CN207089652U - A kind of wing coordinated type verts wing unmanned plane - Google Patents
A kind of wing coordinated type verts wing unmanned plane Download PDFInfo
- Publication number
- CN207089652U CN207089652U CN201721121729.XU CN201721121729U CN207089652U CN 207089652 U CN207089652 U CN 207089652U CN 201721121729 U CN201721121729 U CN 201721121729U CN 207089652 U CN207089652 U CN 207089652U
- Authority
- CN
- China
- Prior art keywords
- wing
- fuselage
- unmanned plane
- adapter
- plane
- Prior art date
- Legal status (The legal status 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 status listed.)
- Active
Links
Abstract
Verted wing unmanned plane, including the fuselage passed perpendicularly through by rotating shaft from side the utility model discloses a kind of wing coordinated type, the both ends of rotating shaft are symmetrical on fuselage, the actuating unit rotated in fuselage provided with drive shaft；The both ends of rotating shaft are equipped with adapter, and propeller is connected with adapter, and wing of the width perpendicular to propeller Plane of rotation is hinged with adapter；Wing, which is provided with, makes the switching mechanism that wing rotates around adapter, the Plane of rotation of the rotational plane of wing parallel to propeller；When unmanned plane is in flat winged state at a high speed, wing is rotated to perpendicular to the direction of fuselage, and wing one end overlap joint or is connected in fuselage；When unmanned plane is in vertical lift state, wing is rotated to the direction parallel to fuselage.Therefore, in addition to the advantages of the utility model is not easy upset damage when with landing, also with cost is low, good reliability and the advantages of lift is big, stability is good in vertical lift.
Description
Technical field
The utility model belongs to unmanned plane field, more particularly to a kind of wing coordinated type verts wing unmanned plane.
Background technology
The wing unmanned plane that verts belongs to the combination of propeller type unmanned plane and fixed-wing unmanned plane, has both hanging down for propeller type
The high speed of a ship or plane, the big voyage function of straight elevating function and fixed-wing formula.The existing wing unmanned plane that verts must all be set below fuselage
Two undercarriages are put, because the inherent structure of unmanned plane limits, the span between undercarriage is limited, i.e. drop point scope is small；Existing
Have also to be difficult to when unmanned plane lands under technical merit and steadily land, be often vertical at a relatively high speed when unmanned plane lands
Landing, this will produce a reverse impact power in landing；Under certain condition, reverse impact power, drop point scope be small and ground
Face injustice three collective effect simultaneously result in unmanned plane upset damage in landing.
Therefore the existing wing unmanned plane that verts has the shortcomings that damage is easily overturn during landing.
Utility model content
The purpose of this utility model is, there is provided a kind of wing coordinated type verts wing unmanned plane.The utility model has drop
The advantages of being not easy upset damage when falling.
The technical solution of the utility model：A kind of wing coordinated type verts wing unmanned plane, including vertical from side by rotating shaft
The fuselage passed through, the both ends of rotating shaft are symmetrical on fuselage, the actuating unit rotated in fuselage provided with drive shaft；Rotating shaft
Both ends are equipped with adapter, and propeller is connected with adapter, and width is hinged with adapter and is rotated perpendicular to propeller
The wing of plane；Wing, which is provided with, makes the switching mechanism that wing rotates around adapter, and the rotational plane of wing is parallel to propeller
Plane of rotation；When unmanned plane is in flat winged state at a high speed, wing is rotated to perpendicular to the direction of fuselage, and wing one end is taken
Connect or be connected in fuselage；When unmanned plane is in vertical lift state, wing is rotated to the direction parallel to fuselage.
Foregoing wing coordinated type verts in wing unmanned plane, and fuselage tail end is provided with downward vertical tail, the tipper
Structure includes the connecting rod of connection vertical tail and wing, and one end of connecting rod connects vertical tail by the first universal joint, connecting rod it is another
One end connects the end of wing by the second universal joint；Switching mechanism also includes the flap of be hinged adapter, and adapter is by turning
Plate connects wing.
Foregoing wing coordinated type verts in wing unmanned plane, and the tie point of second universal joint and wing is located at wing use
In one end of overlap joint or clamping fuselage.
Foregoing wing coordinated type verts in wing unmanned plane, and first universal joint and the second universal joint are universal joint connection
Axle device.
Foregoing wing coordinated type verts in wing unmanned plane, and first universal joint and the second universal joint are flexible pipe.
Compared with prior art, the utility model wing can rotate, and when unmanned plane lands, wing can play undercarriage
Effect, the drop point coverage of undercarriage is very big, and unmanned plane is not easy upset damage during landing.In addition, no matter unmanned plane
In the case of which kind of, for air-flow caused by unmanned plane propeller all the time parallel to wing, airflow function is smooth behind wing edge
Flowed through from wing upper and lower surface, be advantageous to keep unmanned plane stabilization and reduce loss of lift；This with it is existing vert the wing without
It is man-machine be it is different, the wing of the existing wing unmanned plane that verts is fixed-wing formula, in slower flight or vertical lift, propeller
Air-flow large area acts on wing, and wing large area has blocked air-flow, not only causes the lift of unmanned plane to reduce, and air-flow
The area beaten in wing crosses the irregular vortex of conference generation and causes unmanned plane unstable.
Therefore, it is also low, reliable with cost in addition to the advantages of the utility model is not easy upset damage when with landing
Property it is good and the advantages of in vertical lift, lift is big, stability is good.
Brief description of the drawings
Fig. 1 is structural representation of the utility model in vertical lift.
Fig. 2 is state diagram of the utility model when high speed is flat winged.
Mark in accompanying drawing for：1- rotating shafts, 2- fuselages, 3- actuating units, 4- adapters, 5- propellers, 6- wings, 13-
Vertical tail, 14- connecting rods, the universal joints of 15- first, the universal joints of 16- second, 17- steps.
Embodiment
The utility model is further described with reference to the accompanying drawings and examples, but is not intended as to the utility model
The foundation of limitation.
Embodiment.As depicted in figs. 1 and 2, including by rotating shaft 1 fuselage 2 passed perpendicularly through from side, the both ends of rotating shaft 1 are closed
Actuating unit 3 symmetrical in fuselage 2, being rotated provided with drive shaft 1 in fuselage 2, actuating unit 3 are a motors, motor
Motor shaft both ends extension, the motor shaft of motor is rotating shaft 1；The both ends of rotating shaft 1 are equipped with adapter 4, connect on adapter 4
Propeller 5 is connected to, wing 6 of the width perpendicular to the Plane of rotation of propeller 5 is hinged with adapter 4；Wing 6, which is provided with, to be made
The switching mechanism that wing 6 rotates around adapter 4, the Plane of rotation of the rotational plane of wing 6 parallel to propeller 5；Work as unmanned plane
During in flat winged state at a high speed, the rotation of wing 6 is extremely perpendicular to the direction of fuselage, and the one end of wing 6 overlaps or be connected in fuselage 2；
When unmanned plane is in vertical lift state, the rotation of wing 6 to the direction parallel to fuselage 2.
The tail end of fuselage 2 is provided with downward vertical tail 13, and the switching mechanism includes connection vertical tail 13 and wing 6
Connecting rod 14, one end of connecting rod 14 connect vertical tail 13 by the first universal joint 15, and the other end of connecting rod 14 is universal by second
The end of the connection wing 6 of section 16；Switching mechanism also includes the flap 9 of be hinged adapter 4, and adapter 4 connects machine by flap 9
The wing 6.
The tie point of second universal joint 16 and wing 6 be located at wing 6 for overlapping or one end of clamping fuselage 2.
The universal joint 16 of first universal joint 15 and second uses gimbal coupling (can also use flexible pipe).
In embodiment, wing 6 is to control driving by actuating unit 3 around the rotation of adapter 4, and rotating shaft 1, which rotates, drives spiral shell
While revolving 1 rotation around the shaft of oar 5 and wing 6, wing 6 rotates under the drive of connecting rod 14 around adapter 4, is connection between the two
Dynamic relation, the attitudes vibration for flying wing 6 between state and vertical lift state is being put down to complete unmanned plane with this.The utility model
Switching mechanism it is simple in construction, realized in a manner of connection-rod linkage, cost is low, good reliability.
Operation principle：The quick flat for being illustrated in figure 2 unmanned plane flies state, and fly power before the offer unmanned plane of propeller 5, machine
The wing 6 provides lift；As shown in figure 1, when unmanned plane is vertically moved up or down, propeller 5 provides lift.In the flat winged turn of vertical lift of high speed
During, the drive shaft 1 of actuating unit 3 rotates, and drives 1 rotation around the shaft simultaneously of propeller 5 and wing 6；Wing 6 is turning over
Rotated under rotation mechanism effect around adapter 4.When unmanned plane lands, wing 6 can play a part of undercarriage, the drop point model of undercarriage
Enclose very big, unmanned plane is not easy upset damage during landing.In addition, no matter unmanned plane is in the case of which kind of, unmanned plane spiral
All the time parallel to wing 6, airflow function is smooth behind wing edge to be flowed through air-flow caused by oar 5 from the upper and lower surface of wing 6, is had
Beneficial to the stabilization for keeping unmanned plane and reduce loss of lift；This from the existing wing unmanned plane that verts be it is different, it is existing to vert
The wing of wing unmanned plane is fixed-wing formula, and during vertical lift, prop-blast large area acts on wing, the gear of wing large area
Air-flow has been lived, has not only caused the lift of unmanned plane to reduce, and the area that air-flow is beaten in wing crosses the irregular vortex of conference generation
Cause unmanned plane unstable.
Therefore, it is also low, reliable with cost in addition to the advantages of the utility model is not easy upset damage when with landing
Property it is good and the advantages of in vertical lift, lift is big, stability is good.
Claims (5)
- The wing unmanned plane 1. a kind of wing coordinated type verts, it is characterised in that：Including the fuselage passed perpendicularly through by rotating shaft (1) from side (2), the both ends of rotating shaft (1) are symmetrical on fuselage (2), the actuating unit rotated in fuselage (2) provided with drive shaft (1) (3)；The both ends of rotating shaft (1) are equipped with adapter (4), and propeller (5) is connected with adapter (4), and adapter is hinged with (4) Wing (6) of the width perpendicular to propeller (5) Plane of rotation；Wing (6), which is provided with, makes wing (6) turn around adapter (4) Dynamic switching mechanism, the Plane of rotation of the rotational plane of wing (6) parallel to propeller (5)；Fly when unmanned plane is in flat at a high speed During state, wing (6) rotation is extremely perpendicular to the direction of fuselage, and wing (6) one end overlaps or be connected in fuselage (2)；When nobody When machine is in vertical lift state, wing (6) rotation to the direction parallel to fuselage (2).
- The wing unmanned plane 2. wing coordinated type according to claim 1 verts, it is characterised in that：Fuselage (2) tail end be provided with to Under vertical tail (13), the switching mechanism include connection vertical tail (13) and wing (6) connecting rod (14), connecting rod (14) One end vertical tail (13) is connected by the first universal joint (15), the other end of connecting rod (14) passes through the second universal joint (16) even Pick the ends of the wing (6)；Switching mechanism also includes the flap (9) of be hinged adapter (4), and adapter (4) is connected by flap (9) Wing (6).
- The wing unmanned plane 3. wing coordinated type according to claim 2 verts, it is characterised in that：Second universal joint (16) With the tie point of wing (6) be located at wing (6) be used for overlap or clamping fuselage (2) one end.
- The wing unmanned plane 4. wing coordinated type according to claim 2 verts, it is characterised in that：First universal joint (15) It is gimbal coupling with the second universal joint (16).
- The wing unmanned plane 5. wing coordinated type according to claim 2 verts, it is characterised in that：First universal joint (15) It is flexible pipe with the second universal joint (16).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721121729.XU CN207089652U (en) | 2017-09-04 | 2017-09-04 | A kind of wing coordinated type verts wing unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721121729.XU CN207089652U (en) | 2017-09-04 | 2017-09-04 | A kind of wing coordinated type verts wing unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207089652U true CN207089652U (en) | 2018-03-13 |
Family
ID=61540424
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721121729.XU Active CN207089652U (en) | 2017-09-04 | 2017-09-04 | A kind of wing coordinated type verts wing unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207089652U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107380427A (en) * | 2017-09-04 | 2017-11-24 | 陈超 | A kind of wing dual-purpose type verts wing unmanned plane |
| CN109466756A (en) * | 2018-12-06 | 2019-03-15 | 酷黑科技（北京）有限公司 | A kind of multi-rotor aerocraft |
-
2017
- 2017-09-04 CN CN201721121729.XU patent/CN207089652U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107380427A (en) * | 2017-09-04 | 2017-11-24 | 陈超 | A kind of wing dual-purpose type verts wing unmanned plane |
| CN109466756A (en) * | 2018-12-06 | 2019-03-15 | 酷黑科技（北京）有限公司 | A kind of multi-rotor aerocraft |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105059536B (en) | Varying pitch rotor driver and multi-rotor aerocraft | |
| CN106143889B (en) | A kind of quadrotor of undercarriage as handgrip | |
| CN206511121U (en) | Unmanned vehicle | |
| CN207089652U (en) | A kind of wing coordinated type verts wing unmanned plane | |
| CN108100212A (en) | A kind of adaptive response body Flying-wing fighter plane of low aspect ratio | |
| CN110040248A (en) | A kind of vertically taking off and landing flyer | |
| CN205998126U (en) | A kind of unmanned plane during flying system | |
| CN207809757U (en) | A kind of adaptive response body Flying-wing fighter plane of low aspect ratio | |
| CN109733603A (en) | A kind of boxlike solar energy unmanned plane | |
| CN107554783A (en) | A kind of amphibious unmanned plane of VTOL | |
| CN105129097A (en) | Unmanned aerial vehicle capable of taking off and landing vertically | |
| CN206634198U (en) | A kind of inclining rotary mechanism for tiltrotor | |
| WO2018223896A1 (en) | Flip-type propeller device | |
| CN107380427A (en) | A kind of wing dual-purpose type verts wing unmanned plane | |
| CN207173959U (en) | A kind of wing unmanned plane that verts of wing dual-purpose type | |
| CN105346720A (en) | Blades, propeller and unmanned aerial vehicle | |
| CN209176908U (en) | A kind of rotor fixed-wing unmanned plane of composite drive | |
| CN205395679U (en) | Four rotor track aircraft | |
| CN208165273U (en) | A kind of tail sitting posture unmanned vertical flight | |
| CN109703746A (en) | A kind of boxlike has hung down Fixed Wing AirVehicle | |
| CN206914624U (en) | A kind of propeller, Power Component and aircraft | |
| CN208021714U (en) | A kind of aircraft | |
| CN106697257A (en) | Overall design of tilt-rotor aircraft | |
| CN206704538U (en) | The long continuation of the journey aerofoil multi-rotor unmanned aerial vehicle of one kind | |
| CN206841716U (en) | A kind of fixed-wing unmanned plane |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20200716 Address after: Room 2415, building 3, No. 300-11, No. 10 Street (East), Qiantang New District, Hangzhou City, Zhejiang Province Patentee after: Hangzhou ceyindong Electromechanical Technology Co.,Ltd. Address before: Hangzhou City, Zhejiang province 310006 City Park 13 Gen unit 1 Building Room 201 Patentee before: Chen Chao |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20220922 Address after: 310006 Room 201, unit 1, building 13, Gen yuan, Xiacheng District, Hangzhou City, Zhejiang Province Patentee after: Chen Chao Address before: Room 2415, building 3, No. 300-11, No. 10 Street (East), Qiantang New District, Hangzhou City, Zhejiang Province Patentee before: Hangzhou ceyindong Electromechanical Technology Co.,Ltd. |