Allicdata Part #: | 0025-261-3014-ND |
Manufacturer Part#: |
0025-261-3014 |
Price: | $ 2.88 |
Product Category: | Uncategorized |
Manufacturer: | TE Connectivity Deutsch Connectors |
Short Description: | NUT PANEL |
More Detail: | N/A |
DataSheet: | 0025-261-3014 Datasheet/PDF |
Quantity: | 1000 |
250 +: | $ 2.61609 |
Series: | * |
Part Status: | Active |
Due to market price fluctuations, if you need to purchase or consult the price. You can contact us or emial to us: sales@allicdata.com
0025-261-3014 is a gas turbine engine used in industrial, commercial and military aerospace applications. A gas turbine engine is a type of internal combustion engine that utilizes a gas turbine to drive an aircraft propeller or rotorcraft. This type of engine uses the principal of the Brayton cycle to generate power from an air-fuel mixture and is typically composed of four main components: compressor, combustor, turbine and exhaust.
The compressor section of the engine intakes air from the outside environment and then compresses it. This raise the temperature of the air to enable the uptakes of additional fuel flow for combustion. The combination of combustible fuel and air is used to ignite and create a combustion reaction chamber. The heat from the combustion reaction is used to spin a turbine like a fan where the air and fuel are pushed into the turbine. The turbine then uses the force of the hot air and pressurizes it to power the engine.
The turbines of a gas turbine engine are usually constructed from solid metal forgings or composite materials for added longevity and efficiency. The turbines operate on aerodynamic principles which allow the engine to extract more air and fuel to increase the thrust output for a given amount of fuel consumed. The general working principle of a gas turbine engine is to convert the energy released by the combustion of the air-fuel mixture into mechanical energy.
The exhaust section is where the hot gases released from the combustion reaction are exhausted from the engine. This helps to maintain a safe pressure inside the engine and also to regulate the engine temperature. The exhaust gases are cooled and can be routed to either the turbine or the condenser depending on the engine design.
The 0025-261-3014 is a highly reliable gas turbine engine and is suitable for a wide range of applications. It can be used in industrial applications such as gas and oil processing plants, as well as commercial and military aerospace applications such as helicopters and aircraft. Its reliable and efficient operation makes it an ideal choice for many applications.
The specific data is subject to PDF, and the above content is for reference
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