CN201357727Y

CN201357727Y - Air-sea-land aircraft

Info

Publication number: CN201357727Y
Application number: CNU2009200795959U
Authority: CN
Inventors: 文强; 王万琼
Original assignee: Individual
Current assignee: Individual
Priority date: 2009-03-17
Filing date: 2009-03-17
Publication date: 2009-12-09
Anticipated expiration: 2019-03-17

Abstract

The utility model relates to an air-sea-land aircraft, belonging to an air-sea-land motor aircraft. The aircraft comprises a piston engine which is arranged in an airframe; the airframe is formed by connecting a pyramid head, an airframe body and a pyramid tail in sequence, wherein the cross section of the airframe body is isosceles trapezoid; a cabin door is arranged on the airframe body; the left and the right sides of the airframe body are respectively and symmetrically provided with a fixed horizontal aileron; the outer edge of the aileron is articulated with a broken wing which can deflect a certain degree; wings are respectively and symmetrically arranged above the ailerons at the left and the right sides of the airframe body, and the wings are articulated with the airframe body; a rear wing and a stand wing are arranged and fixed at the rear part of the tail, and a tail vane is articulated on the rear edge of the stand wing; the bottom part of the airframe body is provided with a wheel; and the bottom parts of the two fixed ailerons are respectively provided with a wheel. The aircraft has the properties of running on land, sailing on water surface and flying in the air.

Description

A kind of aeroamphibious aircraft

Technical field

The utility model relates to power actuated vehicle, the motor-driven aircraft of particularly flight aloft, land locomotion, surface navigation.

Background technology

Automobile has the branch of car, passenger vehicle, lorry, tractor truck, cross-country car, special purpose vehicle (as van cooler, appearance tank car, fire extinguishing tanker, medical truck etc.), industrial and mineral dumping car.Its basic structure all is to be power system with driving engine (spark ignition engine or diesel engine), is aided with compositions such as driving system, driving system, steering swivel system, brake system again.Automobile can only travel on land.Similarly, boats and ships can only only be used for airflight at surface navigation, aircraft.Existing automobile, boats and ships, aircraft all have its exclusive use, and land, water and air to be used or the general-duty function and do not have.

The utility model content

The purpose of this utility model provides a kind of aeroamphibious aircraft, make its have can land locomotion, again can be at surface navigation, the Combination property that can also aloft fly.

This later-model purpose is achieved in that a kind of aeroamphibious aircraft, comprise the piston engine that is arranged in the body, body is connected and composed in turn by the head of rectangular pyramid shape, fuselage that cross sectional shape is isosceles trapezoid and the tail of rectangular pyramid shape, and fuselage is provided with cabin door; The fuselage left and right sides is provided with the horizontal aileron of fixed type respectively symmetrically, but the aileron outer rim is hinged with the flap of deflection angle, and the fuselage and arranged on left and right sides is positioned at the aileron top and is provided with wing respectively symmetrically, and wing and fuselage are hinged; The tail rear portion is mounted with the empennage and the upright wing, is hinged with tail vane on the upright wing trailing edge; Fuselage bottom is provided with a wheel, and two fixed type ailerons bottom is respectively equipped with a wheel.

Compared with prior art, this later-model beneficial effect is:

1, this aircraft has the function of land locomotion, surface navigation and airflight concurrently.

When land locomotion, by hydraulic control system left and right wing is upwards packed up, wing is upright state, press close to fuselage,, produce propulsive effort by the engine power system in the body, drive wheels advance (, being wheel flutter) with last wheel as being drive wheel with latter two wheel.When surface navigation, same, left and right wing is upwards packed up, at this moment, the fixed type aileron of and arranged on left and right sides produces buoyancy with body (organism bottom is a ship shape), and whole machine body is floated on the surface, and start the engine can freely be go the rounds on the water surface; When carrying out airflight, left and right wing places level attitude, and start the engine after quicken on ground, can rise to the sky, and flies to blue sky.At this moment, can adjust the size of buoyancy, simultaneously, change the direction of cruising by the control tail vane by the inclination angle of control flap.

2, basis is novel both can be made as practical facility, also went for toy and made.

Description of drawings

Fig. 1 is this later-model block diagram (wing is the level of state);

Fig. 2 is the block diagram of shown in Figure 1 novel another view directions;

Fig. 3 is the block diagram that vertical state was packed up afterwards, was to shown in Figure 1 novel wing.

The specific embodiment

Fig. 1 Fig. 2 illustrates, this novel piston engine or other driving engine of aircraft that is arranged in the body that comprise, body is connected and composed in turn by the head 1 of rectangular pyramid shape, fuselage 2 that cross sectional shape is isosceles trapezoid and the tail 3 of rectangular pyramid shape, and fuselage is provided with cabin door 10; The fuselage left and right sides is provided with the horizontal aileron 6 of fixed type respectively symmetrically, but the aileron outer rim is hinged with the flap 6a of deflection angle, and the fuselage and arranged on left and right sides is positioned at aileron 6 tops and is provided with wing 4,5 respectively symmetrically, and wing and fuselage are hinged; Two wings can also turn down be the level of state (rather than the vertical state among Fig. 3) backward, use with as land and surface navigation the time.Be provided with the upright wing (being stabilizer, as the water sailing time, not shown) and rudder (identical with rudder with the upright wing of Fig. 1 postmedian) in the middle of the organism bottom, rudder is hinged on the upright wing.Tail 3 rear portions are mounted with the empennage 7 and the upright wing 8, are hinged with tail vane 9 on the upright wing 8 trailing edges; Fuselage bottom is provided with a wheel 11, two fixed type ailerons 6 bottoms and is respectively equipped with a wheel 12.When using as aircraft, left and right wing is horizontality shown in Figure 1, and when using as land locomotion or surface navigation, left and right wing can be packed up and be vertical state, as shown in Figure 3 or pack up the (not shown) that is the level of state.Cabin door 10 is arranged on vehicle body 2 tops.Cabin door 10 can be plug-type cabin door.Fuselage 2 and arranged on left and right sides are hinged with a pull bar respectively, and the pull bar other end is a crotch-shaped; Be respectively arranged with on the described wing 4,5 for the pull bar crotch and articulate, have " the fastener of [" shape notch.Organism bottom is designed to ship shape.Configuration design aerodynamic principle, air resistance is less when running at high speed.

Claims

1, a kind of aeroamphibious aircraft, comprise, be arranged on the piston engine in the body, it is characterized in that: described body is connected and composed in turn by the head (1) of rectangular pyramid shape, fuselage (2) that cross sectional shape is isosceles trapezoid and the tail (3) of rectangular pyramid shape, and fuselage is provided with cabin door (10); The fuselage left and right sides is provided with the horizontal aileron of fixed type (6) respectively symmetrically, but the aileron outer rim is hinged with the flap (6a) of deflection angle, and the fuselage and arranged on left and right sides is positioned at aileron (6) top and is provided with wing (4,5) respectively symmetrically, and wing and fuselage are hinged; Tail (3) rear portion is mounted with the empennage (7) and the upright wing (8), is hinged with tail vane (9) on the upright wing (8) trailing edge; Fuselage bottom is provided with a wheel (11), and two fixed type ailerons (6) bottom is respectively equipped with a wheel (12).

2, according to the described a kind of aeroamphibious aircraft of claim 1, it is characterized in that: described cabin door (10) is arranged on vehicle body (2) top; Described fuselage (2) bottom midway location is provided with the upright wing and rudder, and rudder is hinged on the upright wing.

3, according to the described a kind of aeroamphibious aircraft of claim 2, it is characterized in that: described cabin door (10) is plug-type cabin door.

4, according to claim 1 or 2 or 3 described a kind of aeroamphibious aircraft, it is characterized in that: described fuselage (2) and arranged on left and right sides is hinged with a pull bar respectively, and the pull bar other end is a crotch-shaped; Be respectively arranged with on the described wing (4,5) for the pull bar crotch and articulate, have " the fastener of [" shape notch.