• 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 shuttle in radio of lever for airplanes, is a platform (2) that slides with its metallic wheels by rails (1), moved by its electrical motors (3) with propellers (4) that will be located in the lateral ends of the platform (2). At its center we will put the plane (5), which will be accelerated, -to the platform (2) -, until the takeoff speed, at which time the plane (5) will only have to accelerate its engines to the maximum .., and, raise the ailerons. In this way, we achieve a good fuel saving, and a considerable increase in take-off safety, since this is usually the most dangerous process in the entire journey of an airplane. (Machine-translation by Google Translate, not legally binding)
    公开号:ES2624628A1
    申请号:ES201600069
    申请日:2016-01-15
    公开日:2017-07-17
    发明作者:Fº JAVIER PORRAS VILA
    申请人:Fº JAVIER PORRAS VILA；
    IPC主号:
    专利说明:

    Shuttle radio lever for aircraft. Object of the invention
    The main objective of the present invention is to accelerate aircraft (5), saving fuel on the one hand, and, increasing the safety of take-off. This is achieved by placing the Plane (5) on a Platform (2), -which has Engines (3) and Propellers (4) located in Lever Radius at the lateral ends of the Platform (2) -, to which we will accelerate on some Rails (1), until you reach the Takeoff Speed, at which time, the Airplane (5), you will only have to accelerate your Engines to the maximum, -to which you kept idling until that moment-, and, raise the ailerons Background of the invention
    The main antecedent of the present invention is found in the Archimedes Principle of the Lever, whereby the Force that is applied at the end of the Lever, increases in direct proportion with the increase in the length of the Radius. On this occasion, the Force we are trying to increase is that of the Motors (3) that we place in a certain Lever Radius, at the lateral ends of a Platform (5) that slides along Rails (1). The second antecedent to highlight is referred to my Airplanes with Motors in Radio de Palanca, one of whose examples already published is in my Patent nº: P2501400259, entitled: Airplane with groups of alleles above and below the fuselage, and, of the wings, in which the Motors are also at the ends of the wings. The third background to highlight is also found in another of my published Patents, which refers to Propellers with Fins Boxes located at the ends of the Blades, which we also include in the present invention. This is my Patent No. P201400244, entitled: Propellers with micropallet ring in lever radius. Description of the invention
    The shuttle in lever radius for airplanes, is a structure to accelerate Airplanes (5), which is formed by three parallel Rails (1), on which we place a Platform (2) that extends beyond the wings of the Airplane ( 5). The Platform (2) has wheels that can be metallic, like those of a train, or, of rubber. When the Plane (5) is placed on the Platform (2) in the take-off position, some Axes moved by Electrohydraulic Actuators, will be raised and placed behind the Wheels of the Plane (5), so that the Plane (5) goes to be pushed forward when the Platform begins to accelerate, moved by the Propellers (4). These propellers, at the ends of the blades, will have a box, open at its front and rear ends, and, inside which they will have a group of parallel fins that will be tilted forward about ten degrees. With these Fins, the Propellers will have more thrust forward. At each end of the Platform (2) we will raise a metal structure twelve meters high, in which we will fix, - one on top of the other -, to two Electric Motors (3), with Propellers (4) of three, Four or six meters. Date of the invention: (15.01.16). Description of the figures
    Figure 1: Plan view of an Airplane (5) located in the center of the Platform (2) of the Shuttle that slides along Rails (1). The Plane (5) is prepared to be accelerated by the Engines (3) with Propellers (4) of the Platform (2), which are located at its lateral ends, forming a Lever Radius.
    Figure 1:
    1) Rails
    2) Platform
    3) Electric motor
    4) Propellers
    5) Plane Description of a preferred embodiment
    The shuttle in lever radius for airplanes, is characterized by being a Platform (2) with metal or rubber wheels, which will slide along three Rails (1) located on the takeoff runway. The Electric Motors (3) with Propellers (4) that we will put on the lateral ends of the Platform (2), higher than the wings of the Plane (5), will be in charge of pushing the Plane (5) with the Force or the Push which will provide you with the Motor Lever Radio Distance (3), to the center of the Platform (2), where we place the Plane (5). We have to understand that an Airplane (5) is the same as a Balance with two arms, which, instead of moving up or down, move to the right or to the left. At the ends of these arms, -wings be-, there will be no Plates to hold a Weight, -like a Balance-, but, in them we will put the Aircraft Engines because, in this position, the larger the Radius of Lever, the greater the Push Force of these Motors. It is also silly that the Weight of these Engines will also increase depending on that Lever Radius, but, the increase in Push Force will be much greater than the increase in Weight. By multiplying the two concepts, -the Weight of the Motors, and, the concept of its Pushing Force-, by the Distance of the Lever Radius, we obtain two values that, later, we will have to subtract from each other, because the Push Force is directed forward, and, the Air Force Weight is directed down. If the Plane took off in Vertical, said Subtraction of the two concepts would be pure, because one Force would direct it upwards, and, the other downwards, and, there would be no reason to divide one concept by the other because nothing is there that divides the Force in Lever Radius that pushes up. There is only one thing that, when directed in the opposite direction, - downwards -, will be subtracted from it, and, it will be the Force of the Weight, which is directed downwards, that will be subtracted from the Force of the Engines of the vertical take-off, directed upwards. In the case of the Plane taking off in Horizontal, it is still better for the result of the Subtraction because it would not be necessary to subtract the entire Weight of the Airplane from the Force in Motor Lever Radio (3), but, only, we would have to subtract one (15%) of this Weight. As is known, the Force that is required of the Engines of an Airplane does not need to exceed (15%) of the Weight of the Airplane, and, therefore, when performing the Subtraction of the two concepts, -Push Force on Radio Lever , and, Weight Strength-, we will only have to perform this
    As we know from Archimedes, the Strength of a Lever increases in direct proportion to the Radius, which also means that, as we see in a Roman Balance, for example, the Weight we put on one end of the axis , will increase in every centimeter, and, not only in every meter. Therefore, the Force of the Propellers (4) of these Motors (3) located in Radio de Palanca, will also increase in sludge and each of the centimeters that measure the length between the Plane (5) located in the center of the Platform (2), and, the Motors (3) located at its lateral ends ... which determines a very high Force value when the value of the isolated Push of each Motor, -without Lever Radius-, is, so only, of a metric ton.
    If each Engine (3) is located (40) meters from the Plane (5), its Force in Lever Radio will be:
    And, as we have put four Engines (3) and four Propellers (4), this Force will have to be multiplied by four as well, which offers a result of (16,000) Metric Tons of Push ..., which will be more than enough to move and accelerate any Airplane (5), whose Weight does not usually exceed the (150) Metric tons. In this case, we will not have to subtract the Weight in Motor Lever Radius (3), because they have Wheels below, and, their Weight does not affect the Weight of the Plane (5), which means that it would not be the same is the weight that increases in the engines that we place at the ends of the wings of an airplane (5), than the weight of the engines (3) of this platform
    (2) that it has wheels that slide along Rails (1) located on the ground, and, that are, exactly, below the Motors (3).
    权利要求:
    Claims (2)
    [1]
    1. Shuttle in lever radius for airplanes, characterized by being a structure formed by three parallel rails (1), on which we place a platform (2) that extends beyond the wings of the plane (5). The platform (2) has metal wheels. Behind the wheels of the plane (5), vertical shafts activated by electro-hydraulic actuators will be located on the platform (2). At the ends of their blades, the propellers (4) will have a small box, open at its front and rear ends, and, inside which they will have a group of parallel fins that will be tilted forward twelve degrees. In each
    10 end of the platform (2) will raise a metal structure of twelve meters high, in which two electric motors (3), with beams (4) six meters in diameter will be fixed, one above the other. .
    [2]
    2. Lever radio shuttle for aircraft, according to claim one,
    15 characterized by being a variant for the wheels of the platform (2), which, on this occasion, instead of being metallic, will be made of rubber.
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    同族专利:
    公开号 | 公开日
    ES2624628B1|2018-04-30|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    GB131650A|
    GB470767A|1936-02-20|1937-08-20|Nicholas Sandor|Improvements in electromagnetic machines with longitudinally moving armatures|
    US20050082424A1|2003-10-20|2005-04-21|Masatada Yamamoto|Flying vehicle-launching apparatus and method|
    DE102005004717A1|2005-02-02|2006-08-10|Hörnicke, Christian|Platform-based runway system for aircraft, has mobile platform that is adjusted and moved according to movement and actual flight phase of starting/landing aircraft , accelerating aircraft while starting, and decelerating landing aircraft|
    WO2013175128A1|2012-05-24|2013-11-28|Steinbrucker Michel|Assisted take‑off and landing system for aircraft using a self-propelled platform|
    法律状态:
    2018-04-30| FG2A| Definitive protection|Ref document number: 2624628 Country of ref document: ES Kind code of ref document: B1 Effective date: 20180430 |
    优先权:
    申请号 | 申请日 | 专利标题
    ES201600069A|ES2624628B1|2016-01-15|2016-01-15|Lever radio shuttle for aircraft|ES201600069A| ES2624628B1|2016-01-15|2016-01-15|Lever radio shuttle for aircraft|
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