• 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 propellers with ring of micropalas in lever radius, are the mechanism of push of an airplane, helicopter, ship, submarine, etc ..., which is formed by four or six blades (2) of propellers, at the end of which, in lever radius, is placed a ring formed by two concentric circular axes (3, 4), so that, between them, we put a set of micropacks (5) that have an angle of thirty-six degrees with respect to the plane of the blades (2) of the propellers. (Machine-translation by Google Translate, not legally binding)
    公开号:ES2546738A1
    申请号:ES201400244
    申请日:2014-03-28
    公开日:2015-09-28
    发明作者:Fº JAVIER PORRAS VILA
    申请人:Fº JAVIER PORRAS VILA；
    IPC主号:
    专利说明:

    DESCRIPTION
    Propellers with microblade ring on lever radius. Object of the invention
    The main objective of the present invention is to take advantage of the qualities of the Archimedean Principle of the Lever Radius, to add more Force to the thrust of the Propellers of an Airplane, Boat, Submarine, Helicopter, etc., while, in these Propellers, we have to multiply the Force of these Microblades (5), by the Radius of the Blade (2) at whose end they are, and, the result must be added to the Force of the thrust of the other Blades (2) of the Propellers. Background of the invention
    The main antecedent of this invention is constituted by the hoop with micro-blades at the ends of the propellers of the inventor named Daniel Reed, from Eagle Lake of Minnesota, invention presented in August of (1897), and entitled: Air Ship. The fundamental difference between this invention and mine is that the Microblades {5) of the Ring, in my invention, present an angle of thirty-six degrees with respect to the plane of the Blades {2) of the Propellers, while, in their In the invention, the Microblades have an angle of ninety degrees with respect to the same plane of the Blades, -that is, with respect to the plane of rotation of the Propellers -. This difference is fundamental insofar as it means that its Microblades cannot push an Airplane forward, although they could push a Ship if they are placed with the plane of the Ring in the same direction as the Ship's advance, as occurs in the typical and well-known New Orleans Ship.
    The mission of the Microblades (5) of my invention is very different, -even in spite of the similarity of the shape-, since it tries to push an Airplane forward when the plane of the Propellers is located perpendicular to the direction of the Advance of the Airplane, and, for that, the Microblades (5) form said angle of thirty-six degrees with respect to the plane of the Blades or with respect to the plane of the circle of this Ring.
    The second antecedent is the invention of BJ Paulson, presented in the United States of America in March (1944), and, entitled: Thrust Ringfor propellers, in which some Propeller Blades are presented that present a Ring at the end in the one with small buckets that rotate with the blades. Description of the invention
    The propellers with a micro-bladed ring on a lever radius are the push mechanism of an Airplane, Helicopter, Boat, etc ... The Blades (2) of the Propellers are located around the Rotation Axis (1) of the Engine, in whose anterior end forms a Cone. At the ends of said Propellers (2), -and, located at Lever Radius-, there is a Ring formed by two Circular Shafts (3, 4) between which we place a set of Helix Microblades (5) that present an angle thirty-six degrees with respect to the vertical plane of the rotation of the Blades (2). Date of the invention: (02.27.13).
    2 Description of the figures
    Figure nº 1: Front view of the Blades (2) of the Propellers located around the Axis of Rotation
    (1) of the Engine, which have, at the ends of said Propellers (2), a Ring formed by two Circular Shafts (3, 4) between which we put a set of Propeller Microblades (5) in Lever Radius.
    Figure No. 1:
    1) Cone of the front end of the Rotation Axis
    2) Propeller Blades
    3) Inner circular axis
    4) Outer circular shaft
    5) Micro-propeller blades Description of a preferred embodiment
    Propellers with a micro-blade ring on a lever radius are characterized by being the mechanism that exerts the push work of an Airplane, Boat, Helicopter, etc ... that has some Propeller Blades (2) located around the Axis of Rotation. (1) of the Engine. At the ends of said Propellers (2), there is a Ring formed by two Circular Shafts (3, 4) between which we put, in Lever Radius, a set of Propeller Microblades (5) that also have the mission to push the Airplane, with the practical advantage that, being located at the end of the Blades (2), they take advantage of the qualities of the Archimedean Principle to add much more Force to the push, while, in this device, the Force own of this Microblades (5), we have to multiply it by the Radius of the Blade (2) at whose end are the Microblades (5), and this result must be added to the force of the thrust of the other Blades (2) of the Propellers.
    3
    权利要求:
    Claims (1)
    [1]
    1. Propellers with a micro-blade ring on a lever radius, characterized by being the push mechanism of an airplane, helicopter, ship, etc ... The blades (2) of the propellers
    5 are located around the axis of rotation (1), which forms a cone at the front end. At the ends of said propellers (2), there is a ring formed by two circular shafts (3, 4) between which we place, in lever radius, a set of propeller micro-blades (5) that present an angle of thirty-six degrees with respect to the vertical plane of the blades (2).
    4
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    同族专利:
    公开号 | 公开日
    ES2546738B1|2016-08-09|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    ES2647371A1|2016-06-21|2017-12-21|Fº JAVIER PORRAS VILA|Wedges for the hoop of the propellers of a helicopter |
    ES2655248A1|2016-08-19|2018-02-19|Fco. Javier Porras Vila|Microplate ring for helicopter propellers |
    法律状态:
    2016-08-09| FG2A| Definitive protection|Ref document number: 2546738 Country of ref document: ES Kind code of ref document: B1 Effective date: 20160809 |
    优先权:
    申请号 | 申请日 | 专利标题
    ES201400244A|ES2546738B1|2014-03-28|2014-03-28|Propellers with micropallet ring in lever radius|ES201400244A| ES2546738B1|2014-03-28|2014-03-28|Propellers with micropallet ring in lever radius|
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