CN203842313U

CN203842313U - Novel remote control model with combination of vertical take-off and landing and level fight characteristic of fixed wing

Info

Publication number: CN203842313U
Application number: CN201420195685.5U
Authority: CN
Inventors: 李忠泽; 何旭东
Original assignee: JIANGYIN XIANGNUO ELECTRONICS TECHNOLOGY Co Ltd
Current assignee: JIANGYIN XIANGNUO ELECTRONICS TECHNOLOGY Co Ltd
Priority date: 2014-04-22
Filing date: 2014-04-22
Publication date: 2014-09-24
Anticipated expiration: 2024-04-22

Abstract

The utility model discloses a novel remote control model with a combination of vertical take-off and landing and a level fight characteristic of a fixed wing. The novel remote control model comprises a body, an empennage and a take-off and landing device. The empennage is arranged at the tail of the body, the take-off and landing device is arranged at the bottom of the body, front wings and rear wings are arranged on the body, wing tips of the front wings and the rear wings are provided with motors, propellers are arranged on the motors, and auxiliary wings are arranged on the rear wings and are connected with the body by control rods. The novel remote control model has the advantages that a structure with double fixed wings and four rotor wings is designed according to an aerodynamics principle, the four rotor wings are arranged on the tops of the double fixed wings, engines can be tilted as needed, and accordingly the novel remote control model which is an aircraft model is flexible and is high in carrying capacity and economic efficiency and low in site requirements.

Description

In conjunction with VTOL and the flat Novel remote-control model that flies characteristic of fixed-wing

Technical field

The utility model relates to model airplane field, especially relates to the flat Novel remote-control model that flies characteristic of a kind of combination VTOL and fixed-wing.

Background technology

Traditional model aircraft is generally divided into gyroplane and fixed wing aircraft, gyroplane flying speed is slow, loading capacity is low, fixed wing aircraft take-off venue requires high, when taking photo by plane and investigate, because speed is inadequate, so mobility is poor, loading capacity is low, so the detection equipment that aircraft can carry is limited, occasion limitation that can be applicable is larger.

Utility model content

The utility model is for the current model aircraft mobility of solution is poor and the low problem of loading capacity, provide a kind of combination VTOL and fixed-wing the flat Novel remote-control model that flies characteristic for this reason, comprise fuselage, empennage and play falling unit, described empennage is arranged on the afterbody of fuselage, described falling unit is arranged on the bottom of fuselage, on described fuselage, be provided with front wing and rear wing, the wingtip of described front wing and rear wing is provided with motor, on described motor, be provided with screw, on described rear wing, be provided with aileron, described aileron is connected with fuselage by control lever.

As preferably, described empennage is fixed-wing.

The beneficial effects of the utility model are: the utility model is according to aerodynamic principle, designed the structure that two fixed-wings top arranges four rotors, the direction of as required engine being verted, thereby model aircraft has been realized to maneuverability, loading capacity is high, economy is high, the advantage little to site requirements.

Accompanying drawing explanation

The utility model will illustrate by example and with reference to the mode of accompanying drawing, wherein:

Fig. 1 is schematic perspective view of the present utility model;

Fig. 2 is elevational schematic view of the present utility model;

In figure: 1, fuselage; 2, empennage; 3, front wing; 4, rear wing; 5, motor; 6, screw; 7, aileron; 8, play falling unit; 9, control lever.

The specific embodiment

Disclosed all features in this description, or the step in disclosed all methods or process, except mutually exclusive feature and/or step, all can combine by any way.

Disclosed arbitrary feature in this description (comprising any accessory claim, summary and accompanying drawing), unless narration especially all can be replaced by other equivalences or the alternative features with similar object.That is,, unless narration especially, each feature is an example in a series of equivalences or similar characteristics.

The flat Novel remote-control model that flies characteristic of a kind of combination VTOL as shown in Figure 1 and fixed-wing, comprise fuselage 1, empennage 2 and play falling unit 8, described empennage 2 is arranged on the afterbody of fuselage 1, described falling unit 8 is arranged on the bottom of fuselage 1, is provided with front wing 3 and rear wing 4 on described fuselage 1, and the wingtip of described front wing 3 and rear wing 4 is provided with motor 5, on described motor 5, be provided with screw 6, as shown in Figure 2, on described rear wing 4, be provided with aileron 7, described aileron 7 is connected with fuselage 1 by control lever 9.Described empennage 2 is fixed-wing.

In running, motor 5 turns to perpendicular to the ground, and screw 6 rotates, and aircraft takes off vertically, realize the flight characteristic of gyroplane, then motor 5 verts, and slowly accelerates, until motor 5 and ground level, flying speed is maximum, front wing 3 and rear wing 4 coordinate motor 5 to realize the flight characteristic of fixed wing aircraft, control the upset of aileron 7 by control lever 9, control the flight attitude of aircraft.

The utility model is according to aerodynamic principle, fully analyzed four axle vertical rising aircrafts can VTOL as helicopter, maneuverability, and the advantage little to site requirements, and that fixed-wing has pneumatic efficiency is high, loading capacity is large, the feature of good economy performance, designed a novel pneumatic contour structures that has both advantages concurrently, by controlling verting of four dynamical systems, realize thrust deflexion, in VTOL or hovering or takeoff condition, by electronic gyroscope, assist the thrust variation of four points of rotational speed regulation of controlling four motors stable, when dynamical system changes into ground level state, become conventional fixed-wing pattern, it is stable that same electronic gyroscope auxiliary control aileron and lifting realize money state.

The utility model is not limited to the aforesaid specific embodiment.The utility model expands to any new feature or any new combination disclosing in this manual, and the arbitrary new method disclosing or step or any new combination of process.

Claims

1. in conjunction with VTOL and fixed-wing, put down the Novel remote-control model that flies characteristic for one kind, comprise fuselage (1), empennage (2) and a falling unit (8), described empennage (2) is arranged on the afterbody of fuselage (1), described falling unit (8) is arranged on the bottom of fuselage (1), it is characterized in that, on described fuselage (1), be provided with front wing (3) and rear wing (4), the wingtip of described front wing (3) and rear wing (4) is provided with motor (5), on described motor (5), be provided with screw (6), on described rear wing (4), be provided with aileron (7), described aileron (7) is connected with fuselage (1) by control lever (9).

2. the flat Novel remote-control model that flies characteristic of a kind of combination VTOL according to claim 1 and fixed-wing, is characterized in that, described empennage (2) is fixed-wing.