What are booster stages in aviation Gas Turbine

AI Thread Summary
Booster stages in aviation gas turbines refer to low-pressure compressor stages that increase air pressure before it enters high-pressure compressor stages. These stages are crucial for enhancing overall engine efficiency, particularly in turbofan designs. The discussion highlights the relationship between fan and booster stages, noting that both can be driven by a single low-pressure turbine. However, due to the speed differences between the low-pressure compressor and the fan, a gearbox may be necessary to synchronize their rotational speeds. Understanding the role of booster stages is essential for effective gas turbine design.
Kshitizagar
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Guys, I was reading about Turbofan and somewhere while browsing Defence Turbofan engines I came across Booster stages, but I didn't find any description or what are booster stages in Gas Turbine (Axial Compressor)
 
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I design gas turbines, & I've never heard that term for turbofans. Only has meaning to me with regard to rockets.
 
The booster is a low pressure compressor stage. Prior to ramping up the pressures with the HP compressor stages, (or in cases where the bypass is used to boost pressure for addition downstream) the air will be gradually brought up in pressure by LP stages, sometimes called booster stages.
 
Thank You Travis King... tell me one thing more if fan and booster stages are driven by one LP turbine then is it necessary that we have gearbox in between booster stage and fan. Because as far as I know there Speed (rotational) difference between LP compressor and fan
 
Due to the constant never ending supply of "cool stuff" happening in Aerospace these days I'm creating this thread to consolidate posts every time something new comes along. Please feel free to add random information if its relevant. So to start things off here is the SpaceX Dragon launch coming up shortly, I'll be following up afterwards to see how it all goes. :smile: https://blogs.nasa.gov/spacex/
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