CN206031759U - Unmanned aerial vehicle vertical tail - Google Patents
Unmanned aerial vehicle vertical tail Download PDFInfo
- Publication number
- CN206031759U CN206031759U CN201620925870.4U CN201620925870U CN206031759U CN 206031759 U CN206031759 U CN 206031759U CN 201620925870 U CN201620925870 U CN 201620925870U CN 206031759 U CN206031759 U CN 206031759U
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- CN
- China
- Prior art keywords
- aileron
- vertical tail
- steering wheel
- rivet
- unmanned plane
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- 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.)
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Abstract
The utility model discloses an unmanned aerial vehicle vertical tail, including vertical tail body, aileron, transfer line and steering wheel, the bottom surface of aileron is tilt up and sets up, the bottom surface of aileron sets up for the polishing, be provided with the recess that agrees with mutually with the aileron appearance on the vertical tail body, the aileron is located the recess, the aileron is connected with the vertical tail body is articulated, the steering wheel passes through the transfer line interlock with the aileron, this unmanned aerial vehicle vertical tail can prevent that the aileron from cliping the connection rope of parachute.
Description
Technical field
This utility model is related to a kind of unmanned plane vertical tail.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft.Without driving cabin on machine, but the equipment such as automatic pilot, presetting apparatus are installed.On ground, naval vessels or
Machine tool remote control station personnel by the equipment such as radar, which is tracked, is positioned, remote control, remote measurement and Digital Transmission.Can be in radio
As conventional airplane take off or launched with booster rocket under remote control, also aerial input can be taken to by machine tool and be flown.Reclaim
When, the mode automatic Landing as conventional airplane landing mission is can use, also can be passed through remote control parachute or block is reclaimed.Can
Repetitiousness is using multiple.It is widely used in aerial reconnaissance, monitoring, communication, antisubmarine, electronic interferences and takes photo by plane.
Current unmanned plane usually can use parachute, but the aileron on current unmanned plane vertical tail is easily pressed from both sides
Firmly the connecting rope of parachute, causes overall balance to be affected.
Utility model content
The technical problems to be solved in the utility model is to provide a kind of connecting rope that can prevent aileron from clamping parachute
Unmanned plane vertical tail.
For solving the above problems, this utility model is adopted the following technical scheme that：
A kind of unmanned plane vertical tail, including vertical tail body, aileron, drive link and steering wheel, the bottom surface of the aileron
In the setting that is inclined upwardly, the bottom surface of the aileron is arranged for polishing, is provided with and aileron external form phase on the vertical tail body
The groove for agreeing with, the aileron are located in groove, and the aileron is articulated and connected with vertical tail body, and the steering wheel is led to aileron
Cross transmission lever linkage.
Preferably, the vertical tail body interior is provided with cavity, overall weight can be reduced, and can be square
Just user installs various electronic equipments in vertical tail body interior.
Preferably, being provided with reinforcement batten in the cavity, described this body side surface of vertical tail is provided with square through hole,
The steering wheel is fixedly connected with reinforcement batten, is provided with steering wheel on the steering wheel, and the steering wheel ovalize is arranged, the steering wheel
End is located at outside vertical tail body through square through hole, is provided with semicircle shape connector, the semicircle shape on the aileron
Connector and steering wheel are articulated and connected with drive link, and structural strength is high, and transmission performance is good.
Preferably, the reinforcement batten is hollow setting, overall weight can be reduced, can prevent from having influence on aircraft
Whole machine balancing.
Preferably, the drive link include the first U-shaped connector, the second U-shaped connector, threaded rod, the first rivet,
Second rivet, the first securing member and the second securing member, the steering wheel and the first U-shaped connector pass through the first rivet and the first fastening
Part connects, and the second U-shaped connector and semicircle shape connector pass through the second rivet and the connection of the second securing member, and stable connection can
Lean on.
The beneficial effects of the utility model are：The bottom surface of aileron is in the setting that is inclined upwardly, and the bottom surface of aileron is polishing
Arrange, the frictional force between aileron and parachute connecting rope can be reduced, the acclivitous design in bottom surface causes parachute connection
Rope touches aileron bottom surface and also rapidly can skid off from aileron bottom surface, can effectively prevent aileron from clamping the connection of parachute
Restrict and cause the malfunction of aileron and parachute, additionally, vertical tail body interior is provided with cavity, can reduce overall
Weight, and various electronic equipments can be installed in vertical tail body interior with convenient use person, reinforcement is provided with cavity
Batten, vertical tail this body side surface are provided with square through hole, and steering wheel is fixedly connected with reinforcement batten, is provided with steering wheel on steering wheel,
Steering wheel ovalize is arranged, and steering wheel end is located at outside vertical tail body through square through hole, is provided with semicircle shape on aileron
Connector, semicircle shape connector and steering wheel are articulated and connected with drive link, and structural strength is high, and transmission performance is good, reinforcement wood
Bar is hollow setting, can reduce overall weight, can prevent from having influence on the whole machine balancing of aircraft, and drive link includes the
One U-shaped connector, the second U-shaped connector, threaded rod, the first rivet, the second rivet, the first securing member and the second securing member, rudder
Disk is connected by the first rivet and the first securing member with the first U-shaped connector, and the second U-shaped connector and semicircle shape connector pass through
Second rivet and the connection of the second securing member, stable connection reliability.
Description of the drawings
For the technical scheme being illustrated more clearly that in this utility model embodiment, below will be to needed for embodiment description
Accompanying drawing to be used is briefly described, it should be apparent that, drawings in the following description are only some realities of the present utility model
Example is applied, for those of ordinary skill in the art, on the premise of not paying creative work, can be with according to these accompanying drawings
Obtain other accompanying drawings.
Fig. 1 is a kind of overall structure diagram of unmanned plane vertical tail of this utility model；
Fig. 2 is a kind of sectional view of unmanned plane vertical tail of this utility model；
Fig. 3 is a kind of drive link of unmanned plane vertical tail of this utility model, the connection of steering wheel and semicircle shape connector is shown
It is intended to.
Specific embodiment
Embodiment 1
As shown in Figure 1-2, a kind of unmanned plane vertical tail, including vertical tail body 1, aileron 2, drive link 3 and steering wheel
4, in the setting that is inclined upwardly, the bottom surface of the aileron 2 is arranged for polishing, on the vertical tail body 1 for the bottom surface of the aileron 2
It is provided with the groove mutually agreed with aileron external form（It is not shown）, the aileron 2 is located in groove, the aileron 2 and vertical tail
Body 1 is articulated and connected, and the steering wheel 4 is interlocked by drive link 3 with aileron 2, and the bottom surface of aileron 2 is in the setting that is inclined upwardly, and
The bottom surface of aileron 2 is arranged for polishing, can reduce the frictional force between aileron 2 and parachute connecting rope, and bottom surface is acclivitous
Design causes parachute connecting rope to touch aileron bottom surface and also rapidly can skid off from aileron bottom surface, can effectively prevent pair
The wing is clamped the connecting rope of parachute and causes the malfunction of aileron and parachute.
The present embodiment has the beneficial effect that：The bottom surface of aileron is in the setting that is inclined upwardly, and the bottom surface of aileron is set for polishing
Put, the frictional force between aileron and parachute connecting rope can be reduced, the acclivitous design in bottom surface causes parachute connecting rope
Touch aileron bottom surface also rapidly to skid off from aileron bottom surface, can effectively prevent aileron from clamping the connecting rope of parachute
And cause the malfunction of aileron and parachute.
Embodiment 2
As Figure 1-3, a kind of unmanned plane vertical tail, including vertical tail body 1, aileron 2, drive link 3 and steering wheel
4, in the setting that is inclined upwardly, the bottom surface of the aileron 2 is arranged for polishing, on the vertical tail body 1 for the bottom surface of the aileron 2
It is provided with the groove mutually agreed with aileron external form（It is not shown）, the aileron 2 is located in groove, the aileron 2 and vertical tail
Body 1 is articulated and connected, and the steering wheel 4 is interlocked by drive link 3 with aileron 2, and the vertical tail body 1 is internally provided with cavity
（It is not shown）, overall weight can be reduced, and various electricity can be installed with convenient use person inside vertical tail body 1
Sub- equipment, is provided with reinforcement batten 5 in the cavity, 1 side of vertical tail body is provided with square through hole 6, the rudder
Machine 4 is fixedly connected with reinforcement batten 5, is provided with steering wheel 7 on the steering wheel 4, and 7 ovalize of the steering wheel is arranged, the steering wheel 7
End is located at outside vertical tail body 1 through square through hole 6, is provided with semicircle shape connector 8 on the aileron 2, and described half
Round shape connector 8 and steering wheel 7 are articulated and connected with drive link 3, and structural strength is high, and transmission performance is good, the reinforcement batten 5
For hollow setting, overall weight can be reduced, can prevent from having influence on the whole machine balancing of aircraft, the drive link 3 is included
There are the first U-shaped connector 9, the second U-shaped connector 10, threaded rod 11, the first rivet 12, the second rivet 13, the first securing member 14
With the second securing member 15, the steering wheel 7 passes through the first rivet 12 with the first U-shaped connector 9 and the first securing member 14 is connected, described
Second U-shaped connector 10 and semicircle shape connector 8 pass through the second rivet 13 and the second securing member 15 connects, stable connection reliability,
The bottom surface of aileron 2 is in the setting that is inclined upwardly, and the bottom surface of aileron 2 is arranged for polishing, can be reduced aileron 2 and is connected with parachute
Frictional force between rope, the acclivitous design in bottom surface is so that the bottom surface that parachute connecting rope touches aileron 2 also can be rapid
Skid off from the bottom surface of aileron 2, can effectively prevent aileron 2 from clamping the connecting rope of parachute and causing aileron 2 and parachute
Malfunction.
The present embodiment has the beneficial effect that：The bottom surface of aileron is in the setting that is inclined upwardly, and the bottom surface of aileron is set for polishing
Put, the frictional force between aileron and parachute connecting rope can be reduced, the acclivitous design in bottom surface causes parachute connecting rope
Touch aileron bottom surface also rapidly to skid off from aileron bottom surface, can effectively prevent aileron from clamping the connecting rope of parachute
And causing the malfunction of aileron and parachute, vertical tail body interior is provided with cavity, can reduce overall weight, and
And various electronic equipments can be installed in vertical tail body interior with convenient use person, reinforcement batten is provided with cavity, is hung down
Fin this body side surface is provided with square through hole, and steering wheel is fixedly connected with reinforcement batten, is provided with steering wheel on steering wheel, and steering wheel is in ellipse
Circular to arrange, steering wheel end is located at outside vertical tail body through square through hole, is provided with semicircle shape connector on aileron, and half
Round shape connector and steering wheel are articulated and connected with drive link, and structural strength is high, and transmission performance is good, and reinforcement batten is set for hollow
Put, overall weight can be reduced, can prevent from having influence on the whole machine balancing of aircraft, drive link includes the first U-shaped connection
Part, the second U-shaped connector, threaded rod, the first rivet, the second rivet, the first securing member and the second securing member, steering wheel and a U
Type connector passes through the first rivet and the first securing member connects, and the second U-shaped connector and semicircle shape connector pass through the second rivet
Connect with the second securing member, stable connection reliability.
The above, specific embodiment only of the present utility model, but protection domain of the present utility model do not limit to
In this, any change or replacement expected without creative work should all be covered within protection domain of the present utility model.
Claims (5)
1. a kind of unmanned plane vertical tail, it is characterised in that：Including vertical tail body, aileron, drive link and steering wheel, the pair
In the setting that is inclined upwardly, the bottom surface of the aileron is arranged for polishing, is provided with and pair on the vertical tail body for the bottom surface of the wing
The groove that wing external form is mutually agreed with, the aileron are located in groove, and the aileron is articulated and connected with vertical tail body, the steering wheel
With aileron by being driven lever linkage.
2. unmanned plane vertical tail according to claim 1, it is characterised in that：The vertical tail body interior is provided with
Cavity.
3. unmanned plane vertical tail according to claim 2, it is characterised in that：Reinforcement batten is provided with the cavity,
Described this body side surface of vertical tail is provided with square through hole, and the steering wheel is fixedly connected with reinforcement batten, arranges on the steering wheel
There is steering wheel, the steering wheel ovalize is arranged, the steering wheel end is located at outside vertical tail body through square through hole, described
Semicircle shape connector is provided with aileron, and the semicircle shape connector and steering wheel are articulated and connected with drive link.
4. unmanned plane vertical tail according to claim 3, it is characterised in that：The reinforcement batten is hollow setting.
5. unmanned plane vertical tail according to claim 4, it is characterised in that：The drive link includes the first U-shaped company
Fitting, the second U-shaped connector, threaded rod, the first rivet, the second rivet, the first securing member and the second securing member, the steering wheel with
First U-shaped connector passes through the first rivet and the first securing member connects, and the second U-shaped connector and semicircle shape connector pass through
Second rivet and the connection of the second securing member.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620925870.4U CN206031759U (en) | 2016-08-24 | 2016-08-24 | Unmanned aerial vehicle vertical tail |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620925870.4U CN206031759U (en) | 2016-08-24 | 2016-08-24 | Unmanned aerial vehicle vertical tail |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206031759U true CN206031759U (en) | 2017-03-22 |
Family
ID=58303434
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620925870.4U Active CN206031759U (en) | 2016-08-24 | 2016-08-24 | Unmanned aerial vehicle vertical tail |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206031759U (en) |
-
2016
- 2016-08-24 CN CN201620925870.4U patent/CN206031759U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |