	Thickness≤63	Axial direction	380	285	5

STANDARD SPECIFICATIONS

DIN 3.1924
DTD 717A
DTD 731B
DTD 745A
DTD 5070B
DTD 5014
DTD 5084A
MSRR 8018
MSRR 8016
BS Pre-1980 H16
CM001-1 T6
CM001-3 H28
Hiduminium 58
GB-D19S
SO7-1103 (S07-1103)
A-U2GN
UNI 9002/6
L-3171
CCT LA 767

AIRBUS-ABM1-1006
BAEM 1101
BAEM 1103
MM 0531
AIR 9048.640 T351
AIR 9048.640 T851
AIR 9051A
AIR 9048.150
AIR 9048.170
AIR 9048.640
Werkstoff Nr. 3.1924 T651
EN 2123 T351
EN 2123 T851
EN 3553 T6511
ASN-A-3355
ASN-A-3357

Product Show

OEM 2618A Forged Aluminum Metal Parts For Airplane Cylinder Head And Piston 0

OEM 2618A Forged Aluminum Metal Parts For Airplane Cylinder Head And Piston 1

Application

OEM 2618A Forged Aluminum Metal Parts For Airplane Cylinder Head And Piston 2

Tags:

Forged Metal Parts,

Forged Metal Components,

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Products

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Waterjet Cutting Services

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Air Disc Brake Core Components

Precision CNC Components

OEM 2618A Forged Aluminum Metal Parts For Airplane Cylinder Head And Piston

MOQ:	1PCS
Price:	Negotiations
Standard Packaging:	Standard Export Wooden Pallet
Delivery Period:	10~20days
Payment Method:	T/T, L/C
Supply Capacity:	10000pcs /per month

Detail Information

Product Description

Detail Information

Place of Origin

CHINA

Brand Name

JIMA

Certification

ISO9001-2008,SGS,ROHS.

Model Number

ALP

Application:

Airplane Cylinder Head And Piston

Name:

OEM 2618A Forged Aluminum Metal Parts For Airplane Cylinder Head And Piston,Metal Parts,Forging Parts

Standard:

JIS, DIN, BS, ASTM, SAE.

Alloy:

AL2618A

Sample:

Can Be Customized

Surface Treatment:

Anodizing,Plating,Satin,Painting,Powder Coating,Anodized Etc

Process:

Forging

Mold:

Can Be Customized

Minimum Order Quantity:

1PCS

Price:

Negotiations

Packaging Details:

Standard Export Wooden Pallet

Delivery Time:

10~20days

Payment Terms:

T/T, L/C

Supply Ability:

10000pcs /per month

Highlight

2618A Forged Aluminum Metal Parts

OEM Forged Aluminum Metal Parts

Airplane Cylinder Head Forging Metal Parts

Product Description

OEM 2618A Forged Aluminum Airplane Cylinder Head, Piston hub Auto Aluminum Parts, Forged Aluminum parts

Product Description

Material	Aluminum Alloy 2618A
Process	Forging+CNC+Heat Treatment
Surface Treatment	Transparent ;Color Anodized;Hard Anodizing;Powder Coating; Sandblasting, Laser Carving, Silk Screening; Nickel-Plated, Chrome, Galvanized, Silver/Gold Plating; Black Oxide Coating; Polishing; etc...
Manufacture Ability	Depends on The Complexity Of Different Products And Quantities
Experience	Aluminum Machining Service for 12 Years
Packaging	Standard Export Wooden Pallets Another Request According to Your Need
MOQ	1pcs
Sample	Can be Customized
Mold	Can be Customized
Lead Time	Mold for 15-20 Days Process for 15-20 Days
OEM	Can be Customized

Chemical Composition of 2618A

Alloy

Others

Each

Total

2618A

0.15-0.25

0.9-1.4

1.8-2.7

0.25

1.2~1.8

0.8~1.4

0.15

0.2

0.05

0.15

Rest

Properties	Metric	Imperial
Density	2.76g/cm³	0.0997 lb/in³
Melting point	549 - 638°C	1020 - 1180°F

Mechanical Properties

Properties	Metric	Tensile
Tensile Strength	372 MPa	54000 psi
Tensile Strength, Ultimate	441 Mpa	64000 psi
Shear Strength	262 Mpa	38000 psi
Fatigue Strength (completely reversed stress; RR Moore machine/specimen)	124 Mpa	18000 psi
			Elastic Modulus (AA; Typical; Average of tension and compression)	74.5 Gpa	10800 ksi
				74.5 Gpa	10800 ksi	Poisson's ratio	0.33	0.33
Elongation at Break	10% at -28.0 °C	10% -18.4 °F
	14% at 149 °C	14% at 300 °F
	50% at 260 °C	50% at 500 °F

Thermal Properties

Thermal Properties	Metric	Imperial
Thermal Conductivity	146 W/m-K	1010 BTU-in/hr-ft²-°F
Specific Heat Capacity	0.875 J/g-°C	0.209 BTU/lb-°F

Room Temperature Tensile Properties of 2618A Aluminum Alloy Forgings in T61 State
Type	Specs/mm	Direction	Tension strength R_m/MPa	Prescribed plastic elongation strength R_p0.2/MPa	Elongation A (%)
Die forgings	Thickness≤100		400	310	4
Die forgings	Thickness≤100		380	290	4
Flat forging	≤50	Portrait	400	325	7
		Long transverse	380	290	5
		Short transverse	360	290	4
	51-76	Portrait	400	315	7
		Long transverse	380	290	5
		Short transverse	360	290	4
	77--100	Portrait	385	310	7
		Long transverse	365	275	5
		Short transverse	350	270	4
Rolling ring	Thickness≤63	Tangential direction	380	285	6
Rolling ring	Thickness≤63	Axial direction	380	285	5

STANDARD SPECIFICATIONS

DIN 3.1924
DTD 717A
DTD 731B
DTD 745A
DTD 5070B
DTD 5014
DTD 5084A
MSRR 8018
MSRR 8016
BS Pre-1980 H16
CM001-1 T6
CM001-3 H28
Hiduminium 58
GB-D19S
SO7-1103 (S07-1103)
A-U2GN
UNI 9002/6
L-3171
CCT LA 767

AIRBUS-ABM1-1006
BAEM 1101
BAEM 1103
MM 0531
AIR 9048.640 T351
AIR 9048.640 T851
AIR 9051A
AIR 9048.150
AIR 9048.170
AIR 9048.640
Werkstoff Nr. 3.1924 T651
EN 2123 T351
EN 2123 T851
EN 3553 T6511
ASN-A-3355
ASN-A-3357

Product Show

OEM 2618A Forged Aluminum Metal Parts For Airplane Cylinder Head And Piston 0

OEM 2618A Forged Aluminum Metal Parts For Airplane Cylinder Head And Piston 1

Application

OEM 2618A Forged Aluminum Metal Parts For Airplane Cylinder Head And Piston 2

Tags: