A novel jet-propelled vertical lifting aircraft and a novel aviation power system

An aerodynamic, vertical lift technology, applied to vertical take-off and landing aircraft, aircraft, vehicles that can be converted into aircraft, etc., to achieve the effect of avoiding instantaneous fluctuations

Active Publication Date: 2019-06-07
珠海市蓝鹰贸易有限公司
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Problems solved by technology

[0007] The technical problem to be solved by the present invention is how to overcome the above-mentioned defects of the existing jet vertical lift aircraft. One of the purposes of the present invention is to provide a lo

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  • A novel jet-propelled vertical lifting aircraft and a novel aviation power system
  • A novel jet-propelled vertical lifting aircraft and a novel aviation power system
  • A novel jet-propelled vertical lifting aircraft and a novel aviation power system

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Embodiment Construction

[0055] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0056] Such as figure 1 , figure 2 , image 3 , Figure 4 , Figure 5 , Figure 6 , Figure 7 , Figure 8 , Figure 9 , Figure 10 , Figure 11 Shown:

[0057] A jet vertically liftable aerial vehicle, comprising a streamlined fuselage 1 with the appearance of a devil ray, a left air inlet 2, a left air inlet 3, a right air inlet 4, a right air inlet 5, a middle inlet Air port cover plate 6, middle air inlet 7, middle air inlet 8, new jet aerodynamic system 9, left empennage 11, left rudder 12, right empennage 13, right rudder 14, left elevator 15, right elevator 16, Rear middle nozzle...

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Abstract

The design thought of an existing jet-propelled vertical lifting aircraft is changed, and the appearance of the jet-propelled vertical lifting aircraft adopts a streamline-shaped aircraft body with anintegrated wing body like a magic fish; two turboshaft aero-engines are used as core machines to save fuel oil, and two contra-rotating fans are used to increase the efficiency of air suction and airflow pressurization. A pressure cavity of the engine is made into a bearing chassis of the aircraft to reduce the weight of the aircraft and fully utilize the internal space of the aircraft; the engine sprays high-flow high-pressure airflow into the pressure cavity, the pressure cavity becomes a buffer for the airflow sprayed by each vector nozzle assembly, and becomes a silencer for reducing noise of the fans and the engines. Therefore, the air flow and the air injection direction sprayed by each vector nozzle connected to the periphery of the aircraft can be opened, closed and continuouslyadjusted, and the controllability of the aircraft is improved. Therefore, the novel jet-propelled vertical lifting aircraft and the novel aviation power system which are easy to control, can fly in acity and can be driven by ordinary people like automobiles are produced.

Description

technical field [0001] The invention belongs to the related technical field of jet vertical lift aircraft, and in particular relates to a jet vertical lift aerial vehicle and a novel aerodynamic system. Background technique [0002] At present, several known vertical lift aerial vehicles all use propellers to provide the lift and thrust of the aircraft, which are just deformations of helicopters, which still retain the characteristics of loud noise, slow speed, short range and difficult control. Although there are several types of jet vertical lift aircraft, they all adopt the world's most cutting-edge technology and production technology, and are extremely difficult to manufacture. At present, only a few countries with the most advanced technology in the world are capable of manufacturing. Not only the price is high, but also the control is complicated, ordinary people can’t afford it, can’t use it, and have nowhere to buy it. It is limited to the military use of a few deve...

Claims

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Application Information

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IPC IPC(8): B64C29/00B60F5/02
Inventor 张鸿元张芷凝张廷琛
Owner 珠海市蓝鹰贸易有限公司
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