CN207000076U - Land and air double-used four axles gyroplane - Google Patents
Land and air double-used four axles gyroplane Download PDFInfo
- Publication number
- CN207000076U CN207000076U CN201720640118.XU CN201720640118U CN207000076U CN 207000076 U CN207000076 U CN 207000076U CN 201720640118 U CN201720640118 U CN 201720640118U CN 207000076 U CN207000076 U CN 207000076U
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- rotor
- connecting rod
- land
- axles
- rotor support
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Abstract
It the utility model is related to gyroplane technical field, a kind of more particularly to land and air double-used four axles gyroplane, including body, the both sides of the body are respectively arranged with two wheels, two rotor supports, rotor accommodating chamber is provided with the middle part of the wheel, the rotor mid-stent is provided with rotor, the rotor support is connected by switching mechanism with the body, when switching mechanism is flipped up, the rotor support is located at the both sides of the body in the horizontal direction, when switching mechanism downwardly turns over, the rotor support rotates down 90 ° of entrance rotor accommodating chamber, the utility model scientific structure, rotor rotational driving body flight is utilized when flight, rotor can be downwardly turned over when ground run to hiding in wheel, reduce resistance and avoid rotor from colliding other objects.
Description
Technical field
Gyroplane technical field is the utility model is related to, more particularly to a kind of land and air double-used four axles gyroplane.
Background technology
Four axle gyroplanes, also referred to as quadrotor, or four-rotor helicopter, it is that one kind has four propellers and spiral
Oar is in the aircraft of decussation.The aircraft is symmetrical using direct driving force source of four rotors as flight, rotor
The four direction around body, four rotors are in sustained height plane, and the structure and radius all phases of four rotors
Together, first rotor and the 3rd rotor rotate counterclockwise, second rotor and the 4th rotor turn clockwise, four motors
The bracket end of aircraft is symmetrically mounted at, when aircraft balances flight, gyroscopic effect and air force moment of torsion effect quilt
Offset.
, can not be in ground run, if four axle rotor functions but existing four axles gyroplane typically only has flight function
It is enough land and air double-used, it can fly in the air, also can be in ground run, then its application will be wider.On the one hand, due on ground
Energy consumption is lower when face travels, and faster, on the other hand, it is also stronger by property for speed, in the case where part overhead is limited still
Can be from ground run.But this also brings a problem, i.e., how to design body construction makes it when realizing ground run,
Rotor can be packed up so as to reduce resistance and avoid rotor from colliding other objects.
The content of the invention
The purpose of this utility model is in view of the shortcomings of the prior art, and provides a kind of land and air double-used four axles gyroplane,
Its scientific structure, during for road traveling, rotor is hidden to wheel, space is saved, it is achieved thereby that land and air double-used.
Technical scheme is used by the utility model solves its technical problem：A kind of land and air double-used four axles gyroplane, its
Including body, the both sides of the body are respectively arranged with two wheels, two rotor supports, and rotation is provided with the middle part of the wheel
Wing accommodating chamber, the rotor mid-stent are provided with rotor, and the rotor support is connected by switching mechanism with the body, when
When switching mechanism is flipped up, the rotor support is located at the both sides of the body in the horizontal direction, when switching mechanism turns over downwards
When turning, the rotor support rotates down 90 ° of entrance rotor accommodating chamber.
The switching mechanism includes first connecting rod, second connecting rod, third connecting rod, and the third connecting rod is the liquid of vertical direction
Strut is pressed, the second connecting rod is expansion link, and one end of the second connecting rod is hinged the third connecting rod, the second connecting rod
The other end is hinged the rotor support, and one end of the first connecting rod is hinged with the body, the other end of the first connecting rod
It is hinged with the rotor support, when third connecting rod moves down, second connecting rod elongation drives the rotor support to overturn to level
Position, when third connecting rod moves up, second connecting rod, which shortens, drives the rotor support to overturn to the rotor accommodating chamber.
Two switching mechanisms on front side of the body share a third connecting rod, two switching mechanisms on rear side of the body
Share a third connecting rod.
The wheel is to be passed through without wagon wheel, the first connecting rod, second connecting rod from the middle part of the wheel.
The wheel is provided with drive gear close to the side of body, and the body is provided with for driving the sliding tooth
Take turns the motor rotated.
Driving cabin is provided with the middle part of the body.
Solar panel is provided with the top of the driving cabin, the bottom for reaching driving cabin is provided with battery, electronic
Machine.
The rotor support is annular, and two spokes are provided with the middle part of the annular.
The rotor motor for driving the rotor rotational is provided with the middle part of the rotor support.
The beneficial effects of the utility model are：A kind of land and air double-used four axles gyroplane, it includes body, and the two of the body
Side is respectively arranged with two wheels, two rotor supports, and rotor accommodating chamber, the rotor support are provided with the middle part of the wheel
Middle part is provided with rotor, and the rotor support is connected by switching mechanism with the body, when switching mechanism is flipped up, institute
The both sides that rotor support is located at the body in the horizontal direction are stated, when switching mechanism downwardly turns over, the rotor support is downward
90 ° of entrance rotor accommodating chamber is rotated, the utility model scientific structure, is flown when flight using rotor rotational driving body
OK, rotor can be downwardly turned in wheel and hidden when ground run, reduced resistance and avoid rotor from colliding other things
Body.
Brief description of the drawings
Fig. 1 is positive structural representation when the rotor of land and air double-used four axles gyroplane of the present utility model is opened.
Fig. 2 is positive structural representation when the rotor of land and air double-used four axles gyroplane of the present utility model is packed up.
Fig. 3 is the structural representation of side when the rotor of land and air double-used four axles gyroplane of the present utility model is opened.
Fig. 4 is the structural representation of side when the rotor of land and air double-used four axles gyroplane of the present utility model is packed up.
Description of reference numerals：
1 --- body 2 --- wheel
21 --- rotor accommodating chamber 3 --- rotor supports
31 --- rotor 4 --- switching mechanisms
41 --- first connecting rod 42 --- second connecting rods
43 --- third connecting rod 5 --- driving cabins.
Embodiment
The utility model is described in further detail with specific embodiment below in conjunction with the accompanying drawings, is not this practicality
New practical range limited to this.
As shown in Figure 1, Figure 2, Figure 3, Figure 4, the land and air double-used four axles gyroplane of the present embodiment, it includes body 1, the machine
The both sides of body 1 are respectively arranged with two wheels, 2, two rotor supports 3, and the middle part of the wheel 2 is provided with rotor accommodating chamber 21,
The middle part of the rotor support 3 is provided with rotor 31, and the rotor support 3 is connected by switching mechanism 4 with the body 1, when turning over
When rotation mechanism 4 is flipped up, the rotor support 3 is located at the both sides of the body 1 in the horizontal direction, after being easy to rotor 31 to rotate
Body 1 is driven to fly up, when switching mechanism 4 downwardly turns over, the rotor support 3 rotates down 90 ° of entrance rotor and accommodated
Chamber 21, using the rotational band motivation body 1 of wheel 2 along road traveling.The utility model scientific structure, 31 turns of rotor is utilized when flight
Dynamic driving body flight, rotor 31 can be downwardly turned over when ground run to hiding in wheel 2, reduce resistance and avoid revolving
The wing collides other objects.
The gyroplane land and air double-used can have very big application prospect, either unmanned plane or manned machine, can be with
Without flying to appointed place, but have the selection of more multidrop points, again along road traveling to specified location after landing, this for
Management is easily facilitated when there are multiple UAVs in the same area, and road traveling energy consumption is lower, and it is stronger by property, for portion
When point position can not be flown through, it can be passed through by road surface.
In addition, for steering, the wheel portion of this gyroplane can set steering, can also be not provided with, when
When not having steering, directly whole body is driven to fly up rear steering using rotor.Because wheel does not disturb with rotor, this reality
With it is new can also wheel and rotor use simultaneously.
Further, the switching mechanism 4 includes first connecting rod 41, second connecting rod 42, third connecting rod 43, first connecting rod
41st, second connecting rod 42, third connecting rod 43 and rotor support 3 form a quadric chain altogether, realize that rotor support 3 is overturn
90 ° of function.Specifically, the third connecting rod 43 is the hydraulic strut of vertical direction, the second connecting rod 42 is expansion link, institute
The one end for stating second connecting rod 42 is hinged the third connecting rod 43, and the other end of the second connecting rod 42 is hinged the rotor support 3,
One end of the first connecting rod 41 is be hinged with the body 1, and the other end of the first connecting rod 41 is cut with scissors with the rotor support 3
Connect, when third connecting rod 43 moves down, the elongation of second connecting rod 42 drives the rotor support 3 to overturn to horizontal level, when the 3rd
Connecting rod 43 moves up, and second connecting rod 42, which shortens, drives the rotor support 3 to overturn to the rotor accommodating chamber 21.
Further, two switching mechanisms 4 of the front side of body 1 share a third connecting rod 43, the rear side of body 1
Two switching mechanisms 4 share a third connecting rod 43.
Further, the wheel 2 is without wagon wheel, and the first connecting rod 41, second connecting rod 42 are from the wheel 2
Middle part passes through.
Further, the wheel 2 is provided with drive gear close to the side of body 1, and the body 1 is provided with for driving
The motor that the dynamic drive gear rotates, the drive gear are located on the excircle of wheel, and its diameter omits than the diameter of wheel
It is small.
Further, the utility model can be unmanned plane, or manned machine, when the utility model is manned machine
Wait, the middle part of the body 1 is provided with driving cabin 5.
Further, the top of the driving cabin 5 is provided with solar panel, and the bottom for reaching driving cabin 5 is provided with
Battery, motor.
Further, the rotor support 3 is annular, and two spokes are provided with the middle part of the annular.
Further, the middle part of the rotor support 3 is provided with the rotor motor for driving the rotor rotational（Do not have in figure
Draw）.
Finally it should be noted that above example is only illustrating the technical solution of the utility model, rather than to this reality
With the limitation of novel protected scope, although being explained with reference to preferred embodiment to the utility model, this area it is general
It is logical it will be appreciated by the skilled person that can be modified to the technical solution of the utility model or equivalent substitution, without departing from this
The spirit and scope of utility model technical scheme.
Claims (9)
1. land and air double-used four axles gyroplane, it is characterised in that：Including body（1）, the body（1）Both sides be respectively arranged with two
Individual wheel（2）, two rotor supports（3）, the wheel（2）Middle part be provided with rotor accommodating chamber（21）, the rotor support
（3）Middle part is provided with rotor（31）, the rotor support（3）Pass through switching mechanism（4）With the body（1）Connection, works as upset
Mechanism（4）When being flipped up, the rotor support（3）It is located at the body in the horizontal direction（1）Both sides, work as switching mechanism
（4）When downwardly turning over, the rotor support（3）Rotate down 90 ° of entrance rotor accommodating chamber（21）.
2. land and air double-used four axles gyroplane according to claim 1, it is characterised in that：The switching mechanism（4）Including
One connecting rod（41）, second connecting rod（42）, third connecting rod（43）, the third connecting rod（43）For the hydraulic strut of vertical direction, institute
State second connecting rod（42）For expansion link, the second connecting rod（42）One end be hinged the third connecting rod（43）, described second connects
Bar（42）The other end be hinged the rotor support（3）, the first connecting rod（41）One end and the body（1）It is be hinged, institute
State first connecting rod（41）The other end and the rotor support（3）It is be hinged, work as third connecting rod（43）Move down, second connecting rod
（42）Elongation drives the rotor support（3）Upset works as third connecting rod to horizontal level（43）Move up, second connecting rod（42）
Shorten and drive the rotor support（3）Overturn to the rotor accommodating chamber（21）.
3. land and air double-used four axles gyroplane according to claim 2, it is characterised in that：The body（1）Two of front side
Switching mechanism（4）Share a third connecting rod（43）, the body（1）Two switching mechanisms of rear side（4）Share one the 3rd
Connecting rod（43）.
4. land and air double-used four axles gyroplane according to claim 2, it is characterised in that：The wheel（2）For without spoke car
Wheel, the first connecting rod（41）, second connecting rod（42）From the wheel（2）Middle part pass through.
5. land and air double-used four axles gyroplane according to claim 2, it is characterised in that：The wheel（2）Close to body（1）
Side be provided with drive gear, the body（1）It is provided with the motor for driving the drive gear to rotate.
6. land and air double-used four axles gyroplane according to claim 2, it is characterised in that：The body（1）Middle part set
There is driving cabin（5）.
7. land and air double-used four axles gyroplane according to claim 6, it is characterised in that：The driving cabin（5）Top set
Solar panel is equipped with, reaches driving cabin（5）Bottom be provided with battery, motor.
8. land and air double-used four axles gyroplane according to claim 1, it is characterised in that：The rotor support（3）For annulus
Shape, annular middle part are provided with two spokes.
9. land and air double-used four axles gyroplane according to claim 8, it is characterised in that：The rotor support（3）Middle part
It is provided with the rotor motor for driving the rotor rotational.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720640118.XU CN207000076U (en) | 2017-06-05 | 2017-06-05 | Land and air double-used four axles gyroplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720640118.XU CN207000076U (en) | 2017-06-05 | 2017-06-05 | Land and air double-used four axles gyroplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207000076U true CN207000076U (en) | 2018-02-13 |
Family
ID=61446573
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720640118.XU Expired - Fee Related CN207000076U (en) | 2017-06-05 | 2017-06-05 | Land and air double-used four axles gyroplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207000076U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110217065A (en) * | 2019-06-05 | 2019-09-10 | 中国科学院深圳先进技术研究院 | A kind of rotor structure and the Gun Pa robot using it |
| CN110975301A (en) * | 2019-12-25 | 2020-04-10 | 刘佳田 | Actuating mechanism for simulating air-ground dual-purpose automobile model and automobile model |
| CN112549886A (en) * | 2020-12-25 | 2021-03-26 | 南京航空航天大学 | Amphibious six-rotor aircraft applicable to multiple terrains and having walking function |
-
2017
- 2017-06-05 CN CN201720640118.XU patent/CN207000076U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110217065A (en) * | 2019-06-05 | 2019-09-10 | 中国科学院深圳先进技术研究院 | A kind of rotor structure and the Gun Pa robot using it |
| CN110975301A (en) * | 2019-12-25 | 2020-04-10 | 刘佳田 | Actuating mechanism for simulating air-ground dual-purpose automobile model and automobile model |
| CN112549886A (en) * | 2020-12-25 | 2021-03-26 | 南京航空航天大学 | Amphibious six-rotor aircraft applicable to multiple terrains and having walking function |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| 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: 20180213 |