CN202528786U - Ground effect type extreme low-altitude dual-purpose flying car - Google Patents
Ground effect type extreme low-altitude dual-purpose flying car Download PDFInfo
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- CN202528786U CN202528786U CN2012201967225U CN201220196722U CN202528786U CN 202528786 U CN202528786 U CN 202528786U CN 2012201967225 U CN2012201967225 U CN 2012201967225U CN 201220196722 U CN201220196722 U CN 201220196722U CN 202528786 U CN202528786 U CN 202528786U
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Abstract
The utility model relates to a ground effect type extreme low-altitude dual-purpose flying car. The ground effect type extreme low-altitude dual-purpose flying car is characterized in that a power device comprises upper and lower rotor wings with coaxial contrarotation, a pair of horizontal duct propellers, a composite air cabinet and a composite air cushion device; the upper rotor wing and the lower rotor wing are arranged on the middle part of a machine frame of a car body and used for providing upward main lifting force; the horizontal duct propellers are arranged on two sides of the rear part of the machine frame of the car body and are used for propelling longitudinally and steering; the composite air cabinet is arranged at the bottom below the machine frame of the car body and used for providing auxiliary lifting force; the composite air cushion device consists of upper and lower gas compressors; the same shaft for mounting the upper rotor wing and the lower rotor wing are coaxially arranged in a vertical duct in the middle of the machine frame of the car body; the composite air cabinet for forming an air cushion consists of three parts A, B and C; and lateral air ducts are arranged on two sides of the machine frame of the car body. The ground effect type extreme low-altitude dual-purpose flying car has a reasonable structure, is easy to manufacture and assemble, can run on the flat road or fly near the ground or the water surface, remits congestion of the urban road, solves the problem of the poor traffic condition of rural and mountainous areas, and has the characteristics of safety, reliability, convenience and flexible travelling mode.
Description
(1), technical field
The utility model relates to a kind of Flight Vehicle Design technical field, and the extreme low-altitude dual-purpose hovercar of formula (also claiming effect level land, the ultralow vacant lot of rotary wind type double-used aircraft) is imitated on particularly a kind of ground that can be used as the car of riding instead of walk.
(2), background technology
Along with expanding economy, be city and rural area traffic construction, or mountain area or Plain network of highways construction have all had great development to improve, still; Have more town dweller to purchase roadlice with the conveniently trip of oneself because of growth in the living standard, at present, the problem of blocking up of urban highway has become the surmountable hardly difficult problem in most cities (or becoming " cancer " that most cities are difficult to cure); Even in rural area and mountain area; Because road width is narrow, transportation condition is poor, often receives the rain drop erosion breakage again; Or the influence of ice and snow sleet, also making originally, unimpeded transportation condition receives very big influence.In addition, the same with all self-propelled vehiclees, roadlice (car) is because of its structural reason; Can only on smooth highway road, go; Even cross-country car also can only be made land locomotion, neither ability with airflight does not have the flight function of air cushion vehicle or other ground effect vehicles yet.Otherwise too, no matter be aircraft or autogyro, or air cushion vehicle or other ground effect vehicles all can't be land locomotion (going) with pointing to; For example, Chinese application number is that 201010263416.4 patent of invention discloses a kind of " VTOL small aircraft ", and this invention is the kinetic energy that utilizes screw propeller to produce; Utilize the blade below the screw propeller to change air flow line again; Make the aircraft can not only VTOL and flight forward, and speed is fast, safety, driver behavior be simple; Be the following desirable vehicle to aerial development, the shortcoming of this small aircraft is can't be land locomotion (going) with pointing to.
In order to overcome above-mentioned defective; China's application number is that 200810045544.4 patent of invention discloses a kind of " hovercar "; This invention is on the structure foundation of existing general-utility car, to install aviation jet engine or rotary propeller type aero-engine again additional and constitute; It has two and overlaps separately independently driving engine and steering unit system, integrates function, the autogyro function of general-utility car.Two kinds of operating mode modes of automobile and autogyro can indiscriminately ad. as one wishes be changed as required, because be in higher high-altitude flight, are equiped with special parachute at the top in compartment, in case of emergency can open to guarantee flight safety.It is safe, reliable, convenient that hovercar has, the characteristic of mode of operation maneuverability.And for example; China's application number is that 201110151353.8 patent of invention also discloses other a kind of " hovercar "; This invention is on the carriage top of existing automobile, to install aero-engine and telescopic movable wing additional; Aero-engine moves in company with telescopic wing with hydraulic operation on wing in roof fixed installation or device; Can the reciprocating type deflection angle of 0 to 90 degree at the propeller type driving engine of roof hydraulic telescopic type wing two end devices, the deflection angle that changes the rotary propeller type driving engine can VTOL.This invention has automobile equally and aircraft two overlaps driving engine and the maneuvering system that works alone, and is provided with fuel tank and multi-layer combined type parachute at car body top, is provided with normal limb at the roof afterbody, and flight safety is reliable, of many uses, and application prospect is fine.But the shortcoming that above-mentioned hovercar exists is a complex structure, installation and maintenance convenience, and the cost cost is high, because be in higher high-altitude flight, though all be equiped with special parachute at car body top, still lacks the sense of security again.
(3), summary of the invention
The purpose of the utility model is the weak point that will overcome prior art; Thereby provide a kind of rational in infrastructure; The manufacturing process and assemble is easy; Can be on highway cruising, again can ground proximity or the ground of the VTOL of water surface flying imitate the extreme low-altitude dual-purpose hovercar of formula (also claim the ultralow vacant lot of rotary wind type imitate the level land double-used aircraft).Use the favourable alleviation urban road congestion of this hovercar problem, and the problem of favourable solution rural area and mountain road unhampered low of traffic condition difference, have safe, reliable, convenient, the characteristics of trip mode maneuverability.
The utility model constitutes with following technical scheme: it comprises car body part, power pack part and the complex control system of forming the ground run system; The body portions branch of forming the ground run system comprises vehicle body frame, chassis, bearing circle, drive wheels; Power pack partly comprises power supply and engine installation, it is characterized in that:
1), said engine installation comprises: the last rotor that contrarotation is housed and following rotor that are installed in the vehicle body central rack; Through last rotor and following rotor contrarotation to provide and to produce the main lift that makes progress; Be installed in a pair of horizontal shrouded propeller and the motor that drives its running that has vertical propelling concurrently and turn to usefulness of both sides, vehicle body frame rear portion, be installed in the composite air cushion device that plaing of vehicle body frame lower bottom part provides the composite air of auxiliary lifting effect cabinet and upper and lower air compressor thereof to form;
2), be provided with a vertical duct at the middle part of said vehicle body frame; The said coaxial conduct that is contained in first main shaft outside by first main shaft and movable installation sleeve as inner main axis that is used to install rotor and following rotor second main shaft of main shaft is outward formed, and they are coaxial to be installed in the vertical duct of vehicle body central rack; The described rotor of going up is mounted in inner main axis, promptly on first main shaft, below first main shaft, is installed with a crowngear assembly, and is connected for last rotor provides the motor output shaft of running power with one through a plunging joint; Described following rotor is mounted in outer main shaft, promptly on second main shaft, below second main shaft, also is installed with a crowngear assembly, and is connected for following rotor provides the motor output shaft of running power through a plunging joint and;
3), in described coaxial outside; Promptly the outside of second main shaft of the outer main shaft of conduct is movably installed with an outer shaft (i.e. the 3rd main shaft); At outer shaft is that the 3rd main shaft upper fixed is equipped with air compressor on (being positioned at vertical duct inlet place); Promptly be installed with a crowngear assembly below the 3rd main shaft at outer shaft, and be connected for last air compressor provides the motor output shaft of running power with one through a plunging joint;
4), be provided with air compressor main shaft (being called four main again) in the bottom of said first main shaft as inner main axis; The bottom of described first main shaft as inner main axis is connected with said air compressor main shaft (claiming four main again) down through the plunging joint that Limit Bearing is housed in; Described air compressor main shaft (i.e. four main) down is installed in the limit shaft bearing; The position of stretching among the composite air cabinet C in following air compressor main shaft (i.e. four main) bottom is installed with air compressor (claiming main air compressor again); In said following air compressor main shaft (i.e. four main) upper fixed one crowngear assembly is installed, and is connected for following air compressor provides the motor output shaft of running power through a plunging joint and;
5), the said air-sprung composite air cabinet that is used to form is made up of A, B, C three parts; Wherein A part buoyance chamber is to be made up of vertical duct; Wherein B part buoyance chamber is to be made up of the space that is positioned at the car chassis below; The admission port of said B part buoyance chamber is and A part buoyance chamber, and promptly the air extractor duct of vertical duct is connected, and the air extractor duct of B part buoyance chamber is distributed in the edge part (side that is below around the automobile is along portion) of car chassis below; Below B part buoyance chamber, has an interlayer board; Wherein C part buoyance chamber is to be made up of the space that is positioned at interlayer board below (being B part buoyance chamber below), is provided with the side direction air channel (duct) that is used to C part buoyance chamber air feed in the both sides of vehicle body frame, and the admission port of said C part buoyance chamber is to be connected with the air extractor duct in said side direction air channel (duct).
The utility model is when specifically manufacturing and designing, and its technical characterictic also can further be specially:
One, the last rotor of described contrarotation and following rotor are to process short limb type (wing) structure; Its length is less than or equal to the width of auto body; Outer at last rotor and following rotor is provided with the rotor guard ring, and said rotor guard ring is to be fixed on the forward and backward taper guard ring frame of vehicle body frame top.
Two, air compressor is the admission port place that is positioned at vertical duct on described.
Three, described coaxial bottom is to be connected with following air compressor main shaft (claiming four main again) through the plunging joint that Limit Bearing is housed in as the bottom of first main shaft of inner main axis promptly.
Four, the body shell above the described frame is a modeling structure of processing arc curve, below the vehicle body frame, is provided with all around and is used to form the air-sprung apron.
Five, the described drive wheels device that is used for ground run is formed (drive wheels that is equivalent to battery-driven car) by forward and backward (vertically advancing usefulness) motorized motions wheel, in each drive wheels device, all be provided with one vertically advance usefulness the level road driving motor.
The utility model is rational in infrastructure; The manufacturing process and assemble is easy, can be on highway cruising, again can ground proximity or the water surface do hedgehopping; Favourable alleviation urban road congestion problem; And solve the problem of rural area and mountain road unhampered low of traffic condition difference, have safe, reliable, convenient, the characteristics of trip mode maneuverability.
(4), description of drawings
Fig. 1 is a kind of integral structure scheme drawing of the utility model hedgehopping automobile.
Fig. 2 is the plan structure scheme drawing of Fig. 1.
Fig. 3 is the right TV structure scheme drawing (the back structural representation of hedgehopping automobile) of Fig. 1.
(5), the specific embodiment
Can know that with reference to accompanying drawing the concrete parts that formula hedgehopping automobile is imitated on the utility model ground comprise: 1～vehicle body frame, 2～go up rotors, 3～following rotor, 4～as first main shaft of inner main axis; 5～rotor guard ring (screened housing), second main shaft of the outer main shaft of 6～conduct, 7～outer shaft (i.e. the 3rd main shaft), 8～upward air compressors; 9～crowngear assembly (claiming the crowngear case again), 10～plunging joint, 11～be the motor that last air compressor provides running power, 12～crowngear assembly; 13～plunging joint, 14～be the motor that following rotor provides running power, 15～crowngear assembly, 16～plunging joint; 17～for last rotor provides the motor of running power, 18～in the plunging joint of Limit Bearing, 19～crowngear assembly, 20～plunging joint are housed; 21～for following air compressor (main air compressor) provides the motor of running power, 22～have vertical propelling concurrently and turn to the horizontal shrouded propeller of usefulness, 23～following air compressor main shaft (i.e. four main), 24～limit shaft bearing; 25～following air compressor (claiming main air compressor again), 26～vertically advance the preceding motorized motions wheel of usefulness, and 27～vertically advance the back motorized motions wheel of usefulness, 28～level road driving motor (drive wheels motor); 29～axletree, 30～electric control and drive controlling bin (be electrical control cubicles, form complex control system), 31～bearing circle; 32～driver's chair, 33～apron, 34～apron hook, 35～battry storage cabinet (interior holding storage battery); 36～battry storage cabinet (interior holding storage battery), 37～front chair, 38～back seat, 39～preceding taper guard ring frame; 40～back taper guard ring frame, 41～vertical duct (air channel is promptly as A part buoyance chamber), 42～B part buoyance chamber; 43～B part buoyance chamber air extractor duct (being distributed in the end end to end of car chassis), 44～interlayer board, 45～C part buoyance chamber, 46～be used for the side direction air channel (duct) of C part buoyance chamber air feed.
With reference to accompanying drawing embodiment; The technical scheme of practical implementation the utility model is: it still comprises car body part, power pack part and the complex control system of forming the ground run system; The body portions branch of forming the ground run system comprises vehicle body frame 1, chassis, bearing circle, drive wheels; Power pack partly comprises power supply and engine installation, it is characterized in that:
1), said engine installation comprises: the last rotor that contrarotation is housed 2 and following rotor 3 that are installed in the vehicle body central rack; Through last rotor and following rotor contrarotation to provide and to produce the main lift that makes progress; Be installed in a pair of horizontal shrouded propeller 22 and the motor that drives its running that has vertical propelling concurrently and turn to usefulness of both sides, vehicle body frame rear portion, be installed in the composite air cushion device that plaing of vehicle body frame lower bottom part provides the composite air of auxiliary lifting effect cabinet and upper and lower air compressor 8,25 thereof to be formed;
2), be provided with a vertical duct (air channel) 41 at the middle part of said vehicle body frame 1; Described be used to install rotor and following rotor coaxial by the conduct that is contained in first main shaft outside as first main shaft 4 of inner main axis and movable installation sleeve outward second main shaft 6 of main shaft form, they are coaxial to be installed in the vertical duct (air channel) 41 of vehicle body central rack; The described rotor of going up is mounted in inner main axis, promptly on first main shaft, below first main shaft, is installed with a crowngear assembly 15, and is connected for last rotor provides motor 17 output shafts of running power with one through a plunging joint 16; Described following rotor is mounted in outer main shaft, promptly on second main shaft, below second main shaft, also is installed with a crowngear assembly 12, and is connected for following rotor provides motor 14 output shafts of running power through a plunging joint 13 and;
3), in described coaxial outside; Promptly the outside of second main shaft 6 of the outer main shaft of conduct is movably installed with an outer shaft (promptly as the 3rd main shaft) 7; At outer shaft is that the 3rd main shaft 7 upper fixed are equipped with air compressor 8 on (being positioned at vertical duct inlet place); Promptly be installed with a crowngear assembly 9 below the 3rd main shaft at outer shaft, and be connected for last air compressor 8 provides motor 11 output shafts of running power with one through a plunging joint 10;
4), be provided with air compressor main shaft 23 (being called four main 23 again) in the bottom of said first main shaft 4 as inner main axis; The bottom of described first main shaft 4 as inner main axis is connected with said air compressor main shaft (being called four main again) 23 down through the plunging joint 18 that Limit Bearing is housed in; Described air compressor main shaft 23 (i.e. four main) down is installed in the limit shaft bearing 24; The position of stretching among the composite air cabinet C in following air compressor main shaft 23 (i.e. four main) bottom is installed with air compressor (claiming main air compressor again) 25; In said following air compressor main shaft 23 (promptly four main 23) upper fixed one crowngear assembly 19 is installed, and is connected for following air compressor (main air compressor) 25 provides motor 21 output shafts of running power through a plunging joint 20 and;
5), the said air-sprung composite air cabinet that is used to form is made up of A, B, C three parts; Wherein A part buoyance chamber is to constitute (formation) by vertical duct (air channel) 41; Wherein B part buoyance chamber 42 is to constitute (formation) by the space that is positioned at the car chassis below; The admission port of said B part buoyance chamber 42 is and A part buoyance chamber; The air extractor duct that is vertical duct (air channel) 41 is connected; The air extractor duct 43 of B part buoyance chamber is distributed in the edge part (side that is below around the automobile is along portion) of car chassis below, below B part buoyance chamber 42, has an interlayer board 44, and wherein C part buoyance chamber 45 is to be made up of the space that is positioned at interlayer board 44 belows (being B part buoyance chamber below); Be provided with the side direction duct (air channel) 46 that is used to C part buoyance chamber 45 air feed in the both sides of vehicle body frame, the admission port of said C part buoyance chamber 45 is to be connected with the air extractor duct in said side direction air channel (duct) 46.
The utility model is when specifically manufacturing and designing, and its technical characterictic also can further be specially:
One, the last rotor 2 of described contrarotation and following rotor 3 are to process short limb type (wing) structure; Its length is less than or equal to the width of auto body; Outer at last rotor and following rotor is provided with rotor guard ring (screened housing) 5, and said rotor guard ring (screened housing) the 5th is fixed on the forward and backward taper guard ring frame 39,40 of vehicle body frame top.
Two, air compressor 8 is the admission port places that are positioned at vertical duct (air channel) 41 on described.
Three, described coaxial bottom is to be connected with following air compressor main shaft 23 (claiming four main 23 again) through the plunging joint 18 that Limit Bearing is housed in as the bottom of first main shaft of inner main axis promptly.
Four, the body shell above the described frame is a modeling structure of processing arc curve (conveyor line), below the vehicle body frame, is provided with all around and is used to form air-sprung apron 33.
Five, the described drive wheels device that is used for ground run is formed (drive wheels that is equivalent to battery-driven car) by 26,27 of forward and backward motorized motions wheels, in each drive wheels device, all is provided with a vertical level road driving motor that advances usefulness.
The principle of work process of the utility model is following:
When making ground run; It (is electrical control cubicles that chaufeur starts the electric control and the drive controlling bin that are positioned at headstock bearing circle 31 the place aheads; The composition complex control system) the flat pavement running button switch on 30 panels; Start the level road driving motor (drive wheels motor) 28 of ground run, drive front and back motorized motions wheel 26,27 runnings of making vertically to advance usefulness, can make level road ground run (control method is identical with existing electronlmobil).
Receive rain drop erosion damaged when running into congestion in road or road; Or influenced by the ice and snow sleet; In the time of should imitating formula hedgehopping with doing; Chaufeur start on the electric control be positioned at headstock bearing circle 31 the place aheads and drive controlling bin (be electrical control cubicles, form complex control system) 30 panels for upper and lower rotor provides the button switch of the motor 17,14 of running power, through last rotor and following rotor contrarotation to provide and to produce the main lift that makes progress; Start the button switch that is used for the composite air cushion device, make motor 11,21 runnings that running power is provided for upper and lower air compressor 8,25, thereby the composite air cabinet below car chassis forms air cushion so that auxiliary lifting to be provided; Start the button switch that vertically advances and turn to usefulness; Make a pair of horizontal shrouded propeller 22 and the motor rotation work that drives its running that has vertical propelling concurrently and turn to usefulness that is installed in both sides, vehicle body frames rear portion, the vertical propelling in the time of hedgehopping can being done and turn to purposes.
Claims (6)
1. the extreme low-altitude dual-purpose hovercar of formula is imitated on a ground; It comprises car body part, power pack part and the complex control system of forming the ground run system; The body portions branch of forming the ground run system comprises vehicle body frame (1), chassis, bearing circle, drive wheels; Power pack partly comprises power supply and engine installation, it is characterized in that:
1), said engine installation comprises: the last rotor (2) that contrarotation is housed and the following rotor (3) that are installed in the vehicle body central rack; Through last rotor and following rotor contrarotation to provide and to produce the main lift that makes progress; Be installed in a pair of of both sides, vehicle body frame rear portion and have vertical propelling concurrently and turn to the horizontal shrouded propeller (22) of usefulness and the motor of its running of driving, be installed in the composite air cushion device that plaing of vehicle body frame lower bottom part provides the composite air of auxiliary lifting effect cabinet and upper and lower air compressor (8,25) thereof to be formed;
2), be provided with a vertical duct (41) at the middle part of said vehicle body frame (1); Described be used to install rotor and following rotor coaxial by be contained in as first main shaft (4) of inner main axis and movable installation sleeve outside first main shaft conduct outward second main shaft (6) of main shaft form, they are coaxial to be installed in the vertical duct (41) of vehicle body central rack; The described rotor of going up is mounted in inner main axis, promptly on first main shaft, below first main shaft, is installed with a crowngear assembly (15), and is connected for last rotor provides motor (17) output shaft of running power with one through a plunging joint (16); Described following rotor is mounted in outer main shaft, promptly on second main shaft, below second main shaft, also is installed with a crowngear assembly (12), and is connected for following rotor provides motor (14) output shaft of running power through a plunging joint (13) and;
3), in described coaxial outside; Promptly the outside of second main shaft (6) of the outer main shaft of conduct is movably installed with i.e. the 3rd main shaft (7) of an outer shaft; At outer shaft is that the 3rd main shaft (7) upper fixed is equipped with air compressor on (8); Promptly be installed with a crowngear assembly (9) below the 3rd main shaft at outer shaft, and be connected for last air compressor (8) provides motor (11) output shaft of running power with one through a plunging joint (10);
4), be provided with air compressor main shaft (23) in the bottom of said first main shaft (4) as inner main axis; The bottom of described first main shaft (4) as inner main axis is to be connected with said air compressor main shaft (23) down through the plunging joint (18) that Limit Bearing is housed in; Described air compressor main shaft (23) down is installed in the limit shaft bearing (24); The position of stretching among the composite air cabinet C in following air compressor main shaft (23) bottom is installed with air compressor (25); In said following air compressor main shaft (23) upper fixed one crowngear assembly (19) is installed, and is connected for following air compressor (25) provides motor (21) output shaft of running power through a plunging joint (20) and;
5), said be used to form air-sprung composite air cabinet by 1, B, C three parts form; Wherein 1 part buoyance chamber is to be made up of vertical duct (41); Wherein B part buoyance chamber (42) is to be made up of the space that is positioned at the car chassis below; The admission port of said B part buoyance chamber (42) is and A part buoyance chamber; The air extractor duct that is vertical duct (41) is connected, and the air extractor duct (43) of B part buoyance chamber is distributed in the edge part of car chassis below, has an interlayer board (44) in the below of B part buoyance chamber (42); Wherein C part buoyance chamber (45) is by being positioned at interlayer board (44) below; The space that is B part buoyance chamber below constitutes, and is provided with the side direction air channel (46) that is used to C part buoyance chamber (45) air feed in the both sides of vehicle body frame, and the admission port of said C part buoyance chamber (45) is to be connected with the air extractor duct in said side direction air channel (46).
2. the extreme low-altitude dual-purpose hovercar of the formula of imitating according to claim 1ly; It is characterized in that: the last rotor (2) of described contrarotation and following rotor (3) are to process short limb type structure; Its length is less than or equal to the width of auto body; Outer at last rotor and following rotor is provided with rotor guard ring (5), and said rotor guard ring (5) is to be fixed on the forward and backward taper guard ring frame (39,40) of vehicle body frame top.
3. the extreme low-altitude dual-purpose hovercar of the formula of imitating is characterized in that according to claim 1ly: air compressor (8) is the admission port place that is positioned at vertical duct (41) on described.
4. the extreme low-altitude dual-purpose hovercar of the formula of imitating is characterized in that according to claim 1ly: described coaxial bottom is to be connected with following air compressor main shaft (23) through the plunging joint (18) that Limit Bearing is housed in as the bottom of first main shaft of inner main axis promptly.
5. the extreme low-altitude dual-purpose hovercar of the formula of imitating is characterized in that according to claim 1ly: the body shell of described frame top is a modeling structure of processing arc curve, below the vehicle body frame, is provided with all around and is used to form air-sprung apron (33).
6. the extreme low-altitude dual-purpose hovercar of the formula of imitating according to claim 1ly; It is characterized in that: the described drive wheels device that is used for ground run is made up of forward and backward motorized motions wheel (26,27), in each drive wheels device, all is provided with a vertical level road driving motor that advances usefulness.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012201967225U CN202528786U (en) | 2012-05-03 | 2012-05-03 | Ground effect type extreme low-altitude dual-purpose flying car |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012201967225U CN202528786U (en) | 2012-05-03 | 2012-05-03 | Ground effect type extreme low-altitude dual-purpose flying car |
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| Publication Number | Publication Date |
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| CN202528786U true CN202528786U (en) | 2012-11-14 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012201967225U Expired - Lifetime CN202528786U (en) | 2012-05-03 | 2012-05-03 | Ground effect type extreme low-altitude dual-purpose flying car |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102649391A (en) * | 2012-05-03 | 2012-08-29 | 张瑞钧 | Ground-effect type extreme low-altitude dual-purpose aerocar or dual-purpose aircraft |
| CN102795070A (en) * | 2012-09-03 | 2012-11-28 | 张廷林 | Aeroamphibious triphibian aircraft with machine body capable of fully balancing stress |
| CN104842728A (en) * | 2014-08-12 | 2015-08-19 | 北汽福田汽车股份有限公司 | Hovercar and control system thereof |
| CN109291744A (en) * | 2018-10-24 | 2019-02-01 | 罗睿轩 | The air-cushion device for traffic traveling flight tool and being remotely controlled traffic toy and its using |
| WO2020083109A1 (en) * | 2018-10-24 | 2020-04-30 | 罗睿轩 | Driving flight vehicle and remote control toy vehicle, and air cushion device used by same |
| CN111891373A (en) * | 2020-07-27 | 2020-11-06 | 淮阴工学院 | Multi-position split type land air-berthing unmanned aerial vehicle |
| RU2746285C1 (en) * | 2020-10-19 | 2021-04-12 | Юлай Масабихович Насибуллин | Autoplane |
-
2012
- 2012-05-03 CN CN2012201967225U patent/CN202528786U/en not_active Expired - Lifetime
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102649391A (en) * | 2012-05-03 | 2012-08-29 | 张瑞钧 | Ground-effect type extreme low-altitude dual-purpose aerocar or dual-purpose aircraft |
| CN102649391B (en) * | 2012-05-03 | 2014-08-27 | 张瑞钧 | Ground-effect type extreme low-altitude dual-purpose aerocar or dual-purpose aircraft |
| CN102795070A (en) * | 2012-09-03 | 2012-11-28 | 张廷林 | Aeroamphibious triphibian aircraft with machine body capable of fully balancing stress |
| CN104842728A (en) * | 2014-08-12 | 2015-08-19 | 北汽福田汽车股份有限公司 | Hovercar and control system thereof |
| CN109291744A (en) * | 2018-10-24 | 2019-02-01 | 罗睿轩 | The air-cushion device for traffic traveling flight tool and being remotely controlled traffic toy and its using |
| WO2020083109A1 (en) * | 2018-10-24 | 2020-04-30 | 罗睿轩 | Driving flight vehicle and remote control toy vehicle, and air cushion device used by same |
| CN111891373A (en) * | 2020-07-27 | 2020-11-06 | 淮阴工学院 | Multi-position split type land air-berthing unmanned aerial vehicle |
| RU2746285C1 (en) * | 2020-10-19 | 2021-04-12 | Юлай Масабихович Насибуллин | Autoplane |
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