ES2624919B1 - Mobile turbine in lever radius - Google Patents

Abstract

The mobile turbine in lever radius, is the rotating engine (4) that we put on the ends of the wings (2) of a fighter plane (1), whose force will increase depending on the length of said wings (2). This turbine (4) can acquire two positions, one of advance, when we place them in horizontal, and, another of vertical takeoff, when we place them in vertical.

Description

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DESCRIPTION

Mobile turbine in lever radius.

Object of the invention

The main objective of the present invention is to achieve that a fighter plane (1) can take off vertically very easily, which is achieved by putting Turbines (4) at the ends of the Wings (2) which forms a Lever radius that increases the Turbine Force (4) in direct proportion to the Length of the Wings (2). In this way, it is much easier to overcome the Weight of the Airplane (1) because the Force increases much more than what increases the Weight of the Turbines (4) by putting them on that same Lever Radius. This fighter plane (1) is optimal to be transported in aircraft carriers.

Background of the invention

The main antecedent of the present invention is found in the Archimedes Principle of the Lever Radius with which he discovered that the user's effort was less in direct proportion to the Length of the Lever Shaft Radius. The second antecedent is in the application that of this Archimedes Principle I have made in my previous Patent n °: P2501400259, entitled: Airplane with groups of fins above and below the fuselage, and, of the wings, in which the Aircraft engines, which were fixed on that occasion, were also located at the ends of the Wings forming a Lever Radius.

Description of the invention

The mobile Turbine in lever radius, is a system for the vertical take-off of an Aircraft, - specially designed for a fighter Aircraft, although it is useful for any other type of Aircraft -, which is formed by two Mobile Turbines (4 ) that we are going to place at the lateral ends of the Wings (2), so that they will form a Lever Radius that will increase the Turbine Force (4) the greater the said Radius or the Length of the Wings (2). A rotating Shaft (3) will make the Turbines (4) can acquire two positions. In the Advance position, -figure n ° 1-, the Turbines (2) will be placed in a horizontal position, and, in the Vertical Takeoff position. -figure n ° 2-, the Turbines (4) will be vertically directed downwards the combustion flow. A fixing shaft (5) will be used to fix the turbines (4) in their Advance position, that is, in a horizontal position. In Figure 1, these Fixing Axes (5) leave the ends of the Wings (2) to be fixed to the Turbines (4), while, in Figure 2, the Fixing Axes have been retracted from of an electrohydraulic actuator, and, have been introduced inside the Wings (2). Date of the invention: (16.01.16).

Description of the figures

Figure 1: Plan view of a fighter plane (1) that has a turbine (4) at each end of its wings (2), forming a Lever Radius. The Turbines (4) are in the Advance position, -that is horizontal-, and, a Fixing Shaft (5) fixes them in their position.

Figure 1: Plan view of the same fighter plane (1), whose Turbines (4) are in Vertical Takeoff position, either vertically, and, the Fixing Axis (5) leaves its fixation and enters the Wings inside (2).

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Figures 1-2:

1) fighter plane

2) Wings

3) Rotating shaft

4) Turbines

5) Fixing shaft

6) Drift rudder

Description of a preferred embodiment

The mobile turbine in lever radius, is characterized by being a system for Vertical Takeoff of a fighter aircraft (1) that must act and be transported from an aircraft carrier. Applying the Principle of Archimedes of the Lever Radius, we put a Turbine (4) at the ends of the Wings (2) of this Plane (1), so that its Strength will increase depending on the Length of the Wings (2). A rotating shaft (5) will allow you to acquire both horizontal and vertical positions, which will allow you to move forward and take off vertically. The problem that arises is that of the relationship between the Turbine Force and its own Weight, to the extent that, when moving away from the body of the Plane, the Lever Radius will cause the two concepts to increase at the same time, by having than multiply by the concept of that Distance. The equations that affect the two concepts will be these two: (FRP = FT ■ x) and (WRP = WT ■ x). In the first, it is the product between the Turbine's own Force and the Lever Radius Distance that will determine the Lever Radius Force. In the second, it is the Lever Radio Weight, which is defined by the product between the Turbine's own Weight, and the Lever Radius Distance. We assume that the turbine's own force is one metric ton, and the distance is four meters, or, what is the same, (400) centimeters. I put it this way because we know that, the Weight, in the plate of a Balance, always increases in each centimeter, and, to increase it does not need to vary in each decimeter, or, in each meter: (FRP = FT • x = 1,000 N • 400 cm = 400,000 N). We assume, now, that the turbine's own weight is (300) newtons, and, the distance is the same, four meters, or, four hundred centimeters: (WRP = WT • x = 300 N • 400 cm = 120,000 N) .

From this data, we find two options. In the first option, we could divide on the one hand, the own Force and the own Weight, and, on the other hand, the Force in Lever Radius and the Weight in Lever Radius. If we do these divisions in this way, the result will be the same ... with which we will not have gained anything in regard to the Turbine Force (4) by putting them at the ends of the Wings (2) forming a Radius of Lever:

Ft I.OOOVt ^, ^, Fgf 400,000 N T WT 300 N i Ww 120,000 N i

Now, why should we do this division, when there is nothing in the phenomenon that divides the Turbine Forces into other minor Forces?

What actually happens, in this problem, is that there is a Force, - that of the Turbine (4) -, which pushes up, and, another Force, that of the Weight, which pushes down ... which determines that a Subtraction of Forces of opposite direction is being played, and, thus, we only have to Subtract, on the one hand, the concepts of Self-Strength and Own Weight 5 of the Turbine, and, on the other hand, the concepts of Force in Radio of Palanca and Weight in Radio de Palanca, to study what we have gained in Strength for Turbines (4) that we put at the ends of the Wings (2), which we will do like this:

Fr- W7 = (1,000 Nt) - (300 N1) = 700 N

Fsr- W „= (400,000 N t) - (120,000 N i) = 280,000

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We obtain, now, a more than significant difference between the two Subtractions, since, in the first, the (700) Newtons of the Turbine Force, are much smaller than the (280,000) Newtons that are obtained in the second, when the Lever Radius has increased (400) centimeters. In this way, we have no doubt that we have achieved a good Strength gain to raise our fighter plane vertically (1).

Claims (1)

ES 2 624 919 A1 1. Mobile turbine in lever radius, characterized by being a system formed by two Mobile Turbines (4) that we are going to place at the lateral ends of the Wings (2), so that they will form a Lever Radius. At each end of the Wings (2) there will be a rotating Axis (3) articulated to the Turbines (4), to which it is fixed. And, another fixing shaft (5) is articulated by one end, - and, inside the Wings (2) -, to an electro-hydraulic actuator, while, at the other end, it is fixed or released from the Turbines ( 4).