T-stage

T-stages, sometimes called booster stages, are mounted on the low pressure (LP) shaft of some turbofan engines directly behind the fan.

T-stages are used to increase overall pressure ratio and, for a given core size, the core mass flow. This is demonstrated by the following relationship:

:$w_2 = (w_2 \sqrt/P_3) )* (P_3/P_2)* (P_2/P_1)*( P_1/ \sqrt)/ (\sqrt * \sqrt ),$

:where:

:hp compressor entry mass flow = $w_2 \,$

:core size = $(w_2 \sqrt/P_3) \,$

:hp compressor total head pressure ratio = $P_3/P_2 \,$

:lp compressor total head pressure ratio = $P_2/P_1 \,$

:lp compressor entry total pressure = $P_1 \,$

:lp compressor entry total temperature = $T_1 \,$

:hp compressor total head temperature ratio = $T_3/T_2 \,$

:lp compressor total head temperature ratio = $T_2/T_1 \,$ which varies more slowly than $P_2/P_1 \,$

So as $P_2/P_1 \,$ increases with the addition of T-stages, $w_2 \,$ also increases.

T-stages are a popular method for uprating the thrust of an engine (see, for example the Pratt & Whitney Canada PW500).

The alternative is to place a zero-stage, mounted on the HP shaft, at the front of the HP compressor. This approach requires a significant change in the HP turbine, whereas a T-stage can, if necessary, be accommodated by simply adding another stage to the rear of the LP turbine.

Although T-stages usually only supercharge the core stream, some engines do feature a deliberately oversized intermediate pressure (IP) compressor, which compresses both the core flow and a proportion of the bypass flow. This enhances the stability of the T-stages during throttling. Where necessary, the alternative is to employ blow-off valves.

References

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Jet engines