• 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 anti-fall system for airplanes is formed by propellers (3) which, when moved by the air against the fall, will move to a gear train-cone (14-16) that, at the other end, will move the axis (5) and the propellers (6) that are inside a conical tube (4) that will take the plane (1) below, one on each side. At the exit of these conical tubes (4), we will place an oblique aileron (8), against which the accelerated air will impinge so that the plane (1) rises through the bow. (Machine-translation by Google Translate, not legally binding)
    公开号:ES2651726A1
    申请号:ES201600661
    申请日:2016-07-28
    公开日:2018-01-29
    发明作者:Fco. Javier Porras Vila
    申请人:Fco. Javier Porras Vila；
    IPC主号:
    专利说明:

    ANTI-CA IDE SYSTEM FOR AIRPLANE OR / J. INVENTION OBJECTIVE
    The main objective of the present invention is to prevent an airplane (1) from counting
    vertical due to eventual breakage of its molores. To prevent this, a system rounded by propellers (3) is installed which, upon receiving the air against the fall, will move to a train of cngranajcs-cone (14-16) which, in turn, will move to the axis (S) from the intcriordc a conical lube (4), which is full of propellers (6). Thus, the air will accelerate a lot, and. when exiting at the rear end, it will strike an aileron (8) located obliquely, which will raise the plane (1) by the bow.
    BACKGROUND OF THE INVENTION
    The main antecedent of this invention is found in my patent no. P20J200690, entitled: Affiliated aircraft stop system, with rear spoiler nozzle stop, in which an airplane was presented with anti-fall tubes like the one presented today. but, empty, without propellers (6) like the ones in this anti-calda system that I invented on the day (26.07.16). It also had a rear wing so that the air coming out of the tube, hitting its surface and allowing the plane (1) to rise up the bow. You can also consult my patent number P20 / 5 {) () 718. titled: Airplane with ollli-cooked tubes, with diaphragm and fin. t. As regards the gear-cone trcn (14 · 16), I have to cite my patent No. P201200419. titled: Fiu! rza multiplier gear and amount of rotation. And, also, my kick No. P2012 () () 498. titled: Bicycle and motorcycle CO II throttle gear. And, when it comes to the conical tube (4) with internal propellers (6), there are several antecedents in my patents, such as #: P201201076, entitled: Avió "COII engines and fins at the ends of the wings, in the that, in those engines, there were groups of propellers on the same axis. DESG'RIPCI6N DE Ul INVENCI6N
    The pam aviÓ "Allticaida System, is funded by a set of semicircular housings (2) located on the sides of an airplane (1). These housings (2) will be multiplied as much as possible according to the length of the fuselage. In figW "Only I have represented two of these housings (2), in whose interior SoC they place the anti-calda propellers (3) themselves, formed by the shaft and several blades, which is best seen in Figure 2. Below the plane we install, on each side, a conical tube (4) that extends from the bow to the stern, inside which there is a longitudinal axis (5) that runs through its center from end to end. Along this axis (5) we put propellers (6), and a few serrated teeth pinwheels (7). It is that the rotation of the annihilated propellers (3), - when the air against the fall, makes them rotate -, can move the propellers (6) of the inside of the conical tube (4), by means of a gear train-rono (14. 16) which is the one described in figW "a No. 2. This train (14-16) will be responsible for maintaining the fucr.la that is transmitted, at the same time. increasing in each gear-cone, the amount of rotation that can be transmitted by the crown (16), to the next piMn (14) The gear train-cone (14 ·
    16) is formed by two or four gears-collO, which have a piMn (14) and a crown (16) each, connected at a distance by metal rods (15). Between the crown (16) of a gear-cone, and, the pinion (14) of the next gear-cone, we put an intentional pinion (13). The last crown (17) of the last gear-cone will be engaged with a cogwheel
    s
    IS
    (18) of the same diameter as the piMn (14) of the cngranajcs * cone, which is located at the end of an axle (19) which, at the other end, has another cogwheel (20), of the same diameter as the pilkmcs (J 4). The last cogwheel (20) of this pair of wheels (J 8-20) will be engaged with the pin (7) that is fixed on the inner shaft (5) of the tube (4), which will be laterally serrated .
    DESCRIPTION OF THE FIGURES
    FIGURE 1: Lateral view] of an airplane in oC! that an anti-fall system installed by the propellers has been installed: i (3) that: receive the air against the fall, which will only move the gear / cone-gear train (14-16) shown in the figure n "2. This train (14-16) will be the one that moves the pinions (7) of the shaft (5) of the conical tube (4), causing the propellers (6) of its interior to spin at high speed.
    Fig. 2: Plan view of the mechanism that meshes the anti-fall propellers (3). with the gear-cone train (14-16), Y. which, on the other hand, meshes the last crown (17) of this train (14-16), with the sprockets (18-20) that will engage with the pinions (7) of the inner shaft
    (5) of the conical tube (4).
    Figures ,, "/ -2: 1) Airplane 2) Mobile protcceration housing 3) Propellers 4) Conical tube 5) Horizontal axis 6) Horizontal shaft propellers 7) Side-toothed ridge 8) Rear spoiler 9) Fixing and articulation axes 10) Electrohydraulic actuator coil {11) Electrohydraulic actuator arm 12) Crown 13) Intermediate PiMn 14) PiMn 15) Metal rods 16) Crown J7) Last Crown of the last En8ranaje-Cone 18) Cogwheel 19) Shaft 20) Cogwheel
    DESCRIPTION OF A PREFERRED EMBODIMENT
    The alicaim system for aviim, is cac'l.lclerizado for being a system in which, when the air against the fall falls against the propellers (3), they will move the crown (12) they have in the e: - .1 row of its axis, and, this oorona (12) will start the gear train-cone (14-16), which will be the one that, in turn, moves to the pair of wheels (18-20) that engage with the pins (7) of the shaft (5) of the conical tube (4), the air entering this tube (4). it will be accelerated by all the propellers that it has in its intentor, and it will come out with a lot of fucrola through the opening of smaller diameter that will be at the rear end of the tube (4), so that this air very accelerated by the propellers, will strike against a spoiler (8) located in an oblique position in front of the exit, which will cause the aircraft (1) to rise up the bow, at the same time as a VC'I: is stabilized, the spoiler (8) will depart, and , let the air that comes out of the conical tube (4), serve as a thrust for the plane (1), which he did. to keep it in flight, without falling by its own weight. There are, therefore, in this anti-calda system, five mechanisms to accelerate the air entering the tube (4). VIlO of them is c1lrcn of gear-cone (14.16) that will make its last wheels spin at high speed ... What will make the propellers (6) of the tube-tube (4) also spin at high speed. The second mechanism is the conical tube (4) itself, whose fonna will cause the air to "gradually become compressed" every "C", which will function as a hose, which will accelerate the fluid that reconnects its inside because it will have to come out in the same amount per second because it will be pushed from behind by the fluid that continues to quote in the tube (4), and, since it cannot come out all at once because the tube (4) has narrowed, He has no choice but to accelerate his departure, leaving in an m ('' Second time. The third mechanism will be the multiplication of the number of propellers (3) and gear-cone trains (14-16) that we put on the plane (1 ), because, the more we multiply them, the propellers (7) inside the conical tube
    (4) they will turn with more force, and, faster. which will accelerate even more to the air. There would also be a fourth air acceleration mechanism that refers to the multiplication of the propellers (7) inside the tube (4). Each propeller (7) C11 will send to the next propeller (7) a more accelerated air, so that, "tc air. All to reach the last propeller (7) of the cje (5), will be much more accelerated than when entering in the conical tube (4), which will increase its outside and its energy, the multiplication of the number of cone-gears that we put on each train (14 · 16) will also influence the acceleration of the air, because, the more pieces of eng : ranajes-cone we put in each train (14 · 16), the greater the amount of rotation that will transmit the last crown (17) of the train (14-16) to the pair of wheels (18-20), 10 that will make the rotation of the shaft (5) inside the tube (4) is also greater.
    I will perform. now. a minimum estimate of the pressure that the air can have at the outlet of the tube (4). This Toral Pressure will be the sum of three Partial Pressures. The first will be the Pressure that prints the PesQ of the Plane (1) when it falls, on the air / liosa that enters the tube (4). The second will be the one that / Jelices, · moved by the train of cngranajcs-cone (14-16) -. they contribute to that same Alosa of air. And, the third, will be the one imposed by the ESlreclramielllo del Tubo
    (4) at the rear exit. This situation YES ~ can express in an equation:
    in which, the last one adding, we "will assume it as a multiple of the sum of the other two addends because we do not know exactly the concrete measures of the Narrowing of the Tube (4). What we know is that it can multiply, approximately by five the Pre!,; ón of the air
    which reaches the outlet of this tube (4), because it will function as the outlet cone of a hose, with which we can say that it will be eplied.
    5 Cakulwi separately the two addends. The first sum will be, -for a large aircraft of 300,000 Newtons of Weight-, and, a tube of 3
    W ,,,,, "= 300,000 N = 42,402'83 N I m '
    diameters meters:
    S 7'075., '
    T '"
    Adding scglmdo is more elaborated because we must first find the value of the Fue / z that the propellers could print to the air that has already entered with a given Pressure, caused by the Weight of the Plane (1) in the previous swnando. In that Fuena the force and the
    amount of rotation that the gear-cone train (14-1 6) brings to the propellers (6).
    The surface of the tube (4) will be:
    Y. The approximate Fuena of the Propellers, - since we do not know exactly its Number, nor the number of coo-gears that we will put on the train (14-16) -, will have to start from the calculation of the 15 Mass of air that enters the tube (4), which we assume to measure about 50 meters: m = V · "= (S · /) ·" = (7'075 m '· 50m) · 1'29kgl m' = 456'34 kg
    If, on the axis (5), we put a set of propellers (6) on each meter of its length, then we will put 50 propellers that will accelerate the air that enters the tube (4), at least, I meter per
    according to squared: F == m · a == 456'34kg. 1mI S 2 == 456'34 N 20 So, the second by adding c ~. and, prepared:
    J ~ liliou == 456'34 N = 64'5 N I m2ST.,. 7'075 m '
    What we can apply in the starting equation:
    P = 5. [300,000 N + 456'34 N '] = , Too.J 7'075 ", 2 7'075 m2
    = 5 [42'402'83 + 64'5] = 5. 42.467'33 = 212.336'63 NI m '25 10 which supposes a pressure more than enough to push the plane hard (1) when its molars are not functioning, especially when we take into account the usual thrust of only one of the engines of lltJl plane, which is usually at least 25,000
    IIewtOI / $.
    The calculation, perhaps, could exaggerate a little IIC the Acceleration that the Propellers (6) print at 30 Air, which could be less than 1 meter per second squared. And, I could also exaggerate a
    little in the number of times that ~ multiply the two addends in the Strait of the Tube. What could it be. just. 3 times, instead of 5 times. Taking into account these two examinations, the result could be a little less ... as it is:
    F = m 'Q = 456'34kg. 0'5 mi s' = 228'17 N
    P _ 3. [300,000 N + 228'17 N] _
    ~ -T <H "I -7'075 m 2 7'075 m 2 _
    = 3 [42'402'83 + 32'25] = 3. 42.435'08 = 127.305'24 NI m 'which is only a little more than half of the cal (; above, in which we continue to observe that it would still be able to compete with the usual reactors of an airplane, when they have a fUCí .the 10 of only 25,000 "ewtolls.
    权利要求:
    Claims (1)
    [1]
      /) Sisl ~ mQ anticaido for airplane, characterized by a set of carca.'I3S semicircuJares (2)
    located .. on both sides of a plane (J); inside these can: a. <;; semicircular IS (2),
    they surround propellers (3) with rectangular blades, whose long edge is parallel to the axis; to
    5 on each side of the plane and in its area, a swap tube (4) is installed, which has a longitudinal axis (5) inside it that runs through its center from the bow to the stern; along this axis (5) we put hclices (6). and, laterally serrated pins (7); the anti-fall propellers (3), are connected to the propellers (6) inside the conical tube (4), by means of the JC-cone crankshaft train (14-16); The gear-cone train (14-16) is formed. at least for
    10 four gears! L-eono, shaped by a pillion (14) and a crown (16) each, joined at a distance by a few metal rods (1 5); We put an intermediate pinion (13) between the crown (16) of a gear-cone. Y. the pinion (14) of the following gear-cone: the last crown (17) of the last gear-cone. It is geared with a pinion (IR) that is the same as the pinion (14) of the cone gears. located at the end of an axis (19) which, at the other end, has another fixed
    15 pii'lón (20), same. also, to the plí100es (14); The last gearwheel (20) of this pair of wheels (18-20) is engaged with the pioon (7) which is fixed in the inner part (5) of the tube (4), which conforms laterally toothed.
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    同族专利:
    公开号 | 公开日
    ES2651726B1|2018-12-17|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    ES2322738A1|2007-03-23|2009-06-25|Fco. Javier Porras Vila|Anti-fall helix, for aircraft |
    ES2446842A2|2012-04-11|2014-03-10|Fº JAVIER PORRAS VILA|Gear multiplier force and amount of rotation |
    ES2439141A2|2012-07-17|2014-01-21|Fº JAVIER PORRAS VILA|Anti-fall propellers with fins and wedges, for autonomous space shuttle |
    ES2457717A1|2012-10-16|2014-04-28|Fº JAVIER PORRAS VILA|Plane with engines and fins on the ends of the wings |
    ES2558031A1|2014-08-01|2016-02-01|Fº JAVIER PORRAS VILA|Anti-fall plane system with tooth wheels in perpendicular lever radius |
    法律状态:
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