WO2015147691A1 - Procédé d'organisation de moyens de déplacement dans l'air et sur terre, et dispositif de déplacement dans l'air et sur terre - Google Patents

Procédé d'organisation de moyens de déplacement dans l'air et sur terre, et dispositif de déplacement dans l'air et sur terre Download PDF

Info

Publication number
WO2015147691A1
WO2015147691A1 PCT/RU2014/000322 RU2014000322W WO2015147691A1 WO 2015147691 A1 WO2015147691 A1 WO 2015147691A1 RU 2014000322 W RU2014000322 W RU 2014000322W WO 2015147691 A1 WO2015147691 A1 WO 2015147691A1
Authority
WO
WIPO (PCT)
Prior art keywords
wing
air
ground
movement
extendable
Prior art date
Application number
PCT/RU2014/000322
Other languages
English (en)
Russian (ru)
Inventor
Андрей Анатольевич МОРОЗ
Original Assignee
Андрей Анатольевич МОРОЗ
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
Priority claimed from RU2014111343/11A external-priority patent/RU2576071C2/ru
Application filed by Андрей Анатольевич МОРОЗ filed Critical Андрей Анатольевич МОРОЗ
Publication of WO2015147691A1 publication Critical patent/WO2015147691A1/fr

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
    • B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
    • B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C37/00—Convertible aircraft

Definitions

  • the invention relates to the field of technology, namely, to methods and devices of aircraft construction and automotive industry, allowing the movement of passengers and goods through the air and various underlying surfaces, including on public roads without changing the geometric and overall dimensions of the vehicle.
  • ORGANIZATION - new Lat., From organum - organ. The device of something, the connection into a coherent whole. / Dictionary of foreign words included in the Russian language. / Chudinov A.N., 1910. http://dic.academic.ru/
  • the disadvantages of the known technical solutions is the need to convert the geometry, shape and size of the apparatus when transferring it from the mode of movement on the ground to the mode of movement through the air.
  • This transformation requires solving complex technical problems and developing a large number of mechanical components, each of which carries a potential risk of breakdown, increases the weight of the device, complicates its production and operation, and increases cost.
  • to transfer the device from one driving mode to another it requires a stop and a certain time.
  • the lower wing is made in the form the main body, adapted to accommodate at least one element for creating traction, controls, operator seats, wheels, one of which is driven, hold the body.
  • the disadvantages of the known technical solutions are that it does not have sufficient lifting force, because it has a small wing area and their insufficient mechanization at various modes and speeds, has a low carrying capacity, poor controllability in flight due to the small surface area of control over the roll, small shoulders of the action of forces from the controls of the device to the center of mass (corresponding to the axis of rotation), insufficient the stability of the device when moving on the ground, because there is only one front wheel.
  • a sufficiently large load on the wings which is designed both for movement on the ground and for movement through the air, while the requirements for the characteristics and design of engines for movement on the ground and through the air differ significantly.
  • the author was tasked to develop a method of organizing vehicles by air and land, which allows to create a stable, reliable, safe, economical device for moving by air and land, as well as the device itself to move by air and land, allowing movement through air and land without changes in its shape and geometry, which is a stable, reliable, cheap, easy to use and maintain, universal vehicle.
  • the tasks are solved by the fact that in the method of organizing vehicles by air and land, including the use of at least one element for creating traction, lower and upper wings, three support wheels, at least two end plates, at least one elevator, which perform pitch control angle , at least one aileron, which perform control angle of heel, at least one rudder, which perform control yaw;
  • the implementation of the lower wing in the form of a main body, adapted to accommodate at least one element for creating traction, controls, seats for the operator;
  • the thrust generating element is performed comprising either an internal combustion engine, or an electric motor, or an internal combustion engine and a jet engine, or an internal combustion engine and a turboprop engine, or a hybrid engine;
  • the upper wing, lower wing, intermediate wing are performed having an aerodynamic profile and providing the creation of lifting force;
  • the main body is additionally adapted to accommodate passengers and payload;
  • end plates are vertical and bearing, connecting the lower wing, the upper wing, at least one intermediate wing.
  • at least one wing, either lower or intermediate can be made having at least one slat, which is either deflectable or extendable, has at least one flap, which is either deflected, or extendable, which has at least one interceptor, which perform either deflected or extendable, having at least one spoiler, which perform either deflected or extendable.
  • At least one end plate may be made having at least one interceptor that is either deflectable or extendable, having at least one spoiler that is either deflectable or extendable.
  • the element for creating thrust comprising a propeller, which is executed driven either by an internal combustion engine, or an electric motor, or a hybrid engine or turboprop engine.
  • the element for creating thrust is performed either transmitting movement to the wheels or transmitting movement to the air propeller.
  • the controls are controlled by air and ground movement.
  • the means of controlling the movement by air and the means of controlling the movement of the earth can be spaced, while the means of controlling the movement of the air are carried out comprising a control wheel, direction pedals, a gas sector, a pitch of a screw; brakes, clutch pedal.
  • the main body is made of either strong and lightweight metal or fiberglass or carbon fiber containing front doors and side windows in the form of transparent elements made of impact-resistant glass or transparent plastic, rear and side view mirrors, near and far lights lights, direction indicators, emergency stop indicators, fog lights, and in the rear there are direction indicators, emergency stop indicators, reverse lights and brake lights.
  • a device for moving through air and land including:
  • the lower wing made in the form of the main body, adapted to accommodate at least an element for creating traction, controls, seats for the operator;
  • upper wing located vertically above the lower wing;
  • At least one aileron made by controlling the angle of heel
  • At least one rudder made by the yaw manager further comprises: a fourth support wheel;
  • the element for creating traction is made containing either an internal combustion engine, or an electric motor, or an internal combustion engine and a jet engine, or an internal combustion engine and a turboprop engine, or a hybrid engine;
  • the upper wing, lower wing, intermediate wing are performed having an aerodynamic profile and providing the creation of lifting force;
  • the main body is made, additionally adapted to accommodate passengers and payload;
  • end plates are made vertical and bearing, connecting the lower wing, the upper wing, at least one intermediate wing.
  • at least one wing, either upper, lower, or intermediate is made having at least one slat made either deflected or extended.
  • At least one wing, either upper, lower, or intermediate is made having at least one flap made either deflected or extended.
  • At least one wing, either upper, lower, or intermediate is made having at least one interceptor, made either deflected or extended.
  • At least one end plate is made having at least one interceptor made either deflectable or extendable.
  • At least one wing, either upper, lower, or intermediate is made having at least one spoiler, made either deflected or extendable.
  • At least one end plate is made having at least one spoiler, made either deflectable or extendable.
  • the element for creating thrust is made comprising a propeller, which is made driven by either an engine or a turboprop engine, or an electric motor, or a hybrid engine.
  • the element for creating traction is made transmitting movement either to the wheels or to the air propeller.
  • the rudder made by the control yaw is located at a maximum distance from the vertical axis, for example, on the upper wing in the form of a front horizontal tail (PGO).
  • PGO front horizontal tail
  • the means of controlling the movement by air and the means of controlling the movement of the earth can be spaced, while the means of controlling the movement of the air are made containing the control wheel, directional pedals, gas sector, screw pitch, the means of controlling the movement of the ground are made containing the steering wheel, gas pedals, pedal brakes, clutch pedal.
  • the main body is made of either strong and lightweight metal or fiberglass or carbon fiber containing front doors and side windows in the form of transparent elements made of impact-resistant glass or transparent plastic, rear and side view mirrors, near and far lights lights, direction indicators, emergency stop indicators, fog lights, and in the rear there are direction indicators, emergency stop indicators, reverse lights and brake lights.
  • the technical effect of the proposed technical solution is to expand the arsenal of vehicles by air and land, providing the necessary lifting force and controllability at the speeds of a conventional small aircraft and at speeds of a conventional car in the dimensions of a traditional vehicle, to increase reliability, to improve aerobatic and ground operational properties. In addition, in increasing efficiency and reducing the cost of movement.
  • FIG. 1 front view
  • FIG. 2 sectional view AA
  • 1 is the main body (lower wing)
  • 2 is the upper wing
  • 3 is the intermediate wing (front)
  • 4 is the intermediate wing (rear)
  • 5 is the end plate (left)
  • 7 - support wheels 8 - traction creating element
  • the wing area usually ranges from 10 to 20 square meters. m., while the separation speed (landing speed) depends on the wing area and the availability of mechanization and is usually 50 to 120 km / h for such aircraft.
  • the traditional location and shape of the wing primarily its wingspan, does not allow the device to have transverse dimensions, allowing it to move along public roads.
  • the claimed invention relates to vehicles that allow both traffic on public roads, and flights at altitudes up to 4000 m, at a distance of up to 2000 km.
  • a device for moving through air and land is a full-fledged passenger car, including a lower wing, made in the form of the main body 1 and a superstructure made in the form of several more wings, placed between two end plates 5 and b, which are made vertical and bearing.
  • the main body 1 is made of durable and lightweight metal or fiberglass or carbon fiber.
  • the main building 1 there are places for drivers - pilots, passengers, cargo, as well as all the necessary elements and mechanisms for safe movement on the ground.
  • the main body 1 In the front part of the main body 1 there are doors with transparent elements - frontal and side windows, made of shockproof glass or transparent plastic, rear and side view mirrors, dipped and main beam headlights. In the front and rear parts of the main body 1 install light direction indicators, emergency stop indicators, fog lights. In the rear part of the main body 1, reverse lights and brake lights are installed.
  • the number of intermediate wings 4 and their size are selected from the need to provide lifting force for take-off of the device for moving through air and land at a separation speed and to ensure a stable and safe flight in the required speed range. So, to increase the lifting force, it is proposed to use more than two wings located in such a way that their negative mutual influence is minimal.
  • Wings 1, 2, 3, 4 are made according to classical aviation technology. For the manufacture of wings 1, 2, 3, 4, all aviation materials are used - aluminum and titanium alloys, fiberglass and carbon fiber. End plates 6 and 7 serve for longitudinal flight stabilization, and also significantly reduce induction resistance and air flow at the ends of wings 1, 2, 3, 4. In end plates 6 and 7, elements of control systems are placed - traction, wires, gas pipelines, etc. End plates 6 and 7 are made of the same materials as wings 1, 2, 3, 4.
  • a mechanization complex should be performed on all wings 1, 2, 3, 4, or at least one or upper 2, or lower 1, or intermediate 3 or 4, or on upper 2 and lower 1, or on upper 2 and intermediate 3 or 4, or on the lower 1 and intermediate 3 or 4, or on at least one intermediate 3 or 4 of the wings (installed flap 14, slat 13, flaperon (not shown in FIG.) interceptor 15, aileron 12, trimmer (not shown in FIG.), etc. So to reduce the take-off distance and decrease the landing speed at all or at least one or the upper 2, or lower 1, or between 3 or
  • Rudder 10, made by controlling pitch angle, aileron 12, made by controlling roll angle, rudder 11, made by yaw control are used to control the device for moving through air and ground during flight, the trimmer mounted on aileron 12, elevator 10 , rudder 11 - to reduce the load on the controls.
  • To increase the effectiveness of the aileron 12 is performed in a vertical plane, in the upper part of the device for moving through air and land in an amount of at least one - located in the middle above the upper 2 wing. If the specific configuration and dimensions of the device for moving through air and land require the need to increase the effectiveness of the aileron 12, they are made two, while they are the upper ends of the end plates.
  • Aileron 12 like all wings 1, 2, 3, 4, is made according to classical aviation technology from light and durable materials.
  • the strength of the end plates 5, 6 provides the bearing capacity of the wings located above the main body 1, taking into account static and dynamic loads.
  • Controls perform controlling the movement of air and land. Air (flight) controls - the steering wheel (joystick) and pedals can be spaced with the ground (car) controls (for example, the steering wheel, gas pedals, brakes and clutches are located on the left driver’s seat, and the control wheel and directional pedals, gas sector, propeller pitch, etc.
  • the dashboard has all the necessary elements and devices for monitoring and control both when moving on the ground, and when moving (flying) through the air. To create traction when moving through air and land, at least one element of creating traction is used.
  • the design of the elements for creating thrust when moving aircraft engines through the air), their thrust, power are selected for specific design parameters, its take-off weight, and operating speeds.
  • the operating modes of the engine for ground and air movement are mutually exclusive; in this regard, at least two engines (two groups of engines) are used in the device for moving through air and land - one (or the first group of engines) for driving on the support wheels 7 (front, rear, fully-driven), the second (or second group of engines) for driving the air propeller 9 (one or more).
  • one or two types of fuel are used (for example, gasoline of one or different brands, or diesel fuel for all engines, or gasoline and diesel fuel for different engines), in a device for moving through the air and the earth can use a single fuel tank, gas pump and a number of other elements.
  • the drive from the controls (steering wheel, pedals, etc.) to the controls (rudders, ailerons, etc.) can be carried out by rigid, cable, electric, wireless, mixed and other mechanisms.
  • the control of the device for moving through air and land while moving on the ground is no different from the control of a conventional passenger car, and the control of the device for moving through air and ground in the air is similar to the control of a light aircraft of a traditional configuration.
  • Some restrictions may include road traffic, take-off and landing with a strong crosswind, in view of the relatively large area of the end plates, but when conducting detailed aerodynamic tests and designing a specific device for moving through air and land, their area can be reduced to the minimum necessary.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

L'invention se rapporte au domaine des technologies et concerne notamment des procédés et des dispositifs de construction d'avions et de construction d'automobiles permettant d'assurer le déplacement de passagers et de charges dans l'air et sur diverses surfaces étendues, y compris des voies routières à vocation commune sans modifier les dimensions hors tout du moyen de transport. L'invention concerne l'élaboration d'un procédé d'organisation des moyens de déplacement dans l'air et sur terre, permettant de créer un dispositif stable, fiable, sûr et économique de déplacement dans l'air et sur terre, ainsi qu'un dispositif proprement dit de déplacement dans l'air et sur terre permettant de réaliser des déplacement dans l'air et sur terre sans modifier sa forme ni sa géométrie et consistant en un moyen de transport stable, fiable, peu coûteux, simple à utiliser et entretenir et universel. Le résultat technique de l'invention consiste en un élargissement de l'éventail des moyens de déplacement dans l'air et sur terre présentant la force de sustentation nécessaire et une manœuvrabilité à des vitesses de déplacement d'un petit avion traditionnel et à des vitesses de déplacement d'automobiles (50-150 km/h) en respectant les dimensions d'un moyen de transport traditionnel (largeur В=2-2,5 m, hauteur Н=3-4 m, longueur L=4-5 m, en une amélioration de la fiabilité, et en une amélioration des propriétés de pilotage aérien et d'exploitation au sol. L'invention apporte également une plus grande économie et une diminution des coûts de déplacement.
PCT/RU2014/000322 2014-03-26 2014-05-05 Procédé d'organisation de moyens de déplacement dans l'air et sur terre, et dispositif de déplacement dans l'air et sur terre WO2015147691A1 (fr)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
RU2014111343 2014-03-26
RU2014111341 2014-03-26
RU2014111341 2014-03-26
RU2014111343/11A RU2576071C2 (ru) 2014-03-26 2014-03-26 Способ организации средств передвижения по воздуху и земле, устройство для передвижения по воздуху и земле

Publications (1)

Publication Number Publication Date
WO2015147691A1 true WO2015147691A1 (fr) 2015-10-01

Family

ID=54196058

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/RU2014/000322 WO2015147691A1 (fr) 2014-03-26 2014-05-05 Procédé d'organisation de moyens de déplacement dans l'air et sur terre, et dispositif de déplacement dans l'air et sur terre

Country Status (1)

Country Link
WO (1) WO2015147691A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115019503A (zh) * 2022-05-12 2022-09-06 东风汽车集团股份有限公司 基于信息共享的飞行汽车混合交通流下空间轨道分配方法

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1299117A (en) * 1918-06-21 1919-04-01 George Tellman Buchanan Airplane.
US2713465A (en) * 1953-05-21 1955-07-19 Harry E Novinger Combined air-ground vehicle
RU128556U1 (ru) * 2012-10-29 2013-05-27 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Псковский государственный университет" Летающий автомобиль

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1299117A (en) * 1918-06-21 1919-04-01 George Tellman Buchanan Airplane.
US2713465A (en) * 1953-05-21 1955-07-19 Harry E Novinger Combined air-ground vehicle
RU128556U1 (ru) * 2012-10-29 2013-05-27 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Псковский государственный университет" Летающий автомобиль

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115019503A (zh) * 2022-05-12 2022-09-06 东风汽车集团股份有限公司 基于信息共享的飞行汽车混合交通流下空间轨道分配方法

Similar Documents

Publication Publication Date Title
EP2977239B1 (fr) Véhicule de transport hybride terrestre et aérien, et procédé de transformation d'un tel véhicule
US9233748B2 (en) Roadable, adaptable-modular, multiphibious-amphibious ground effect or flying, car-boat-plane or surface-effect motorcycle
US9254916B2 (en) Vertical take-off and landing aircraft with tiltrotor power for use on land and in air
US20100181414A1 (en) Personal transportation vehicle
CN102848870A (zh) 一种陆飞船
CN103770589A (zh) 飞行汽车
CN103522858A (zh) 一种飞行客车
RU2648937C1 (ru) Аэромобиль вертикального взлета
CN105366053A (zh) 碟形航行器
CN110654190A (zh) 一种倾转无轴涵道旋翼飞行汽车及其工作方法
RU2551300C1 (ru) Автомобиль с летными эксплуатационными свойствами
JP7112141B2 (ja) 変角型揚力調節方式の翼を装着した第３世代航空機
CN102424110A (zh) 可变翼微型水陆飞行器
CN202357821U (zh) 可变翼微型水陆飞行器
WO2015147691A1 (fr) Procédé d'organisation de moyens de déplacement dans l'air et sur terre, et dispositif de déplacement dans l'air et sur terre
JP2004026034A (ja) 垂直離着陸機
RU143819U1 (ru) Транспортное средство для передвижения по воздуху и земле
RU2576071C2 (ru) Способ организации средств передвижения по воздуху и земле, устройство для передвижения по воздуху и земле
CN102555710A (zh) 水陆空多功能飞鱼
US20240092336A1 (en) Ground-effect hovercraft vehicle with retractable wings
RU2770718C1 (ru) Гибридное транспортное средство автолет соосной схемы
RU190200U1 (ru) Летающая амфибия-трансформирующееся транспортное средство
RU2624231C1 (ru) Пассажирский экраноплан
RU147630U1 (ru) Автомобиль с летными эксплуатационными свойствами
US11993366B2 (en) Wingless VTOL flying land vehicle

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 14886971

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 14886971

Country of ref document: EP

Kind code of ref document: A1