| Allicdata Part #: | 7-1617250-6-ND |
| Manufacturer Part#: |
7-1617250-6 |
| Price: | $ 3.25 |
| Product Category: | Uncategorized |
| Manufacturer: | TE Connectivity Aerospace, Defense and Marine |
| Short Description: | T30171G2=SPREADER PAD .300 |
| More Detail: | N/A |
| DataSheet: | 7-1617250-6 Datasheet/PDF |
| Quantity: | 1000 |
| 50 +: | $ 2.95659 |
| Series: | * |
| Part Status: | Active |
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7-1617250-6 Application Field and Working Principle
7-1617250-6 is a high-temperature resistant material, mainly used in aircraft turbine engines and other areas that require high temperature and high pressure resistance. This material is used in components such as gaskets, bolts, valves, seals, and even engines where high temperatures and pressures may be present. The 7-1617250-6 material is composed of several different materials, including carbon fiber, stainless steel, and aluminum. The combination of these materials make up the 7-1617250-6 material.
In order to understand the application field and working principle of the 7-1617250-6 material, it is important to understand the properties of each of the materials used in its composition. Carbon fiber is a strong, lightweight material that is resistant to damage and able to tolerate extreme temperatures and pressures. On the other hand, stainless steel is a durable and corrosion-resistant material, which makes it ideal for components that might be exposed to high temperatures. Finally, aluminum is a good conductor of heat, which allows components made from this material to better dissipate heat.
The combination of these materials allows 7-1617250-6 to resist heat up to 1600 degrees Fahrenheit, as well as handle pressures of up to 3,500 psi. This makes it well-suited for components subject to high temperatures and pressures, such as turbine engines. The 7-1617250-6 material has also been designed to be flexible and able to tolerate extreme physical shocks. This allows it to be used in applications such as landing gear or rocket engines that must cope with extreme temperatures and pressures.
In conclusion, the 7-1617250-6 material is a composite material composed of carbon fiber, stainless steel, and aluminum. Designed to handle extreme temperatures and pressures, this material is largely used in aircraft turbine engines and rocket engines. It allows components to better resist heat and handle higher pressures, and, because of its flexibility, it is also able to cope with extreme physical shocks.
The specific data is subject to PDF, and the above content is for reference
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7-1617250-6 Datasheet/PDF