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    • 专利摘要:
    The helicopter with four gear trains-double-cone, is an aircraft of security and force, which obtains them from the four trains of gear-double-cone (4 - 8 ') that surround the axis (11) of the propellers (13) and which engage, simultaneously, the pinion (10) that is fixed on this shaft (11). With these trains (4 - 8 '), the origin force of the engines (1) is multiplied to values that allow the helicopter to perform some special force functions, such as lifting a lot of weight, or, transporting a lot of cargo, or, much passage. Since it has four engines (1), and, four trains (4 - 8 '), and, since only one can keep moving, the other three can remain inactive until the pilot activates them.
    公开号:ES2680646A1
    申请号:ES201700252
    申请日:2017-03-10
    公开日:2018-09-10
    发明作者:Francisco Javier Porras Vila
    申请人:Francisco Javier Porras Vila；
    IPC主号:
    专利说明:

    DESCRIPTION

    Helicopter with four gear-double-cone trains.

    Object of the invention 5

    The main objective of the present invention is to create a system that offers great flight safety, and that, in addition, can develop a lot of strength. These two objectives can be achieved by installing four electric motors (1) that will move to four double-cone gear trains (4-8 ') whose last crown (8') is engaged with the pinion (10) of the shaft (11 ) 10 of the propellers (13). In these trains (4-8 ') the force of the engine (1) will be multiplied in a value proportional to the dimensions of its parts, such as the long (5, 5') and short (7, 7 ') spokes They work just like the principle of the Archimedes lever. Thus, the longer the long radii (5, 5 ’), and, the shorter the short radii (7, 7’), the force will increase proportionally to these values. fifteen

    By increasing in this way the force and number of engines (1) and trains (4-8 '), flight safety will also increase because it will be very difficult for all engines (1) to break down at the same time, obviously, without that an act of unforeseen sabotage has been executed.
     twenty
    Background of the invention

    The main antecedent of my invention of the days ((27-29) .01.17) is found in the Archimedes Lever Principle which is where the logic and structure of the double-cone gears (4-8) and (4'-8 ') that form the trains (4-8'). Depending on the measures of 25 their long (5, 5 ') and short (7, 7') radii, the force that their motors (1) can apply, may be greater or lesser at will, which means that with a Less power from the engines (1) will be able to achieve enough strength so that the helicopter can perform its usual functions.
     30
    Another background of these double-cone gear trains (4-8 ') can be found in my previous patent n ° P201200374, entitled: Swing toy with spirals, in which I presented gear-cone trains that comes to be , in its form and structure, only half of the pieces or wagons (4-8) and (4'-8 ') that form today's trains (4-8'), because they would only be formed, -in each car - by the pinion (4) and the rods of the long radius (5) of each 35 car of the train (4-8 ') that I present today.

    As regards the two wheels with an axle that we add in each car (4-8) and (4'-8 '), they can be found in my patent No. P201500445, entitled: Recursive force gear for motor explosion or electric, where the crankshaft of the crank of a piston, was related to two cone-gears put in series. Below the crankshaft, two wheels joined by an axle, were engaged in the last wheel of the second gear-cone, and, in the first wheel of the system, which offered a return of the force that had increased in the gear-cone, from the last wheel, to the first, which reiterated again and again the process of increasing strength. Four. Five

    In the present invention, - as shown in Figure 3-, we add two sprockets (29, 31) attached to an axle (30), which will be put in contact with the crown (8) of the first car of the double-cone gear train (4-8 '), - in the first double-cone gear (4-8) and (4'-8') -, and, the crown (28) that we will adhere to the pinion (4). fifty
    Description of the invention

    The helicopter with four double-cone gear trains is an aircraft whose thrust system, both vertically and horizontally, is determined by an electric motor (1) whose crown (3) moves to a gear train -double-cone (4-8 '), whose last crown (8') 5 moves the pinion (10) of the shaft (11) of the propellers (13). From this axis (11) of the propellers (13) it can be said that it can pivot on the horizontal axis of a bearing (12) that is in the upper third of said axis (11). Said horizontal axis of the bearing (12) is fixed in a metallic circular panel that will surround all the double-cone gear trains (4-8 ’) and the axis (11) of the propellers (13). Around the axis (11), four or six gear-double-10-cone trains (4-8 ’) with an electric motor (1) each can be installed. Each of these double-cone-gear trains (4-8 ') are formed by two “wagons”, or, what is the same, by two double-cone-gears (4-8) and (4'- 8 ') that have exactly the same dimensions.

    The crown (3) of each of the electric motors (1) will move to the pinion (4) of the first car 15 (4-8) of its own train (4-8 ’). The two or four rods that form its long radius (5), and, which are fixed on the sides of the perimeter of this pinion (4), join a hundred centimeters beyond, in the place where a bearing (6) will surround them ) which is fixed by an axis to the metal circular panel that surrounds the entire system described. From this bearing (6), then two or four rods that form a short radius (7) extend and join at the sides of the 20 perimeter of a crown (8), whose diameter will be at least the double, than the pinion (4). This crown (8) is meshed with an intermediate pinion (9) that will have the same diameter as the pinion (4), and which, on the other hand, meshes with the pinion (4 ') of the second carriage (4'- 8 ') of the train (4-8'), which is exactly the same as the one just described, although it is located in an inverted position with respect to the previous one. The crown (8 ’) of this second car (4’-8’) engages 25 with the pinion (10) that is fixed on the shaft (11) of the propellers (13). In the train (4-8 ') we can add a third car more (4 ”-8”), or, even a fourth car (4 ”' - 8 '”), which will increase even more the force that reaches the pinion (10) of the shaft (11) of the propellers (13).

    At the lower end of this axis (11), the mechanism that moves the axis (11) with the 30 propellers (13) is located. At the lower end of the shaft (11), therefore, a crown (15) is fixed that will be moved by the last pinion (14) of a gear reduction gear, -moved by another electric motor-, which will serve so that the axis (11) moves, only, three or four centimeters forward, or, backwards, which serves so that the helicopter can move forward or backward, because its propellers (13) will form the sufficient angle that will send the air that remove, both backward and forward.

    As the entire system described will be enclosed in a circular panel, all its elements will pivot with it depending on the rotation determined by the pinion (14), on the crown (15). The circular panel, on the outside, will have two horizontal axes that will be fixed to the fuselage of the helicopter, and, in this way, the entire circular panel can pivot, leaning forward or backward, by the action of the pinion and crown mechanism (14, 15) which is in the lower area of the shaft (11) of the propellers (13).

    In figure 3, an element is presented that will allow us to further increase the force of the double-cone gear train (4-8 ’). We add two gear wheels (29, 31) attached to an axle (30), which will contact the crown (8) of the first wagon of the double-cone gear train (4-8 '), -or of the first double-cone gear (4-8) and (4'-8 ') -, and, the crown (28) that adheres to the pinion (4), which forms, at this point, a crown gear piece ( 28) and pinion (4). fifty

    The piece (29-31) that we add now, will fit in the crown teeth (28), where there is no contact between the crown teeth (3) of the engine (1), -o, the engine (27) -, with the crown teeth (28). The force that will have increased upon reaching the crown (8),
    will return to the crown (28) after crossing the axle (30) of the wheels (29, 31). This is because the force will always tend to balance on these two wheels (29, 31), and, if the wheel (29) receives a greater dose of force from the crown (8), this force will be transmitted along the entire axle ( 30), and, it will reach the wheel (31), so that it will affect the crown (28), it will double in the pinion (4), and, it will reach the crown (8), depending on the 5 measurements of the long radius (5) and the short radius (7). This process will be repeated continuously.

    An alternative mechanism is presented in Figure 2 that will allow not all engines (1) of the gear-double-cone trains (4-8 ’) to be activated at all times. With this mechanism, the engines (1) can remain inactive until the pilot of the 10 helicopter voluntarily puts them into operation.

    In the upper area of Figure 2, we see the crown (3) of the motor (1) of Figure No. 1. However, now, in the alternative mechanism, its rods (2) have an axis (16) which ends in a short striated tube (17), which is striated inside, and, which is part of an inverted "u" shaped structure. At the lower ends of the two vertical axes (19, 20) of this inverted "u" structure, there are magnets (21), which face electromagnets (22) that are in the striated axis (22) of the motor alternative electric (27). This motor (27) is fixed to a support (24) that is fixed, at the other end, to axles (25) with wheels (26).
     twenty
    When the pilot activates the electromagnets (22), the spline shaft (23) will not yet be attached to the striated interior of the tube (17), but will still be far away, and the motor (27) should still remain deactivated until that the electromagnets (22) and magnets (21) are in the turning phase, at which time the coupling with the striated tube (17) will be made. At that moment, the spline shaft (23) will be rotating at the same speed as the spline tube 25 (17), because this spline tube (17), which is the one that also moves the inverted “u” structure already the magnets (21) -, is the one that rotates at all times by the turn transmitted by its own double-cone gear train (4-8 ') whose last crown (8') is always engaged with the pinion (10 ) of the shaft (11) of the propellers (13). This axis (11) will always be rotating by the movement that the electric motor (1) of the double-cone gear train (4-8 ’) that 30 is activated at that moment.

    Therefore, and, in summary, when the pilot activates the electromagnets (22), the motor (27) will remain off. The spline shaft (23), this shaft (23) will soon phase its electromagnets (22) with the rotation of the magnets (21) that rotate with the crown (3) that will always be rotating, just like its own double-cone gear train (4-8 '). That will be the time for the pilot to activate the approach of the motor (27) so that its spline shaft (23) approaches the fluted tube (17), and, only after coupling, the pilot, or, a computer program, will activate the engine (27).
     40
    As each of the trains (4-8 ') develops a lot of force, with only one of them it will be enough to perform all the usual movements of the helicopter, and, when more force is needed, the other three can be activated independently five engines (27) of the trains (4-8 ') that have been installed around the axis (11) of the propellers (13).
     Four. Five
    In this way, the helicopter acquires great safety in flight, because, in the event that one of its engines fails (1), the pilot can activate any of the other three or five engines (1) that he has installed on the other trains ( 4-8 ').

    Description of the figures 50

    Figure 1: Front view of the shaft (11) of the propellers (13) with the motor (1), whose crown (3) moves two of the four or six double-cone gear trains (4-8 ' ) to be installed around the shaft (11) of the propellers (13). In the upper area is the pivot bearing (12) which
    It has an axis that extends towards the bottom of the blade and is fixed on a circular metal panel that supports the entire system shown in this figure. In the lower area is the engine mechanism and a crown (15) and a pinion (14) engaged, which will cause the shaft (11) of the propellers (13) to move forward, or, backward, so that the helicopter can move forward too, or, backward. 5

    Figure 2: Front view of the coupling or uncoupling system of the spline shaft (23), in the spline tube (17) located at the lower end of the shaft (16) of the crown rods (2) (3) ) which, in figure 1, is the crown (3) of the electric motor (1).
     10
    Figure 3: Front view of the axle (30) that has a cogwheel (29, 31) at each end. The wheel (29) is meshed with the crown (8) of the first double-cone gear (4-8), and, the wheel (31) is meshed with the crown (28) that we add to the pinion (4). This creates a recursive return to the force that reaches the crown (8), which will always return to the crown (28).
     fifteen
    Figures 1-3:

    1) Electric motor.

    2) Metal rods. twenty

    3) Crown

    4) and 4 ’) Pinion.
     25
    5) and 5 ’) Long radius.

    6) and 6 ’) Bearing.

    7) and 7 ’) Short radius. 30

    8) and 8 ’) Crown.

    9) Intermediate pinion.
     35
    10) Propeller shaft pinion.

    11) Propeller shaft.

    12) Pivot bearing. 40

    13) Propellers.

    14) Pinion of an electric motor.
     Four. Five
    15) Propeller shaft crown.

    16) Axis.

    17) Internally fluted tube. fifty

    18) Horizontal rod of the inverted "U" structure.

    19) Left vertical rod of the inverted "U" structure.
    20) Left vertical rod of the inverted "U" structure.

    21) Magnet.

    22) Electromagnets of the shaft (23) of the alternative motor. 5

    23) Shaft with splined end.

    24) Fixing support.
     10
    25) Sliding support.

    26) Wheels.

    27) Alternative engine. fifteen

    28) Crown.

    29) Cogwheel.
     twenty
    30) Axis

    31) Cogwheel.

    Description of a preferred embodiment 25

    The helicopter with four double-cone gear trains, is characterized by being a safety and force aircraft, which obtains them from the four double-cone gear trains (4-8 ') that surround the axis (11) of the propellers (13) and which are geared simultaneously to the pinion (10) that is fixed on this axis (11). With these trains (4-8 '), the force of origin of the 30 engines (1) is multiplied to values that allow the helicopter to perform some special force functions, such as lifting a lot of weight, or, carrying a lot of cargo, or, A lot of passage. As it has four engines (1), and, four trains (4-8 ’), and, as with only one it can keep moving, the other three can remain inactive until the pilot activates them. 35

    The amount of rotation that will be transmitted by the crown (3) of the engines (1) to the last crown (8 ') of the train (4-8') can be measured by this equation: CG = v • N (n-1) , where (v) will be the number of turns of the last crown (8) of the first car (4-8), and, (n) will be the largest number of the proportion of diameters between the last crown (8) of the first wagon (4-8), and, the first pinion (4 ') 40 of the second wagon (4'-8'). We must take into account, now, that this amount of rotation of the last crown (8 ’), will double or triple later, when transmitting its turn towards the pinion (10) of the axis (11) of the propellers (13). At the same time the force of origin of the engine (1), will also be multiplied in the double-cone gear train (4-8 ’), which we can obtain with the equation of the Archimedes lever: 45




     fifty
    It must be taken into account, now, that the force of the crown (8 '), when transmitted to the pinion (10) of the shaft (11) of the propellers (13), will still increase double or triple, depending on the proportion of diameters that relates them. If we assume, in one example, that the force of the engine is 100 Newtons, the long radii (5, 5 ') being 100 centimeters, and the short radii (7, 7'), 10 centimeters, in a proportion of diameters of pinions and crowns of (2: 5 1), and, an alpha angle of 32 °, the force of the crown (8 ') will be this:



    And now, in the second car (4’-8 ’): 10

     =

    As this force is multiplied by two when it reaches the pinion (10), then, the final value of the force, -in each of the double-cone-gear trains (4-8 ’) -, will be: 15

    2 • 7.191’04 = 14,382'08 newtons

    which will add a total of:
     twenty
    4 • 14,382’08 = 57,528’32 newtons

    That is, 57'5 tons of Newtons, when we are using engines (1) of only 100 Newtons of force. If we increase this value, the increase is considerable. If each engine (1) has a force of 1,000 Newtons, the final value would be 575 tons of Newtons. 25

    In addition, we can always increase the number of wagons of each train (4-8 ’), so that the force will increase even more. In the previous calculation, in reality, the force of the engine (1) would be only 50 Newtons, but when this force is transmitted to the pinion (4) of the first car of the train (4-8), it will double because of the difference in diameters between the crown 30 (3) and the pinion (4), which will reach the figure of 100 Newtons which is the one with which I have started the calculation. I will now calculate the value that would reach the force that reached the crown (8 ”) of the third train car (4-8”):

     = 35

    which, with only one double-cone gear train (4-8 '), is a higher figure than the sum of the forces of the four double-cone gear trains (4-8') of the calculation previous.
    If we multiply the last result by four trains (4-8 ”), with three cars each, then the total number for the force would be: 40

    4 • 60.980’02 = 243.920'07 newtons

    And, as when arriving at the pinion (10) this force that will have reached the crown (8 ”), would still double twice, because of the difference in its diameters, the total figure would be: 45

    2 • 243.920’07 = 487.840’14 newtons

    In all these calculations, nothing is said about the force that would add the presence of the piece (29-31) in the first car of each train (4-8 ”), which would still be a much higher figure. fifty
    权利要求:
    Claims (1)
    [1]

    1. Helicopter with four double-cone gear trains, characterized by being an aircraft whose thrust system, both vertically and horizontally, is determined by an electric motor (1) whose crown (3) meshes with the first pinion (4) of a double-cone gear train-5 (4-8 '), whose last crown (8') meshes with the pinion (10) of the shaft (11) of the propellers (13); this axis (11) of the propellers (13) pivots on the horizontal axis of a bearing (12) that is in the upper third of said axis (11); said horizontal axis of the bearing (12) is fixed in a circular metallic panel that surrounds all the double-cone gear trains (4-8 ’), and, to the axis (11) of the propellers (13); around the shaft (11), a minimum of four 10 double-cone gear trains (4-8 ’) with an electric motor (1) each is installed; each of these double-cone-gear trains (4-8 ') are formed by a minimum of two “wagons”, or, what is the same, by a minimum of two double-cone-gear (4-8 ) and (4'-8 ') that have exactly the same dimensions; the crown (3) of each of the electric motors (1), meshes with the pinion (4) of the first car (4-8) of its own train (4-8 ’); the four 15 rods that form its long radius (5), and, which are fixed on the sides of the perimeter of this pinion (4), join a hundred centimeters further, in the place where a bearing (6) will surround them , which is fixed by an axis to the metal circular panel that surrounds the entire system described; the circular panel, on the outside, pivots on two horizontal axes that will be fixed to the fuselage of the helicopter; from this bearing (6), another four rods that form a short radius (7) are extended, and, which are joined at the sides of the perimeter of a crown (8), whose diameter will be at least double , that of the pinion (4); this crown (8) is engaged with an intermediate pinion (9) that has the same diameter as the pinion (4), and, which, on the other hand, meshes with the pinion (4 ') of the second carriage (4' -8 ') of the train (4-8'), which is exactly the same as the one just described, although it is located in an inverted position with respect to the previous one; The crown (8 ') of this second car (4'-8') is engaged with the pinion (10) that has been fixed on the shaft (11) of the propellers (13), at the lower end of this axis (11) the axis mechanism (11) of the propellers (13) is located; at the lower end of the shaft (11), therefore, a crown (15) is fixed which is engaged with the last pinion (14) of a gear reduction gear, articulated with another electric motor; an element is added to the first carriage (4-8) of the double-30-cone gear train (4-8 ') which is formed by two gear wheels (29, 31) attached to an axle (30), which is they put in contact with the crown (8) of the first wagon of the double-cone gear train (4-8 '), and, the crown (28) that adheres to the pinion (4), which forms, at this point , a piece of crown gear (28) and pinion (4); This part (29-31) is fitted in the crown gear (28), where there is no contact between the crown teeth (3) of the motor (1), -o, the motor (27) -, with the crown teeth (28); The alternative mechanism for activating or deactivating the motors (1) of the double-cone gear trains (4-8 ') is formed by an axis (16) that joins the crown rods (2) (3) ); this axis (16) ends in a short fluted tube (17), which is fluted inside, and which is part of an inverted "u" shaped structure; at the lower ends of the two vertical axes (19, 20) of this inverted "u" structure, there are magnets (21), which face electromagnets (22) that are in the striated axis (22) of the alternative electric motor (27); this motor (27) is fixed to a support (24) that is fixed, at the other end, to axles (25) with wheels (26); the last crown (8 ’) of the double-cone gear train (4-8’) is always engaged with the pinion (10) of the shaft (11) of the propellers (13). Four. Five
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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
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    ES2461567A2|2012-04-02|2014-05-20|Fº JAVIER PORRAS VILA|Push-pull toy with spirals |
    ES2446842A2|2012-04-11|2014-03-10|Fº JAVIER PORRAS VILA|Gear multiplier force and amount of rotation |
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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
    ES201700252A|ES2680646B1|2017-03-10|2017-03-10|Helicopter with four gear-double-cone trains|ES201700252A| ES2680646B1|2017-03-10|2017-03-10|Helicopter with four gear-double-cone trains|
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