• 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 anti-fall system for aircraft, with double-cone gears, is formed by air wedges (1, 2) that, when moved by air against a possible fall, are responsible for moving a train of gears-double-cone (5-9) and (5'-9 ') which, in turn, can rotate, with great force and speed, the shaft (15) with blades (17) of propellers that is in the interior of the anti-fall tube (18) that is installed on the sides of an aircraft fuselage. With this system, the airplane will recover the thrust it needs to stay in flight, because it will be pushed by the air that removes the blades (17) from the propellers, whose speed still increases more in the narrowing (19) of the rear area of the tube anti-fall (18).
    公开号:ES2677239A1
    申请号:ES201700106
    申请日:2017-01-30
    公开日:2018-07-31
    发明作者:Francisco Javier Porras Vila
    申请人:Francisco Javier Porras Vila；
    IPC主号:
    专利说明:

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    ANTI-FLOW SYSTEM FOR AVIDN, WITH GEAR-DOUBLE-CONE
    OBJECTIVE OF THE INVENTION
    The main objective of the present invention is to create a system that prevents an airplane from falling due to lack of thrust. To avoid this, a system is created that will take advantage of the air against the broth, to move some air cuffs (1, 2), whose crown (4) will move to a gear train - double-cone (5-9 ), (5'-9 ') which, in turn, move the blades (17) of the hdlices inside the anti-fall tubes (18) that we will have installed in the fuselage of the airplane.
    BACKGROUND OF THE INVENTION
    The main antecedent of my invention of the day (27.01.17) is found in my previous patent n ° P201600661, entitled: Airplane anti-fall system, where it showed a similar system, which was moved by air cuffs, which moved to a gear train-cone, and, not to a gear train-double-cone (5-9), (5'-9 '), like the one I present today, which can achieve a force much greater than its precedent . The double-cone gears (5-9), are based on the Ibgica of the principle of lever of Archimedes, - what supposes to be its main antecedent -, which means that the force that is applied at the end of the radius mbs long (6), serb so much greater, the larger said radius long (6), as tradition shows us in one of the first laws of mathematical physics, such as the Archimedes formulations. The metal rods (6, 8) of these double-cone gears (5-9) form the axis of the lever, which is supported by a bearing (7) that functions as a fulcrum. In this way, a pair of forces is formed, which are those of two levers located at the ends of the dibmeters of the piflbn (5) and the crown (9). In this sense, and, as will be shown in a later section, the force achieved with a double-cone gear train (5-9) and (5'-9 ') is very large, with only two gears -double-cone. If, on the train, we add a third gear-double-cone (5-9), the force still multiplies a lot mbs, which makes it possible to believe in the possibility that the blades (17) of the horns, are capable of Remove, with the force required by the airplane to stay in flight, the air that enters through the anterior opening of the anti-fall tube (18). DESCRIPTION OF THE INVENTION
    The anti-fall system for avidn, with double-cone gears, is formed by air cuffs (1, 2), fixed on a shaft (3) that has a crown (4) at the end, which engages with the piflbn (5) of the first double-cone gear (5-9) of the double-cone gear train (5-9), (5'-9 '). Depending on the ratio between the crown diameters (4) and the piflbn (5), the latter will rotate three or four turns for each round of the crown (4), if the ratio that relates them is (3: 1 ), or, of (4: 1). The double-cone gear train (5-9), (5'-9 ') is formed by two double-cone gears (5-9), and, (5'-9') which, in turn , are formed by a piflbn (5, 5 ') and a crown (9, 9'), joined at a distance by
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    methyl rods (6, 8), (6 ’, 8’), which are joined in a bearing (7, 7 ’) that functions as the fulcrum of a balance. This bearing (7, 7 ') seems to divide the rods (6, 8), (6', 8 '), into a long radius (6, 6'), and, a short radius (8, 8 ') , although, in reality, the rods (6, 8), (6 ', 8'), are attached inside the bearing (7, 7 '). The crown (9) of the first double-cone gear (5-9) is meshed with an intermediate pifldn (10) which, on the other hand, is engaged with the pifldn (5 ') of the second double-cone gear ( 5'-9 '), in which, in the last crown (9'), the pifldn (11) of an axis is engaged
    (12), which has another pifldn (13) at the other end, which is the one that engages with the pifldn (14) of figure 3, which is inside the anti-fall tube (18). The anti-brown tube (18), is open at its two extremes, and narrows at the rear end (19). Figure 3 shows the connection of the pifldn (13), of the shaft (12) that I have just described, -as long as they are inserted inside the anti-fall tube (18) -, with the pifldn (14 ) of the axis (15) that runs, longitudinally, the center of the anti-fall tube (18). Said shaft (15) is fixed to the anti-fall tube (18) by means of vertical shafts (16). The blades (17) of the hdlices are also placed on the shaft (15).
    DESCRIPTION OF THE F1GURES
    Figure 1: Plan view of the air cuffs (1, 2), which are fixed to an axis (3) that has a crown (4) at the end, which engages with the pinion (5) of the first double-cone gear (5-9) of the double-cone gear gear (5-9), (5'-9 '). The air cuffs (1, 2) of this figure, are those that protrude from the fuselage on the right side of the avidn, and, connect with the anti-brown tube that we have placed on that side, either on the outside of the avidn, or inside.
    Figure 2: Plan view of the double-cone gear train (5-9), (5'-9 '), in which the pifldn (11) of the last crown (9') is engaged. an axis (12), which has another pifldn (13) at the other end which is the one that engages with the pifldn (14) of figure 3, which is inside the anti-fall tube (18) .
    Figure 3: Plan view of the anti-fall tube (18), which shows the connection of the pifldn
    (13), of the shaft (12), with the pifldn (14) of the shaft (15) that runs through the center of the anti-fall tube (18). Said axis (15) is fixed on vertical axes (16). The blades (17) of the propellers are placed on the shaft (15). The anti-fall tube (18) narrows at the rear end.
    Figures 1-3:
    1) Air cuff showing the outer vdrtice
    2) Air cuff showing the inner hole
    3) Axis
    4) Crown
    5) Pifidn
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    6) Long radius metal rods
    7) Bearing or fulcrum
    8) Short radius methyl rods
    9) Crown
    10) Intermediate Pipidn
    5 ’) Pifidn of the second gear-double-cone train
    6 ') Metallic rods of the long radius, of the second gear-double-cone of the train 7') Bearing or fulcrum, of the second gear-double-cone of the train 8 ') Metallic rods of the short radius, of the second gear-double-cone of the train 9 ') Crown, of the second gear-double-cone train
    11) Pifldn
    12) Shaft
    13) Piflon
    14) Pifldn
    15) Tube shaft (18) anti-fall
    16) Shaft fixing axles (15)
    17) Propeller blades
    18) Anti-fall tube
    19) Rear narrowing of the anti-fall tube (18)
    DESCRIPTION OF A PREFERRED EMBODIMENT
    The anti-fall system for aircraft, with double-cone gears, is characterized by being a thrust mechanism that takes advantage of the air of the descent to propel, in the opposite direction, the air, that is, upwards. Said air, incidird against the air cuffs (1,2), which, in turn, move to the double-cone gear train (5-9), (5'-9 '), which increase ^ the force of said air against the air cuffs (1, 2) depending on the difference in diameter of their pipions (5, 5 ') and their crowns (9, 9'). And, at the same time, increase, also, the amount of rotation of these same sprockets. These two increases could be applied to the shaft (15) that runs longitudinally to the anti-fall tube (18), where the blades (17) of the propellers are also, which will receive all that force and that amount of rotation that has increased in the double-cone gear train (5-9), (5'-9 '). The equation of Arqulmedes
    measures the balance of forces and radii of a balance, or, that of a lever: (F, ■ / , = F2 • R2). If we clear force two, we can find its value, depending on the values of others.
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    _ Ft-Rt
    concepts: (r2 -
    R,
    ). And, as crowns (9, 9 ’) have a double, or triple, or,
    at least, than the piplons (5, 5 '), the short radii (8, 8') will form an alpha angle, with respect to the virtual extension of the long radii (6, 6 '), which will reduce the force they receive in a value
    F, R.
    —1 ------- ■ COS a. ). In this sense,
    Rz
    we can calculate, in an example, the force two that would receive the crown (9 ') of the second gear-double-cone (5'-9') of this gear train-double-cone (5-9), (5 '-9') of figure 2. We assume that the force with which the air pushes the air cuffs (1, 2), when the air falls, for example, only ten degrees from the horizontal, is a minimum value, such as 10 Newtons. The long radius (6) measures 100 centimeters, and, the short radius (8) measures 10 centimeters. The alpha serf angle, for example, 18 degrees. We apply these data in the last equation, and, we will obtain two strength that will balance the balance in the first double-cone gear (5-9): (
    as indicated by the cosine of said alpha angle: (F7
    f -fl__
    2 R:
    10 100
    • cos a = ---------
    10
    • COS 18 ° = 100 ■ 0.95 = 95 Newtons). We apply, now,
    This force two, which will be that of the crown (9) -, as applied to the pifldn (5 ’) of the second gear - double-cone (5’-9’). We assume that the ratio between the dripmeters between piplons and crowns is (3: 1), which allows us to multiply by three, the value of force two that we have obtained before: (
    3 • F, • R,
    3 -95 ■ 100
    F, = -——------ cos a = -——------ • cos 18 ° =
    R.
    10
    = 2,850 ■ 0'95 = 2,707'5 newtons). This force will multiply even more when we put a third gear-double-cone (5 ”-9”) on the train. Now, again, according to the proportion of the diameters, the force two we have just obtained is multiplied by three:
    (Fi =
    3 ■ F, R
    i,
    R,
    cos a =
    3 ■ 2,707'5 • 100 10
    cos 18 ° =
    = 3 • 27,075 • 0'95 = 77,163'75 newtons). A thrust of 77 tons, in a single gear-double-cone train, will be able to keep the avidn in flight. And, like, in each anti-drop tube (18), we can put at least three double-cone gear trains (5-9), (5'-9 '), (5 ”-9”) , we will have a total of six, - three in each tube (18) - that is, six thrusts of 77 tons, which makes
    a total of 462 tons of thrust, which can keep a large number of airplanes of different weight in flight.
    权利要求:
    Claims (1)
    [1]
    RE1VIND1CA CIONES
    1) Anti-fall system for avidn, with double-cone gears, characterized by being connected by air cuffs (1, 2), fixed on an axis (3) that has a crown (4) at the end, the which meshes with the pifldn (5) of the first double-cone gear (5-9) of the double-cone gear train (59), (5'-9 '); the double-cone-gear train (5-9), (5'-9 ') is connected by two double-cone-gear (5-9), and, (5'-9') which, at its instead, they are formed by a pipid (5, 5 ') and a crown (9. 9'), joined at a distance by metal rods (6, 8), (6 ', 8'), which are joined in a bearing (7, 7 '); This bearing (7, 7 ') seems to divide the rods (6, 8), (6', 8 '), into a long radius (6, 6'), and, a short radius (8, 8 ') , although, in reality, the rods (6, 8), (6 ', 8'), are attached inside the bearing (7, 7 '); the crown (9) of the first double-cone gear (5-9) is meshed with an intermediate pipid (10) which, on the other hand, meshes with the pipidn (5 ') of the second double-cone-gear ( 5'-9 '), in which, in the last crown (9'), the pifidn (11) of an axis (12) is engaged, which has another pifldn (13) at the other end, which is what it engages with the pifldn (14), which is inside the anti-fall tube
    (18); the anti-fall tube (18), is open at its two ends, and narrows at the rear end
    (19); the pifkm (13), of the shaft (12) just described is inserted inside the anti-fall tube (18), and, it engages with the pifldn (14) of the shaft (15) that runs, longitudinally, the center of the anti-fall tube (18); said axis (15) is fixed a) anti-fall tube (18) by means of vertical axes (16); the blades (17) of the propellers are fixed on the shaft (15).
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    同族专利:
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    ES2677239B1|2019-05-14|
    引用文献:
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    法律状态:
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    优先权:
    申请号 | 申请日 | 专利标题
    ES201700106A|ES2677239B1|2017-01-30|2017-01-30|Anti-fall system for aircraft, with gears - double - cone|ES201700106A| ES2677239B1|2017-01-30|2017-01-30|Anti-fall system for aircraft, with gears - double - cone|
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