• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    The system anti-fall plane with wheels of teeth in perpendicular lever radius, is a mechanism formed by air wedges (4), which are activated with air against a possible fall. The cogwheel of the shaft (3) of these wedges (4) rotates two very long parallel cylinders, (6, 7) and (11 - 13), which extend from the front wings (19) to the wings later (21). These two cylinders are engaged with their respective gears (7, 10), located, one of them (7), at the rear end of the first cylinder (6, 7), and, the other (10), at the front end of the second cylinder (11-13), so that the wheel (13) of the end of the second cylinder (11-13) meshes with the gearwheel (14) of the shaft (15) of the propellers (17). (Machine-translation by Google Translate, not legally binding)
    公开号:ES2558031A1
    申请号:ES201400658
    申请日:2014-08-01
    公开日:2016-02-01
    发明作者:Fº JAVIER PORRAS VILA
    申请人:Fº JAVIER PORRAS VILA；
    IPC主号:
    专利说明:

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    DESCRIPTION
    Anti-calda aircraft system with teeth wheels in perpendicular lever radius object of the invention.
    The main objective of the present invention is to ensure that an Airplane (18) can rise in height when a possible rupture of its engines has occurred. At the same time, the Anti-Calda System presented may also serve as an Additional Engine, which may increase the Air Force, or, in the event that the same Force is maintained, may reduce the consumption of others. Engines, whether these are fuel, or electric.
    Background of the invention
    The main antecedent of this invention is the Principle of Arqulmedes del Radio de Palanca, well known. In this invention, we apply this Principle to two very long Serrated Cylinders, (6, 7) and (11-13), - which enforced a Perpendicular Lever Radius Principle -, which are traversed by an Axis (8) by their interior, the latter being independent of the Cylinder.
    Description of the invention
    The anti-calda plane system with teeth wheels in perpendicular lever radius, is a mechanism formed by Air Cradles (4), which when turning on its axis (3), move the Cogwheel (5) from its end . This Axis (3), is held, inside the Plane (18), in two Bearings (2), ending said Axis (3) in another Bearing that acts as a Stop (1). These Air Cots (4) are metal pieces whose shape would be similar to one of the two halves that would remain after cutting, by the plane of its Diagonal, a parallelepiped box. The four Air Cradles (4) are oriented in the same direction, so that the Air will always affect the inner hollow of at least two of them, - while the other two, at that precise moment, will meet showing its vertex -. This will cause the Axis (3) to turn with the Force that will transmit the Air against an eventual broth of the Plane, that is, with the Force of the Plane while it is falling, accelerated by the Force of Gravity. Precisely, the Force of this Air against it will be the one that activates, - by means of the Air Cots (4) whose Axis protrudes in Perpendicular of the lateral Fuselage of the Plane (18) -, to the Anti-Calda System that is presented, and, that It is described below. In connection with the Wheel (5) -, the one of the end of the Axis (3) of the Air Cradles (4) -, the Teeth of a very long Serrated Cylinder (6, 7) are engaged, whose Inner Shaft (8) it extends, from the Previous Wings (19), to the Rear Wings (21), where this Axis (8) will be firmly fixed, - and, at both ends -, to these two Wings (19, 21). In figure 1 it is observed that, at the rear end, this Cylinder (6), has a Cogwheel (7) that engages with another Cogwheel (10) of smaller Diameter, - although in the figure it presents the same Diameter -, which is in the previous zone, - I say "previous" depending on the direction of the Force transmission, and, not in the direction of the advance of the Plane -, of another Cylinder (10-13), which is a little longer than the previous one (6, 7), and, which extends in parallel with the previous one (6,
    7), until reaching the height of the Helices (17) that are in the anterior area of the Anterior Wings (l9). Shortly before, this Cylinder (11) will have expanded forming a Cone (12), so that the Base of this Cone (12) joins the side of the Perimeter of the Cogwheel (13), which is the one that meshes with the Wheel (14) of the Axis (15) of the Helices
    (17). This Shaft (15) is fixed in two Bearings (1, 2), in which the Rear Bearing
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    (1) acts as a stop. It should be added that, also the Cylinder (6) can form a Cone (12), like that of the Cylinder (11, 12, 13) that it has in parallel with it. This will help the Force that has increased due to the Perpendicular Lever Radius in the Cylinder
    (6), do not reduce later when you reach the Wheel (7) because this Wheel (7) has a Diameter larger than the Cylinder Diameter (6). With the Cone (12), the Force that has been increased due to the Cylinder Length, will not only be maintained upon reaching the Wheel
    (7) of greater Diameter, but, it will also have increased a little more because the Length extends even more. The two Cylinders (6, 7) and (11-13) add two Inner Bearings, - one at its front end, and, another, at its rear end, which are not seen in the figure -, which will serve to stabilize its position with the Inner Axes (8, 9), and, so that the outer Cylinder does not vary the circularity of its rotation. Figure I shows the Anti-Calda System that has been located on the Outside of the Airplane Fuselage
    (18), although, this does not necessarily have to be asl, since, this same System can be placed inside the Airplane (18), extending, - after the Wheel (13) -, an Axle with two Wheels Serrated at the ends, - and, Parallel to the Anterior Wings
    (19) -, to be engaged, at the other end, with the Wheel (14) of the Helices. Therefore, this Anti-Calda System for Aircraft, is activated with the Air Cradles (4), and, these, when turning, -and, when turning your Cogwheel (5) -, will make the Helices ( 17) also turn, with a Force greatly increased by the mechanism described, which will be responsible, at the same time, to increase as much as possible the Number of Turns that could rotate the Helices (17), which solves the second problem commented at the beginning of this section. This increase in the Number of Turns is achieved from the Difference of Diameters that have all the Cogwheels involved in the mechanism described. The Wheel (5) will have the same Diameter as the Diameter of the rotation of the outer end of the Cribs (4), which would be at least double that of the Cylinder Diameter (6). This will double the Number of Laps that the Cylinder will give (6, 7), with respect to the Laps that the Wheel will give (5). In the same way, the Wheel (7) can have twice the Diameter as the Wheel (10), which will still double the number of Laps that the Cots (4) have turned a second time.
    And, later, also the Wheel (13) will have double ... - or, triple -, of Diameter than the Wheel (14) of the Helices (17), with which, for each Turn that the Cots rotate ( 4), the Helices (17) will rotate eight Laps .., or, thirteen Laps .., if the Wheel (13) has three times the Diameter as the Wheel (14). Thus, when the Cots (4) rotate three Laps per second, the Helices (17) may rotate twenty-four Laps, - or, thirty-nine Laps -, which will be more than enough to be able to make this Plane rise and keep in flight as long as it takes, just by taking advantage of the Air Force against it, a Calda that does not require it to maintain a great Angle with respect to the Horizontal. I want to say with this that, even without Calda, this Airplane could use this System, as an additional Engine, which could either replace it with the Push of other Engines, or it could contribute to its Push, if it is activated while the Engines, and, this will reduce much of the consumption and maintain the health of the engines. To activate or deactivate the Cots (4) you just have to enter, or, extend, - towards the inside or outside of the Fuselage of the Plane (18) -, a Cradle-shaped Plate, -not drawn in the figure n ° 1 -, which will be placed in front of these same Air Cots (4), allowing, or, preventing, the Air from hitting the Cots (4). Date of the invention: (06.30.14).
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    Description of the figures
    Figure 1: View from the bottom of the Plane, in which the Anti-Calda mechanism is shown, which, in this figure, is located outside the Airplane Fuselage (18). This Anti-Calda System begins in an Air Cradle (4), whose Toothed Wheel (5) is engaged with the Teeth of a Toothed Cylinder (6, 7) that meshes its Toothed Wheel (7) at the rear end, with another Cylinder Toothed (10-13) which ends in a Toothed Cone (12, 13), which meshes with the Cogwheel (14) of the Helices (17). Two Inner Axes (8) run through the hollow of the two Cylinders (6, 11) and are fixed at their ends in the Anterior Wings (19) and the Rear Wings (21).
    Figure 1:
    1) Stop and shaft bearing
    2) Bearings
    3) Axis
    4) Air cradles
    5) Cogwheel
    6) Serrated cylinder
    7) Cogwheel
    8) Inner shaft
    9) Inner shaft
    10) Cogwheel
    11) Cylinder-cone
    12) Cone of the cylinder-cone
    13) Cogwheel
    14) Cogwheel
    15) Shaft
    16) Shaft end
    17) Helices
    18) Airplane fuselage
    19) Anterior wings
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    20) Ailerons
    21) Back wings
    Description of a preferred embodiment
    The plane anti-fall system with teeth wheels in perpendicular lever radius, is characterized by being a mechanism that can be installed inside an airplane, - or, in its exterior r-, to take advantage of the qualities of the Principle of the Arqulmedes Lever Radius which, when applied to the Cylinder-shaped Cogwheels described in the previous sections, may increase the Air Force that falls against the Cots (4), from an eventual broth of the Airplane (18), so that this Force can move the Helices (17) with enough Strength that allows the Aircraft to climb height.
    This Air will, in the first place, affect the hollow of these Air Cots (4) which, when moving its Shaft (3) and the Cogwheel (5) at its end, will activate two Serrated Cylinders (6, 7) and ( 11-13) located in Parallel and meshed by the Cogwheels (7, 10) of one of its ends. The second Cylinder (11-13) gears its Cogwheel (13) with the Cogwheel (14) of the Helixes (17), so that the Air against the Calda will, paradoxically, serve to make the Plane lift high when this safety mechanism activates the Helices (17).
    The problems presented by such a mechanism are: first, to increase the Force of the Air that hits the Cribs (4), and, secondly, to get the Number of Turns that the Helices can rotate ( 17), be enough for the Air to be removed, have sufficient Strength so that it can overcome the Force of Gravity, because only then, the Airplane will be able to climb high.
    To achieve, in the first place, the increase of the Air Force against the Cribs (4), these Sprockets are presented in the form of a very long Cylinder, (6, 7) and (11-13) that have the quality of increasing the Force, - Applied to its Teeth of the previous end, with the Wheel (5) of the Axis (3) of the Cribs (4) -, depending on the Archimedean Principle, which, on this occasion, is presented as a Radio Principle of Lever Perpendicular which, as we will see below, is not exactly the same as the Principle of Radio de Palanca de Arqulmedes, even though it is formed from it. To better understand what is involved in the Force transmitted by these Cylinders (6, 7) and (11-13), we just have to think that, when we extend our two Arms forward and put a couple of thick Books on them Hands, these books are going to weigh more the further they are from the shoulders, either in their perpendicular position with respect to the Body Plane. If we now think that our Body is the Plane of a Wheel, the Fingers of our Hands will be the Teeth of the Cylinder that extend in Perpendicular to the Plane of the Wheel-Body. Thus, the farther away from the Wheel-Body Plane is the point of Force Application, - that is, the further we put the Books from said Wheel-Body Plane, the greater the Force that this Plane will feel of the Wheel-Body, and, at the same time, less Effort will have to realize the Force that is Applied, - be that which the Books make downwards -, to spin the Wheel-Body. In this sense, the Force Applied at the previous end of the Cylinder (6), - be it in its previous Teeth -, will be multiplied by the Length of the Cylinder (6), so that the Force will increase, only by the presence of this
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    Length. It must also be said that the Perpendicular Lever Radius increases the Force a little less than the Archimedes Lever Radius.
    The example is immediate. If, instead of putting the Arms extended forward, we extend them to the sides, - in Parallel to the plane of the Body -, the Force of the Weight of the Books on the Hands will be greater than when we extend the Arms with the same Books forward , in Perpendicular to the Body Plane. However, the fact that, in Parallel, - with the Arms stretched to the sides -, the Force is greater, does not prevent that, in Perpendicular, the Force will also increase to a large extent depending on the Length of the Arms , - although it increases less than with the Arms in Parallel with the Body Plane -, with which, whenever we extend, in Perpendicular, an Axis, from the Plane of a Wheel, the Force of rotation that is applied on the end of This Perpendicular Axis, will have to be multiplied by the Length of this Axis, and, the result will be the Perpendicular Sense Force that will reach it, or, that the Wheel Plane will feel.
    Abundant in the explanations, I must now establish the difference between what would be the Wheel-Cylinder (6, 7), and, a very large Radius Wheel (RR), be a Radius equal to the Length of the Wheel-Cylinder ( 6, 7) of the figure n ° 1. This second Wheel would be really great, and, the Force that was applied in its Perimeter, would have to be multiplied by its Radius, which would be measured with the equation of the Force of Archimedes: (FArq = Fa • R). We will now assume that this Wheel (RR), - of Radius equal to the Length of the Wheel-Cylinder (6, 7) -, instead of being a continuous Plane, like a disk, was formed by Teeth in the form of Radii independent. What we are going to do now is to bend these Radii so long, so that we are going to turn this Wheel (RR) into the Wheel-Cylinder (6, 7), in which the Independent Radii of the Wheel (RR) above they are grouped in a Circumference to give it the shape of a Cylinder. Its final appearance will therefore be that of the Wheel-Cylinder (6, 7) in Figure 1, in which the Cogwheel (7) at the rear end will indicate the exact point where the Radii of the Wheel (RR) of very long diameter, would have begun to bend in an Angle of (90 °).
    We can now understand that, in this Wheel-Cylinder (6, 7) that we have formed, its Radios could not transmit the same Force that they could transmit to their Central Axis when the Radios had not yet bent in the original Wheel (RR) , which means that the Force will have been reduced by an amount yet to be determined, which I will try to express in an equation that I will present shortly. Therefore, we have, on the one hand, the original Archimedes Force of the Wheel (RR), and, on the other hand, the Archimedes Force in Perpendicular, of the Wheel-Cylinder (6, 7). These are two different Forces, in which the first will always be greater than the second. However, the second Perpendicular Force is also a Force that increases according to the Cylinder Length, although it does not increase as much as in the case that the Radii or Teeth of this Cylinder were put back in the original position, that is, in the Wheel position (RR), position prior to being bent at the Angle of (90 °). From this Difference between the two Forces, we must establish two different equations for them. The first we know already by Archimedes, and, the second, I will propose it shortly after: (FAq = FA • R). What we can call the Force Sense in Perpendicular that will reach the Wheel (7) of the rear end of the Wheel-Cylinder (6, 7), will then be the result of Subtracting, from the Force of Archimedes, the Force that it will have been reduced because of having put the Radii in Perpendicular to the Plane of the Wheel, which we will write like this: (FS-P = FArq - FRed).
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    And, in turn, this Reduced Force will be the Product of the Reduction Percentage, and, the Arquulmedes Force: (FRed = P% • FAr). Said Reduction Percentage is calculated based on the Quotient between the (50%) in which the Force is reduced when the Radii pass to the Perpendicular position, and, the (90 °) determined by the Angle of that change of position. This Quotient will have to be divided by (100), and, all that has to be multiplied
    (50% / "i
    for the value of the Alpha Angle:

    90 °
    100
    ■ a).
    Therefore, the Reduced Force,
    Y
    Now it can be expressed in this other way:
    image 1
    We only have to apply these values to the starting equation, that of the Force Sense in Perpendicular: (FS-P = FArq - FRed), which, when extended, becomes the same as this other expression:
    ■ {FaR)
    In this equation, we assume that, the Applied Force, - after having converted the original and imaginary Wheel (RR), into a Wheel-Cylinder (6, 7), as in Figure 1 -, or, as stated , that the Applied Force, when bending in the Angle of (90 °), has been reduced by (50%), and, for this reason, this value appears in the last equation, dividing the (90 °) of the Angle in which it has folded. This offers the Percentage of Force that is lost in the Perpendicular Transmission for each Degree of the Angle, which, when multiplied with the Arquulmedes Force, and, Subtracted from this Product, of the same Arquulmedes Force, offers the concrete result of the Force Sense Perpendicular, which would be the one to reach the Cogwheel (7) of the device of figure 1.
    And, now, and, since it could always happen that the Radios were not exactly located Perpendicular to the plane of the Wheel, - as if it occurs in the Wheel- Cylinder (6, 7) -, but could form a Cone of different Angles, - as in a segment of the Wheel-Cylinder (11-13), or, also, in a Gear-Cone -, in the previous equation this variety is planned, and, for this reason it can be used for all Possible angles that these Radii can acquire, or, the body of this Cylinder (6, 7), between (0 °), and, (90 °).
    The equation will also serve to measure the Force transmitted by the Gear-Cone, in which we will only have to make a small modification in the Angle of (90 °), because, in a Gear-Cone, this Angle is greater, since that the rods that remotely join their two wheels, still bend inwards a little more than those (90 °).
    The increase of the distance that separates the two wheels of the Gear-Cone, can determine that this Alpha Angle approaches the Angle of (90 °), but, this does not happen in
    image2
    all cases, and, thus, in the equation, only the Beta Angle that is the excess that experiences - in the previous equation -, the Angle of (90 °) of the Gear-Cone, to which we must add now must be added to the value of (90 °). That is, for the Gear-Cone, the equation would be:
    image3
    权利要求:
    Claims (3)
    [1]
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    1. Airplane anti-calda system with teeth wheels in perpendicular lever radius, characterized by being a mechanism formed by Air Cots (4), which have a Cogwheel (5) at the end of its Axis (3) . This Axis (3), is held, inside the Plane (18), in two Bearings (2), finishing said Axis (3) in a Stop (1) that is at the same time a Bearing. These Air Cots (4) are metal pieces whose shape would be similar to one of the two halves that will remain after dividing, by the plane of its Diagonal, a parallelepiped box. The four Air Cots (4) will be oriented in the same direction on their Axis (3). The Axis (3) of these Air Cradles (4) protrudes in Perpendicular from the lateral Fuselage of the Plane (18). In connection with the Wheel (5) of the Axis end (3) of the Air Cradles (4), the Teeth of a long Serrated Cylinder (6, 7), whose Inner Shaft (8) extends, from the Previous Wings (19), to the Rear Wings (21), where this Axis (8) will be fixed, - and, at both ends -, to these two Wings (19, 21). At the rear end, this Cylinder (6), has a Cogwheel (7) that engages with another Cogwheel (10) of smaller Diameter, which is at the end of another Cylinder (10-13), which is like the previous one (6, 7), and, which extends in parallel with the previous one (6, 7), until reaching the height of the Helices (17) that are in the previous area of the Previous Wings (19). The two Cylinders (6, 7) and (11-13) add two Inner Bearings, one at its front end, and another at its rear end, located between the inner face of the Cylinders (6, 7) and (11 -13), and, the Inner Axes (8, 9). Shortly before, this Cylinder (11) will have expanded forming a Cone (12), so that the Base of this Cone (12) joins the side of the Perimeter of the Cogwheel (13), which is the one that meshes with the Wheel (14) of the Axis (15) of the Helices (17). This Shaft (15) is fixed in two Bearings (1, 2), in which the Rear Bearing (1) stops. The Wheel (5) has the same Diameter as the length between the ends of two opposite Cots (4), which will be twice the Cylinder Diameter (6). The Wheel (7) has a Diameter larger than the Cylinder Diameter (6). And, in the same way, the Wheel (7) will have twice the Diameter as the Wheel (10). And, later, also the Wheel (13) will have triple the Diameter that the Wheel (14) of the Helices (17).
    [2]
    2. Airplane anti-calda system with teeth wheels in perpendicular lever radius,
    - according to the first claim - characterized in that the System described will now be located inside the Airplane Fuselage (18). On this occasion, it is necessary to extend, - in connection with the Wheel (13) -, an Axle with two Cogwheels at the ends, - and, Parallel to the Anterior Wings (19) -, which is engaged, by one end, with the Wheel (13), and, on the other end, with the Wheel (14) of the Helices.
    [3]
    3. Airplane anti-calda system with teeth wheels in perpendicular lever radius,
    - according to the first claim - characterized in that, also the Cylinder (6) will form a Cone (12), like that of the Cylinder (11, 12, 13) that it has in parallel with it, in which the Wheel (7) has a Diameter greater than the Cylinder Diameter (6).
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    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    US500326A|1893-06-27|Georg theodor lagus gabrielii |
    US591692A|1897-10-12|Air-ship |
    ES1044293U|1999-10-13|2000-03-16|Vila F Javier Porras|Parachute mechanic with blades, driven by these tiles and driven by air during the fall. |
    ES1052228U|2002-02-06|2002-12-01|Vila F Javier Porras|Paracaidas cylinder. |
    ES1054224U|2002-12-26|2003-07-01|Vila F Javier Porras|Horizontal propeller blades with frenacaidas wedges in a plane skate. |
    ES2277539A1|2005-10-18|2007-07-01|Fco. Javier Porras Vila|Pedal for mechanical traction of bicycle is placed on major plate whose diameter is crossed by double axis|
    ES2322738A1|2007-03-23|2009-06-25|Fco. Javier Porras Vila|Anti-fall helix, for aircraft |
    ES2446842A2|2012-04-11|2014-03-10|Fº JAVIER PORRAS VILA|Gear multiplier force and amount of rotation |
    ES2439141A2|2012-07-17|2014-01-21|Fº JAVIER PORRAS VILA|Anti-fall propellers with fins and wedges, for autonomous space shuttle |ES2651726A1|2016-07-28|2018-01-29|Fco. Javier Porras Vila|Anti-fall system for aircraft |
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