• 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 helicopter with thrust scales, is a ship that will increase its strength up, taking advantage of the downward thrust of the air of its horizontal propellers (18) against the plates (3) of the thrust scales (3-8) that go to redirect upwards the force downwards that the plates feel (3). The push scales (3-8) are placed in a circle, at the base of the helicopter, and, are two arms (5, 7) of a balance (3-8) whose fulcrum rests on a pivot (6) of the end of the diameter of a wheel (9), which has two vertical axes (10) at its center that are fixed at the base of the cockpit (15) of the helicopter, and, at the other end of the diameter, has another axle (11) which is supported, also, at the base of the cabin (15). These push scales (3-8) serve to push the wings (1) of an airplane. (Machine-translation by Google Translate, not legally binding)
    公开号:ES2658763A1
    申请号:ES201600790
    申请日:2016-09-12
    公开日:2018-03-12
    发明作者:Fº JAVIER PORRAS VILA
    申请人:Fº JAVIER PORRAS VILA；
    IPC主号:
    专利说明:

    HELICOPTER WITH PUSH BALANCES OBJECT TO THE INVENTION
    The main objective of the present invention is to increase the force with which a helicopter can be lifted, which is achieved with the Push Scales (3-8) that we place at the base of the cabin (15), so that take advantage of the force of the air that the horizontal propellers (18) of the helicopter remove downwards, so that they also push down the plates (3) of the thrust scales (3-8) that will be commissioned later, to redirect that force to push the helicopter up. These same push scales (3-8) will serve to push the wings (1) of an airplane forward, when we place the plates (3) behind the propellers (13) of the turbo-fans (14). In another version, the push scales (3-8) will directly push the wings (1) of the plane, taking advantage of the air against the advance of the plane, which will be made to pass through conical-truncated cylinders (2) that will be placed by in front of the plates (3) of the push scales (3-8) to increase their strength and speed. BACKGROUND OF THE INVENTION
    I do not know if there is any history of this invention that I have completed between days (22.08.16) and «09-10) .09.16). DESCRIPTION OF THE INVENTION
    The helicopter with push scales, is an airship in which, at the base of the cabin (15), we put in a circle a set of push scales (3-8) so that, your dishes (3) take advantage of the force of the air that removes the horizontal propellers (18) towards it, so that the second arm (7) of the balance will cause its protector (8) to push the helicopter upwards. Figures 1 and 4 show the fundamental elements of these push scales (3-8) that support their fulcrum in the pivot (6) of the right end of the diameter of a wheel (9), at whose left end it has a vertical axis (11) that rests on a protector (12) that is in contact with the base of the cabin (15). From the center of the wheel (9), two axles (10) that are fixed at the base of the cab (15) are upwards. The fulcrum of the thrust balance (3-8) is, on this occasion, a hole in which the right pivot (6) of the wheel diameter (9) is inserted. The balance has two arms (5, 7) of different radii, which affects the lever radius force of each arm. The first arm (5) has a horizontal plate (3) at the end. The second arm (7) curves upwards and has at its end a protector (8) that will be in contact with the base of the cabin (15). Next to it we put another push scale (3-8) that will cause, this same air that is directed downwards, -to the horizontal plate (3 )-, push the helicopter forward, because its second arm (7) will that its protector (8) is put in contact with a vertical plate that will have the cabin in that place. At the same time, we can also put other push scales (3-8) forward, in which the plates (3) were placed vertically, and, the second arm (1, 8) push it forward. These push scales (3-8) have multiple applications. Among them, we can highlight the one that we can apply on the wings (1) of an airplane, which can be in two ways. Figure 3 shows the plate (3) of the first arm (5) of the balance (4-8) that is now placed vertically, so that it balances with the second arm (7) and its protector (8) which contacts the wing (1). The figure does not show the other elements, such as the wheel (9) and its axles (10, 11) for convenience of exposure. It is, on this occasion, to take advantage of the air that the vertical propellers (13) of an electric motor (14), or, of a turbomotor, take back. The wing (1) will be pushed forward, in this way, by the protector (8) of the second arm (7). The second application of the thrust balance (3-8) on the wings (1) of an airplane, is presented in figure 4, in which the fundamental elements of the thrust balance (3-8) are the same, although, instead of putting a single plate (3), several plates (3) are added that rest on the same axis (4) that is connected to the first arm (5) of the push scale ( 3-8), which can serve as an anti-fall system because, in an airplane, any extra dose of thrust ahead becomes an anti-fall insurance. In figure 4 we see conical-trunk-cylinders

    (2) which are on the wings (1) and focus on the plates (3). It is that, the air against the advance of the plane, enters these conical-trunk-cylinders (2) and increases its force and speed before hitting the plates (3) of the Push scale (3 -8) . In figure 4 we have a wing
    (one) of airplane that, in the later zone has a scale of push (3-8) anti-fall. On its wings (1) we see the conical-trunk cylinders (2) that narrow in the back area and face the plates (3) of the balance (4-8), which are fixed to an axis (4) , -parallel to the wings (1) -, which is actually part of the first arm (5) of the push scale (3-8). This arm (5) extends to the fulcrum hole, where the first pivot (6) of the end of the diameter of a wheel (9) is introduced. As in the helicopter I have described before, this first pivot (6), in figure 4, is at the right end of the wheel diameter (9). At the left end, there is a second pivot in which a vertical axis (11) is fixed, -vertical in figure 4, although, in reality, it would be horizontal-, which extends, then, towards the wing (1 ), relying on a protector (12) that touches the wing (1), but which is not fixed to it, - unless we fix it to a spring, fixed at the other end on the protector (12), since it does not It is going to move a lot from its position. In the center of the two faces of the wheel (9), we put two axes (10), -vertical in the figure and horizontal in reality-, which are fixed to the central axis of the wheel (9) by one end, and , are fixed to the wing (1), at the other end. From the first pivot (6), the second arm (7) of the thrust balance (3-8) is now extended, ending in a protector (8) that is not fixed to the wing (1), but only in Contact with her.
    DESCRIPTION OF THE FIGURES
    Figure # J: Side view of a helicopter in which only two push scales (38) are presented. One of them, the one below, is located horizontally and will push up the base of the cabin (15). The second will push it forward, because it is located vertically.
    Figure # 2: Plan view of the hebcopter of the previous figure, which highlights the position of the many first arms (5) of the push scale (3-8), as they are circled around and below of the cabin (15). In each first arm (5) we put two or more plates (3).
    Figure # 3: Side view of the wing (1) of an airplane, which has a motor (14) of vertical hebces (13). After these propellers (13) we place the plates (3) of the push scales (3-8) of which, in the figure only the plate (3) has been represented, and, the second arm (1) with its protector (8) which is in contact with the wing (1) to which it will push forward.
    Figure 4: Plan view of a plane wing (1), in which a thrust balance (3-8) with several plates (3) is placed, which are located behind the conical-trunk-cylinders ( 2) that we put on the wings (1) to increase the strength and speed of the air that enters them.
    Figures No 1-2:
    1) Airplane wing 2) Conical-trunk-cylinder 3) Plate 4) Axle 5) First balance arm 6) Wheel pivot 7) Second balance arm 8) Protector 9) Wheel 10) Central vertical axis 11 ) Vertical axis of the end of the diameter 12) Protector 13) Vertical propellers of an engine located on the wings 14) Engine 15) Helicopter cabin 16) Helicopter tail 17) Vertical tail propellers 18) Horizontal helicopter propellers
    DESCRIPTION OF A PREFERRED EMBODIMENT
    The helicopter with push scales is characterized as a ship that will increase its
    upward force, taking advantage of the downward air thrust of its horizontal propellers (18)
    against the plates (3) of the push scales (3 -8) that will redirect the force upwards
    5 down that they feel the dishes (3). The push scales (3-8) are put in a circle, at the base of the
    helicopter, and, are two arms (S, 7) of a push scale (3-8) whose fulcrum rests on a pivot
    (6) of the right end of the diameter of a wheel (9), which has two vertical axes (10) in its center
    which are fixed at the base of the cabin (15) of the helicopter, and, at the other end of the diameter, has another
    shaft (11) that also rests on the base of the cabin (15). These push scales (3-8) are used to
    10 push forward to the wings (1) of an airplane. I have already presented this scale (3 -8) in another invention
    in which the plates (3) were pushed by the combustion gases of a reactor. Little bit
    later, I thought, that they could also be pushed by the same air against an eventual
    fall, and, the device would work just as well. The reason is that, the force with which the air
    I would push the plates back (3), I wouldn't push the plane from the plates position (3), -like
    ] 5 It is logical - because they are not in direct contact with the plane. The plates (3) are in contact
    direct with the first pivot (6), which will cause the force that pushes you back, will push towards
    back to the first pivot (6), and, this, to the central axles (10) of the wheel (9). Now how does it happen
    that, on the second pivot of the left end of the wheel diameter (9), there is an axle (11) that is
    puts in contact with the wing (1), -in figure 4, or, which contacts the base of the cabin
    twenty (15) in Figure 1-, the force that pushes back the axles (10) of the wheel (9), will be seen
    compensated with the force that pushes the shaft (11) forward, which will push the wing (1) forward
    also, and, to the cabin (15), upwards. Therefore, we can say that this push scale (3
    8) Anti-fall will work just as well as the one I put behind the reactor, because the force
    backwards, -or, down-, that the dishes (3) will receive from the air, will go forward, -or, towards
    25 above-, and, with the same value, on the protector (8) of the second arm (7) of the thrust balance (3-8).
    In other words, the force that pushes down on the two central axes (10) of the wheel (9), is
    will be compensated by the force that pushes up on the shaft (11), which is directed towards it
    place where the central axes (10) push down. This will nullify the force that pushes towards
    down to the wheel (9), so that, now, the force of the two arms (S, 7) of the
    30 balance, in which one of them (5) will receive a downward air force of value (v), which of
    immediately it becomes that the second arm (7) will receive an upward force, of the same value
    (v), which will be applied on its end shield (8). To all this, I must now add a detail that
    It has all its importance. The force that will push back the two axles (10) of the wheel center
    (9), will be less than the force that will push the axle (11) forward, because this axle (11) is at the end of the wheel diameter (9), so that it will form a lever radius, so I can say that, there will be forward thrust gain on the shaft ( 1) with respect to the back thrust of the shafts (10), - which will be even better for the second arm (7) of the thrust balance (3 -8), because ea
    S force in lever radius of the shaft (11), shall be added to the forward force received by the guard (8), by the arm path (7) ... which, moreover, is also in radius of lever, because it will push on the end of the wing (1), as can be seen in figure # 1. This anti-fall push scale (3-8), will also be used for ships, because it will add push your propellers, or, to the engine they have installed. It will also be used for trucks, helicopters, submarines, and even for trains and cars ... It will be especially useful for formula-I cars, in which it is about increasing its speed and strength as much as possible. The great force that these formula-I cars develop can be used to redirect the force against the air, so that it pushes the car forward, which will increase its acceleration and speed much more.
    权利要求:
    Claims (1)
    [1]
    1) Helicopter with push scales, characterized by being an air craft in which, at the base of the cabin (15), we circle a set of push scales (3-8), in which their plates (3 ) are placed below the horizontal propellers (18), so that the second arm (7) of the balance will cause its protector (8) to be in contact with the base of the cabin (15); the thrust scales (3-8) rest their fulcrum on the pivot (6) of the right end of the diameter of a wheel (9), at whose left end it has a vertical axis (J 1) that rests on a protector (12 ) which is in contact with the base of the cabin (15); from the center of the wheel (9) two axles (10) start at the base of the cabin (J 5), which are fixed on said base; the fulcrum of the thrust balance (3-8) is, on this occasion, a hole in which the right pivot (6) of the wheel diameter (9) is introduced; The balance has two arms (5, 7) of different radii. The first arm (5) has a horizontal plate (3) at the end, and, is longer than the second arm (7); the second arm (7) bends towards artiba and has, at its end, a protector (8), which is in contact with the base of the cabin (15); next to it we put another push scale (3-8) located vertically, instead of being in a horizontal position, like the ones I have just described, in which, your plates (3) will be located horizontally; its second arm (7) will cause its protector (8) to contact a vertical plate that will have the cabin (15) in that
    place; at the same time, other push scales (3-8) will also be placed, in which the plates (3) will be placed vertically, and, the second arm (7, 8) is directed forward. 2) Helicopter with push scales, -according to first claim-, characterized in that it is another application of the push scales (3-8), which will now be located behind vertical propellers (13) that are placed on wings ( 1) sharpened in this helicopter; the plate (3) of the first arm (5) of the balance (4-8) is now placed vertically, so that it balances with the second arm (7), and, with its protector (8), which will be in contact with him at (1). 3) Helicopter with push scales, -according to first claim-, characterized in that it is a second application of the push scales (3-8) on the sharpened wings (J) of the helicopter; the fundamental elements of the push scale (3-8) are now the same, although several plates (3) are supported that rest on the same axis (4) that is connected to the first arm (5) of the balance (3-8), which serves as an anti-calda system; conical trunk-cylinders (2) are placed on the wings (1) of the helicopter, which focus the narrowing of the trunk-cone towards the plates (3) of the balance (4-8); the first arm (5) extends to the fulcrum hole, into which the first pivot (6) of the end of the diameter of a wheel (9) is introduced; as in the helicopter described above, this first pivot (6) is at the right end of the wheel diameter (9); at the left end, there is a second pivot in which a horizontal axis (11) is fixed, which extends, then, towards the wing (1), relying on a protector (12) that touches the wing (1), although it is not fixed to her; In the center of the two faces of the wheel (9), we place two horizontal axes (10), which are fixed to the central axis of the wheel (9) by one end, and, are fixed to the wing (1), by the other extreme; of the first pivot (6), the second arm (7) of the balance (4-8) is now extended, ending in a protector (8) that
    5 is not fixed to the wing (1), but only so in contact with it.
    18
     Figure 1
    Figure # 2
    Figure # 3
    1 3 2
    Figure # 4
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    同族专利:
    公开号 | 公开日
    ES2658763B1|2018-12-19|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    GB255936A|1925-04-28|1926-07-28|Harold Frederick Pitcairn|Improvements relating to aircraft|
    US1668052A|1927-05-17|1928-05-01|Davis Claud|Helicopter|
    法律状态:
    2018-12-19| FG2A| Definitive protection|Ref document number: 2658763 Country of ref document: ES Kind code of ref document: B1 Effective date: 20181219 |
    优先权:
    申请号 | 申请日 | 专利标题
    ES201600790A|ES2658763B1|2016-09-12|2016-09-12|Helicopter with push scales|ES201600790A| ES2658763B1|2016-09-12|2016-09-12|Helicopter with push scales|
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