| 摘要 |
A turbojet with a hollow spool 1 connected to a turbine 2, the turbine blades of the turbine having hollow ducts inside them which run their length which are open at both ends and which are linked to the hollow spool 1 through which a coolant, preferably water or distilled water, will flow. An inlet, positioned near or attached via bearings to the front end 3 of the spool 1, may be used to supply the coolant and may be connected to a pump 4 and a coolant tank 5. The hollow spool 1 may also be connected to subsequent sets of turbines, the blades of these turbines having hollow ducts inside them which run their length, and which are open at both ends which are linked to the hollow spool 1.
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