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

Inactive Publication Date: 2019-02-12
FOSHAN SHENFENG AVIATION SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the existing passenger-carrying aircraft almost all use the large pressure difference generated by the run-up to lift the aircraft up and fly smoothly. Extreme airflow is easily affected by airflow. For example, if the aircraft encounters chaotic airflow during the flight process, if the aircraft does not adjust its course in time, it will cause turbulence or even lose control and cause danger
And adopt the aircraft flight mode in the prior art, need to build the special airport with enough big area to run-up and land, so the airport is mostly built in the outskirts of sparsely populated, and this also brings a little inconvenience to the traveler

Method used

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  • Passenger plane capable of vertically lifting and lowering
  • Passenger plane capable of vertically lifting and lowering
  • Passenger plane capable of vertically lifting and lowering

Examples

Experimental program
Comparison scheme
Effect test

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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PUM

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Abstract

The invention provides a passenger plane capable of vertically lifting and lowering. According to the passenger plane capable of vertically lifting and lowering, rotatable wings are adopted to combinewith a plurality of rotor wings arranged in the wings, different angle force to a plane can be provided by the rotor wings through the rotation of the wings, adjustment can be realized according to requirements, so that vertically lifting and lowering of the plane can be realized. When encountering chaotic airflow in the navigation process, the plane can carry out emergency hovering outside a airflow area until the airflow disappears, or the rotating speeds of the rotor wings in the wings on both sides can be adjusted to be different to provide rotating force for the plane to make emergency steering and change course, so that the comfort and safety of the plane are increased; and meanwhile, the plane capable of vertically lifting and lowering does not need to run up, so that the area of an airport is greatly reduced, the airport can even be constructed in a city, the convenience of traveling is increased, and the application value and popularization value are high.

Description

technical field [0001] The invention relates to the field of flight technology, in particular to a vertically liftable passenger plane. Background technique [0002] As a high-end travel tool, airplanes are increasingly becoming the first choice for people to travel due to their high speed, high safety and good service. However, the existing passenger-carrying aircraft almost all use the large pressure difference generated by the run-up to lift the aircraft up and fly smoothly. Extreme airflow is easily affected by the airflow. For example, if the aircraft encounters chaotic airflow during the flight process, if the aircraft does not adjust its course in time, it will cause turbulence or even lose control and cause danger. And, adopt the aircraft flight mode in the prior art, need to build the special airport that area is big enough to run-up and land, so the airport is built in sparsely populated suburbs more, and this also brings a little inconvenience to the traveler. ...

Claims

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Application Information

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IPC IPC(8): B64C27/28B64C3/38B64C5/10B64C29/00
CPCB64C27/28B64C3/385B64C5/10B64C29/0008
Inventor 李玉龙王志成
Owner FOSHAN SHENFENG AVIATION SCI & TECH
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