CN211076309U

CN211076309U - Electric heating inflatable flying aircraft

Info

Publication number: CN211076309U
Application number: CN201922173156.0U
Authority: CN
Inventors: 杨礼诚
Original assignee: Individual
Current assignee: Individual
Priority date: 2019-12-06
Filing date: 2019-12-06
Publication date: 2020-07-24
Anticipated expiration: 2029-12-06

Abstract

An electric heating inflatable flying aircraft comprises a buoyant air bag, an electric heater cabin and a cabin, wherein a rechargeable battery, a blast motor, blades, an electric heating wire box and an air jet are mounted in the electric heater cabin; the cabin is hung below the buoyancy air bag and the electric heater cabin through a traction rope. The cabin is internally provided with a battery, an electric control console and a passenger seat, the rear wall of the cabin is provided with a propulsion propeller and a rudder, and a propeller motor wire and an electric control console wire are electrically connected with the battery. The device heats the air in the buoyancy lifting air bag in an electric heating mode, so that the buoyancy lifting air bag is lifted off, the lifting range is large, and the flying distance is long.

Description

Electric heating inflatable flying aircraft

Technical Field

The utility model relates to a fly the field of wafing, in particular to electric heat is aerifyd and is flown aircraft that wafts.

Background

More than 2000 years ago, ancient people just put the Kongming lantern into practical use, and the air in the lantern is heated through the flame generated after the candle is ignited, so that the lantern is lifted. In the hot air balloon which appears in recent times, air in the balloon of the balloon is heated by a burner, the density of the heated air in the balloon is reduced, the weight of the heated air is lighter than that of cold air with the same volume outside the balloon, and then the balloon generates buoyancy to lift off. Such as a standard AX-7 grade hot air balloon with a balloon volume of 2180 cubic meters and a total air mass of 2670 kilograms at sea level at 15 c of cold air. When the combustor heats the air in the balloon, the air in the balloon is expanded and has low density, and the redundant air after expansion is discharged from the bottom opening of the balloon. When 2180 cubic meters of hot air in the bladder reaches 100 ℃, the mass becomes 2070 kilograms, which is 600 kilograms lighter than the same volume of cold air (15 ℃). At the moment, the balloon generates 600 kilograms of lift force, the total flying mass of the balloon is less than 600 kilograms, and the balloon can be lifted off. However, the fire balloon aircraft has great potential safety hazard, and a serious human casualty accident is often reported, when the balloon rises to a higher altitude, the burning flame is extinguished due to oxygen deficiency, and additionally, the fire balloon fuel is limited, so that the flight distance and the lifting altitude of the fire balloon are greatly limited.

Disclosure of Invention

The utility model aims at solving the problems of the prior hot air balloon aircraft, and provides an electric heating inflatable flying aircraft with good safety, longer flying distance and higher flying height.

The technical scheme of the utility model as follows: the utility model provides an electric heat is aerifyd and is flown aircraft that wafts, this flies aircraft that includes buoyancy lift gasbag, electric heater cabin and passenger cabin, installs rechargeable battery, blower motor, blade, heating wire case and jet orifice in the electric heater cabin of buoyancy lift gasbag lower part, and rechargeable battery sets up in the cabin bottom, and blower motor and blade are installed in the rechargeable battery top, and blower motor and blade are connected with the heating wire case, and the battery powered blower motor blows the high-energy steam that the heating wire produced and aerifys to the buoyancy lift gasbag through the jet orifice. The electric heating wire box is tightly connected with an air jet port arranged on the buoyancy air bag, the upper box body plate and the lower box body plate of the electric heating wire box are provided with vent holes, and a lead of the blast motor is electrically connected with the rechargeable battery; the cabin is hung below the buoyancy air bag and the electric heater cabin through a traction rope. A cabin battery, an electric control operation platform and a passenger seat used by power supply equipment are arranged in the cabin, and two sides of the cabin are provided with viewing windows; the rear wall of the cabin is provided with a propulsion propeller and a rudder for controlling the direction, a propeller motor lead and an electric control lead of an electric control console are electrically connected with a battery, and the electric control lead of the electric control console is electrically connected with an electric heating wire box and a blower motor in an electric heater cabin.

Use the utility model discloses the time, operating personnel operates automatically controlled operation panel button and makes the heating wire case conductive heating in the electric heater under-deck to operation blower motor rotates fast, and when the air heating in the buoyancy lift gasbag can rise empty the temperature to, the buoyancy lift gasbag drives the cabin and slowly rises to the air. After the aircraft is lifted to the required height, a propulsion propeller arranged on the rear wall of the cabin is started to propel the flying device to move forwards slowly. And when the aircraft approaches a preset descending airspace and is ready to land, the propulsion propeller is closed, and the flying device slowly descends to a preset place. The starting and the closing of the propulsion propeller are realized by the control of an electric control console arranged in the cabin.

The utility model discloses the positive effect that reaches as follows:

1. due to the fact that the electric heater cabin is installed, the air in the buoyancy lifting air bag is heated in an electric heating mode through battery power supply, the buoyancy lifting air bag is made to lift off, the lifting range is large, and the flying distance is long.

2. Wide application range and multiple functions. Use the utility model discloses can carry out aerial scientific experiment and survey, can carry out large-scale air activities such as aerial photography, tourism sightseeing, aerial media advertisement, three-dimensional transportation, celebration, still can carry out spraying of agricultural, forestry seed seeding or chemical fertilizer as required.

3. The utility model is energy-saving and environment-friendly, and does not use fuel oil or natural gas and other fuels which pollute the air.

4. The utility model discloses compare with the fire balloon that uses the burning natural gas raw materials, flight safety is more reliable.

5. The utility model discloses an automatically controlled operation panel control rises to the air, descends, gos forward, turns to, drives easily, controls the convenience.

Drawings

Fig. 1 is a schematic view of the overall structure of the present invention.

As shown in the figure: 1-buoyancy air bag, 2-traction lifting rope, 3-cabin, 4-rudder, 5-propulsion propeller, 6-cabin battery, 7-observation window, 8-electric control console, 9-electric heater cabin, 10-rechargeable battery, 11-blower motor, 12-blade, 13-electric heating wire box and 14-air jet.

Detailed Description

The embodiments of the present invention will be described with reference to the accompanying drawings.

As shown in fig. 1, an electric heating inflation flying aircraft comprises a buoyancy airbag 1, an electric heater cabin 9 and a cabin 3, wherein a rechargeable battery 10, a blower motor 11, blades 12, a heating wire box 13 and an air nozzle 14 are installed in the electric heater cabin 9 arranged at the lower part of the buoyancy airbag 1, the rechargeable battery 10 is arranged at the bottom of the cabin, the blower motor 11 and the blades 12 are installed above the rechargeable battery 10, the blower motor 11 and the blades 12 are connected with the heating wire box 13, and the heating wire box 13 is closely connected with the air nozzle 14 installed on the buoyancy airbag 1. The heating wire box 13 is made of high-temperature resistant material, the heating wire is arranged in the box body, the upper box body plate and the lower box body plate of the heating wire box 13 are provided with vent holes, and hot air is blown to rapidly enter the air jet port by blowing the heat of the heating wire during the high-speed rotation of the blower motor, so that the temperature rise speed of the air bag is improved. The blower motor wire is electrically connected with a rechargeable battery 10, and the cabin 3 is hung below the buoyancy lifting air bag 1 and the electric heater cabin 9 through a traction rope 2. A cabin battery 6, an electric control operation platform 8 and passenger seats used by power supply equipment are arranged in the cabin 3, and two sides of the cabin 3 are provided with viewing windows 7; the rear wall of the cabin 3 is provided with a propulsion propeller 5 and a rudder 4 for controlling the direction, a propeller motor lead and an electric control lead of an electric control console 8 are electrically connected with a cabin battery 6, and the electric control lead of the electric control console 8 is electrically connected with an electric heating wire box lead and a blast motor lead in an electric heater cabin 9.

Claims

1. An electric heating inflation flying aircraft is characterized by comprising a buoyancy airbag, an electric heater cabin and a cabin, wherein a rechargeable battery, a blast motor, blades, an electric heating wire box and an air jet are mounted in the electric heater cabin at the lower part of the buoyancy airbag; the cabin is hoisted below the buoyancy lifting air bag and the electric heater cabin through a traction rope; a cabin battery, an electric control operation platform and a passenger seat used by power supply equipment are arranged in the cabin, and two sides of the cabin are provided with viewing windows; the rear wall of the cabin is provided with a propulsion propeller and a rudder for controlling the direction, a propeller motor lead and an electric control lead of an electric control console are electrically connected with a battery, and the electric control lead of the electric control console is electrically connected with an electric heating wire box and a blower motor in an electric heater cabin.

2. The electrically heated, air-filled, airborne aircraft of claim 1, wherein the box body of the electrically heated wire box is made of a high temperature resistant material.