Chalco can produce DTD 5110 7014 O/T6/T651 Clad Plate and AMS-QQ-A-250/13 7014 T7451/T79/T651 aviation ty so bong da truc tiep alloy plates, which are made of two different metal material layers through cold rolling or explosive welding Pressed together by technology, usually used in the manufacture of components that require high strength and light weight in aircraft structures.
7014 aircraft ty so bong da truc tiep alloy product specification
| specification | |
| Alloy | 7014 |
| Temper | O, T6, T651, T7451, T79 |
| Thickness | DTD 5110, AMS-QQ-A-250/13, ASTM B209-14, EN 485-2 |
| Width | 1.0 mm, 1.5 mm, 2.0 mm, 3.0 mm, 4.0 mm, 5.0 mm, 6.0 mm, 8.0 mm, 10.0 mm |
| Length | 2000 mm, 2500 mm, 3000 mm, 4000 mm |
If you need customized size and length range, suggest you to consult Chalco is a high-quality manufacturer and supplier of 7014 ty so bong da truc tiep alloy material, the following is the general specification of 7049 ty so bong da truc tiep products that can be manufactured by 7014, please refer to.
7014 ty so bong da truc tiep alloy chemical composition
| Chemical composition | |||||||||
| chemical composition | Si | Fe | Cu | Mn | Mg | Cr | Zn | Ti | Al |
| maximum value | 0.4 | 0.5 | 0.1 | 0.3 | 1.2 | 0.25 | 0.25 | 0.15 | margin |
7014 ty so bong da truc tiep plate sheet physical properties
| Standard | Density | Expansion Thermal | Conductivity | Conductivity |
| DTD 5110 7014Clad aluminium Plate | 2.78 g/cm³ | 23.8 μm/m·°C | 124 W/(m·K) | 32.7 MS/m |
| AMS-QQ-A-250/13 7014 aluminium plate | 2.78 g/cm³ | 23.1 x 10^-6/℃ | 121 W/m-K | 0.035 μΩ-m |
DTD 5110 7014 clad aluminium plate physical properties
| Tensile strength | Yield strength | Elongation | Hardness |
| 470-510 MPa | ≥345 MPa | ≥6% | 135-150 HV |
AMS-QQ-A-250/13 7014 aluminium plate physical properties
| Tensile strength | Yield strength | Elongation | Hardness | Tensile strength |
| ≥485 MPa | ≥435 MPa | ≥6% | ≥10% | ≤155 |
Application of 7014 ty so bong da truc tiep alloy plate in aircraft
7014 O aircraft ty so bong da truc tiep plate
Without artificial aging treatment, it is suitable for some parts that do not require high strength and hardness, such as aircraft interior panels, wheels, seats, etc.
7014 T6 aircraft ty so bong da truc tiep plate
After artificial aging treatment, the highest strength and hardness are obtained. It is suitable for parts that require high strength and hardness, such as wings, leading edge panels, wheels, armrests, seats, etc.
7014 T651 aircraft ty so bong da truc tiep plate
After artificial aging treatment and stretching treatment, it has excellent strength and toughness, and is suitable for parts that require high strength and crack resistance, such as fuselage, wing spar, leading edge plate, ground equipment, etc.
7014 T7451 aircraft ty so bong da truc tiep plate
Aviation ty so bong da truc tiep plate in T7451 temper is suitable for parts that require high strength and crack resistance, such as fuselage, wing spar, leading edge plate, ground equipment and other parts.
7014 T7651 aircraft ty so bong da truc tiep plate
Aviation ty so bong da truc tiep plate in T7651 temper is suitable for parts that require high strength and high toughness, such as wing spars, leading edge panels, armrests, seats and other parts.
7014 T79 aircraft ty so bong da truc tiep plate
Aviation ty so bong da truc tiep plate in T79 temper is suitable for parts under high temperature, such as engine casing, nozzle, gas turbine blade and other parts.
7014 ty so bong da truc tiep alloy plate used in aircraft parts has the following advantages
Lightweight and high-strength:the density of ty so bong da truc tiep alloy is relatively small, and the use of 7014 ty so bong da truc tiep alloy plate can reduce the weight of the aircraft and improve fuel economy while ensuring the strength.
Good corrosion resistance:the surface of ty so bong da truc tiep alloy is generally treated with anti-corrosion treatment, and the surface of 7014 ty so bong da truc tiep alloy plate is coated with ty so bong da truc tiep or other anti-corrosion treatment methods are used, which can maintain good corrosion resistance in harsh environments.
Excellent processing performance:7014 ty so bong da truc tiep alloy plate can be processed in various ways, such as stamping, cutting, welding, etc., with wide adaptability.
High reliability:ty so bong da truc tiep alloy has a long fatigue life, and aircraft parts made of 7014 ty so bong da truc tiep alloy plate have high reliability and safety.
Low production cost:compared with other metal materials, ty so bong da truc tiep alloy materials have the advantage of lower production costs, which can reduce aircraft manufacturing costs.
To sum up, the 7014 ty so bong da truc tiep alloy plate used in aircraft parts has the advantages of light weight, high strength, corrosion resistance, excellent processing performance, high reliability, and low production cost. It is widely used in aircraft structural parts, fuselage, shell, etc.
7014 aviation ty so bong da truc tiep plate weight
7014 ty so bong da truc tiep alloy density: 2.77 g/cm³.
ty so bong da truc tiep plate weight calculation: length (mm) x width (m) x density 2.85g/cm³
7014 aviation ty so bong da truc tiep plate price
7014 ty so bong da truc tiep plate price:
(LME ingot price + processing fee) x weight + packaging fee + transportation fee
The price of 7014 ty so bong da truc tiep alloy will be affected by many factors, such as market supply and demand, raw material prices, processing costs, specifications and sizes, etc. Different manufacturers and suppliers may have different pricing strategies and price levels. In addition, it is also affected by factors such as currency exchange rate and international economic situation.
Therefore, please contact Chalco ty so bong da truc tiep for inquiry, we will provide you with the best quotation and service.
Production requirements and process control of 7014 aviation ty so bong da truc tiep alloy plate
The AMS-QQ-A-250/13 and DTD 5110 standards specify the production requirements and process control of 7014 ty so bong da truc tiep alloy plates. Among them, the following is the basic process for the production of 7014 ty so bong da truc tiep alloy plates specified in the standard:
Preparation of ty so bong da truc tiep alloy raw materials:firstly, it is necessary to select suitable ty so bong da truc tiep alloy raw materials that meet the AMS-QQ-A-250/13 standard, such as 7175, 7075, etc., and process them into ty so bong da truc tiep alloy plate raw materials through mixing, casting and other processes.
Heat treatment:after being rolled into plates, heat treatment processes, including solutionization and artificial aging treatment, are required to adjust the structure and properties of the alloy. Among them, solution treatment requires high-temperature heating to uniformly dissolve the elements in the alloy material in the solid solution; artificial aging treatment is to keep the material at a lower temperature for a certain period of time, so that the elements in the solid solution are rearranged and form corresponding strengthening. phase to increase the strength and toughness of the material.
Panel rolling:after heat treatment, the ty so bong da truc tiep alloy plate needs to be rolled to make it reach the required size and flatness.
ty so bong da truc tiep cladding:after the rolling process, the ty so bong da truc tiep alloy plate needs to be clad with ty so bong da truc tiep, that is, a layer of pure ty so bong da truc tiep material is pressed to one side of the ty so bong da truc tiep alloy plate to improve its surface quality and corrosion resistance.
Machining and surface treatment:finally, machining and surface treatment are required to meet the requirements in the AMS-QQ-A-250/13 standard, such as flatness, surface finish, dimensional accuracy, chemical composition, etc.
It should be noted that the production process of aviation ty so bong da truc tiep alloy plates needs to be strictly controlled in every link to ensure that the quality and performance of the products meet the standards and customer requirements. At the same time, the heat treatment process and manufacturing process required for aviation ty so bong da truc tiep alloy plates in different tempers may also be different.
When purchasing 7014 ty so bong da truc tiep alloy aircraft ty so bong da truc tiep plate, you need to pay attention to the following items
Material certification:when purchasing ty so bong da truc tiep plates, suppliers are required to provide certification documents that meet aviation standards, such as AMS, DTD, QQ and other certification documents.
Dimensional requirements:according to specific application needs, suppliers are required to provide ty so bong da truc tiep plates that meet the specifications, including dimensional parameters such as thickness, width, and length.
Surface treatment:suppliers are required to provide surface treatment that meets the requirements, such as ty so bong da truc tiep cladding, anodizing, painting, etc., to meet the use requirements of aircraft parts.
Delivery time requirement:according to the project progress requirements, the supplier is required to provide a satisfactory delivery time to ensure the smooth progress of the aircraft parts production plan.
Quality assurance:suppliers are required to provide quality assurance that meets aviation standards to ensure that the supplied ty so bong da truc tiep sheets meet the specifications and have stable quality performance.
Price advantage:on the premise of meeting quality requirements, suppliers are required to provide competitive prices to reduce aircraft production costs.
To sum up, when purchasing 7014 ty so bong da truc tiep alloy aircraft ty so bong da truc tiep plate, you need to pay attention to material certification, size requirements, surface treatment, delivery time requirements, quality assurance and price advantages, etc., to ensure that the purchased ty so bong da truc tiep plate meets the production requirements and has a stable quality performance.