| 摘要 |
The present invention relates to an individual flight apparatus, consisting of two internal combustion engines (1) which drive two propellers (2) arranged in a horizontal plane. The two engines (1) have rotation which is synchronised by four conical toothed wheels (3) and (5) and by a shaft (6) which is in a tube (7) which supports the two engines and which, in its centre, supports the flying harness (17) of the pilot. On this tube (7) there are also two vertical bars (8) with two handles (9) and (10): one for acceleration and the other for manoeuvring the apparatus in rotation, via two steerable wings (14). In these bars two other bars (15) can fit telescopically, which serve as legs for the apparatus. On the said bars (8) there are two tanks (16). <IMAGE>
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