WO2019205187A1 - Dispositif de transport - Google Patents

Dispositif de transport Download PDF

Info

Publication number
WO2019205187A1
WO2019205187A1 PCT/CN2018/085881 CN2018085881W WO2019205187A1 WO 2019205187 A1 WO2019205187 A1 WO 2019205187A1 CN 2018085881 W CN2018085881 W CN 2018085881W WO 2019205187 A1 WO2019205187 A1 WO 2019205187A1
Authority
WO
WIPO (PCT)
Prior art keywords
dish
traveling device
housing
shaped housing
flying
Prior art date
Application number
PCT/CN2018/085881
Other languages
English (en)
Chinese (zh)
Inventor
刘均
刘新
金武超
Original Assignee
深圳市元征软件开发有限公司
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 深圳市元征软件开发有限公司 filed Critical 深圳市元征软件开发有限公司
Publication of WO2019205187A1 publication Critical patent/WO2019205187A1/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
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/16—Aircraft characterised by the type or position of power plant of jet type
    • B64D27/20—Aircraft characterised by the type or position of power plant of jet type within or attached to fuselage

Definitions

  • the utility model belongs to the technical field of vehicles, in particular to a traveling device.
  • the flying wings are foldable, but most of the exposure is disposed on both sides or the rear of the flying car, so that the flying wings exposed to the external environment are significantly increased.
  • the drag coefficient of a flying car is not conducive to saving fuel consumption when the flying car is in the landline mode.
  • the purpose of the utility model is to provide a traveling device, which aims to solve the technical problem that the flying wing of the prior art is exposed to the outside when the flying vehicle is in the land mode, and the drag coefficient of the whole vehicle is increased, and the fuel consumption is increased. .
  • a traveling device comprising a housing assembly, a power unit and a flying wing mechanism
  • the housing assembly comprising a dish housing and a canopy cover
  • the dish shell The upper end of the body is provided with a cockpit, the canopy cover is closably mounted on the dish-shaped casing and sealed to the cockpit, and the lower end of the dish-shaped casing is provided with a land wheel set
  • the power The device includes an electric motor and two turbojet engines, the electric motor is fixedly mounted in the disc-shaped housing, the electric motor includes a first driving end, and the first driving end of the electric motor is drivingly connected with the ground traveling wheel set, two
  • the turbojet engine is fixedly mounted to a rear end of the dish-shaped housing,
  • the flying wing mechanism includes a vertical tail wing and two flying wings fixedly mounted on an upper end of the dish-shaped housing and located at the a rear end of the canopy cover, wherein the outer edges of the two sides of the dish-shaped housing are respectively provided with a receiving
  • the power device further includes a lift fan
  • the lower end of the dish-shaped housing is provided with a mounting cavity
  • the lift fan includes a rotating shaft and a plurality of rotating blades
  • the rotating shaft is rotatably mounted to the mounting
  • the motor further includes a second driving end
  • the rotating shaft is drivingly connected to the second driving end of the electric motor
  • each of the rotating blades is fixedly mounted on an outer wall of the rotating shaft and is wound around the same
  • the central axis of the rotating shaft is radially evenly distributed.
  • a camera module is fixedly mounted on the wing tip of the vertical tail, and a lens end of the camera module is disposed toward a rear end of the vertical tail.
  • the cockpit is provided with a display control system, and the camera module is provided.
  • the group is electrically connected to the display control system.
  • a front air inlet is opened at a front end of the dish-shaped housing, and an intake end of each of the turbojet engines is in communication with the front air inlet.
  • the lower ends of the opposite sides of the dish-shaped casing are respectively provided with side air inlets, and the two side air inlets are respectively communicated with the intake ends of the two turbojet engines.
  • front air inlet and the two side air inlets are both DSI air inlets.
  • turbojet engines are vector turbojet engines.
  • both of the flying wings are variable swept wings.
  • a front end of the canopy cover is provided with an observation through cavity, and a front windshield piece is embedded in the observation through cavity.
  • the land wheel set includes a rear drive wheel and two front driven wheels, the rear drive wheel and the two front driven wheels are arranged at a rear three points, and the rear drive wheel and the first drive end of the motor are driven connection.
  • the utility model has the beneficial effects: the travel device of the utility model, when the travel device is in the flight mode, the two turbojet engines provide the thrust required for flight, and at the same time, the original device is accommodated on both sides of the dish-shaped casing.
  • the two flying wings in the accommodating cavity of the edge can also be driven away from the two accommodating cavities by the oscillating motor in the accommodating cavity, thereby being deployed to the outside, so that the traveling device can be in two flying wings, the vertical tail and
  • the two turbojet engines work together to achieve flight.
  • the land wheel set of the lower end of the dish-shaped housing is connected with the first driving end of the motor provided in the dish-shaped housing, the land wheel set can be rotated by the motor to drive the traveling equipment to drive on the road surface.
  • the landline function of the travel device When the traveling device is in the landline mode, the two flying wings can be retracted into the two accommodating cavities under the driving of the two oscillating motors, thereby effectively reducing the overall vehicle drag coefficient of the traveling equipment, and also significantly reducing the traveling equipment. Fuel consumption in the land mode.
  • FIG. 1 is a schematic structural view 1 of a traveling device provided by an embodiment of the present invention.
  • FIG. 2 is a schematic structural view 2 of a traveling device provided by an embodiment of the present invention.
  • FIG. 3 is a schematic structural diagram 3 of a traveling device according to an embodiment of the present invention.
  • first and second are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated.
  • features defining “first” and “second” may include one or more of the features either explicitly or implicitly.
  • the meaning of "a plurality” is two or more unless specifically and specifically defined otherwise.
  • the terms “installation”, “connected”, “connected”, “fixed” and the like shall be understood broadly, and may be fixed or detachable, for example, unless otherwise explicitly defined and defined.
  • Connected, or integrated; can be mechanical or electrical; can be directly connected, or indirectly connected through an intermediate medium, can be the internal communication of two components or the interaction of two components.
  • the specific meanings of the above terms in the present invention can be understood on a case-by-case basis.
  • the traveling device provided by the embodiment of the present invention comprises a housing assembly 10, a power unit 20 and a flying wing mechanism 30.
  • the housing assembly 10 includes a dish housing 12 and a canopy cover 11 and a dish shape.
  • the upper end of the casing 12 is provided with a cockpit (not shown).
  • the canopy cover 11 is detachably mounted on the dish-shaped casing 12 and sealed to the cockpit.
  • the lower end of the dish-shaped casing 12 is provided with a land wheel set 40.
  • the power unit 20 includes an electric motor (not shown) and two turbojet engines 21.
  • the motor is fixedly mounted in the dish housing 12.
  • the electric motor includes a first driving end, and the first driving end of the electric motor is drivingly connected with the land wheel set 40.
  • the turbojet engines 21 are fixedly mounted to the rear end of the dish casing 12, and the flying wing mechanism 30 includes a vertical tail 32 and two flying wings 31 fixedly mounted to the upper end of the dish casing 12 and located at the canopy 11
  • the outer edges of the two sides of the dish-shaped casing 12 are respectively provided with a receiving cavity (not shown), and the two flying wings 31 are respectively accommodated in the two accommodating cavities, and the two accommodating cavities are respectively provided with a oscillating motor ( The driving end of the two swinging motors is respectively connected with the two flying wings 31.
  • the two flying wings 31 are respectively driven to swing away from the two accommodating cavities and unfolded.
  • the traveling device provided by the embodiment of the present invention when it is in the flight mode, the two turbojet engines 21 provide the thrust required for the flight, and at the same time, the capacity originally accommodated on the outer edges of the two sides of the dish casing 12
  • the two flying wings 31 in the cavity can also be driven away from the two accommodating cavities under the driving of the oscillating motor in the accommodating cavity, thereby being deployed to the outside, so that the traveling device of the embodiment of the present invention can be used in two flying wings. 31.
  • the vertical tail 32 and the two turbojet engines 21 cooperate to achieve flight.
  • the traveling wheel set 40 at the lower end of the dish-shaped housing 12 is connected to the first driving end of the motor provided in the dish-shaped housing 12, the land wheel set 40 can be rotated by the motor to drive the utility model.
  • the traveling equipment of the embodiment travels on the road surface to realize its land function.
  • the traveling device of the embodiment of the present invention is in the landline mode, the two flying wings 31 can be retracted into the two accommodating cavities under the driving of the two oscillating motors, thereby effectively reducing the overall drag coefficient of the traveling device. It also significantly reduces fuel consumption in its land mode.
  • the front end of the dish-shaped casing is provided with a lighting assembly 13, and the lighting assembly 13 includes a strong headlight 131 and two rows of lights 132, and the two rows of lights 132 are respectively disposed on both sides of the strong head or the like.
  • the strong optical head can provide sufficient illumination for the traveling equipment, thereby improving the safety of taking off or landing at night.
  • the traveling device of the embodiment of the present invention travels on a night road, the two lights can be turned on to provide illumination.
  • the power unit 20 further includes a lift fan 22, and the lower end of the dish casing 12 is provided with a mounting cavity 123.
  • the lift fan 22 includes a rotating shaft 222 and a plurality of rotating blades 221, and a rotating shaft
  • the 222 is rotatably mounted in the mounting cavity 123.
  • the motor further includes a second driving end.
  • the rotating shaft 222 is drivingly connected to the second driving end of the motor.
  • Each of the rotating blades 221 is fixedly mounted on the outer wall of the rotating shaft 222 and rotates around.
  • the central axis of the shaft 222 is radially evenly distributed.
  • the inner lift fan 22 installed in the mounting cavity 123 can be driven by the motor.
  • the lower rotation provides a considerable lift for the traveling equipment of the embodiment of the present invention, which further shortens the take-off distance and further improves the safety of the landing.
  • the camera module 321 is fixedly mounted on the wing tip of the vertical tail 32.
  • the lens end of the camera module 321 is disposed toward the rear end of the vertical tail 32, and the display is provided in the cockpit.
  • the control system, the camera module 321 is electrically connected to the display control system.
  • the camera module 321 is fixedly mounted on the wing tip of the vertical tail 32, and the lens end of the camera module 321 is disposed toward the rear end of the vertical tail 32, so that the camera module 321 can capture the rear end of the travel device.
  • the image module 321 can electrically transmit the captured real-time image image to the display control system, so that the personnel in the cockpit can be electrically connected to the display control system provided in the cockpit. Get the image information of the back end of the travel device in real time.
  • the front end of the dish-shaped housing 12 is provided with a front air inlet 121, and the intake ends of the two turbojet engines 21 are all in communication with the front air inlet 121.
  • the two turbojet engines 21 establish an intake passage with the external environment, so that the outside air can continuously enter the two vortices through the front air inlet 121.
  • the intake end of the injection engine 21 further satisfies the gas demand of the two turbojet engines 21.
  • the lower ends of the opposite sides of the dish-shaped casing 12 are respectively provided with side air inlets 122, and the air inlets 122 on both sides are respectively connected to the two turbojet engines 21.
  • the gas ends are connected.
  • the side air inlets 122 are opened at the lower ends of the opposite sides of the dish-shaped casing 12, and the air inlets 122 on both sides are respectively communicated with the intake ends of the two turbojet engines 21.
  • Such more gas can enter the intake end of the two turbojet engines 21 from the inlet ports 122 on both sides, thus further ensuring the abundance of gas in the two turbojet engines 21, significantly improving the two turbojet engines 21
  • the gas efficiency further increases the thrust of the two turbojet engines 21.
  • the front air inlet 121 and the two side air inlets 122 are both DSI air inlets (no supersonic inlet supersonic air inlet).
  • the gas stream can be compressed as it enters the inlet and both inlet ports 122, forming a high velocity gas stream, then with the gas entering the two turbojet engines 21
  • the speed of the two turbojet engines 21 can be correspondingly improved, and the thrust of the two turbojet engines 21 can be effectively improved.
  • both turbojet engines 21 are vector turbojet engines. Specifically, since both turbojet engines 21 are vector turbojet engines, the traveling device of the embodiment of the present invention can obtain excellent maneuverability by adjusting the jet direction of the vector nozzle of the turbojet engine 21 in the flight mode. .
  • the traveling device of the embodiment of the present invention when the traveling device of the embodiment of the present invention is in the take-off state, by rotating the vector nozzle of the turbojet engine 21 toward the ground, the two turbojet engines 21 and the lift fan 22 can provide three sets of downwards for the traveling device. Thrust, so that it can achieve its vertical takeoff and landing.
  • both flight wings 31 are variable swept wings. Specifically, thanks to the characteristics of the variable swept wing, when the travel equipment needs to increase its flight speed, the variable swept wing can be gathered to form a delta-like layout. When the variable swept wing is fully opened, the line device can be glided to save fuel.
  • the front end of the canopy cover 11 is provided with an observation through cavity (not shown), and the front windshield glass piece 111 is embedded and fixed in the through cavity.
  • the driver can observe the front situation through the front windshield piece 111.
  • the driver can observe the image of the rear of the traveling device captured by the camera module 321 by observing the display control system, thereby eliminating the need to open a rear window at the rear end of the canopy cover 11 , thereby ensuring the cockpit.
  • the overall strength of the cover 11 is not reduced by the presence of excessive portholes.
  • the road running wheel set 40 includes a rear driving wheel 42 and two front driven wheels 41.
  • the rear driving wheel 42 and the two front driven wheels 41 are arranged at the last three points, and the rear driving wheel 42 is disposed. It is connected to the first drive end of the electric motor.
  • the structure benefiting from the rear three-point layout is relatively simple, suitable for a low-speed aircraft and making the aircraft slip and landing distance shorter.
  • the manufacturing cost of the land wheel set 40 is significantly reduced, and the running and landing distances of the travel equipment of the present embodiment of the land wheel set 40 having the last three points layout are also significantly shortened.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

Un dispositif de transport comprend un ensemble boîtier (10), un dispositif d'alimentation (20) et un mécanisme d'aile (30). L'ensemble boîtier (10) comprend un boîtier en forme de disque (12) et une verrière du poste de pilotage (11). Le boîtier en forme de disque (12) est pourvu d'un poste de pilotage. La verrière du poste de pilotage (11) est installée au niveau du boîtier en forme de disque (12) pour sceller le poste de pilotage. Le boîtier en forme de disque (12) est pourvu d'un ensemble roue de déplacement terrestre (40). Le dispositif d'alimentation (20) comprend un moteur électrique et deux turboréacteurs (21). Le moteur électrique est installé au niveau du boîtier en forme de disque (12), et est relié à l'ensemble roue de déplacement terrestre (40). Les deux turboréacteurs (21) sont installés au niveau du boîtier en forme de disque (12). Le mécanisme d'aile (30) comprend un empennage vertical (32) et deux gouvernes de profondeur (31). L'empennage vertical (32) est monté au niveau du boîtier en forme de disque (12). Deux cavités de logement sont disposées sur deux côtés du boîtier en forme de disque (12). Les deux gouvernes de profondeur (31) sont logés dans les deux cavités de logement. Deux moteurs de rotation sont respectivement disposés à l'intérieur des deux cavités de logement. Les deux moteurs de rotation sont reliés aux deux gouvernes de profondeur. En mode vol, les moteurs de rotation entraînent les deux gouvernes de profondeur pour se déplacer hors des cavités de logement et s'étendre. En mode déplacement terrestre, les moteurs de rotation entraînent le logement des deux gouvernes de profondeur dans les deux cavités de logement. L'agencement ci-dessus permet de réduire le coefficient de traînée et la consommation de carburant du dispositif de transport.
PCT/CN2018/085881 2018-04-28 2018-05-07 Dispositif de transport WO2019205187A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN201820639464.0 2018-04-28
CN201820639464.0U CN208306290U (zh) 2018-04-28 2018-04-28 出行设备

Publications (1)

Publication Number Publication Date
WO2019205187A1 true WO2019205187A1 (fr) 2019-10-31

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ID=64714651

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Application Number Title Priority Date Filing Date
PCT/CN2018/085881 WO2019205187A1 (fr) 2018-04-28 2018-05-07 Dispositif de transport

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CN (1) CN208306290U (fr)
WO (1) WO2019205187A1 (fr)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101380881A (zh) * 2007-09-04 2009-03-11 刘新广 变形飞车
US20110042507A1 (en) * 2009-08-19 2011-02-24 Seiford Sr Donald S Convertible Vehicle For Road, Air, and Water Usage
CN102133847A (zh) * 2011-02-28 2011-07-27 孙洪胜 飞行汽车
WO2012148035A1 (fr) * 2011-04-25 2012-11-01 Jung Eun-Ju Automobile volante
US20160272314A1 (en) * 2013-12-31 2016-09-22 Bogdan Radu Flying Car or Drone
CN206357938U (zh) * 2016-12-16 2017-07-28 深圳光启合众科技有限公司 飞行汽车

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101380881A (zh) * 2007-09-04 2009-03-11 刘新广 变形飞车
US20110042507A1 (en) * 2009-08-19 2011-02-24 Seiford Sr Donald S Convertible Vehicle For Road, Air, and Water Usage
CN102133847A (zh) * 2011-02-28 2011-07-27 孙洪胜 飞行汽车
WO2012148035A1 (fr) * 2011-04-25 2012-11-01 Jung Eun-Ju Automobile volante
US20160272314A1 (en) * 2013-12-31 2016-09-22 Bogdan Radu Flying Car or Drone
CN206357938U (zh) * 2016-12-16 2017-07-28 深圳光启合众科技有限公司 飞行汽车

Also Published As

Publication number Publication date
CN208306290U (zh) 2019-01-01

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