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WO2015065240A1 - Dispositif pour piloter un véhicule de transport hybride - Google Patents

Dispositif pour piloter un véhicule de transport hybride Download PDF

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Publication number
WO2015065240A1
WO2015065240A1 PCT/RU2014/000745 RU2014000745W WO2015065240A1 WO 2015065240 A1 WO2015065240 A1 WO 2015065240A1 RU 2014000745 W RU2014000745 W RU 2014000745W WO 2015065240 A1 WO2015065240 A1 WO 2015065240A1
Authority
WO
WIPO (PCT)
Prior art keywords
wheel
steering
control
steering rack
bearings
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/RU2014/000745
Other languages
English (en)
Russian (ru)
Inventor
Дмитрий Николаевич ХАРИТОНОВ
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of WO2015065240A1 publication Critical patent/WO2015065240A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60FVEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
    • B60F5/00Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
    • B60F5/02Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft

Definitions

  • the utility model can be used to control a conventional gyroplane and simplify the control of a specified aircraft.
  • the device can also be used to create hybrid vehicles that can move on ordinary roads like a motorcycle, and in the air like a gyroplane.
  • a V-shaped steering wheel is currently used to change the direction of motion of a motorcycle.
  • the steering rack is attached directly to the front wheel fork, and is also connected to the frame of the motorcycle using a bearing (s).
  • turning the steering wheel means turning the front wheel of the motorcycle in the right direction and, accordingly, changing the direction of movement (See Fig. 1 from the website http: //motocafe.r zfaele; mvi-ceh-teor
  • the lower part of the rotor control knob (1) is connected to two steering racks (2).
  • the slopes of the rotor control handle back and forth cause corresponding longitudinal displacements of one steering rack relative to another.
  • the slopes of the rotor control knob left and right cause the corresponding lateral movements of one steering rack relatively different (see Fig. 2).
  • the steering racks are connected by hinges with vertical rods, which, in turn, are connected to the rotor head.
  • the tilts of the handle cause changes in the angles of the plane of rotation of the rotor and, accordingly, the direction of movement of the apparatus.
  • An increase or decrease in engine speed occurs by moving the engine control lever (ORE).
  • a person needs to use two hands (one hand changes the position of the rotor control handle, the other hand changes the position of the ore) and two legs (to control the rudder).
  • the specified design contains constructive solutions standard for gyroplane control (in addition to the motorcycle steering wheel, the design includes a rotor control knob and pedals for controlling the rudder), which leads to inconvenience of controlling the device.
  • the task of creating this utility model was to design a unified control system that would simplify the control of the gyroplane, and could also be used to control a hybrid device that can move on the ground like a motorcycle and in airspace as gyroplane.
  • the result of using this utility model will be the emergence of a mobile switchable device that allows you to convert motorcycle control into control of the aircraft and vice versa.
  • the steering rack consists of two parts.
  • the lower part of the steering struts has a cylindrical shape, with the lower end it is attached to the front wheel fork, the CV joint is attached to the other end, which connects the lower steering rack and the upper steering rack.
  • the lower steering rack is inserted into the round tube, which is connected to the beam of the frame of the motorcycle. Inside the tube there is a bearing that allows you to make free turns of the lower steering rack around its axis.
  • the upper steering rack also has a cylindrical shape, however, of a smaller section. The upper end of the upper steering rack is attached directly to the steering wheel.
  • the upper steering rack has an opening into which a stud can be inserted, on which the end of the control switch sleeve can be supported to fix the upper position of the sleeve.
  • the sleeve of the control switch is a cylindrical tube that is capable of moving up and down along the axes of the steering racks.
  • the sleeve of the control switch fits snugly enough to the surfaces of both bearings.
  • the control switch sleeve is snug against the surface of the lower steering rack.
  • the surface of the sleeve has a hole in the lower part that can be combined with the hole in the lower steering rack and the sleeve can be fixed in this position with a hairpin.
  • the control switch sleeve has a vertical slot in order to guiding rails connecting the outer sides of the bearings and the rotor control handle could pass through this gap.
  • the rotor control handle has a standard gyro mount for mounting with rotor control rails.
  • Tail guides On the lower part of the lower steering rack are mounted tail guides, which are two small pins. Tail cables are attached to their edges, which can be attached to the rudder guides.
  • the control of the device on the ground (when the sleeve of the control switch is locked in the lower position) is reduced to steering wheel rotations around the axis. In this position, the control switch sleeve does not allow steering wheel tilting.
  • the control of the device in the air, or in the “take-off” or “landing” modes (when the sleeve of the control switch is fixed in the upper position) is reduced to steering wheel rotations around the axis and steering wheel tilts in any direction. In this position, the sleeve of the control switch allows not only to make steering wheel rotations around the axis, but also its inclinations in any direction. ORE with this control can be replaced, used on motorcycles, with a gas adjustment knob.
  • the device has simpler controls than a gyroplane, since it excludes the use of pedals to control the rudder. If you use the front wheel of a motorcycle of a sufficient size, with a lightweight solid disk, then you can completely abandon the rudders, since the front wheel itself will perform the function of the rudder.
  • the utility model can be used in hybrid aircraft moving on the ground, like a motorcycle, and in the air like a gyroplane. In this case, the utility model avoids the creation of dual control systems.
  • FIG. 2 shows commonly used gyroplane controls.
  • Fig. 4 shows the changes that must be made to the design of the front wheel of the motorcycle to create a hybrid control device gyroplane and motorcycle.
  • the hybrid control device gyroplane and motorcycle can be materialized as follows.
  • the device contains (see. Fig. 4):
  • a metal V-shaped steering wheel that is attached to the upper end of the upper control strut.
  • the metal sleeve of the control switch is in the form of a cylindrical tube. A hole was drilled in the tube to secure the tube with a pin to the lower control post. The tube has a vertical slot through which guide rails must pass.
  • the metal bearings of the control switch are fixed to the axis of the upper control strut.
  • the diameter of the bearings is slightly smaller than the inner diameter of the control switch sleeve and the control switch sleeve can move along the axis of the upper control column.
  • Guide rails are attached to the outer surface of the bearings using horizontal hinges.
  • the metal guide rails are in the form of thin elongated cylinders. They are attached at one end with horizontal joints to the outer sides of bearings mounted on the axis of the upper steering rack, and at the other ends with horizontal joints at the rotor control handle.
  • the metal upper steering strut is cylindrical.
  • the steering wheel is attached to the upper end of this rack, the lower end is connected to the CV joint.
  • On the axis of the upper steering rack are two bearings of the control switch.
  • the upper steering rack has a hole above the junction with the constant velocity joint for installation with a pin (there is no pin in the diagram) of the upper position of the control switch sleeve.
  • the metal rotor control knob has a cylindrical shape and is fastened with the lower part to the rotor control rails. Guide rails are attached to the side of the rotor control knob using horizontal hinges.
  • the CV joint of the lower steering rack connects the upper and lower steering racks, which are attached to it by the ends. The diameter of the CV joint is slightly smaller than the inner diameter of the sleeve of the control switch.
  • the metal lower steering strut is cylindrical.
  • the diameter of the lower steering rack is slightly smaller than the inner diameter of the sleeve of the control switch, and when moving the sleeve onto this steering rack, it is snug enough to it.
  • the upper end of the lower steering rack is connected to the CV joint of the lower steering rack.
  • the metal rails of the rotor control are cylindrical in shape, connected by hinges to the rotor control handle. At the same time, the lower rail is hinged to the frame beam. Thus, the rails can move relative to each other in the longitudinal and transverse planes.
  • the metal beam of the frame has a cylindrical shape, is part of the structure of the apparatus frame.
  • a steel tube with an integrated steering bearing is attached to its front end.
  • a metal steering bearing is mounted in a steel tube that ends with the frame beam:
  • a lower steering column is attached to the inside of the bearing, which can rotate freely around its axis.
  • the metal fork of the front wheel is connected to the end of the lower steering rack, which transmits rotation to it.
  • the lower parts of its branches fork connected to the axis of the front wheel, which passes through the front wheel bearing.
  • the front wheel of the unit can be made as a light wheel of a motorcycle or moped and have spokes and a rim.
  • the wheel rim is connected to the bearing using a continuous (or semi-continuous) plate made of light material.
  • the tail guides are steel pins, one of its ends attached to the sides of the lower steering rack. At the opposite ends of the steel pins, the ends of the tail cables are fixed.
  • the tail cables are attached at one end to the ends of the tail guides, and at the other ends are connected to the rudder guides (not shown in the diagram).
  • the sleeve of the control switch (2) When operating the device in ground mode, the sleeve of the control switch (2) is installed in the lower position - it covers the lower steering rack (8).
  • the lower bearing of the control switch (3) is pressed against the inner upper part of the sleeve of the control switch (2), the other end of the sleeve is attached through a hole with a pin to the lower steering rack (8)
  • Now the torque from the steering wheel (1) is transmitted through the upper steering rack (5) , CV joint (7), lower steering rack (8), front wheel fork (12) to the front wheel (13), causing it to turn in the desired direction.
  • the sleeve of the control switch (2) When the sleeve of the control switch (2) is in the lower position, it does not allow tilting the steering wheel (1), since it tightly covers the lower bearing of the control switch (3) and the lower steering rack (8). As soon as the sleeve of the control switch (2) is moved to the upper position and mounted on top of the stud placed in the hole in the lower edge of the upper steering column (5), the tilt of the steering wheel (1) becomes possible, since the sleeve of the control switch (2) does not simultaneously fix the position of the bearing control switch (3) and lower steering rack (8), and covers only two bearings. The tilt of the steering wheel (1) is transmitted through the guide rails (4) to the rotor control knob (6), and through it to the rotor control rails (9).
  • rudder rotations (1) around the axis are possible, which, firstly, rotate the front wheel (13), which can act as a rudder, and secondly, rotate the rudder (1) cause the tail guides to move (14), which, through the tail cables (15), cause the rudder to move.
  • the utility model “A device for controlling a hybrid vehicle” allows, firstly, to simplify control of the gyroplane (since pedals are not involved), and secondly, to optimally (using the minimum number of devices) control a hybrid device that can move on the ground as a motorcycle, and in the air like a gyroplane.
  • This device is used to simplify control of the gyroplane, as well as to control hybrid devices that can move on the ground as motorcycle and in the air like a gyroplane.
  • Hybrid devices can be used by citizens, organizations, government bodies to perform various tasks: personal and official transport, tourism, monitoring, patrolling, ambulance, etc.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Automatic Cycles, And Cycles In General (AREA)

Abstract

L'invention concerne le domaine de l'aviation et notamment de la conception de véhicules de transport transformables. Le dispositif pour piloter un véhicule de transport hybride comprend une jambe supérieure avec deux paliers sur son axe et une jambe inférieure reliée, qui sont reliées par des rotules de train. Un manchon de commutation de commande peut se déplacer entre la position dans laquelle il entoure uniquement les paliers de la jambe supérieure de manière à permettre les inclinaisons du gouvernail et sa rotation autour de son axe et la position dans laquelle il entoure le palier inférieur de la jambe supérieure, la rotule de train et la jambe inférieure, de manière à permettre la rotation du gouvernail autour de son axe. Le manchon comporte une fente verticale à travers laquelle passent des tringles de direction qui sont reliées par une extrémité, au moyen de rotules horizontales, aux côtés extérieurs des paliers de la jambe supérieure et sont reliées par l'autre extrémité au moyen de rotules horizontales à la poignée de commande du rotor. Les inclinaisons du gouvernail provoquent des inclinaisons de la poignée de commande du rotor. En vol, la fonction du gouvernail de direction est assumée par la roue avant de l'appareil dont la jante est reliée au palier de l'axe de la roue par une jante à toile pleine ou semi-pleine constituée d'un matériau léger. L'invention permet de piloter le véhicule transformable au moyen d'un seul et même organe de pilotage, dans les airs ou au sol.
PCT/RU2014/000745 2013-10-08 2014-10-06 Dispositif pour piloter un véhicule de transport hybride Ceased WO2015065240A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
RU2013144942 2013-10-08
RU2013144942 2013-10-08

Publications (1)

Publication Number Publication Date
WO2015065240A1 true WO2015065240A1 (fr) 2015-05-07

Family

ID=53004690

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/RU2014/000745 Ceased WO2015065240A1 (fr) 2013-10-08 2014-10-06 Dispositif pour piloter un véhicule de transport hybride

Country Status (1)

Country Link
WO (1) WO2015065240A1 (fr)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5915649A (en) * 1996-08-23 1999-06-29 Mcdonnell Douglas Helicopter Company Roadable helicopter
US6978969B1 (en) * 2003-03-05 2005-12-27 Neal Larry R Fly-drive vehicle
US20080251308A1 (en) * 2005-08-24 2008-10-16 Dezso Molnar Ground Air Water Craft
RU127039U1 (ru) * 2012-12-14 2013-04-20 Василий Владимирович Кириченко Аэробайк

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5915649A (en) * 1996-08-23 1999-06-29 Mcdonnell Douglas Helicopter Company Roadable helicopter
US6978969B1 (en) * 2003-03-05 2005-12-27 Neal Larry R Fly-drive vehicle
US20080251308A1 (en) * 2005-08-24 2008-10-16 Dezso Molnar Ground Air Water Craft
RU127039U1 (ru) * 2012-12-14 2013-04-20 Василий Владимирович Кириченко Аэробайк

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