WO2021109529A1 - Flying car - Google Patents
Flying car Download PDFInfo
- Publication number
- WO2021109529A1 WO2021109529A1 PCT/CN2020/095625 CN2020095625W WO2021109529A1 WO 2021109529 A1 WO2021109529 A1 WO 2021109529A1 CN 2020095625 W CN2020095625 W CN 2020095625W WO 2021109529 A1 WO2021109529 A1 WO 2021109529A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- folding
- wing
- folding shaft
- motor box
- propeller
- Prior art date
Links
- 239000011521 glass Substances 0.000 claims description 11
- 238000010586 diagram Methods 0.000 description 4
- 238000009434 installation Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
-
- 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
Definitions
- the invention relates to the technical field of aircraft design, in particular to a flying car.
- flying cars such as four flying cars with ducted rotors, a flying car with foldable wings, and two flying cars with ducted fans placed inside the body.
- Cars etc. four flying cars with ducted rotors can provide lift and forward power by controlling the speed and direction of the four ducts at the same time, but the structure of this flying car is too heavy and complicated to handle; it has a foldable
- the wings are folded and folded on both sides when driving on the ground and need to be unfolded when flying.
- the folding and folding of the wings after landing is more troublesome, and it cannot be completely folded, and it is easy to damage the wing. .
- the objective of the present invention is to address the shortcomings of the current technology and provide a flying car, which solves the problem of folding and folding the wings after landing in the prior art, which cannot be completely folded, and is easy to be damaged by bumps.
- Technical problems of the wing are to address the shortcomings of the current technology and provide a flying car, which solves the problem of folding and folding the wings after landing in the prior art, which cannot be completely folded, and is easy to be damaged by bumps.
- the present invention provides a flying car, including a fuselage and wheels, characterized in that: a first wing compartment and a second wing compartment are provided on the fuselage, and the first wing compartment is provided on the fuselage.
- a wing compartment is provided with two wing compartments respectively located on both sides of the fuselage, the second wing compartment is located above the fuselage, the first wing compartment and the second wing compartment are respectively provided with folding wings, so
- the folding wing includes a first folding shaft, a second folding shaft, and a third folding shaft.
- the first, second, and third folding shafts are sleeved, and the size of the first folding shaft is larger than The size of the second folding shaft, the size of the second folding shaft is larger than the size of the third folding shaft, the third folding shaft is connected with a motor box, and the motor box is rotatably arranged relative to the third folding shaft.
- a propeller is installed above the motor box, a propeller driving motor is arranged in the motor box, and the propeller is folded relative to the propeller groove.
- the first folding shaft is provided with a folding wing installation hole, and the folding wing is respectively installed in the first wing compartment and the second wing compartment through the folding wing installation holes.
- the end of the first folding shaft is in the shape of an arc, and a number of protrusions are arranged along the circumferential direction of the arc, and the first wing compartment and the second wing compartment are respectively provided with circles.
- the arc-shaped groove is provided with a number of indents along the circumferential direction of the groove, the end of the first folding shaft is installed in the arc-shaped groove, and the protrusions are embedded in the indents.
- a motor box slot is provided on the third folding shaft, and the motor box is rotatably placed in the motor box slot.
- propeller grooves are respectively provided on the sides of the motor box, and the propellers are foldably placed in the propeller grooves.
- a mudguard is installed on the wheel, the mudguard includes a front mudguard and a rear mudguard, the front mudguard is installed behind the wheel in the direction of rotation, and the rear mudguard The plate is installed in front of the direction of rotation of the wheel.
- the fuselage is further provided with a glass window, a front lamp and a turn signal
- the glass window is semicircular and is located above the fuselage
- the front lamp and the turn signal are provided with two pairs and are respectively located at Both sides of the glass window.
- a trunk and a taillight are provided at the rear of the fuselage, and a trunk key hole for opening the trunk is provided on the trunk.
- the present invention has the following beneficial effects:
- the present invention is provided with folding wings in the first wing compartment and the second wing compartment, so that the folding wings can be quickly retracted into the first wing compartment and the second wing compartment when the flying car is running on the ground.
- the first folding axis, the second folding axis, the third folding axis, the propeller and the motor box are tightly stowed to ensure that the flying car will not have folding wings protruding out of its surface when driving on the ground, ensuring the folding wings
- the folding wings are quickly unfolded, the first folding axis is unfolded outside the first wing compartment and the second wing compartment, and then the second folding axis extends from the first folding axis ,
- the third folding shaft extends from the second folding shaft, and the rear motor box unfolds from the motor box slot on the third folding shaft, and then the propeller unfolds from the propeller slot.
- the unfolding is rapid and orderly, ensuring that the flying car is ready to take off. There is less preparation for the stage and the take
- Figure 1 is a schematic diagram of the three-dimensional structure of a flying car in this embodiment
- FIG. 2 is a schematic diagram of the structure of the flying car on the ground in this embodiment
- FIG. 3 is a schematic diagram of the structure of the flying state in the hole of the flying car in this embodiment
- Figure 4 is a schematic diagram of the three-dimensional structure of the propeller in this embodiment.
- the motor box 20 is arranged to rotate relative to the third folding shaft 18, a propeller 19 is installed above the motor box 20, a propeller drive motor is arranged in the motor box 20, and the propeller 19 is folded relative to the propel
- the fuselage 6 is also provided with a glass window 7, a front lamp 1 and a turn signal 2, the glass window 7 is semicircular and located above the fuselage 6, the front lamp 1 and The turn signal 2 is provided with two pairs and located on both sides of the glass window 7 respectively.
- a trunk 10 and a taillight 9 are provided behind the fuselage 6, and a trunk 10 key hole 11 for opening the trunk 10 is provided on the trunk 10.
- the present invention proposes a flying car, including a fuselage 6 and wheels 4, the fuselage 6 is provided with a first wing compartment 3 and a second wing compartment 5, and the first wing compartment 3 is provided with Two are located on both sides of the fuselage 6, the second wing compartment 5 is provided with one located between the glass window 7 and the trunk 10, and the first wing compartment 3 and the second wing compartment 5 are respectively provided with a folding machine
- the wing 8, the folding wing 8 includes a first folding shaft 16, a second folding shaft 17 and a third folding shaft 18 that are sleeved.
- a motor box 20 is connected to the third folding shaft 18, and the motor box 20 is relative to the first folding shaft.
- the three-folding shaft 18 rotates, the propeller 19 is installed above the motor box 20, the propeller drive motor is installed in the motor box 20, the propeller 19 is folded relative to the propeller groove 21, and the first wing compartment 3 and the second wing compartment 5 are in the
- the folding wing 8 is provided so that the folding wing 8 can be quickly retracted into the first wing compartment 3 and the second wing compartment 5 when the flying car is running on the ground, and the first folding shaft 16 and the second folding shaft 17.
- the third folding shaft 18, the propeller 19 and the motor box 20 are tightly stowed to ensure that when the flying car is running on the ground, there will be no parts of the folding wing 8 protruding outside, ensuring that the folding machine is The safety and service life of the wing 8, when the car needs to fly, the folding wing 8 is quickly unfolded, the first folding shaft 16 is unfolded to the outside of the first wing compartment 3 and the second wing compartment 5, and the second folding shaft 17 is from the first wing compartment 3 and the second wing compartment 5.
- a folding shaft 16 protrudes, a third folding shaft 18 protrudes from the second folding shaft 17, the motor box 20 is unfolded from the motor box groove 181 on the third folding shaft 18, and the propeller 19 is unfolded from the propeller groove 21 ,
- the deployment is rapid and orderly, to ensure that the flying car has less preparation work during the take-off phase, and the take-off is faster
- the first folding shaft 16 is provided with a folding wing 8 mounting hole, and the folding wing 8 is respectively installed in the first wing compartment 3 and the second wing through the folding wing 8 mounting holes In cabin 5.
- the first folding shaft 16 is provided with a folding wing 8 mounting hole, and the folding wing 8 is installed in the first wing compartment 3 and the second wing compartment 5 through the folding wing 8 mounting holes, respectively. Installation and fixing of the folding wing 8.
- the end of the first folding shaft 16 is arc-shaped, a number of protrusions 22 are provided along the arc-shaped circumferential direction, the first wing compartment 3 and the second wing compartment 5 are respectively provided with arc-shaped grooves, and a number of dents are provided along the circumferential direction of the grooves, the end of the first folding shaft 16 is installed in the arc-shaped grooves, and the protrusions 22 Embedded in the dent.
- the end of the first folding shaft 16 is arc-shaped, and a number of protrusions 22 are provided in the circumferential direction of the arc-shaped end for installing the first wing compartment 3 and the second wing compartment of the folding wing 8.
- the two wing compartments 5 are respectively provided with grooves adapted to the arc-shaped ends, and a number of dents are provided on the circumference of the grooves.
- the third folding shaft 18 is provided with a motor box slot 181, and the motor box 20 is rotatably placed in the motor box slot 181.
- the third folding shaft 18 is provided with a motor box slot 181 for placing the motor box 20.
- the motor box slot 181 is rotatably arranged relative to the third folding shaft 18.
- the motor box 20 rotates so that it can be quickly rotated out of the motor box slot 181 to a suitable position to ensure that the flying car takes off quickly and orderly .
- the sides of the motor box 20 are respectively provided with propeller grooves 21, and the propellers 19 are foldably placed in the propeller grooves 21.
- a number of propeller grooves 21 are provided on the side of the motor box 20 for placing the propeller 19, the propeller 19 is installed above the motor box 20 and can be folded relative to the motor box 20, when the flying car is running on the ground , The propeller 19 stops rotating, and folds down, so that it is stowed in the propeller groove 21.
- the propeller 19 folds upwards from the propeller groove 21 to the designated position and starts to rotate to realize the flying car Take off quickly and orderly.
- a mudguard is installed on the wheel 4, the mudguard includes a front mudguard 14 and a rear mudguard 12, and the front mudguard 14 is installed on the rotation direction of the wheel 4 At the rear, the rear fender 12 is installed in front of the rotation direction of the wheel 4.
- the wheel 4 is provided with a mudguard
- the mudguard includes a front mudguard 14 and a rear mudguard 12
- the front mudguard 14 and the rear mudguard 12 are respectively arranged in front of and behind the wheel 4 , To prevent muddy water from spilling on the floor of the flying car when the flying car is driving on the ground.
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Transportation (AREA)
- Body Structure For Vehicles (AREA)
Abstract
Description
Claims (8)
- 一种飞行汽车,包括有机身(6)和车轮(4),其特征在于:所述机身(6)上设置有第一机翼舱(3)和第二机翼舱(5),所述第一机翼舱(3)设置有两个分别位于机身(6)的两侧,所述第二机翼舱(5)位于机身(6)上方,所述第一机翼舱(3)和第二机翼舱(5)中分别设置有折叠机翼(8),所述折叠机翼(8)包括有第一折叠轴(16)、第二折叠轴(17)以及第三折叠轴(18),所述第一折叠轴(16)、第二折叠轴(17)以及第三折叠轴(18)套接设置,所述第一折叠轴(16)的尺寸大于第二折叠轴(17)的尺寸,所述第二折叠轴(17)的尺寸大于第三折叠轴(18)的尺寸,所述第三折叠轴(18)上连接有电机箱(20),所述电机箱(20)相对于第三折叠轴(18)转动设置,所述电机箱(20)上方安装有螺旋桨(19),所述电机箱(20)中设置有螺旋桨驱动电机,所述螺旋桨(19)相对于螺旋桨槽(21)折叠设置。A flying car, comprising a fuselage (6) and wheels (4), characterized in that: the fuselage (6) is provided with a first wing compartment (3) and a second wing compartment (5), The first wing cabin (3) is provided with two wing cabins (3) respectively located on both sides of the fuselage (6), the second wing cabin (5) is located above the fuselage (6), and the first wing cabin (3) and the second wing compartment (5) are respectively provided with a folding wing (8), and the folding wing (8) includes a first folding shaft (16), a second folding shaft (17), and a second folding shaft (17). Three folding shafts (18), the first folding shaft (16), the second folding shaft (17) and the third folding shaft (18) are sleeved and arranged, and the size of the first folding shaft (16) is larger than that of the second folding shaft (16). The size of the folding shaft (17), the size of the second folding shaft (17) is larger than the size of the third folding shaft (18), the third folding shaft (18) is connected with a motor box (20), the The motor box (20) is arranged to rotate relative to the third folding shaft (18), a propeller (19) is installed above the motor box (20), and a propeller driving motor is provided in the motor box (20), and the propeller ( 19) Folding arrangement relative to the propeller groove (21).
- 根据权利要求1所述的一种飞行汽车,其特征在于:所述第一折叠轴(16)上设置有折叠机翼(8)安装孔,所述折叠机翼(8)通过折叠机翼(8)安装孔分别安装在第一机翼舱(3)和第二机翼舱(5)中。The flying car according to claim 1, characterized in that: the first folding shaft (16) is provided with a folding wing (8) mounting hole, and the folding wing (8) passes through the folding wing ( 8) The mounting holes are respectively installed in the first wing compartment (3) and the second wing compartment (5).
- 根据权利要求2所述的一种飞行汽车,其特征在于:所述第一折叠轴(16)的端部为圆弧状,沿圆弧状的圆周方向上设置有若干凸起(22),所述第一机翼舱(3)和第二机翼舱(5)中分别设置有圆弧状的凹槽,沿凹槽的圆周方向上设置有若干凹痕,所述第一折叠轴(16)的端部安装在圆弧状的凹槽中,所述凸起(22)嵌入凹痕中。The flying car according to claim 2, characterized in that the end of the first folding shaft (16) is arc-shaped, and a number of protrusions (22) are provided along the arc-shaped circumferential direction, The first wing compartment (3) and the second wing compartment (5) are respectively provided with arc-shaped grooves, and a number of dents are provided along the circumferential direction of the grooves, and the first folding shaft ( The end of 16) is installed in the arc-shaped groove, and the protrusion (22) is embedded in the dent.
- 根据权利要求1所述的一种飞行汽车,其特征在于:所述第三折 叠轴(18)上设置有电机箱槽181,所述电机箱(20)可转动的放置在电机箱槽181中。The flying car according to claim 1, characterized in that: the third folding shaft (18) is provided with a motor box slot 181, and the motor box (20) is rotatably placed in the motor box slot 181 .
- 根据权利要求1所述的一种飞行汽车,其特征在于:所述电机箱(20)的侧面上分别设置有螺旋桨槽(21),所述螺旋桨(19)可折叠的放置在螺旋桨槽(21)中。The flying car according to claim 1, characterized in that: the sides of the motor box (20) are respectively provided with propeller grooves (21), and the propellers (19) are foldably placed in the propeller grooves (21). )in.
- 根据权利要求1所述的一种飞行汽车,其特征在于:所述车轮(4)上安装有挡泥板,所述挡泥板包括有前挡泥板(14)和后挡泥板(12),所述前挡泥板(14)安装在车轮(4)转动方向的后方,所述后挡泥板(12)安装在车轮(4)转动方向的前方。The flying car according to claim 1, characterized in that: the wheels (4) are equipped with fenders, and the fenders include a front fender (14) and a rear fender (12). ), the front fender (14) is installed behind the rotation direction of the wheel (4), and the rear fender (12) is installed forward of the rotation direction of the wheel (4).
- 根据权利要求1所述的一种飞行汽车,其特征在于:所述机身(6)上还设置有玻璃窗(7)、前车灯(1)以及转向灯(2),所述玻璃窗(7)为半圆状且位于机身(6)上方,所述前车灯(1)和转向灯(2)设置有两对且分别位于玻璃窗(7)的两侧。The flying car according to claim 1, characterized in that: the fuselage (6) is further provided with a glass window (7), a front lamp (1) and a turn signal (2), and the glass window (7) It is semicircular and located above the fuselage (6). The front lamp (1) and the turn signal (2) are provided with two pairs and are respectively located on both sides of the glass window (7).
- 根据权利要求7所述的一种飞行汽车,其特征在于:所述机身(6)后方设置有后备箱(10)和车尾灯(9),所述后备箱(10)上设置有用于打开后备箱(10)的后备箱(10)钥匙孔(11)。The flying car according to claim 7, characterized in that: a trunk (10) and a taillight (9) are provided behind the fuselage (6), and a trunk (10) is provided for opening The key hole (11) of the trunk (10) of the trunk (10).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE212020000084.0U DE212020000084U1 (en) | 2019-12-05 | 2020-06-11 | Flying car |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201911232202.8 | 2019-12-05 | ||
CN201922154540.6U CN211000802U (en) | 2019-12-05 | 2019-12-05 | Flying automobile |
CN201922154540.6 | 2019-12-05 | ||
CN201911232202.8A CN110789281A (en) | 2019-12-05 | 2019-12-05 | Flying automobile |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2021109529A1 true WO2021109529A1 (en) | 2021-06-10 |
Family
ID=76221122
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/CN2020/095625 WO2021109529A1 (en) | 2019-12-05 | 2020-06-11 | Flying car |
Country Status (1)
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WO (1) | WO2021109529A1 (en) |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1833895A (en) * | 2005-03-14 | 2006-09-20 | 田晓虹 | Three-purpose traffic vehicle and power unit |
US20150102155A1 (en) * | 2012-06-07 | 2015-04-16 | Ivan Krastev | Road-and-air transport vehicle |
CN105730170A (en) * | 2016-03-24 | 2016-07-06 | 南京航空航天大学 | Four-duct aerocar with vertical take-off and landing function |
CN107150801A (en) * | 2016-03-03 | 2017-09-12 | 上海奥科赛飞机有限公司 | Use rotary wing aircraft in a kind of land, water and air three |
CN107984992A (en) * | 2017-11-28 | 2018-05-04 | 北京航空航天大学 | It is a kind of can VTOL land and air double-used vehicle |
CN207658045U (en) * | 2017-12-14 | 2018-07-27 | 长安大学 | Foldable quadrotor suitable for hovercar |
CN108501638A (en) * | 2018-02-28 | 2018-09-07 | 佛山市神风航空科技有限公司 | A kind of hovercar of foldable rotor |
CN110789281A (en) * | 2019-12-05 | 2020-02-14 | 金陵科技学院 | Flying automobile |
-
2020
- 2020-06-11 WO PCT/CN2020/095625 patent/WO2021109529A1/en active Application Filing
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1833895A (en) * | 2005-03-14 | 2006-09-20 | 田晓虹 | Three-purpose traffic vehicle and power unit |
US20150102155A1 (en) * | 2012-06-07 | 2015-04-16 | Ivan Krastev | Road-and-air transport vehicle |
CN107150801A (en) * | 2016-03-03 | 2017-09-12 | 上海奥科赛飞机有限公司 | Use rotary wing aircraft in a kind of land, water and air three |
CN105730170A (en) * | 2016-03-24 | 2016-07-06 | 南京航空航天大学 | Four-duct aerocar with vertical take-off and landing function |
CN107984992A (en) * | 2017-11-28 | 2018-05-04 | 北京航空航天大学 | It is a kind of can VTOL land and air double-used vehicle |
CN207658045U (en) * | 2017-12-14 | 2018-07-27 | 长安大学 | Foldable quadrotor suitable for hovercar |
CN108501638A (en) * | 2018-02-28 | 2018-09-07 | 佛山市神风航空科技有限公司 | A kind of hovercar of foldable rotor |
CN110789281A (en) * | 2019-12-05 | 2020-02-14 | 金陵科技学院 | Flying automobile |
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