Suspension aircraft by using barometric pressure to fly

An aircraft and atmospheric pressure technology, applied in the aerospace field, can solve problems such as wasting energy, failing to increase fuel utilization, and failing to achieve low-carbon environmental protection, energy saving and emission reduction, etc., to achieve convenient operation principles, improve flight efficiency, and simple structure Effect

Pending Publication Date: 2018-07-20
唐国东
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Problems solved by technology

[0002] With the development of science and technology, the flight technology is becoming more and more perfect. After several product iterations, humans have invented jet aircraft and helicopter gliders. Although the existing technology is advanced, it cannot be low-carbon and environmentally friendly in the actual flight process. Energy saving and emission reduction can not increase the utilization rate of fuel to a high value, it will waste energy and cannot effectively use air for flying

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  • Suspension aircraft by using barometric pressure to fly
  • Suspension aircraft by using barometric pressure to fly
  • Suspension aircraft by using barometric pressure to fly

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Embodiment Construction

[0013] The present invention will be described in further detail below in conjunction with the accompanying drawings.

[0014] When the present invention is implemented, a suspended aircraft utilizing atmospheric pressure includes an aircraft body 1 and a suspension device 2, the aircraft body 1 is connected with a deck 3, and the deck 3 is connected with a hull 4, The surface of the hull 4 is provided with evenly distributed small holes, and the shape of the hull 4 is the curve of the fastest descending line. The steepest descending line can greatly reduce the resistance of the airflow when it is attached to the slope of the steepest descending line. The deck 3 is connected with a cabin 5, the cabin 5 is connected with a fixed rod 6, the fixed rod 6 is connected with a suspension device 2, and the suspension device 2 includes a housing 7, The center of the housing 7 is provided with a housing air outlet 8, the housing air outlet 8 is a circular through hole, the housing 7 is ...

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Abstract

The invention discloses a suspension aircraft capable of using barometric pressure to fly. The suspension aircraft capable of using the barometric pressure to fly comprises an aircraft body and suspension devices. A deck is arranged on the aircraft body in a connecting mode. A hull is arranged under the deck in a connecting mode. Small holes which are evenly distributed are formed in the surface of the hull. A cabin is arranged on the deck in a connecting mode. Fixing rods are arranged on the cabin in a connecting mode. The suspension devices are arranged on the connecting rods in a connectingmode. The suspension devices comprise shells. A shell wind outlet is formed in the center of each of the shells. The shell wind outlets are circular through holes. Connecting frames are arranged on the shells in a connecting mode. Wind supply pipes are connected with the connecting frames in a matched mode. Wind outlets are formed in the wind supply pipes in a connecting mode. Wind blades are arranged on the end portions of the wind outlets in a connecting mode. Motors are arranged on the end portions of the wind blades in a connecting mode. Compared with the prior art, the suspension aircraft capable of using the barometric pressure to fly has the advantages that the structure is simple, the operation principle is convenient and the flight efficiency can be improved.

Description

technical field [0001] The invention relates to the field of aerospace, in particular to a hovercraft flying under atmospheric pressure. Background technique [0002] With the development of science and technology, the flight technology is becoming more and more perfect. After several product iterations, humans have invented jet aircraft and helicopter gliders. Although the existing technology is advanced, it cannot be low-carbon and environmentally friendly in the actual flight process. Energy saving and emission reduction cannot increase the utilization rate of fuel to a high value, which will waste energy and cannot effectively use air for flight. Contents of the invention [0003] The technical problem to be solved by the present invention is to provide an aircraft capable of flying efficiently in view of the above problems. [0004] In order to solve the above-mentioned technical problems, the technical solution provided by the present invention is: a hovering aircra...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/20B64C1/00B64C1/38
CPCB64C1/0009B64C1/38B64C27/20B64U50/14
Inventor 唐国东
Owner 唐国东
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