CN203294305U

CN203294305U - High-speed floating aircraft

Info

Publication number: CN203294305U
Application number: CN201320194475XU
Authority: CN
Inventors: 杨礼诚
Original assignee: Individual
Current assignee: Individual
Priority date: 2013-04-18
Filing date: 2013-04-18
Publication date: 2013-11-20
Anticipated expiration: 2023-04-18

Abstract

The utility model relates to a high-speed floating aircraft with floating air bags. The technical scheme is that the floating aircraft comprises an aircraft body, the floating air bags, electric-driven lift force airscrews, balancing wings, a seat cabin, a cockpit, an equipment cabin, an undercarriage and tires. The floating air bags are installed between an outer shell of the aircraft body and a hollow inner shell. The seat cabin is installed between the hollow inner shell and the outer shell of the aircraft body and the cockpit is arranged at the front end of the seat cabin. A motor is installed in the hollow inner shell and a thrusting airscrew is installed on the motor. The motor is fixedly installed on the hollow inner shell through a motor supporting frame. The electric-driven lift force airscrews are arranged on the balancing wings. All sorts of control buttons and a steering wheel are installed on an operation platform in the cockpit. According to the high-speed floating aircraft, electric energy which is a natural and clean energy source is used as power, the requirements of saving energy, protecting the environment and low-carbon economy are met, and the high-speed floating aircraft with the floating air bags can maintain the advantages of being large in loading capacity and high in fight safety of a regular airship. The high-speed floating aircraft with the floating air bags is high in flight speed, wherein the flight speed can be improved to 400KM per hour from 200KM per hour of an ordinary low-level aircraft.

Description

A kind of high speed flight device

Technical field

The utility model relates to the field of wafing that flies, and particularly relates to the high speed flight device with the buoyance lift air bag, and this flight device, except can aloft flying, also can sail on the water.

Background technology

Existing aircraft, roughly there are three kinds: aircraft, dirigible and fire balloon, most of aviation aircrafts all adopt fuel oil equal energy source power to start aircraft, and the aviation aircraft that adopts the energy to do power does not meet the requirement of low-carbon economy and environmental protection, and flight cost is also very high; Aircraft flight speed is very fast, but safety problem is not solved so far; Fire balloon is because self flight theory determines that it can not be as load transportation instrument professional purpose; Flying speed can not get significantly improving always although dirigible has utility function.Up to now, also do not find existing flight device with air bag and high-speed flight.

The utility model content

The purpose of this utility model is the weak point for existing aircraft, fire balloon and dirigible, propose a kind of by using a plurality of inflation buoyance lift air bags and electronic thrust screw propeller, according to aerodynamic principle, change the arrangement mode of buoyance lift air bag, reach the brand new technical scheme of the flight device of high-speed flight.

The technical solution of the utility model is: this flight device comprises aircraft fuselage, buoyance lift air bag, electronic lifting propeller, balance wing, passenger cabin, driving compartment, equipment compartment, alighting gear and tire.A plurality of buoyance lift air bags are arranged between the shell and hollow inner casing of aircraft fuselage, and passenger cabin is between the shell of hollow inner casing and aircraft fuselage, and driving compartment is positioned at the front end of passenger cabin.In hollow inner casing, electrical motor is installed, the thrust screw propeller is installed on electrical motor, electrical motor is fixedly mounted on hollow inner casing by motor bracket, and electronic lifting propeller is installed on balance wing, on the operation bench in driving compartment, various control buttons and bearing circle is installed.A plurality of buoyance lift air bags in aircraft fuselage are 6-8, around hollow inner casing, have arranged the large half-turn of whole fuselage, in the buoyance lift air bag, have been full of unreactable gas.The equipment compartment that is positioned at the passenger cabin below is equipped with gasoline engine generator and current distributor.After between the hollow inner casing of aircraft fuselage, fragment position is equipped with the yaw rudder of controlling heading.The utility model is the same with aircraft can normally stop on the ground, need not need a large amount of ground staff to carry out mooring as dirigible and fixes and safeguard.

While using the utility model, by the control button of installing on the driving compartment operating console, start gasoline engine generator, gasoline engine generator delivers power to the electronic lifting propeller that is positioned on balance wing and is positioned at hollow inner casing thrust screw propeller by current distributor, effect by electronic lifting propeller and buoyance lift air bag, make the utility model at the original place VTOL function, do not need the such plane track of conventional airplane.After lift-off, under the effect of thrust screw propeller fast rotational, fly, promote the utility model and fly fast.The utility model, by the pilot control bearing circle, is realized by yaw rudder while changing direction.When the utility model descended, the control by electronic button and Multichannel remote controller on operating console, stopped the rotation of thrust propeller blade, gradually reduces the rotating speed of lifting propeller, and slow decreasing, until land.With several buoyance lift air bags, the utility model also can sail on the water and be unlikely to sink due to the utility model.

The utlity model has following remarkable result:

1, because the utility model mainly leans on nature clean energy resource-electric energy as power, meet the requirement of energy-saving and environmental protection and low-carbon economy;

2, the utility model has kept the characteristics that conventional dirigible load carrying ability is large, flight safety is high;

3, the utility model flying speed is fast.Flying speed can be brought up to from 200KM/ hour of common aircraft 400KM/ hour;

4, the utility model not only can aloft fly, and also can on the water surface, advance, and has air-sea two function of dwelling;

5, the utility model, because electronic lifting propeller symmetry is arranged on the balance wing of fuselage both sides, can keep having a smooth flight in-flight;

6, the utility model does not use the engine petrol of aircraft, and the most of space of fuselage is the buoyance lift air bag in addition, has greatly reduced deadweight of the present utility model and oil consumption, has improved flight efficiency;

7, in the utility model fuselage, be hollow duct shape structure, advance the thrust screw propeller that moves ahead that flies to waft to be arranged on wherein, effectively brought into play the progradation of screw propeller High Rotation Speed;

8, due to integral body of the present utility model and air bag by the parcel of interior hard coat, greatly improved wind loading rating of the present utility model.

Brief Description Of Drawings

Fig. 1 is structural representation of the present utility model.

Fig. 2 is fuselage longitudinal construction schematic diagram of the present utility model.

As shown in the figure: the hollow inner casing 15-of the electronic lifting propeller 4-of 1-aircraft fuselage 2-buoyance lift air bag 3-balance wing 5-motor support frame 6-electrical motor 7-thrust screw propeller 8-passenger cabin 9-equipment compartment 10-engine petrol 11-flight tire 12-alighting gear 13-current distributor 14-driving compartment 16-taper buoyance lift air bag head 17-yaw rudder 18-flight tire 19-alighting gear

The specific embodiment

The specific embodiment of the present utility model is illustrated by reference to the accompanying drawings: as shown in the figure, this flight device comprises aircraft fuselage (1), buoyance lift air bag (2), electronic lifting propeller (3), balance wing (4), passenger cabin (8), driving compartment (15), equipment compartment (9), alighting gear and tire.a plurality of buoyance lift air bags (2) are arranged between the shell and hollow inner casing (14) of aircraft fuselage (1), passenger cabin (8) is positioned between the shell of hollow inner casing (14) and aircraft fuselage (1), driving compartment (15) is positioned at the front end of passenger cabin, electrical motor (6) is installed in hollow inner casing (14), thrust screw propeller (7) is installed on electrical motor (6), electrical motor (6) is fixedly mounted on hollow inner casing (14) by motor bracket (5), electronic lifting propeller (3) is installed on fuselage both sides balance wing (4), on operation bench in driving compartment (15), various control buttons and bearing circle are installed.

A plurality of buoyance lift air bags (2) that are arranged in aircraft fuselage (1) are 6-8, around hollow inner casing (14), have arranged the large half-turn of whole fuselage, and the buoyance lift air bag has been full of unreactable gas in (2).In the equipment compartment (9) of passenger cabin (8) below, gasoline engine generator (10) and current distributor (13) are installed.After between the hollow inner casing (14) of aircraft fuselage (1), fragment position is equipped with the yaw rudder (17) of controlling heading.

Claims

1. high speed flight device, this flight device comprises aircraft fuselage (1), buoyance lift air bag (2), electronic lifting propeller (3), balance wing (4), passenger cabin (8), driving compartment (15), equipment compartment (9), alighting gear and tire, it is characterized in that: a plurality of buoyance lift air bags (2) are arranged between the shell and hollow inner casing (14) of aircraft fuselage (1), passenger cabin (8) is positioned between the shell of hollow inner casing (14) and aircraft fuselage (1), driving compartment (15) is positioned at the front end of passenger cabin, electrical motor (6) is installed in hollow inner casing (14), electrical motor is equipped with the thrust screw propeller on (6), electrical motor (6) is fixedly mounted on hollow inner casing (14) by motor bracket, electronic lifting propeller (3) is installed on balance wing (4), on operation bench in driving compartment (15), various control buttons and bearing circle are installed.

2. a kind of high speed flight device according to claim 1, a plurality of buoyance lift air bags (2) that it is characterized in that being arranged in aircraft fuselage (1) are 6-8, around hollow inner casing (14), arranged the large half-turn of whole fuselage, the buoyance lift air bag has been full of unreactable gas in (2).

3. a kind of high speed flight device according to claim 1, is characterized in that the equipment compartment (9) that is positioned at passenger cabin (8) below is equipped with gasoline engine generator (10) and current distributor (13).

4. a kind of high speed flight device according to claim 1, is characterized in that rear fragment position is equipped with the yaw rudder (17) of controlling heading between the hollow inner casing (14) of aircraft fuselage (1).