ES2284300B1

ES2284300B1 - VERTICAL AIRCRAFT AIRCRAFT.

Info

Publication number: ES2284300B1
Application number: ES200402553A
Authority: ES
Inventors: Francisco Angel Garcia Perez; Manuel Muñoz Saiz
Original assignee: Individual
Current assignee: Individual
Priority date: 2004-10-07
Filing date: 2004-10-07
Publication date: 2008-10-16
Anticipated expiration: 2024-10-07
Also published as: ES2284300A1

Abstract

La aeronave de despegue vertical se caracteriza por presentar un fuselaje monocasco cuya mitad inferior adopta forma similar a la de un barco convencional sin quilla, minialas delanteras (5), alas principales (7) y barquillas (8, 8¿), disponiendo de múltiples turbinas o miniturbinas en su contorno o zona periférica lateral, añadiendo sobre las alas y el fuselaje dos o más grandes fanes impulsados por motores eléctricos y por un caudal de aire a presión proveniente de las turbinas de gas principales.The vertical take-off aircraft is characterized by presenting a monocoque fuselage whose lower half adopts a shape similar to that of a conventional ship without keel, front minialas (5), main wings (7) and wafers (8, 8¿), having multiple turbines or mini-turbines in its contour or lateral peripheral area, adding on the wings and the fuselage two or more large fans driven by electric motors and by a flow of pressurized air from the main gas turbines.

Description

Aeronave de despegue vertical.Vertical take-off aircraft.

Field of the Invention

En naves y aeronaves.In ships and aircraft.

State of the art

Los barcos actuales por su configuración peso etc. no pueden pasar a la situación de vuelo, en el caso de los hidroaviones tan solo se trata de aviones con barquilla o barquillas las cuales solo se utilizan para poder posarse en el agua. La presente invención permite que su comportamiento sea mixto en el sentido de que pueda navegar como barco siendo su transformación casi total.Current ships for their weight configuration etc. they cannot go to the flight situation, in the case of seaplanes are only airplanes with a wafer or wafers which are only used to settle on the Water. The present invention allows its behavior to be mixed in the sense that you can sail as a ship being your almost total transformation.

Description of the invention

La aeronave de despegue vertical de la invención, del tipo de turbinas de gas y fanes, caracterizada por presentar un fuselaje monocasco cuya mitad inferior adopta forma similar a la de un barco convencional sin quilla, disponiendo de múltiples turbinas o miniturbinas en su contorno o zona periférica lateral del fuselaje, añadiendo dos o más grandes fanes impulsados por un caudal de aire a presión proveniente de las turbinas de gas principales, aunque también pueden ser movidos por motores eléctricos.The vertical take-off aircraft of the invention, of the type of gas turbines and fans, characterized by present a monocoque fuselage whose lower half takes shape similar to that of a conventional boat without keel, having multiple turbines or mini turbines in its contour or peripheral area side of the fuselage, adding two or more large driven fans by a flow of pressurized air from the gas turbines main, although they can also be moved by motors electric

Los grandes fanes se colocan en la zona central de las alas y en la zona central delantera del fuselaje.The big fans are placed in the central zone of the wings and in the front central area of the fuselage.

Puede presentar una disposición canard y tener las alas plegables o basculantes con el fin de que su comportamiento como barco sea mas ostensible.You can present a canard provision and have the folding or tilting wings in order that your Behavior as a ship is more obvious.

Dispone de un sistema de estabilización para vuelo consistente en unos giróscopos que detectan el cambio de actitud respecto a la horizontal, generándose una señal que actúa sobre los motores o turbinas de modo que corrige los desvíos o inclinaciones indeseadas.It has a stabilization system for flight consisting of gyroscopes that detect the change of attitude towards the horizontal, generating a signal that acts on the engines or turbines so that it corrects the deviations or unwanted inclinations.

Como propulsores se utilizan unos turborreactores situados en la zona superior de la cola o popa.Some propellants are used Turbo-reactors located in the upper area of the tail or stern.

También pueden utilizarse las pequeñas turbinas situadas en las zonas periféricas, dándoles inclinación de morro abajo para que parte del empuje se utilice para sustentar y el resto como propulsor.Small turbines can also be used located in the peripheral areas, giving them a nose inclination below so that part of the thrust is used to support and the rest as a propellant.

El monocasco puede utilizarse para transporte de pasaje, mercancías, agua para apagar fuegos, etc.The monohull can be used to transport passage, goods, water to extinguish fires, etc.

Las alas son plegables hacia arriba.The wings are foldable up.

Ventajas: Es práctico, es muy sencillo, económico, versátil pudiendo utilizarse para apagar fuegos y como nave de recreo.Advantages: It is practical, it is very simple, economical, versatile and can be used to extinguish fires and as pleasure ship.

Brief description of the drawings

La figura 1 muestra una vista esquematizada y en perspectiva, desde la zona superior, de la aeronave de la invención.Figure 1 shows a schematic view and in perspective, from the upper zone, of the aircraft of the invention.

La figura 2 muestra una vista esquematizada y transversalmente seccionada de la misma.Figure 2 shows a schematic view and cross section of it.

More detailed description of the invention

La invención, vista figura 1, consta de un monocasco (1), fanes (3, 4 y 4'), minialas delanteras (5), miniturbinas (6), articulación y giro del ala principal (7), barquillas (8 y 8'), barquillas opcionales (9 y 9') y turbopropulsores (10). (A-A) representa un corte del fuselaje. La zona inferior del casco (1) y las barquillas (8 y 8') y barquillas opcionales (9 y 9') permiten posarse sobre el agua, el empuje vertical para el despegue y aterrizaje se realiza mediante las miniturbinas de gas (6) y/o la ayuda de dos o mas grandes fanes (3, 4 y 4') sustentadores y estabilizadores accionados eléctricamente mediante motores eléctricos o neumáticamente mediante flujo de aire a presión procedente de las turbinas, un sistema de estabilización para vuelo consistente en unos giróscopos que detectan el cambio de actitud respecto a la horizontal, generan una señal que actúa sobre los motores o turbinas de modo que corrige los desvíos o inclinaciones indeseadas. Durante el ascenso o al final de este se aplica empuje hacia delante mediante las turbinas propulsoras (10), proporcionando de este modo la sustentación mediante las alas y opcionalmente mediante los fanes accionados eléctrica o neumáticamente. Las alas pueden girarse hacia arriba mediante las articulaciones (7).The invention, seen in figure 1, consists of a monohull (1), fans (3, 4 and 4 '), front minialas (5), mini turbines (6), articulation and rotation of the main wing (7), wafers (8 and 8 '), optional wafers (9 and 9') and turboprops (10). (A-A) represents a cut of the fuselage. The lower part of the hull (1) and the wafers (8 and 8 ') and optional wafers (9 and 9') allow you to perch on the water, the vertical thrust for takeoff and landing is done by means of gas mini-turbines (6) and / or the help of two or more large fans (3, 4 and 4 ') powered sustainers and stabilizers electrically by electric motors or pneumatically by flow of pressurized air from the turbines, a flight stabilization system consisting of gyroscopes that detect the change in attitude towards the horizontal, generate a signal that acts on engines or turbines so that Correct unwanted deviations or inclinations. During the ascent or at the end of this, forward thrust is applied by propeller turbines (10), thus providing the lift by the wings and optionally by the fans electrically or pneumatically operated. The wings can be turned upwards through the joints (7).

La figura 2 muestra una cubierta monocasco (1) según la sección (A-A), muestra una zona del fuselaje sin turbinas de gas ni fanes accionados eléctrica o neumáticamente.Figure 2 shows a monocoque cover (1) according to section (A-A), it shows an area of the fuselage without gas turbines or electric powered fans or pneumatically

Claims

1. Vertical take-off aircraft characterized by presenting a monocoque fuselage whose lower half adopts a shape similar to that of a conventional ship without keel, front minialas (5), main wings (7) and wafers (8, 8 '), having multiple turbines or mini-turbines in its contour or lateral peripheral area, adding on the wings and the fuselage two or more large fans driven by electric motors and by a flow of pressurized air from the main gas turbines.

2. Aircraft according to claim 1, characterized by placing the large fans in the central area of the wings.

3. Aircraft according to claim 1, characterized by placing the large fans in the central front area of the fuselage.

4. Aircraft according to claim 1, characterized by presenting a canard arrangement.

5. Aircraft according to claim 1, characterized by having the wings foldable or tilting upwards.

6. Aircraft according to claim 1, characterized by having a stabilization system for flight consisting of gyroscopes that detect the change of attitude with respect to the horizontal, generating a signal that acts on the engines or turbines so as to correct the deviations or inclinations unwanted

7. Aircraft according to claim 1, characterized by using turbojet engines located in the upper area of the tail or stern as thrusters.

8. Aircraft according to claim 1, characterized by using small turbines located in the lateral peripheral areas of the fuselage, which allow lower inclination of the nose so that part of the thrust is used to support and the rest as a propellant.