• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
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  • 优先权
    • 专利摘要:
    The helicopter with crown and fins, is a vertical take-off craft whose cabin (1) has the shape of a gaussian bell, and, at its ends, it has groups of fins (4) that connect one wing (2) to the other. Top of the cabin (1). Underneath the cabin floor (1) are the horizontal propellers (13), which have their axis of rotation in the center of a crown (16), which has the same diameter as the horizontal propellers (13). This crown (16) is connected to the pinion (14) of the axis of the vertical helices (15) located in the rear area of the crown (16). An engine (5), -in the anterior area of the crown (16) -, connects its cogwheel (6) with a gear train-cone (8, 9, 10, 11), which, on the other end, connects its last crown (11), with the cogwheel of the axis of the horizontal propellers (13). (Machine-translation by Google Translate, not legally binding)
    公开号:ES2586727A1
    申请号:ES201500335
    申请日:2015-04-14
    公开日:2016-10-18
    发明作者:Fº JAVIER PORRAS VILA
    申请人:Fº JAVIER PORRAS VILA；
    IPC主号:
    专利说明:

    HELICOPTER WITH GREAT CROWN AND ORIENTING FINS OF THE INVENTION The main objective of the present invention is to greatly increase the usual speed of a helicopter °, which is achieved with the gear of this great Crown (16) and the 5 Pinon (14 ) of the Axis of Vertical Helices (15), because the great perimeter of the Crown (16) will spin this Pifion (14) many times. At the same time, the Fin Groups (4) will grant greater stability to the Helicopter ° because, being located in Radio de Palanca, - according to the well-known Archimedes Principle-, the Sustaining Force will increase in direct proportion to the length of the Radius which are located, which will be the same as that of the Horizontal Propeller Blades (13). With these two objectives, flight safety will be greatly increased. BACKGROUND OF THE INVENTION The main antecedent of the present invention is found in several previous patents of mine. The first refers to the Groups of Fins (4, 17) of the ends of the Blades 15 of the Helices (13, 15) already presented in Patent No. P201201076, entitled: Avian with motors and fins at the ends of the wings It is also presented in my other Patent No. P201200932, entitled: Anti-falling propellers with fins and cuPias for an autanomo space shuttle. The third patent is No. P201200764, entitled: Avian wings with stabilizer tubes. The fourth is Patent No. P201200913, entitled: Arm fins of 20 perpendicular lever, for the ends of the wings of an airplane. The fifth is Patent No. P201200934, entitled: Helicopter and Avian Helices with groups of fins. The sixth Patent, refers to the Gear Train-Cone (8, 9, 10, 11) found in ml Patent No. P201200419, entitled: Gear multiplier of force and amount of rotation, which is also found in my Other Patent No. P201200498, entitled: Bicycle and motorcycle with 25 throttle gear. In the present invention, these inventions contribute to improving and perfecting the performance of the Helicopter in which they are installed. DESCRIPTION OF THE INVENTION The Helicopter with a crown and fins, is a vertical take-off ship whose most significant element is the great Crown (16) that it carries in its lower zone, which has the mission of 30 to make the Niko take many turns (14) with the one in connection, which is installed in the axis of the rear propellers (15, 17). These Helices (15, 17) have a Group of Fins (17) at the ends. The presence of these Fins (17) at the ends of the Palm, implies that the Force that they determine when turning against the wind, becomes a Force in Lever Radius that increases with the Length of the Blades of those Vertical Helices 35 ( fifteen). These Fins (17), as well as the Fins (4) of the ends of the Cab (1), are
    inclined upwards, by its previous end, about twelve degrees. In the very center of the great Crown (16), whose diameter it will be. only five centimeters smaller than that of its Horizontal Propellers (13) -, the Axis with Cogwheel (12) of the Horizontal Propellers (13) is placed, which also have a Group of Fins (17) at the end of their Blades. These Fin Groups (17) are joined together by means of a Circular Guide (18).
    An Electric Motor (5), by rotating its Cogwheel (6), -which is located in the anterior area of the Crown's perimeter (16), and, at the same time, through the upper part of the Crown-, engages on the other hand, to its Cogwheel (6), with an Intermediate Wheel (7) that is geared, in turn, -by the other side-, with the Pinion (8) of a Gear-Cone (8, 9, 10) formed by a Pinion (8) and a Crown (10) that are joined at a distance by some Metal Rods (9). This Gear-Cone (8, 9, 10) is the first of a Cog Gear Train (8, 9, 10), in which the Crown (10) of each Gear-Cone (8, 9, 10) is engaged, with the Pinion (8) of the Gear-Cone (8, 9, 10) next. The last Crown (11) of the last Gear-Cone (8, 9, 11) of the Train, meshes with the Cogwheel (12) of the Horizontal Axis of the Horizontal Propellers (13). This Gear-Cone Train will increase the Force applied by the Motor (5) and the amount of rotation it can offer to its Horizontal Propellers (13). The Horizontal Propellers (13) and the Vertical Propellers (15) rotate in opposite directions. To compensate for the tendency to turn the Cabin (1) in a circle, as a result of the rotation of the two Propellers (13, 15), two Tubes will be added, below the Horizontal Propellers (13), -one on each side of the perimeter of the Propellers (13) -, which, at the front end, -opened up-, will receive the Air that these Propellers descend (13), and, by the rear end of the Tube, they will divert it to the outside, or that is, in the opposite direction to the tendency towards the lateral rotation of the Cab (1). It is, therefore, a Tube, -not drawn in the figures-, which bends up the front end, and, to the side, the rear end. It only remains to add that the shape of the Cockpit (1) of this Helicopter, seen from the front, looks like a Gaussian bell, -the figure of the German mathematician's Statistics-, and, at its lateral ends, it also has a Fin Group (4), which extend to the rear end of the helicopter, and, two Drift Rudders (3). Under the floor of the Cab (1) all the components described here are placed. Above the Cab (1) extends a Wing (2), which connects the two Fin Groups (4). Date of the invention: (10.04.15).
    DESCRIPTION OF THE FIGURES
    Figure 1: Front view of the Helicopter, which shows the position of the Great Crown (16) at the base of the Cab (1), and, below it, has the Horizontal Propellers (13) that serve to take off vertical. At the ends of the Cab (1) there are two Groups of
    Fins (4) with a Drift Rudder (3) for its upper zone. A wing (2) extends between the two groups of fins (4). Figure # 2: Plan view of the mechanism that forms the great Crown (16), with the Pinion
    (14) located on the Axis of Vertical Propellers (15), which show a Group of Fins
    (17) at the ends of their Blades, as they have, also, the ends of the Horizontal Propeller Blades (13). An Electric Motor (5) connects its Cogwheel (6), with the Crown (16) through the upper area of this Crown (16). At the same time, the Wheel
    (6) of the Motor (5) is connected to an Intermediate Wheel (7) which, in turn, contacts the Pinion (8) of the first Gear-Cone (8,9, 10) of a Gear Train- Cone (8, 9, 10, 11) whose last Crown (11) meshes with the Cogwheel (12) of the Horizontal Propeller Shaft (13).
    Figure 1-2:
    1) Cab 2) Upper wing 3) Drift rudder 4) Fin groups 5) Electric or fuel motor 6) Cogwheel 7) Intermediate gearwheel 8) Pinion 9) Metal rods 10) Crown 11) Crown with oblique teeth 12 ) Cogwheel with oblique teeth 13) Horizontal propellers 14) Sprocket of vertical propellers 15) Vertical propellers 16) Crown 17) Fin groups 18) Guide for fixing fin groups
    DESCRIPTION OF A PREFERRED EMBODIMENT
    The helicopter with crown and fins, is characterized by being a vertical takeoff ship, whose main quality is that, with its large Crown (16), for every turn that it turns, the Pinion (14) of the Vertical Propellers (15) that are responsible for the advance of the ship, in total absence of friction could turn about a hundred turns. And, like, in a second,
    the Horizontal Propellers of a Helicopter can rotate at least three times, this means that the Pinion (14), -in ideal conditions, I insist-, would rotate three hundred turns per second. In this way a great forward speed is ensured, which ensures, at the same time, a much safer vertical takeoff, because, at the same time as it rises, the spacecraft advances very quickly. If the Horizontal Propellers (13) have a Diameter of eleven meters, their Perimeter will be (34'56). If we make the Perimeter of the Wheel (14) of the Vertical Propellers have eleven centimeters, its Perimeter will be (34'56) centimeters, which is one hundred times smaller than that of the Crown (16). At the same time, the Gear Train-Cone (8-11), will be responsible for increasing, not only the Force of the Motor (5), but, at the same time, also the amount of rotation that the last Crown (11 ), may transmit to the Cogwheel (12) of the Horizontal Propeller Shaft (13), which means that the latter will not only rotate three times per second, but will do so more times, so that the Pinion (14) of the Vertical Propellers (15), you can still turn many more laps than the three hundred laps I've calculated before. To all this, the great safety that can be achieved in flight is added, not only because of the increase in speed that ensures lift, but also because of the presence of the Fin Groups (4) that the Cab (1 ) has both ends. Moreover, the Fin Groups (17) that we put on the ends of the Propeller Blades (13, 15) ensure a higher index of air penetrability, which further increases the forward speed, as well as the force and the vertical take-off speed, which also results in the safety of the ship.
    权利要求:
    Claims (1)
    [1]
      1) Helicopter with crown and fins, characterized by being a vertical takeoff ship whose most significant element is the large Crown (16) that it carries in its lower zone, which is in connection with the Pinion (14) that is installed in the Shaft of the rear propellers (15, 17). These propellers (15, 17) have a group of fins (17) at the ends. These Fins (17), - as well as the Fins (4) of the ends of the Cab (1) -, are tilted upwards, by their front end, about twelve degrees. In the same center of the great Crown (16), - whose Diameter will be only five centimeters smaller than that of its Horizontal Propellers (13) -, the Axis with Cogwheel (12) of the Horizontal Propellers (13) is placed, which They also have a Fin Group (17) at the end of their Blades. These Fin Groups (17) are joined together by means of a Circular Guide (18). An Electric Motor (5), connects its Cogwheel (6) with the Crown (16), and, is located in the anterior area of the Crown's perimeter (16), and, at the same time, through the upper zone Of the same. On the other hand, this Cogwheel (6), is geared with an Intermediate Wheel (7), which is in turn, -by the other side-, with the Pinion (8) of a Gear-Cone (8, 9, 10) formed by a Pinion (8) and a Crown (10) that are joined at a distance by some Metal Rods (9).
    This Gear-Cone (8, 9, 10) is the first of a Gear-Cone Train (8, 9, 10,
    11), in which the Crown (10) of each Gear-Cone (8, 9, 10) is engaged, with the Pinion
    (8) of the Gear-Cone (8, 9, 10) below. The last Crown (11) of the last Gear-Cone (8, 9, 11) of the Train, has oblique teeth and meshes with the Cogwheel (12) of the Horizontal Axis of the Horizontal Propellers (13), which also has them oblique . The Horizontal Propellers (13) and the Vertical Propellers (15) rotate in opposite directions. Two Tubes are added, below the Horizontal Propellers (13), - one on each side of the perimeter of the Propellers (13) -, which have the front end open upwards, - towards the Propellers (13) -, and, Its rear end bends to the side. The shape of the Cockpit (1) of this Helicopter, seen frontally, resembles the statistical figure of a Gaussian bell, and, at its lateral ends, also has a Group of Fins (4), which extend to the rear end of the helicopter-, and, two Drift Rudders (3). Under the floor of the Cab
    (one) all the components described here are located. Above the Cab (1) extends a Wing (2), which connects the two Fin Groups (4).
    1 2
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    同族专利:
    公开号 | 公开日
    ES2586727B1|2017-08-07|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    ES2680646A1|2017-03-10|2018-09-10|Francisco Javier Porras Vila|Helicopter with four gear trains-double-cone |
    法律状态:
    2017-08-07| FG2A| Definitive protection|Ref document number: 2586727 Country of ref document: ES Kind code of ref document: B1 Effective date: 20170807 |
    优先权:
    申请号 | 申请日 | 专利标题
    ES201500335A|ES2586727B1|2015-04-14|2015-04-14|Helicopter with large crown and fins|ES201500335A| ES2586727B1|2015-04-14|2015-04-14|Helicopter with large crown and fins|
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