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Single-rotor air jet type carrying aircraft

A carrier aircraft and jet technology, applied in the field of aircraft, can solve the problems of short cruising range, slow movement, high price, etc., and achieve the effects of high safety, eliminating the worry of endurance problems, and being convenient to carry and purchase.

Pending Publication Date: 2018-10-09
GUANGDONG HYDROGEN ENERGY SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, similar means of transportation generally use expensive, slow-moving airships and hot air balloons, etc.
However, small carrier aircraft are limited to electric drives, and large-capacity batteries are expensive, so the problem of flight power continuity is difficult to solve, and short cruising range has become an increasingly prominent technical problem that is difficult to overcome.

Method used

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  • Single-rotor air jet type carrying aircraft
  • Single-rotor air jet type carrying aircraft
  • Single-rotor air jet type carrying aircraft

Examples

Experimental program
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Effect test

Embodiment Construction

[0024] The specific implementation manner of the present invention will be further described below in conjunction with the accompanying drawings.

[0025] Such as figure 1 , figure 2 As shown, a single-rotor jet carrier aircraft of the present invention includes a body 11, a rotor 13 mounted on the body 11 and positioned above the body, a water hydrogen machine 31 located on the body, driving the rotor 13 to operate and interacting with the water hydrogen The pressure heat energy residual gas output end of the engine 31 is connected to the docked heat engine 16 or the air motor unit 17, the jet power system that can generate a downward jet flow, and the support feet 19 located on the lower side of the body 11. The hydrogen output of the water hydrogen machine 31 is The port is connected in series to the heat engine 16 or the air motor unit 17 through the air pump 22 and the one-way air valve 23, and the jet power system includes a connection with the output end of the pressu...

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PUM

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Abstract

The invention discloses a single-rotor air jet type carrying aircraft, which comprises an aircraft body, a rotor arranged on the aircraft body and positioned above the aircraft body, a water-hydrogenmachine arranged on the aircraft body, a heat engine used for driving the rotor to operate and communicated to the pressure heat energy residual gas output end of the water-hydrogen machine, an air jet device, an air jet power system and a support foot, wherein the air jet power system comprises the air jet device capable of providing a pressure air flow, and the hydrogen output port of the water-hydrogen machine is communicated to the heat engine and the air jet device through an air pump and a one-way air valve. According to the present invention, the heat energy pressure residual gas outputted by the water-hydrogen machine is used as the power source, the hydrogen and the air are sucked to ignite so as to increase the internal energy and the internal pressure, the air jet flow is generated by the pressurization expansion in different driving equipment or the mechanical energy is output by the pneumatic motor to drive the rotor to rotate, the rotor rotating and the air jet power arecombined to drive the aircraft to fly, the lifting force and the propulsion are comprehensively provided, and the direction of the aircraft body can be adjusted by adjusting the air jet angle so as tocontrol the flying state of the aircraft.

Description

technical field [0001] The invention relates to an aircraft, in particular to a single-rotor jet carrier aircraft used as a means of transport for manned or loaded operating equipment. Background technique [0002] Aircraft that fly in the atmosphere are called aircraft, such as balloons, airships, and airplanes. They rely on the static buoyancy of the air or the aerodynamic force generated by the relative motion of the air to lift into the air. Among them, the unmanned aircraft is referred to as "drone" for short, and the English abbreviation is "UAV". It is an unmanned aircraft controlled by radio remote control equipment and its own program control device. From a technical point of view, it can be divided into: unmanned fixed-wing aircraft, unmanned vertical take-off and landing aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aircraft, unmanned parawing aircraft, etc. The application fields of drones can be divided into military and civilian. In t...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/06B64C27/12B64C15/12B64D27/24B64D27/20
CPCB64C15/12B64C27/06B64C27/12B64D27/20B64D27/24Y02T90/40
Inventor 向华
Owner GUANGDONG HYDROGEN ENERGY SCI & TECH
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