Passenger plane capable of vertically lifting and lowering
A vertical lift, passenger aircraft technology, applied in the field of flight, can solve the problems of bumps, loss of control, travel inconvenience, etc., to achieve the effect of enhancing the overall strength, avoiding the influence of airflow, and providing good support
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Embodiment 1
[0034] as attached figure 1 As shown, a passenger aircraft that can be lifted vertically includes a fuselage 1 and a wing 2, the wing 2 is symmetrically arranged, and is a double-layer hollow structure, including a first upper deck 21 and a first lower deck 22 arranged in parallel, A first rotor 3 is installed in the hollow structure, and the rotation plane of the first rotor 3 is perpendicular to the first upper plate 21 and the first lower plate 22;
[0035] The fuselage 1 is provided with a first motor 4 and a second motor 5;
[0036] The first motor 4 and the second motor 5 are connected to the two wings 2 through the first rotating shaft 41 and the second rotating shaft 51 respectively.
[0037] The hollow structure of the wing 2 is divided into several spaces equally spaced by a plurality of first partitions 23 , and each space is provided with a first rotor 3 .
[0038] Also includes: a third motor 11 and a fourth motor 12;
[0039] The first rotor 3 in the wing 2 on...
Embodiment 2
[0044] as attached figure 2 , attached image 3 And attached Figure 4 , a passenger aircraft that can be lifted vertically, including a fuselage 1 and a wing 2, the wing 2 is symmetrically arranged, and is a double-layer hollow structure, including a first upper deck 21 and a first lower deck 22 arranged in parallel, the hollow structure A first rotor 3 is installed in it, and the rotation plane of the first rotor 3 is perpendicular to the first upper plate 21 and the first lower plate 22;
[0045] The fuselage 1 is provided with a first motor 4 and a second motor 5;
[0046] The first motor 4 and the second motor 5 are respectively connected to the two wings 2 through the first rotating shaft 41 and the second rotating shaft 51 .
[0047] The hollow structure of the wing 2 is divided into several spaces equally spaced by a plurality of first partitions 23 , and a first rotor 3 is arranged in each space.
[0048] Also includes: a third motor 11 and a fourth motor 12;
...
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