阅读说明：本技术 一种充气飞行器 (Inflatable aircraft ) 是由 林子超 于 2021-03-30 设计创作，主要内容包括：本发明公开了一种充气飞行器。它包括飞行器结构、荷载仓、操控台、储气罐、气体压缩机构和发动机构；飞行器结构为气囊结构；飞行器结构内设置支撑骨架；荷载仓连接在飞行器结构下方；座椅和/或载物空间可拆卸地设置在荷载仓内；操控台、储气罐和气体压缩机构均设置在荷载仓内；发动机构设置在飞行器结构上。本发明具有结构简单、造价低廉、可载人载物、使用和维护方便的优点。(The invention discloses an inflatable aircraft. The aircraft comprises an aircraft structure, a load bin, a console, a gas storage tank, a gas compression mechanism and an engine mechanism; the aircraft structure is an airbag structure; a support framework is arranged in the aircraft structure; the load bin is connected below the aircraft structure; the seat and/or the carrying space are/is detachably arranged in the load cabin; the console, the gas storage tank and the gas compression mechanism are all arranged in the load bin; the launch mechanism is disposed on the aircraft structure. The invention has the advantages of simple structure, low cost, capability of carrying people and goods, and convenient use and maintenance.)

1. An inflatable aircraft, characterized in that: the aircraft comprises an aircraft structure (1), a load cabin (2), a console (5), an air storage tank (7), a gas compression mechanism (8) and an engine mechanism (9);

the aircraft structure (1) is an airbag structure;

a support framework (11) is arranged in the aircraft structure (1);

the load bin (2) is connected below the aircraft structure (1);

the seat (6) and/or the loading space (10) are/is detachably arranged in the loading bin (2);

the control platform (5), the gas storage tank (7) and the gas compression mechanism (8) are all arranged in the load bin (2);

the starting mechanism (9) is arranged on the aircraft structure (1).

2. The inflatable aircraft of claim 1, wherein: a safety valve (3) is arranged on the aircraft structure (1);

the tire (4) is arranged at the lower end of the load bin (2).

3. The inflatable aircraft of claim 2, wherein: the load bin (2) comprises a first load bin (2.1) and a second load bin (2.2);

the gas storage tank (7) and the gas compression mechanism (8) are both arranged in the first load bin (2.1);

the console (5), the seat (6) and/or the loading space (10) are arranged in the second loading compartment (2.2).

4. The inflatable air vehicle of claim 3, wherein: the seat (6) is arranged between the console (5) and the object space (10);

or only the seat (6) is arranged in the load cabin (2);

a plurality of seats (6) are provided; the plurality of seats (6) are arranged at intervals;

or only the loading space (10) is arranged in the loading bin (2).

5. The inflatable aircraft of claim 4, wherein: the aircraft structure (1) is in the shape of an airplane; the aircraft structure (1) is a hollow structure; the outer wall of the aircraft structure (1) is made of high-strength film or fabric, and light gas is filled inside the aircraft structure;

the supporting framework (11) is made of light high-strength aviation materials.

6. The inflatable aircraft of claim 5, wherein: the aircraft structure (1) is respectively connected with an air storage tank (7), a gas compression mechanism (8) and an engine mechanism (9);

the engine mechanism (9) is a fan engine.

Technical Field

The invention relates to an inflatable aircraft.

Background

Fire balloons and airships have emerged as early-stage aircraft for over two hundred years. It has the advantages that: the lift force is provided by the light gas, the vertical (or short-distance take-off and landing) can be realized, and the lift force is maintained without additionally consuming a large amount of energy; the structure is simple, and the manufacturing cost is low; the disadvantage is poor flight and handling. And thus the use is greatly restricted. It is now difficult to see the shadow, except in very few areas. Airplanes are coming out later and are widely used due to their excellent aerodynamic layout and maneuverability and relatively high flight speed. Its disadvantages are complex manufacture, high cost of use and maintenance, high fuel consumption and large carbon emission.

Therefore, there is a need to develop an aircraft that is cost effective and reduces the cost of use and maintenance.

Disclosure of Invention

The invention aims to provide an inflatable aircraft which is simple in structure, low in manufacturing cost, cost-saving, convenient to use and capable of reducing use and maintenance cost.

In order to achieve the purpose, the technical scheme of the invention is as follows: an inflatable aircraft, characterized in that: the aircraft comprises an aircraft structure, a load cabin, a console, a gas storage tank, a gas compression mechanism and an engine mechanism;

the aircraft structure is an airbag structure;

a support framework is arranged in the aircraft structure;

the load bin is connected below the aircraft structure;

the seat and/or the carrying space are/is detachably arranged in the load cabin;

the console, the gas storage tank and the gas compression mechanism are all arranged in the load bin;

the launch mechanism is disposed on the aircraft structure.

In the technical scheme, a safety valve is arranged on the aircraft structure;

the tire sets up in the load storehouse lower extreme.

In the above technical solution, the load bins include a first load bin and a second load bin;

the gas storage tank and the gas compression mechanism are both arranged in the first load bin;

the console, the seat and/or the object space are arranged in the second loading bin.

In the technical scheme, the seat is arranged between the console and the object carrying space;

or only the seat is arranged in the load cabin;

the number of the seats is multiple; the plurality of seats are arranged at intervals;

or only the loading space is arranged in the loading bin.

In the above technical solution, the aircraft structure is in the shape of an airplane; the aircraft structure is a hollow structure; the outer wall of the aircraft structure is made of high-strength film or fabric, and light gas is filled in the aircraft structure;

the supporting framework is made of light high-strength aviation materials.

In the technical scheme, the aircraft structure is respectively connected with the gas storage tank, the gas compression mechanism and the starting mechanism;

the engine mechanism is a fan engine.

The invention provides (maintains) the lift force through the light gas, does not need to consume a large amount of fuel additionally to provide (maintain) the lift force, can take off and land vertically (or in a short distance); the aircraft structure is in an airplane shape, and has excellent flight and control performance due to the excellent aerodynamic layout of the airplane; the inflatable aircraft has the following advantages:

the structure is simple, the cost is low, the use and the maintenance are simple and convenient, a large amount of fuel is saved, the carbon emission is reduced, the use and the maintenance cost are low, and unmanned driving or manned driving can be realized; has wide application prospect.

The invention has strong applicability and can be used for: tourism, agriculture, animal husbandry, fishery, people and goods transportation, patrol and survey, and advertising; the invention can be used for long-time sky detention without consuming a large amount of fuel, and can also be used for military training, patrol early warning and weapon carrying to implement ground and air attacks; the invention has the advantages of less metal materials, exquisite and light structure, cost saving, better stealth performance and the like.

Drawings

Fig. 1 is a schematic perspective view of the present invention.

Fig. 2 is a schematic cross-sectional structure of the present invention.

Fig. 3 is a perspective view of the aircraft structure according to the invention.

Fig. 4 is a schematic sectional view of a loading bin in embodiment 1 of the present invention.

Fig. 5 is a schematic view of a support skeleton structure of the aircraft structure according to the invention.

Fig. 6 is a schematic sectional view of a load cell in embodiment 2 of the present invention.

Fig. 7 is a schematic sectional view of a loading chamber in embodiment 3 of the present invention.

In fig. 1, 2, 3, a denotes a wing of the aircraft structure; b denotes the tail of the aircraft structure.

In the figure, 1-aircraft structure, 2-load cabin, 3-safety valve, 4-tire, 5-control platform, 6-seat, 6.1-seat hollow structure, 7-gas storage tank, 8-gas compression mechanism, 9-starting mechanism, 10-carrying space and 11-supporting framework.

Detailed Description

The embodiments of the present invention will be described in detail with reference to the accompanying drawings, which are not intended to limit the present invention, but are merely exemplary. While the advantages of the invention will be clear and readily understood by the description.

With reference to the accompanying drawings: an inflatable aircraft comprises an aircraft structure 1, a load cabin 2, a console 5, an air storage tank 7, a gas compression mechanism 8 and an engine mechanism 9;

the aircraft structure 1 is an airbag structure; both the wings and the fuselage of the aircraft structure 1 are filled with gas;

a support framework 11 is arranged in the aircraft structure 1;

the load bin 2 is connected below the aircraft structure 1;

the seat 6 and/or the cargo space 10 are/is arranged detachably in the load compartment 2; the loading bin 2 is used for carrying people and/or goods;

the console 5, the gas storage tank 7 and the gas compression mechanism 8 are all arranged in the load chamber 2 (as shown in fig. 1, 2, 3, 4 and 5); the control platform 5 can be a manned control platform or an unmanned control platform, and can realize manned driving or unmanned driving, wherein the control platform 5 is in the prior art;

the launch mechanism 9 is arranged on the aircraft structure 1.

Further, the aircraft structure 1 is equipped with a safety valve 3 (shown in fig. 1, 3); when the pressure of the air bag of the aircraft structure 1 reaches a pressure-bearing limit value, the air bag is automatically exhausted and decompressed, so that the safety is ensured;

the tyre 4 is arranged at the lower end of the load compartment 2 (as shown in fig. 2, 4, 6, 7), and the tyre 4 relieves the damping force of the load compartment 2 when the aircraft structure 1 is taking off or landing.

Further, the load compartment 2 comprises a first load compartment 2.1 and a second load compartment 2.2; the first load bin 2.1 and the second load bin 2.2 are separated by a partition plate, so that the space is reasonably utilized;

the gas storage tank 7 and the gas compression mechanism 8 are both arranged in the first load bin 2.1;

the console 5, the seat 6 and/or the loading space 10 are arranged in the second load compartment 2.2 (see fig. 1, 2, 4).

Further, when the seat 6 and the loading space 10 are both arranged in the second loading compartment 2.2, the seat 6 is arranged between the console 5 and the loading space 10 (as shown in fig. 4); a seat 6 and a carrying space 10 are simultaneously arranged in the second load chamber 2.2, and people and objects are simultaneously conveyed;

or only the seat 6 is disposed within the second load compartment 2.2 (as shown in figure 6); seats 6 are arranged in the whole space of the second load cabin 2.2 and are used for transporting people;

the seat 6 is provided with a plurality of seats; a plurality of seats 6 are arranged at intervals (as shown in fig. 4 and 6);

or only the cargo space 10 is arranged in the second load compartment 2.2 (as shown in fig. 7); the whole space of the second loading bin 2.2 is used as a loading bin for conveying objects.

Further, the aircraft structure 1 is in the shape of an airplane (as shown in fig. 1, 2, 3, 5); the aircraft has excellent aerodynamic layout and good flight and control performance;

the aircraft structure 1 is a hollow structure; the outer wall of the aircraft structure 1 is made of high-strength films or fabrics (such as nylon), and light gas (including hydrogen, helium and the like) is filled inside the aircraft structure; the appearance of the aircraft structure 1 is made of a high-strength film or fabric, a framework made of high-strength light aviation materials is used for supporting and bearing load in the aircraft structure 1, and the structure is stable;

the supporting framework 11 is made of light high-strength aviation materials (such as aviation aluminum materials and aviation carbon fiber materials), so that the structural strength is improved, the overall weight is reduced, and the use cost is reduced.

Furthermore, the aircraft structure 1 is connected with a gas storage tank 7, a gas compression mechanism 8 and a starting mechanism 9 respectively (see fig. 1, 2, 3, 4 and 5); the gas compression mechanism 8 is connected with the gas storage tank 7; the volume of the aircraft structure 1 is changed by inflating (or compressing) gas, so that the lift force is changed, and the lift-off and landing are realized;

the engine mechanism 9 is a fan type engine; a fan type engine is used for generating driving force, unmanned driving can be achieved, and meanwhile the starting mechanism 9 can assist the aircraft structure 1 in achieving lift-off and landing; the engine mechanism can be a battery-driven engine or a fuel engine.

Example 1

The present embodiment is used for transporting people and things simultaneously.

The inflatable aircraft comprises an aircraft structure 1, a load cabin 2, a console 5, an air storage tank 7, a gas compression mechanism 8 and an engine mechanism 9; the aircraft structure 1 is an airbag structure, the aircraft structure 1 is in an airplane shape, and the safety valve 3 is arranged on the aircraft structure 1; the outer wall of the aircraft structure 1 is made of high-strength nylon fabric, and light gas is filled inside the aircraft structure; both the wings and the fuselage of the aircraft structure 1 are filled with gas; a support framework 11 is arranged in the aircraft structure 1, and the support framework 11 is made of aviation aluminum; the load bin 2 is connected below the aircraft structure 1; the seats 6 and the loading space 10 are arranged in the loading bin 2, and the number of the seats 6 is multiple; a plurality of seats 6 are arranged at intervals; the load bin 2 is used for carrying people and objects; the console 5, the gas storage tank 7 and the gas compression mechanism 8 are all arranged in the load bin 2; wherein, the console 5 is an unmanned console, and is the prior art; the starting mechanism 9 is arranged on the aircraft structure 1, the starting mechanism 9 is a fan-type engine, and the starting mechanism adopts a battery to drive the engine; the aircraft structure 1 is respectively connected with an air storage tank 7, a gas compression mechanism 8 and an engine mechanism 9; the tire 4 is arranged at the lower end of the load cabin 2.

The method for transporting a pneumatic aircraft according to the present embodiment comprises the steps of,

the personnel and the goods are both positioned in the load bin 2;

light gas (helium gas) is filled into the aircraft structure 1 through a gas compression mechanism 8 and a gas storage tank 7, and the volume of the aircraft structure 1 is gradually increased until the aircraft structure 1 is filled with the light gas; the starting mechanism 9 is started to generate a driving force to assist in driving the aircraft structure 1 to lift off; controlling the flight direction of the aircraft structure 1 by means of the console 5; repeating the above steps until the aircraft structure 1 reaches the destination;

under the effect of the gas compression mechanism 8, gas in the aircraft structure 1 is pumped into the gas storage tank 7 through the gas compression mechanism 8, the volume of the aircraft structure 1 gradually becomes smaller, the starting mechanism 9 generates a pushing force to assist in pushing the aircraft structure 1 to land, and the tires 4 buffer and absorb shock when the aircraft structure 1 lands, so that the safety of personnel and goods in the load bin 2 is ensured (as shown in fig. 1, fig. 2, fig. 3, fig. 4 and fig. 5).

Example 2

The inflatable aircraft and the transportation method thereof in the embodiment are the same as those in embodiment 1, except that: the embodiment is only used for transporting people, and only seats are arranged in the load cabin 2; and the engine mechanism is a fuel or electric drive engine (as shown in fig. 6).

Example 3

The inflatable aircraft and the transportation method thereof in the embodiment are the same as those in embodiment 1, except that: the present embodiment is only used for transporting goods, and only the loading space 10 (as shown in fig. 7) is provided in the loading compartment 2.

Other parts not described belong to the prior art.