• 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 wings with arches, and tubes on the lower surface, are a simple way to increase the incidence of air against the wings (2), or, more specifically, against the arcs (3) that we have added below. These arcs (3) will work as if we had increased the wing surface, without needing to lengthen the wings (2), both along and across. (Machine-translation by Google Translate, not legally binding)
    公开号:ES2633608A1
    申请号:ES201600243
    申请日:2016-03-21
    公开日:2017-09-22
    发明作者:Fco. Javier Porras Vila
    申请人:Fco. Javier Porras Vila；
    IPC主号:
    专利说明:

    WINGS WITH ARCHES, AND, TUBES IN THE LOWER SURFACE OBJECT OF THE INVENTION
    The main objective of the present invention is to increase the AJar surface, without having to add more wings, or, without having to lengthen them, both in length and width. The arches (3) have a larger interior surface that implies a greater incidence of the advance air, which it will make them work as if the surface of the wings had been increased. BACKGROUND OF THE INVENTION
    I do not know background of the present invention as regards the arches (3) located in the base of the wings (2). Yes there are as for the diaphragm (1) that narrows the outlet air of the tubes (5), which have been in the state of the art, and, can be observed present, for example, in aircraft reactors and on space rockets In the present invention, this diaphragm (7) is an element that can be added or removed. DESCRIPTION OF THE INVENTION
    The Wings with arches, and, tubes on the lower surface, are airplane wings (2) (1) that have added arches (3) that can increase the alar surface, without modifying anything in the ajas (2). This increase is produced by increasing the area of incidence of the air against the advance, against the curved walls inside the arches (3). The plane (J) can multiply its wings (2) with bows, as can be seen in figure 5, and, in addition, it can carry another more added wing, in which tubes (5) are put in place of arches (3). These tubes (5) have a mobile tube (6-8) added at the rear end, which also has a diaphragm (7) that can narrow the exit space of the alfe.
    DESCRIPTION OF THE FIGURES Figure 1: Front view of an airplane, on whose wings (2) and rear wings (4) we have placed arches (3) on the lower surface. The base of the plane has tubes (5).
    Figure # 2: Side view of a representation of the wing (2), which is used to study the incident air mass that occurs with the advance of the plane (1), which corresponds to the base area of some wings (2) smooth, from its anterior edge inclined upwards, to its posterior edge, located lower.
    Figure 3: Side view of a representation of the wing (2), which helps us to study the incident air mass that occurs with the advance of the plane (1), which corresponds to the area of the base of the wings (2 ), from its anterior edge inclined upwards, to its posterior edge, located lower, when we have added arcs (3). Two horizontal reference lines are created, corresponding to

    the wings (2) and the lower ends of the arches (3), which concentrates much more the air mass
    incident.
    Figure 4: View [Tontal of an arc (3) in which the air lines strike its surface
    intelior, forming different angles according to the point of incidence.
    S Figure # 5: Front view of an airplane (1) in which we have added two more wings with bows (3), and,
    another wing with tubes (S) that have a mobile diaphragm (6-8) at the rear end
    Figure 6: Side view of the mobile diaphragm (6-8) which is an added tube (6) at the end
    rear of the tube (S) that can pivot on a thyme (8) so that it can move towards
    above. The added tube (6), in this figure, is shown in the forward position.
    10 Figure # 7: Side view of the mobile diaphragm (6-8) - <>, added tube (6) of the rear end of the
    tube (5) -, which has pivoted on the screw (8), and, has been raised. The added tube (6), in this figure, is
    shows in the ascent position, and, the diaphragm (7) has narrowed the exit space of the
    air.
    Figures 1-7:
    fifteen 1) Airplane
    2) Wings
    3) Arches
    4) Rear spoilers
    S) Tubes
    twenty 6) Tube added
    7) Diaphragm
    8) Pivot
    DESCRiPTION OF A PREFERRED EMBODIMENT
    Wings with bows, and, tubes in the lower supeljicie, are characterized by being a form of
    25 greatly increase the alar surface of an airplane, without, in fact, it seems that we have
    increased. It consists of putting areos (3) on the lower surface of the wings and the ailerons
    later, -as can be seen in figure 1, with the opening facing down. With this
    arrangement of the arches (3), we increase the attack surface of the air against the advance, because
    it will hit a much larger surface than if this surface is smooth.
    30 To verify this statement, we just have to find the measure of this new surface
    formed by the arches. We assume that the plane has two smooth wings that measure, each, (20) meters
    long and (3) meters wide. The total supe / jieie alar for these smooth wings will be: (
    20 · 3 = 60 m 2). And, since there are two ajas, then: (2, 60 m 2 = 120 m 2). On these smooth wings it will push up the air against the advance, determining a vertical thrust value, which will be proportional to that alar surface. We are going to install, now, all the arches of figure 1, on the underside of the smooth ajas
    S previous. We will assume that the diameter of these arches is (25) centimeters: (rjJ = 0'25 m)
    - Your semi-perimeter will then be: ePer= 2; rr R = 2; rr'O'12 = 0'78 m)
    (p er =2; rr R = 0.78 = 0.39 m). 2 2
    As it is about wings (20) meters long, in each of them, bows (lOO) will fit,
    10 because, in each meter, we will put (5) arcs: (20 · 5 = 100 Arc) Now we multiply the value obtained for the semi-perimeter of the arcs, by the number of
    arches of a soybean wing, and, we get: (0.39. 100 Arc = 39 m2).
    - And, as each arch is (3) meters long, although, in a transverse direction to the ajas, - that is, the same
    long than the width of the wings-, then: (3, 39 m2 = 117 m2).
    - As the plane has two wings, the tolal surface of all the arches located in them will be:
    --We observe, thus, that the total surface of the arches, is almost twice that of the alar surface when the wings are smooth or flat on the underside: (234 m 2> 120 m 2), (234 m 2 ~ 2 120 m 2).
    20 25 In this way, we will have almost doubled the attack surface of the air against the advance, without further extending the wings, and, without adding additional ajas. Only the shape of the underside of them will be sufficient for the miracle of the multiplication of the surface to be produced. - The second problem today is well related to the first, and, refers to the mass of air that falls against the ajas, both in the case that these ajas are smooth .., as in the case that they have arches, like the ones I present today. We now look at figure 2 in which we see a smooth wing, which is inclined upwards by the anterior edge, as is customary. The air rate that will hit the underside of this smooth aja, will measure, in height, which indicates the vertical double fl. - We now look at Figure 3, in which I have depicted an aja that has arches, which we see, from that lateral position, as another line parallel to that of the inclined wing.
    We see, then, to figure # 2, to which we add the arcs in figure # 3. In it there will be two virtual horizontal lines, -or, two dotted lines-, which defend the accumulation of the mass of air that it will enter and concentrate on the arches, from the anterior area of the wings that are always inclined upwards, to the posterior area that is inclined downwards. If we think about what is happening now, we will notice that the air against the advance not only covers a vertical zone that corresponds to the extension of the inclined wing, with respect to the dotted line that represents the horizontal. Now, we have added the arcs, which would be those that would be between the upper line and the second line, which has forced us to put two horizontal reference lines, or, two dotted lines. Therefore, now, the incident air mass will almost have doubled with respect to figure 3, which means that, e! Air is going to concentrate much more on the arches, and, therefore, will push harder vertically, and, upwards, which will contribute to a better lift of the plane. - The importance of having studied the difference between the two types of wings, the smooth wings, and those with arcs, will help us understand one of the problems that arise in these arcs. Figure 5 shows one of these arcs seen frontally, in which the air entering it will push in all directions. The problem lies, now, in the fact that, these different directions of incidence of the air against the inner walls of the arches, suppose a very different angle of wing in each line of air force, which means that, the greater be the angle that forms any line of air, with respect to the vertical, the lower the force of its upward thrust, because, as we know from Newton, every force that forms a certain angle, which moves away from the line in which the force is exerted, it will reduce its value in direct proportion to the cosine of said angle. In this sense, all the increase in the alar surface that we have achieved with these arches, would not help us at all, because, e! increase of the alar surface, would be compensated with the reduction of the force of the air against the advance, when hitting against that alar surface that forms arcs, reduction caused by the angle of incidence on the inner walls of the arches.
    We must now recover the meaning of the two previous figures, n ° 2 and 3, because, in them is the key that can make us understand that the invention of these arcs will serve well for what it intends to serve. The problem of the increase in the mass of air incident against the arches is that it determines that this air now acquires a much greater concentration, which increases the thrust upwards, so that it will compensate well for the reduction of the force of! incident air caused by the increased angle of attack.
    Here is how the question of reducing the force caused by the angle of attack is resolved. Therefore, having doubled the alar surface, it is going to be protected for something, so that the sustainability will increase much more because the mass of air that attacks the arches has doubled. The reduction of the thrust caused by the angle of attack, could only reduce by half the force increased by the doubling of the alar surface, because, in that half, it will be where it would match the force of the air when it comes to smooth wings . Obviously, if we have doubled the alar surface, the bearing force will also have doubled, so that if, now, the angle of attack of the air against the inner face of the arches, reduce the bearing force, obviously, this reduction only It is exercised halfway. Therefore, as we know that the mass of the attack air has also doubled, it will be this duplication that will recover half of the lift force lost by the angle of attack, with which it will be worth, then, the duplication of the alar surface, and, these arcs will also be worth.
    In figure 5 I have doubled the wings with arches, and, I have added a third wing with longitudinal tubes (5), which extend along the wings, also transversely. With these tubes, the concentration of the air against the advance will still be much greater than when there are only two wings with arches, which will push the plane up much more strongly. --The lower tubes (5) will be inclined upwards by the front end, and, downwards by the rear end. These lower tubes (5), in addition, will have an added mobile tube (6), - Figure 6, which will lean upwards from the rear end, so that they will push the tail of the plane down, causing the plane to lift up the bow. To avoid having to put a pair of ailerons in the rear area of the anti-fall tubes, it occurs to me to put an end that moves and can pivot on a screw (8). In figure 6, the end of the tube (5) has an added tube (6) that pivots on a screw (8). In this figure, the position of the added tube is consistent with the rectilinear advance of the plane. Note that, for the lower zone, the added tube (6) is longer than in the upper zone. This extension will keep so that the air does not come out of the tube on the left, and, you can keep pushing when the added tube (6) moves up.
    In figure 7, the added tube (6) will have risen so that, now, the air finds a smaller area of exit than before, which will increase its force and its thrust, to which is added the fact that The diaphragm (7) has been compressed and has even narrowed the air outlet. In addition, the air will now push down any added tube (6) that has risen, and, as it is in the tail of the plane, will cause it to rise up the bow.
    The advantages of increasing the alar surface or better lift, are that the plane will have real problems to fall, which increases the security of the passage. In addition, the engines, when pushing forward, will not have to overcome the force of the weight that pushes down, with which, with much less force of thrust, we will achieve the same performance ..., or, the same speed as with wings smooth, which means good fuel savings, and better maintenance, in good condition, of the engines.
    权利要求:
    Claims (1)
    [1]
    1) Wings with arches, and, tubes on the il / ferior surface, characterized by being aircraft wings (2) (1) that
    they have arcs (3) added in the base, which increase the alar surface, without having to modify
    nothing on the wings (2). The plane (1) can put two wings (2) with bows, and, in addition, it will carry a third
    added wing, in which, tubes (5) are placed instead of arches (3). These tubes (5) have a mobile tube
    (6-8) added at the rear end, which also has a diaphragm (7) that can narrow the
    air outlet space.
     Figure 1
    -r --- Z
    ------- !. ~ -----------------
     Figure 2
    Figure # 3
     Figure # 4
    /
    8 6/ .5,, I
    (
    ', 7
     Figure # 6
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    同族专利:
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    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    RU2060211C1|1992-02-21|1996-05-20|Валерий Туркубеевич Пчентлешев|Tailless aeroplane|
    US6199796B1|1996-07-18|2001-03-13|Prospective Concepts Ag|Adaptive pneumatic wing for fixed wing aircraft|
    WO1999061313A1|1998-05-25|1999-12-02|Prospective Concepts Ag|Adaptive pneumatic wings for flying devices with fixed wings|
    US20040248496A1|2001-09-25|2004-12-09|Harvey William B.|Remote-controlled long-range airplane|
    RU2392189C1|2009-03-30|2010-06-20|Батор Бамуевич Бадмацыренов|Bioaerodynamic aircraft with oscillating wings|
    法律状态:
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    ES201600243A|ES2633608B1|2016-03-21|2016-03-21|Wings with bows and tubes on the bottom surface|ES201600243A| ES2633608B1|2016-03-21|2016-03-21|Wings with bows and tubes on the bottom surface|
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