专利摘要:
The gear train-cone in the aircraft-launcher engine of an aircraft carrier, is a mechanism that can increase the force and the amount of rotation of the cylinder (2) that winds the rope (3) responsible for dragging and accelerating an aircraft -ship (5) of those who go on an aircraft carrier (1). The mechanism is formed by two or more gears-cone (8-10), formed by a pinion (8) and a crown (10), connected at a distance by metal rods (9). We connect the pinion (8) of a gear-cone, with the crown (10) of the next gear-cone, and so on. The train that we form with these gear-cone (8-10), we connect it, by one end, to the gear wheel of the motor (6), and, on the other side, to the pinion (12) of the cylinder axis (2). (Machine-translation by Google Translate, not legally binding)
公开号:ES2657050A1
申请号:ES201600745
申请日:2016-08-30
公开日:2018-03-01
发明作者:Fco. Javier Porras Vila
申请人:Fco. Javier Porras Vila;
IPC主号:
专利说明:

 GEAR-CONE TRAIN IN THE LAUNCHES-A VIONES ENGINE OF AN AIRCRAFT OBJECTIVE OF THE / NVENC / 6N The main objective of the present invention is to accelerate with greater force and with greater speed to the planes (5) that take off from an aircraft carrier (1), which can be achieved by adding a gear-cone train (8-10) between the gearwheel (7) of the engine (6), and, the pinion (12) of the cylinder (2) where the rope (3) that pushes and drags the plane (5) is wound, by means of its drag axis (4). BACKGROUND OF THE / NVENC / 6N 10 The main antecedent of my invention of the day (27.08.16), is found in some of my previous patents, such as, for example, in P201200374, entitled: Swing toy with spirals, which featured the gear-cone train (8-10), which doubled in two, to move the rear wheels of a toy car. In the present invention, the gear-cone train (8-10), has the mission of accelerating as much as possible to a fighter plane of those traveling in an aircraft carrier, while 15 that can increase the original force of the engine, at the same time it can increase, at the same time, the amount of rotation of the last crown (ID), and, of the pinion (12) that we associate with it, which, in this case, will be the pinion (12) of the axis of the cylinder (2) where the rope (3) that will drag the fighter plane 20 (5) is wound. DESCRIPC / 6N OF THE / NVENC / 6N The gear train-cone in the aircraft-launch engine of an aircraft carrier, is the mechanism that we are going to connect to the gearwheel (7) of the engine (6) that, usually, is in charge of winding the rope (3) of a cylinder (2), which is what drags a fighter plane (5), of which the aircraft carrier (1) carries, to accelerate it. The plane (6) has in the bow, an axis that goes towards the ground, and, joins the drag axis (4) of the rope (3), so that the plane (5) will be accelerated by that rope 25 (3), when the motor (6) rolls it into a cylinder (2). To further accelerate this aircraft (5), we are going to connect a gear-cone train (8-10) between the gearwheel (7) of the engine (6), and, the pinion (12) of the cylinder shaft ( 2). The cone-gear train (8-10) is formed by at least two cone-gears (8-10), formed by a pinion (8) and a crown (10), connected remotely by metal rods (9 ). We connect the gearwheel (7) of the motor (6), with the pinion (8) of the first 30 gear-cone (8-10), whose crown (ID) will be connected to an intermediate pinion (11) which, on the other side, it will be connected to the pinion (8) of the second gear-cone (8-10), whose crown (10) will be connected to another intermediate pinion (1 1), and so on, until it reaches the last crown (10) of the last gear-DESCRIPTIONcone (8-10), to which we connect to another intermediate pinion (11) that, on the other hand, connects to the pinion (12) of the cylinder shaft (2) of the rope (3). DESCRIPTION OF THE FIGURES Figure # J: Side view of an aircraft carrier (1) in which only the cylinder (2) of the 5 rope, the rope (3), the drag axis (4), and the plane are highlighted (5) to which the rope will accelerate (3) when it is enlisted in the cylinder (2). 10 Figure # 2: Plan view of the gear-cone train (8-10) that connects its first pinion (8), to the engine sprocket (6). Its last crown (10) is connected to an intermediate pinion (11) which, on the other hand, is connected to the pinion (12) of the cylinder axis (2) of the rope (3). Figures 1-2: 1) Aircraft carrier 2) Rope cylinder 3) Rope 4) Airplane drive axle 15 5) Airplane 6) Engine 7) Engine sprocket 8) Pinion 9) Metal rods 20 10) Crown 11 ) Intermediate sprocket 12) Sprocket DESCRiPTION OF A PREFERRED EMBODIMENT The gear train-cone in the aircraft carrier of an aircraft carrier is characterized by being the mechanism that can increase the amount of rotation of its last crown (10) , at the same time that it can also increase the original force of the motor (6), because, this force and the amount of rotation, will increase in each transmission, from a gear-cone (8-JO), to the next, to cause of the difference in the diameters between the crown (10) and the pinion (8). Depending on the increase of these two parameters, the airplane (5) that is intended to take off from the aircraft carrier (1), may be accelerated 30 with greater force and with greater speed. We can calculate the force and the number of turns that the last crown (10) of the last gear-cone (8-10) will rotate with these two equations: (NV_T = nV_M. (P: 1) "), where the Total Power , -or, in the second equation, the Total Number of Turns of the last Crown (10) -, are the product between the Fuetza delMotor, -o, the Number of Motor Turns-, and, the Proportion between the diameters of the Pinion (8) and the Crown (10), -which will all be the same in all cone-gears (8-10) -, raised to the Power of the number of gear-cone (8-10) that we have put on the train. If, now, we want to find the Total Force and the Total Number of Spins of the Pinion (12) associated to 5 the last crown (10) of the last gear-cone (8, 10) of the train, we will have to use these two other equations, where only the Power of the Proportion of diameters between the pinion (8) and the crown (10) changes, which now increases by one unit, with respect to the total number of cone-gears (8, 10) that we have put on the train: (FT = FM. (P: l) <c + I), NV_T = nV_M. (p: l) (c + I). 10 15 20 25 30 
权利要求:
Claims (1)
[1]
CLAIMS 1) Cone-gear train in the aircraft launcher mold of a Porlaaviones, characterized by being the mechanism that we are going to connect between the toothed wheel (7) of the motor (6), and the pinion (12) of the shaft of the cylinder (2) of the chord (3) of the trailing shaft (4) of an airplane - <: aza (5). The gear train-cone 5 (8-10) is formed by at least two gears-cone (8-10), formed by a pinion (8) and a crown (10), connected remotely by means of metal rods ( 9). We connect the toothed wheel (7) of the motor (6), with the pinion (8) of the first cone-gear (8-10), whose crown (10) will be connected to an intermediate pinion (11) that, on the other side , it will be connected to the pinion (8) of the second cone-gear (8-10), whose crown (10) will be connected to another intermediate gear (11), and, so on, until reaching the last crown (10) of the last gear-cone (8-10), to which we connect to another intermediate pinion (11) which, on the other side, connects to the pinion (12) of the cylinder shaft (2) of the rope (3) that fixes at its end to the thrust shaft (4) that connects to the plane's drag shaft (5). 15 20 25 30 35
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优先权:
申请号 | 申请日 | 专利标题
ES201600745A|ES2657050B1|2016-08-30|2016-08-30|Train gear-cone in the engine launches-aircraft of an aircraft carrier|ES201600745A| ES2657050B1|2016-08-30|2016-08-30|Train gear-cone in the engine launches-aircraft of an aircraft carrier|
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