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A gas turbine engine having speed an intermediate stage booster configured to provide speed change to a boost compressor. The boost compressor and fan stage are driven by a low pressure turbine; the fan stage rotates with the low pressure turbine shaft and the boost compressor rotates counter to the

A gas turbine engine having speed an intermediate stage booster configured to provide speed change to a boost compressor. The boost compressor and fan stage are driven by a low pressure turbine; the fan stage rotates with the low pressure turbine shaft and the boost compressor rotates counter to the low pressure turbine shaft. The intermediate speed booster has an epicyclic gear train that includes an outer annulus, a sun gear, and a planetary gear, and may be engaged by a clutch in some embodiments.

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1. A turbofan engine comprising: turbomachinery components limited to two shaft driven spools, the components including a low pressure spool and a high pressure spool, the low pressure spool including a low pressure turbine;a low pressure shaft coupled to and rotatable by operation of said low press

1. A turbofan engine comprising: turbomachinery components limited to two shaft driven spools, the components including a low pressure spool and a high pressure spool, the low pressure spool including a low pressure turbine;a low pressure shaft coupled to and rotatable by operation of said low pressure turbine;a bladed air moving device coupled to said low pressure shaft;a boost compressor located downstream of said bladed air moving device and substantially free from driven rotation with respect to the high pressure spool; anda mechanical speed booster coupled with said low pressure shaft and said boost compressor, said mechanical speed booster operable to drive said boost compressor at a rotational speed different than the rotational speed of said low pressure shaft. 2. The turbofan engine of claim 1, wherein the mechanical speed booster is operable to drive said boost compressor at a rotational speed greater than the rotational speed of said shaft. 3. The turbofan engine of claim 1, wherein said mechanical speed booster includes a gear train. 4. The turbofan engine of claim 3, wherein the gear train is an epicyclic gear train having a sun gear, an annulus gear, and a plurality of planet gears. 5. The turbofan engine of claim 1, wherein the mechanical speed booster is operable to drive said boost compressor at a rotational speed within a range from 1.5 to 3 times the rotational speed of said shaft. 6. The turbofan engine of claim 1, which further includes a clutch operable to selectively engage and disengage said mechanical speed booster with said shaft. 7. The turbofan engine of claim 1, which further includes a radial intershaft bearing to support said boost compressor. 8. The turbofan engine of claim 1, which further includes means for carrying the load associated with said bladed air moving device. 9. The turbofan of claim 1, wherein said bladed air moving device rotates at the rotational speed of said shaft, and wherein said bladed air moving device is a fan. 10. The turbofan engine of claim 1, wherein the mechanical speed booster is operable to drive said boost compressor at a rotational speed less than the rotational speed of said shaft. 11. The turbofan engine of claim 1, wherein said mechanical speed booster includes a gear train, said gear train is an epicyclic gear train having a sun gear, an annulus gear, and a plurality of planet gears; which further includes means for carrying the load associated with said bladed air moving device; andwherein said bladed air moving device rotates at the rotational speed of said shaft. 12. The turbofan engine of claim 1, wherein said boost compressor includes a plurality of stages. 13. The turbofan engine of claim 1, wherein said bladed air moving device and boost compressor rotate in opposite directions. 14. A gas turbine engine comprising: a dual spool turbine having a low pressure turbine and a high pressure turbine;a high pressure compressor;a shaft coupled to and rotatable by operation of said low pressure turbine;a boost compressor located upstream of said high pressure compressor and incapable of mechanical connection with respect to rotation of the high pressure compressor; anda transmission coupled with said low pressure shaft and said boost compressor, said transmission operable to drive said boost compressor at a rotational speed different than the rotational speed of said low pressure shaft;wherein the gear train is an epicyclic gear train having a sun gear, an annulus gear, and a plurality of planet gears. 15. The gas turbine engine of claim 14, wherein said transmission is operable to drive said boost compressor at a rotational speed greater than the rotational speed of said low pressure shaft. 16. The gas turbine engine of claim 14, which further includes means for selectively engaging and disengaging the transmission of power from said low pressure shaft to said transmission. 17. The gas turbine engine of claim 14, wherein said transmission operable to drive said boost compressor at a rotational speed less than the rotational speed of said low pressure shaft. 18. The gas turbine engine of claim 14, wherein the gas turbine engine is a turboprop. 19. The gas turbine engine of claim 14, wherein the gas turbine engine is a turboshaft. 20. A turbofan engine comprising: a relatively low pressure turbine;a shaft coupled to and rotatable by operation of said relatively low pressure turbine;a bladed rotor coupled to said shaft;a boost compressor located downstream of said bladed rotor;means for rotational speed change of said boost compressor stage; andmeans for selective coupling of the boost compressor to the shaft. 21. A turbofan engine comprising: a turbine;a shaft coupled to and rotatable by operation of said turbine;a fan coupled to said shaft and fixed to the rotational speed of said shaft;a boost compressor coupled to said shaft;a gear box between said shaft and said boost compressor, said gear box operable to drive said boost compressor at a rotational speed different than the rotational speed of said shaft; anda clutch operable to selectively engage and disengage the transmission of power from said shaft to said boost compressor. 22. The turbofan engine of claim 21, wherein said gear box is operable to drive said boost compressor at a rotational speed greater than the rotational speed of said shaft. 23. The turbofan engine of claim 21, which further includes means for carrying the load associated with said fan. 24. The turbofan of claim 21, wherein said fan rotates in the same direction as said shaft and wherein said boost compressor rotates in the opposite direction of said fan.