| 摘要 |
<p> This thrust generation device, which has an axial flow compressor, is configured so that, for rotors of the axial flow compressor in which a plurality of stages of blade rows are concentric and alternately rotate in reverse, blades inclined in a direction along the direction from which the air is fed can be placed in a front stage and the subsequent rear stage rotor, and the rotary shaft of the rotors rotating in the forward direction and in the reverse direction forms a rotary body for forward rotation on which a plurality of rows of rotors are arranged, and a rotary body that alternately rotates in reverse on which a plurality of rows of rotors are arranged.</p> |
