CN105947203A - Folding tail pipe of single-rotor unmanned aerial vehicle - Google Patents
Folding tail pipe of single-rotor unmanned aerial vehicle Download PDFInfo
- Publication number
- CN105947203A CN105947203A CN201610278456.3A CN201610278456A CN105947203A CN 105947203 A CN105947203 A CN 105947203A CN 201610278456 A CN201610278456 A CN 201610278456A CN 105947203 A CN105947203 A CN 105947203A
- Authority
- CN
- China
- Prior art keywords
- tail pipe
- unmanned vehicle
- folding
- metal self
- joints
- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- 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
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Refuge Islands, Traffic Blockers, Or Guard Fence (AREA)
Abstract
The invention relates to an unmanned aerial vehicle, and in particular to a folding tail pipe of a single-rotor unmanned aerial vehicle. The folding tail pipe comprises two separated tail pipes, a movable hinge and metal self-lock catches, wherein the movable hinge and the metal self-lock catches are mounted at the connecting position of the two separated tail pipes; a hinge fixing support of the movable hinge is mounted on the two separated tail pipes; each of the lock bodies of the metal self-lock catches and each of lock catch boxes are separately mounted on the two separated tail pipes. When the unmanned aerial vehicle works, the two separated tail pipes are straightly connected through the metal self-lock catches to be stably connected; when the unmanned aerial vehicle parks, the metal self-lock catches can be opened, and the two folded separated tail pipes are connected through the movable hinge, so that the occupied space of the unmanned aerial vehicle is reduced.
Description
Technical field
The present invention relates to unmanned vehicle, be specifically related to the folding tail pipe of the unmanned vehicle of single rotor.
Background technology
Owing to the distance between tail rotor and the main rotor of the unmanned vehicle of single rotor is determined by its dynamical system,
Unmanned vehicle is when loading flight, owing to flight load-carrying is so large that the distance between its main rotor and tail rotor is relatively big,
So the unmanned vehicle of the single rotor sold in the market, the design of the tail pipe being connected with tail rotor is the most long,
Unmanned vehicle result in its shared length space when being in inactivity very big, thus result in this design to unmanned
The transport of aircraft brings the biggest inconvenience, and to also results in the system of unmanned vehicle relative due to longer tail pipe
Become big, and the longest tail pipe also can make unmanned vehicle the most unstable in transportation, thus also make unmanned vehicle
Maintenance becomes troublesome.
Summary of the invention
It is an object of the invention to provide the folding tail pipe of the unmanned vehicle of single rotor of a kind of simple in construction, to solve mesh
The unmanned vehicle of the single rotor sold on front market, owing to the design of its tail pipe is unreasonable, system that is that cause is relatively big, not side
Just the shortcomings such as numerous and diverse with maintenance work are transported.
To achieve these goals, the folding tail pipe of the unmanned vehicle of single rotor that the present invention provides comprises two joints and divides tail
Pipe, hinges and metal self-locking button；Wherein said hinges and metal self-locking button are mounted in two joints and divide tail pipe
Connection；And the fixed hinge bearing of hinges is separately mounted to two joints and divides on tail pipe, the lock body of metal self-locking button and
Keeper is separately mounted to two joints and divides on tail pipe.Described two joint point tail pipes are the activities dividing tail pipe connection by being positioned at two joints
Hinge is buckled with metal self-locking and is connected or separates folding.
By metal self-locking button, two joint point tail pipes are carried out straight line connection when unmanned vehicle works, make two joints divide tail pipe
Consolidate and be connected, described metal self-locking button can be opened when unmanned vehicle is parked, connected by described hinges after folding
Two joint point tail pipes, thus reduce the space shared by unmanned vehicle.
Preferably, the interface of two described joint point tail pipes is all the structure at square interface, and its material used is that non-carbon is fine
The metal of dimension, includes but not limited to use aerolite.
Preferably, described hinges can connect two joints and divide the joint point tail in tail pipe, and described two joint point tail pipes
Pipe can carry out the folding of 180 degree with hinges for rotary shaft.
Preferably, the quantity of described hinges is 1.
Preferably, described metal self-locking button divides tail pipes to carry out fixing two joints when straight line connects for two joints and divides tail pipe.
Preferably, the quantity of described metal self-locking button is 3.
Preferably, described hinges and metal self-locking button are mounted in two joints and divide the connection of tail pipe, are 3 gold
Belong to self-fastening button and 1 hinges is separately mounted on four faces folding tail pipe of square unmanned vehicle.
Described unmanned vehicle can be fixed on means of transport by fixed support and fixture, makes unmanned vehicle in vanning
During transport more stable, provide convenient for unmanned vehicle vanning transport.Described tail pipe (can be by having four by having bolt
The fixture of individual bolt) fixture be fixed on fixed support, it is possible to by the dismounting of bolt, so that the dimension of unmanned vehicle
Protect and also become simple.
The folding tail pipe of the unmanned vehicle of single rotor of the present invention is to be fixed by metal self-locking button by two joint point tail pipes
The tail pipe of the unmanned vehicle that Cheng Yigen is longer, opens metal self-locking button, can connect two after folding by described hinges
Joint point tail pipe so that two joint point tail pipes fold and are in juxtaposition, and cause and are substantially reduced unmanned flight when parked unmanned vehicle
Space shared by device, and by fixture, tail pipe is fixed on a fixed support, thus improve unmanned vehicle in transport
During stability, carry out unmanned vehicle providing convenient during vanning transport so that the maintenance of unmanned vehicle is simpler
Single.
Other technical characteristic and the technique effect of the present invention will give specifically in detailed description of the invention part subsequently
Bright.
Accompanying drawing explanation
Accompanying drawing is used to provide a further understanding of the present invention, and constitutes the part of description, with following tool
Body embodiment is used for explaining the present invention together, but is not intended that limitation of the present invention.In the accompanying drawings:
Fig. 1 is the knot folding tail pipe of the unmanned vehicle of the single rotor in a kind of embodiment according to present invention offer
Structure schematic diagram.
Description of reference numerals
2 second points of tail pipe 3 metal self-locking button 4 hinges of 1 first point of tail pipe
Detailed description of the invention
Below in conjunction with accompanying drawing, the detailed description of the invention of the present invention is described in detail.It should be appreciated that this place is retouched
The detailed description of the invention stated is merely to illustrate and explains the present invention, is not limited to the present invention.
Embodiment 1
Refer to Fig. 1.The folding tail pipe of the unmanned vehicle of single rotor comprises by first point of tail pipe 1 and second point of tail pipe 2
Two joint point tail pipes of composition and hinges 4 and metal self-locking button 3 are constituted；Wherein first point of tail pipe 1 and the phase of second point of tail pipe 2
There are a hinges 4 and three metal self-locking buttons 3 in junction, and the fixed hinge bearing of described hinges 4 is respectively
Being arranged on first point of tail pipe 1 and second point of tail pipe 2, the lock body of metal self-locking button 3 and keeper are separately mounted on first point
On tail pipe 1 and second point of tail pipe 2；By being positioned at first point of tail pipe 1 and the activity of 2 liang of joint point tail pipe connections of second point of tail pipe
Hinge 4 is buckled 3 and is connected or separates and fold with metal self-locking, and two joint point tail pipes are carried out directly by described metal self-locking button 3
Line connects and fixes two joints and divides tail pipe；Opening described metal self-locking button 3, wherein a joint point tail pipe can be with hinges 4 for turning
Moving axis carries out the folding of 180 degree.
The material that two described joint point tail pipes use is the metal of not the carbon fiber, includes but not limited to use aviation aluminum to close
Gold.
By metal self-locking button 3, two joint point tail pipes are carried out straight line connection when unmanned vehicle works, make two joints divide tail
Pipe is firm to be connected, and can open described metal self-locking button 3 when unmanned vehicle is parked, connect folding by described hinges 4
Two joint point tail pipes of poststack, thus reduce the space shared by unmanned vehicle.
When unmanned vehicle transports, can be fixed on means of transport by fixed support and fixture, make nobody fly
Row device is more stable when vanning transport, provides convenient for unmanned vehicle vanning transport.Described tail pipe is by having four spiral shells
The fixture of bolt is fixed on fixed support, it is possible to by the dismounting of bolt, so that the maintenance of unmanned vehicle also becomes letter
Single.
Embodiment 2
The folding tail pipe of the unmanned vehicle of single rotor is the most same as in Example 1, two the most described joint point tail pipes
Interface be all the structure at square interface, and three metal self-locking buttons 3 and a hinges 4 are separately mounted on unmanned flight
On four faces of the square-folded tail pipe of device.
Technical scheme is described in detail above in association with accompanying drawing, but, the present invention is not limited to above-mentioned embodiment party
Detail in formula, in the technology concept of the present invention, can carry out multiple simple change to technical scheme
Type, these simple variant belong to protection scope of the present invention.
It is further to note that each the concrete technical characteristic described in above-mentioned detailed description of the invention, at not lance
In the case of shield, can be combined by any suitable means, in order to avoid unnecessary repetition, the present invention to various can
The compound mode of energy illustrates the most separately.
Additionally, combination in any, the technology after a combination thereof can also be carried out between the various different embodiment of the present invention
Scheme can realize the purpose of the present invention, reaches the technique effect of the present invention, as long as it is without prejudice to the thought of the present invention, its
Content disclosed in this invention should be considered as equally.
Claims (9)
1. a folding tail pipe for the unmanned vehicle of single rotor, is characterized in that: described folding tail pipe comprise two joints divide tail pipe,
Hinges and metal self-locking button；Wherein said hinges is mounted in two joints with metal self-locking button and divides being connected of tail pipe
Meet place.
The folding tail pipe of the unmanned vehicle of single rotor the most according to claim 1, is characterized in that: described hinges
It is mounted in two joints with metal self-locking button and divides the connection of tail pipe, be that the fixed hinge bearing of hinges is separately mounted to two
On joint point tail pipe, the lock body of metal self-locking button and keeper are separately mounted to two joints and divide on tail pipe.
The folding tail pipe of the unmanned vehicle of single rotor the most according to claim 1 and 2, is characterized in that: two described joints
The interface of point tail pipe is all the structure at square interface.
The folding tail pipe of the unmanned vehicle of single rotor the most according to claim 1 and 2, is characterized in that: described activity
Hinge and metal self-locking are buckled and are mounted in two joints and divide the connection of tail pipe, be 3 metal self-locking buttons and 1 hinges respectively
It is arranged on four faces folding tail pipe of square unmanned vehicle.
The folding tail pipe of the unmanned vehicle of single rotor the most according to claim 1 and 2, is characterized in that: described metal
Self-fastening button is that straight line connects and fixes two joints and divide tail pipe.
The folding tail pipe of the unmanned vehicle of single rotor the most according to claim 4, is characterized in that: described metal self-locking
Button is that straight line connects and fixes two joints and divide tail pipe.
The folding tail pipe of the unmanned vehicle of single rotor the most according to claim 1 and 2, is characterized in that: described metal
The quantity of self-fastening button is 3.
The folding tail pipe of the unmanned vehicle of single rotor the most according to claim 1 and 2, is characterized in that: two described joints
Point tail pipe, wherein a joint point tail pipe is to carry out the folding of 180 degree with hinges for rotary shaft.
The folding tail pipe of the unmanned vehicle of single rotor the most according to claim 1 and 2, is characterized in that: described activity
The quantity of hinge is 1.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610278456.3A CN105947203A (en) | 2016-04-29 | 2016-04-29 | Folding tail pipe of single-rotor unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610278456.3A CN105947203A (en) | 2016-04-29 | 2016-04-29 | Folding tail pipe of single-rotor unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105947203A true CN105947203A (en) | 2016-09-21 |
Family
ID=56916349
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610278456.3A Pending CN105947203A (en) | 2016-04-29 | 2016-04-29 | Folding tail pipe of single-rotor unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105947203A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3116896A (en) * | 1961-04-05 | 1964-01-07 | Eltra Corp | Combination helicopter-automobile |
| US3921938A (en) * | 1973-08-28 | 1975-11-25 | Westland Aircraft Ltd | Helicopters |
| CN201120165Y (en) * | 2007-12-07 | 2008-09-24 | 雷虎科技股份有限公司 | Tail pipe transition transmission structure |
| CN201988179U (en) * | 2011-01-30 | 2011-09-28 | 重庆市电力公司杨家坪供电局 | Wireless remote-control model helicopter with foldable tail pipe |
| CN202953170U (en) * | 2012-09-26 | 2013-05-29 | 北京观典航空设备公司 | Unmanned aerial vehicle (UAV) empennage connecting rod |
| CN205059990U (en) * | 2015-10-15 | 2016-03-02 | 湖南云顶智能科技有限公司 | A collapsible horn for unmanned aerial vehicle |
-
2016
- 2016-04-29 CN CN201610278456.3A patent/CN105947203A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3116896A (en) * | 1961-04-05 | 1964-01-07 | Eltra Corp | Combination helicopter-automobile |
| US3921938A (en) * | 1973-08-28 | 1975-11-25 | Westland Aircraft Ltd | Helicopters |
| CN201120165Y (en) * | 2007-12-07 | 2008-09-24 | 雷虎科技股份有限公司 | Tail pipe transition transmission structure |
| CN201988179U (en) * | 2011-01-30 | 2011-09-28 | 重庆市电力公司杨家坪供电局 | Wireless remote-control model helicopter with foldable tail pipe |
| CN202953170U (en) * | 2012-09-26 | 2013-05-29 | 北京观典航空设备公司 | Unmanned aerial vehicle (UAV) empennage connecting rod |
| CN205059990U (en) * | 2015-10-15 | 2016-03-02 | 湖南云顶智能科技有限公司 | A collapsible horn for unmanned aerial vehicle |
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| PB01 | Publication | ||
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| RJ01 | Rejection of invention patent application after publication | ||
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Application publication date: 20160921 |