CN204674321U - Light-weight vertical landing hovercar - Google Patents
Light-weight vertical landing hovercar Download PDFInfo
- Publication number
- CN204674321U CN204674321U CN201520307227.0U CN201520307227U CN204674321U CN 204674321 U CN204674321 U CN 204674321U CN 201520307227 U CN201520307227 U CN 201520307227U CN 204674321 U CN204674321 U CN 204674321U
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- CN
- China
- Prior art keywords
- landing
- ducted fan
- wing
- vertical takeoff
- hovercar
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Abstract
The utility model provides a kind of light-weight vertical landing hovercar, and hovercar all needs to take off by runway and land mostly at present, brings great inconvenience to user.The utility model body tail is provided with the vertical takeoff and landing ducted fan (9) providing vertical takeoff and landing power, drives the driving engine of vertical takeoff and landing ducted fan (9) to drive rear wheel hub by drop-gear box.Body forward structure bilateral symmetry is provided with two and advances ducted fan (13), by control setup vert advance the spout of ducted fan (13) downwards and vertical takeoff and landing ducted fan (9) together forms 3 thrusts and stablizes rising.Having can the feature of vertical takeoff and landing, can be used as automobile at ordinary times and travels on road surface, can save the energy to greatest extent; And can free flight aloft in crucial moment, show its advantage fast and easily fully.
Description
Technical field
The utility model relates to a kind of vehicle that can be exchanged into aircraft, is specially a kind of vertical take-off and landing flying car.
Background technology
Current ground automobile is all travelled on the ground by transmission device driving automobile wheel by driving engine, and when Modern Traffic automobile is increasing, traffic jam has been the subject matter of ground automobile.Aircraft and helicopter can aloft fly, but cost is too high, and consumption of fuel is large, and driving technique is complicated.For this reason, all someone proposes in conjunction with existing automobile and aeronautical technology recent domestic, development can dual-purpose " hovercar " in empty land, these hovercars proposed at present mostly adopt to install additional on existing automobile basis wing also with provide automobile go up to the air needed for lift.But these hovercars all need to take off by runway and land, and need just can go up road traveling after specific place is by wing-folding, therefore they are when carrying out road running and airflight, all need to have come by specific place, bring great inconvenience to user.
Summary of the invention
For solving the problem, the utility model provides a kind of hovercar being suitable for the petite profile of road running, extremely low noise and pollution, and this hovercar can realize, from highway to aerial direct conversion, not needing by any place.
For achieving the above object, the utility model adopts following technological means: a kind of light-duty can vertical take-off and landing flying car, it is the relative theory in conjunction with automobile and aircraft, composition can the lightweight aircraft of vertical takeoff and landing, comprise vehicle body, wheel 1, wing, ducted fan and yaw rudder etc., vehicle body head is provided with whole wing 2, and the afterbody of whole wing 2 is provided with winglet 3, and winglet 3 can reduce to induce power-assisted; Vehicle body middle front part is provided with driving compartment 4, and driving compartment 4 is provided with boot compartment 5 below.
Vehicle body top is provided with the ring wing 6, be provided with annular aileron 7 and ring wing yaw rudder 8 below the ring wing 6 successively, whole wing 2 and the ring wing 6 provide lift jointly, ensure lift during flight, in automobile tail install flight during operate rudder face accordingly, ensure flight during handling; The described ring wing 6 is in streamlined structure, and top and both sides hide.
Body tail is provided with the vertical takeoff and landing ducted fan 9 providing vertical takeoff and landing power, drives the driving engine of vertical takeoff and landing ducted fan 9 to drive rear wheel hub by drop-gear box.Be provided with whole wing yaw rudder 10 below body tail, be provided with aileron 11 and wing flap 12 below whole wing yaw rudder 10, aileron 11 is for controlling rolling, and wing flap 12 can increase lift.
Body forward structure bilateral symmetry is provided with two and advances ducted fans 13, by control setup vert advance the spout of ducted fan 13 downwards and vertical takeoff and landing ducted fan 9 together forms 3 thrusts and stablizes rising.
When travelling on the ground, the lid of its body tail vertical takeoff and landing ducted fan mouth closes, and becomes a car, drives the driving engine of vertical takeoff and landing ducted fan to drive rear wheel hub by drop-gear box, moves forward.
During vertical takeoff and landing, the lid of vertical takeoff and landing ducted fan mouth is opened, by two advance ducted fans 13 by control setup vert spout downwards and vertical takeoff and landing ducted fan 9 together forms 3 thrusts and stablizes rising, and two that are verted by control 360 ° of directions advance ducted fan 13 spouts, control complete machine and stablize vertical takeoff and landing, hover, turn to, advance and reversing etc.
When aloft flying, the lid of vertical takeoff and landing ducted fan mouth closes, only advance ducted fan 9 to provide onward impulse by two, provide lift by whole wing and the ring wing, realized the balance of aircraft aerial sports by conventional airplane maneuvering systems such as wing flap, aileron and yaw rudders.
beneficial effect:1. described in the utility model light-duty can vertical take-off and landing flying car, as the one of small sized personal aircraft, it to be suitable in the petite profile of road running, extremely low noise and pollution, culvert type structure and airworthiness unique advantage, makes it particularly be with a wide range of applications in stereo urban traffic in civilian.
2. described in the utility model light-duty can vertical take-off and landing flying car size little, can vertical takeoff and landing, can in average highway or meadow landing, flight, can free shuttling between each building, realize hedgehopping.
3. described in the utility model light-duty can vertical take-off and landing flying car be a kind of aircraft in conjunction with aircraft and automobile, can be used as automobile at ordinary times and travel on road surface, the energy can be saved to greatest extent; And can free flight aloft in crucial moment, show its advantage fast and easily fully.
4. two advance ducted fan not only can provide power, also provide corresponding deflecting torque, ensure that hovercar does not spin during landing.
Accompanying drawing explanation
Fig. 1 is the utility model spatial structure schematic views.
Fig. 2 is the utility model inner structure schematic views.
In figure: wheel 1, whole wing 2, winglet 3, driving compartment 4, boot compartment 5, the ring wing 6.Annular aileron 7, ring wing yaw rudder 8, vertical takeoff and landing ducted fan 9, whole wing yaw rudder 10, aileron 11, wing flap 12.
Detailed description of the invention
embodiment 1:a kind of light-duty can vertical take-off and landing flying car, it is the relative theory in conjunction with automobile and aircraft, composition can the lightweight aircraft of vertical takeoff and landing, comprise vehicle body, wheel 1, wing, ducted fan and yaw rudder etc., vehicle body head is provided with whole wing 2, the afterbody of whole wing 2 is provided with winglet 3, and vehicle body middle front part is provided with driving compartment 4, and driving compartment 4 is provided with boot compartment 5 below.Vehicle body top is provided with the ring wing 6, is provided with annular aileron 7 below the ring wing 6 successively, ring wing yaw rudder 8, and the described ring wing 6 is in streamlined structure, and top and both sides hide.Body tail is provided with the vertical takeoff and landing ducted fan 9 providing vertical takeoff and landing power, drives the driving engine of vertical takeoff and landing ducted fan 9 to drive rear wheel hub by drop-gear box.Be provided with whole wing yaw rudder 10 below body tail, be provided with aileron 11 and wing flap 12 below whole wing yaw rudder 10, aileron 11 is for controlling rolling, and wing flap 12 can increase lift.
Body forward structure bilateral symmetry is provided with two and advances ducted fans 13, by control setup vert advance the spout of ducted fan 13 downwards and vertical takeoff and landing ducted fan 9 together forms 3 thrusts and stablizes rising.When travelling on the ground, the lid of its body tail vertical takeoff and landing ducted fan mouth closes, and becomes a car, drives the driving engine of vertical takeoff and landing ducted fan to drive rear wheel hub by drop-gear box, moves forward.During vertical takeoff and landing, the lid of vertical takeoff and landing ducted fan mouth is opened, by two advance ducted fans 13 by control setup vert spout downwards and vertical takeoff and landing ducted fan 9 together forms 3 thrusts and stablizes rising, and two that are verted by control 360 ° of directions advance ducted fan 13 spouts, control complete machine and stablize vertical takeoff and landing, hover, turn to, advance and reversing etc.When aloft flying, the lid of vertical takeoff and landing ducted fan mouth closes, only advance ducted fan 9 to provide onward impulse by two, provide lift by whole wing and the ring wing, realized the balance of aircraft aerial sports by conventional airplane maneuvering systems such as wing flap, aileron and yaw rudders.
Claims (2)
1. a light-weight vertical landing hovercar, comprise vehicle body, wheel (1), wing, ducted fan and yaw rudder, it is characterized in that: vehicle body head is provided with whole wing (2), the afterbody of whole wing (2) is provided with winglet (3), vehicle body middle front part is provided with driving compartment (4), and driving compartment (4) is provided with boot compartment (5) below;
Vehicle body top is provided with the ring wing (6), and the ring wing (6) below is provided with annular aileron (7) and ring wing yaw rudder (8) successively;
Body tail is provided with the vertical takeoff and landing ducted fan (9) providing vertical takeoff and landing power, drives the driving engine of vertical takeoff and landing ducted fan (9) to drive rear wheel hub by drop-gear box; Be provided with whole wing yaw rudder (10) below body tail, whole wing yaw rudder (10) below is provided with aileron (11) and wing flap (12);
Body forward structure bilateral symmetry is provided with two and advances ducted fan (13), by control setup vert advance the spout of ducted fan (13) downwards and vertical takeoff and landing ducted fan (9) together forms 3 thrusts and stablizes rising.
2. light-weight vertical landing hovercar according to claim 1, is characterized in that: the described ring wing (6) is in streamlined structure, and top and both sides hide.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520307227.0U CN204674321U (en) | 2015-05-14 | 2015-05-14 | Light-weight vertical landing hovercar |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520307227.0U CN204674321U (en) | 2015-05-14 | 2015-05-14 | Light-weight vertical landing hovercar |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204674321U true CN204674321U (en) | 2015-09-30 |
Family
ID=54174038
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520307227.0U Expired - Fee Related CN204674321U (en) | 2015-05-14 | 2015-05-14 | Light-weight vertical landing hovercar |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204674321U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109649648A (en) * | 2019-01-15 | 2019-04-19 | 王越 | A kind of twin screw VTOL vesica piscis rotor aircraft |
| CN110524521A (en) * | 2019-09-11 | 2019-12-03 | 孙文卿 | A kind of transfer of intellect service robot |
-
2015
- 2015-05-14 CN CN201520307227.0U patent/CN204674321U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109649648A (en) * | 2019-01-15 | 2019-04-19 | 王越 | A kind of twin screw VTOL vesica piscis rotor aircraft |
| CN109649648B (en) * | 2019-01-15 | 2019-12-17 | 王越 | Manufacturing method of double-propeller vertical take-off and landing elliptical ring wing aircraft |
| CN110524521A (en) * | 2019-09-11 | 2019-12-03 | 孙文卿 | A kind of transfer of intellect service robot |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150930 Termination date: 20160514 |