7149/7150/7249 Aircraft Aerospace Aluminum Extrusions Section for Aviation

• Customization: Available
• Type: Transport Aluminium Profile, Industrial Aluminium Profile, Aviation
• Shape: Round/Flat/Angle/Square/ Hexagon
• Model NO.: 7149/7150/7249
• Temper: T73511/T74511/T76511/T77511
• Alloy: Alloy
• Surface Finishing: Anodized,Electrophoresis,Powder/PVDF Coated.
• Alloying Ingredient: 7149/7150/7249
• Certification: ISO, En755 GB5237-2008 Astmb221 DIN
• Extrusion Machine: 1000-4000 Tons, 35 Press Lines.
• Transport Package: Export Standard Wooden Pallet or as Your Requsts
• Specification: According to Customer Requirement
• Trademark: Chalco Aluminum
• Origin: Henan China
• HS Code: 7604210000
• Production Capacity: 4000mt/Month

Product Description

7149/7150/7249 Aircraft Aerospace Aluminum Extrusions Section for Aviation   

7149 aluminum alloy forgings profile

The 7149 is to reduce the content of Fe and Si impurities on the basis of 7049, to further improve the fracture properties of the alloy, and mainly to produce forgings. It has good strength and resistance to SCC, and the fracture property is better than 7049. It is a modified alloy with 7049. 7149 aluminum alloy forgings profile is mainly used in the forging parts of the main landing gear of the aircraft.
 

Chemical Composition of 7049alloy

Alloy

Si

Fe

Cu

Mn

Mg

Cr

Ni

Zn

Ti

Zr

Others

Al

Each

Total

7149

0.15

0.20

1.2~1.9

0.20

2.0~2.9

0.10~0.22

~

7.2~8.2

0.10

~

0.05

0.15

Remainder

Alloy	Alloy series	Main features	σb Value/MPa	Work Temperature/ºC
7149	7049 series(Europe)	The 7149 is to reduce the content of Fe and Si impurities on the basis of 7049, to further improve the fracture properties of the alloy, and mainly to produce forgings.	~	<125

Alloy	Main features	Main type and temper	Application parts and typical parts
7149	It has good strength and resistance to SCC, and the fracture property is better than 7049. It is a modified alloy with 7049.	Aluminum forgings: T73,T74,T7452 Aluminum Extrusion:T73511,T76511	The main landing gear of the aircraft is forged.

               
7150 aluminum alloy sheet profile 

The 7150 is the second generation modification of 7050 Alloy, the main varieties have thick plates and profiles, the use of the state of T7751 and T77511. Compared with other 7 * * * * system alloys, 7150 T77 alloys have obtained the best combination of strength and corrosion properties.

The 7150 alloy is mainly supplied in the form of T7751 thick plate, T77511 extruded parts and T76511 extrusion parts. 7150 aluminum alloy sheet profile
 is used for the main stress parts of the upper wing structure and aircraft structure, such as wing upper wall panels, beams, edge strips and so on.7150

Chemical Composition of 7150 alloy

Alloy

Si

Fe

Cu

Mn

Mg

Cr

Ni

Zn

Ti

Zr

Others

Al

Each

Total

7150

0.12

0.15

1.9~2.5

0.1

2.0~2.7

0.04

~

5.9~6.9

0.06

0.08~0.15

0.05

0.15

Remainder

 

Alloy	Alloy series	Main feature	σb  Value/MPa	Work Temperature/ºC
7150	7050 series	The 7150 is the second generation modification of 7050 Alloy, the main varieties have thick plates and profiles, the use of the state of T7751 and T77511. Compared with other 7 * * * * system alloys, 7150 T77 alloys have obtained the best combination of strength and corrosion properties.	579~622	<125

 

Physical Property of 7150 Alloy
Alloy	Type	Temper	Size/mm	Direction	σb/MPa	σp 0.2/MPa		KIC oR KC	δ %
7150	Aluminum sheet	T7751	δ6.35~12.69	L	552		510	-	8
				LT	552		510
			δ12.70~19.04	L	572		531	-	8
				LT	572		524
			δ19.05~25.40	L	579		538	L - T 22 T -L19.8	8
				LT	579		531
			δ25.41~38.10	L	579		53	L -T 24.2 T -L 22	8
				LT	579		531
			δ38.11~76.20	L	565		524		7
				LT	565		517		6
				ST	531		462		1
	Aluminum profile	T77511	δ1.0~6.34	L	594		545	-	7
				LT	566		510
			δ6.35~12.69	L	608		573		8
				LT	573		531
			δ12.70~19.04	ST	615		580		9
				L	580		552
			δ19.05~50.80	LT	622		587	L -T 23.1 T -L 18.7	8
				ST	580		545

 

Alloy	Temper	Aircraft type	Application parts and typical parts
7150	Aluminum plate:  T7751 Aluminum profile: T77511	Widely used abroad, domestic ARJ21 and so on	he main force parts of an aircraft structure, such as the panel on the wing, the beam, the flange and so on.

7249 aluminum alloy forgings profile

On the basis of 7149 alloy, the impurity content of Fe and Si can be reduced. Compared with 7249 T7651 and 7075 T7651, it has better resistance to peeling corrosion, stress corrosion resistance, fracture toughness and fatigue life, and is also convenient for heat treatment. 7249 aluminum alloy forgings profile is mainly used for the forging parts of the aircraft's main landing gear.
 

Alloy	Alloy series	Main Features	σb  Value/MPa	Work Temperature/ºC
7249	7049 series(Europe)	On the basis of 7149 alloy, the impurity content of Fe and Si can be reduced. Compared with 7249 T7651 and 7075 T7651, it has better resistance to peeling corrosion, stress corrosion resistance, fracture toughness and fatigue life, and is also convenient for heat treatment	~	<125

 

Alloy	Main Features	Main products and states	Application parts and typical parts
7249	The comprehensive performance is better than 7149, and it is an improved alloy of 7049.	Aluminum forgings: T73,T74,T7452 Aluminum extrusion:T73511,T76511	The main landing gear of the aircraft is forged.

Chemical Composition of 7049Alloy

Alloy

Si

Fe

Cu

Mn

Mg

Cr

Ni

Zn

Ti

Zr

Others

Al

Each

Total

7249

0.10

0.12

1.3~1.9

0.10

2.0~2.4

0.12~0.18

~

7.5~8.2

0.06

~

0.05

0.15

Remainder

Detailed Photos