CN202379089U

CN202379089U - Novel unmanned aerial vehicle

Info

Publication number: CN202379089U
Application number: CN2011204782334U
Authority: CN
Inventors: 金嘉豪
Original assignee: Individual
Current assignee: Individual
Priority date: 2011-11-28
Filing date: 2011-11-28
Publication date: 2012-08-15
Anticipated expiration: 2021-11-28

Abstract

The utility model relates to a novel unmanned aerial vehicle. The novel unmanned aerial vehicle is characterized in that main airfoils are arranged on the two sides at the back end of an aircraft main body, the included angle between the back end of each main airfoil and a balancing tail wing is 10 degrees, auxiliary wings are arranged on the main airfoils, L-shaped vertical tail wings are arranged on the two sides of the aircraft main body on the main airfoils, one end of each L-shaped vertical tail wing is connected with the back end of the main airfoil, the other end of each L-shaped vertical tail wing is connected with the balancing tail wing, oblique tail wings are respectively arranged on the two sides of each balancing tail wing, the included angle between each oblique tail wing and the balancing tail wing is 125 degrees, canards are arranged on the two sides of the front part of the aircraft main body, camera heads are arranged on the front part of the aircraft main body, an airflow needle is arranged at the front end of the aircraft main body, an engine propeller is arranged at the tail end of the aircraft main body, and an antenna is further arranged on the aircraft main body. The novel unmanned aerial vehicle disclosed by the utility model has the advantages of small resistance and good aerodynamic performance, and can increase the flight of an aircraft and the high-altitude mobility, reduce the wings of the aircraft, further reduce the frontal resistance, also reduce the balancing resistance of the aircraft, shorten the takeoff flying distance and be more suitable for civil use.

Description

Novel unmanned plane

Technical field

The utility model relates to aviation flight equipment, a kind of specifically novel unmanned plane.

Background technology

Shortcomings such as unmanned plane great majority traditional in the prior art are the flat wing or swept wing, and its volume is big, and take-off distance is far away, and lift is little, and resistance is big when flight, and manoevreability is little.

Summary of the invention

The utility model technical matters to be solved is the deficiency that overcomes prior art, and a kind of novel unmanned plane is provided, and the utility model solves the technical scheme that its technical matters adopted and is: the structure of the utility model comprises balance empennage, aileron, host wing, preceding canard, air-flow pin, camera, driving engine screw propeller, aircraft main body, L shaped perpendicular empennage, oblique empennage, front-wheel, trailing wheel, antenna, balance tail aileron, perpendicular tail aileron; The both sides, rear end that it is characterized in that the aircraft main body are provided with host wing, and the angle between host wing rear end and the balance empennage is 10 degree, and host wing is provided with aileron; The board a plane both sides of main body of host wing are provided with L shaped perpendicular empennage; L shaped perpendicular empennage rear end is provided with perpendicular tail aileron, and L shaped perpendicular empennage one end is connected with the rear end of host wing, and the other end of L shaped perpendicular empennage is connected with the balance empennage; The balance empennage is provided with balance tail aileron; The both sides of balance empennage are provided with oblique empennage, and tiltedly the angle between empennage and the balance empennage is 125 degree, and aircraft body front part both sides are provided with preceding canard; Be provided with camera above the aircraft body front part; The front end of aircraft main body is provided with the air-flow pin, and the tail end of aircraft main body is provided with the driving engine screw propeller, and the following rear portion of aircraft main body is provided with two trailing wheels; The following front portion of aircraft main body is provided with a front-wheel, on the aircraft main body, also is provided with antenna.

Description of operation: it is elevating rudder that the utility model adopts canard, and host wing is a buzzard-type wing, and the buzzard-type wing angle is 10 degree; Be that angle between host wing rear end and the balance empennage is 10 degree, the structure of buzzard-type wing ensures between wing and the fuselage and can better be connected, thereby increases the intensity of aircraft; The host wing of the formula of falling the wing can reduce the in-flight resistance of aircraft, has improved the manoevreability of aircraft, and canard can improve the steering effort of aircraft when dogled; Empennage is designed to the balance empennage of connecting type, and this empennage can improve the stability of aircraft, and piston engine provides corresponding power; The side installs the high-pixel camera machine additional aboard, can let driver's video fly.

The beneficial effect of the utility model is, the utility model resistance is little, and aeroperformance is good; Can increase the manoevreability in flight and high-altitude; Thereby aircraft wing dwindles the head resistance that has reduced aircraft, has also reduced the trim resistance of aircraft, and the airborne reduced distances more is adapted to civilian.

Description of drawings

Fig. 1: the utility model embodiment plan structure scheme drawing;

Fig. 2: the utility model embodiment side-looking structural representation;

Fig. 3: the utility model embodiment balance empennage and oblique empennage connection structure scheme drawing;

Among the figure: balance empennage 1, aileron 2, host wing 3, preceding canard 4, air-flow pin 5, camera 6, driving engine screw propeller 7, aircraft main body 8, L shaped perpendicular empennage 9, tiltedly empennage 10, front-wheel 11, trailing wheel 12, antenna 13, balance tail aileron 14, perpendicular tail aileron 15.

The specific embodiment

Concrete detailed description below with reference to description of drawings the utility model being done.Shown in accompanying drawing, the structure of the utility model comprises balance empennage 1, aileron 2, host wing 3, preceding canard 4, air-flow pin 5, camera 6, driving engine screw propeller 7, aircraft main body 8, L shaped perpendicular empennage 9, tiltedly empennage 10, front-wheel 11, trailing wheel 12, antenna 13, balance tail aileron 14, perpendicular tail aileron 15, it is characterized in that the both sides, rear end of aircraft main body 8 are provided with host wing 3; Angle between host wing 3 rear ends and the balance empennage 1 is 10 degree; Host wing 3 is provided with aileron 2, and the board a plane both sides of main body 8 of host wing 3 are provided with L shaped perpendicular empennage 9, and L shaped perpendicular empennage 9 rear ends are provided with perpendicular tail aileron 15; L shaped perpendicular empennage 9 one ends are connected with the rear end of host wing 3; The other end of L shaped perpendicular empennage 9 is connected with balance empennage 1, and balance empennage 1 is provided with balance tail aileron 14, and the both sides of balance empennage 1 are provided with oblique empennage 10; Tiltedly the angle between empennage 10 and the balance empennage 1 is 125 degree; Aircraft main body 8 front part sides are provided with preceding canard 4, and the aircraft main body is provided with camera 6 above 8 front portions, and the front end of aircraft main body 8 is provided with air-flow pin 5; The tail end of aircraft main body 8 is provided with driving engine screw propeller 7; The following rear portion of aircraft main body 8 is provided with two trailing wheels 12, and the following front portion of aircraft main body 8 is provided with a front-wheel 11, on aircraft main body 8, also is provided with antenna 13.

Embodiment recited above describes the preferred implementation of the utility model; Be not that design and scope to the utility model limits; Under the prerequisite that does not break away from the utility model design concept, common engineering staff make the technical scheme of the utility model in this area various modification and improvement all should fall into the protection domain of the utility model; The technology contents that the utility model is asked for protection all is documented in claims.

Claims

1. novel unmanned plane; Comprise balance empennage (1), aileron (2), host wing (3), preceding canard (4), air-flow pin (5), camera (6), driving engine screw propeller (7), aircraft main body (8), L shaped perpendicular empennage (9), oblique empennage (10), front-wheel (11), trailing wheel (12), antenna (13), balance tail aileron (14), perpendicular tail aileron (15); The both sides, rear end that it is characterized in that aircraft main body (8) are provided with host wing (3), and the angle between host wing (3) rear end and the balance empennage (1) is 10 degree, and host wing (3) is provided with aileron (2); The board a plane both sides of main body (8) of host wing (3) are provided with L shaped perpendicular empennage (9); L shaped perpendicular empennage (9) rear end is provided with perpendicular tail aileron (15), and L shaped perpendicular empennage (9) one ends are connected with the rear end of host wing (3), and the other end of L shaped perpendicular empennage (9) is connected with balance empennage (1); Balance empennage (1) is provided with balance tail aileron (14); The both sides of balance empennage (1) are provided with oblique empennage (10), and tiltedly the angle between empennage (10) and the balance empennage (1) is 125 degree, and aircraft main body (8) front part sides is provided with preceding canard (4); Aircraft main body (8) is provided with camera (6) above the front portion; The front end of aircraft main body (8) is provided with air-flow pin (5), and the tail end of aircraft main body (8) is provided with driving engine screw propeller (7), and the following rear portion of aircraft main body (8) is provided with two trailing wheels (12); The following front portion of aircraft main body (8) is provided with a front-wheel (11), on aircraft main body (8), also is provided with antenna (13).