CN208102308U - A kind of telescopic device of unmanned plane horn - Google Patents
A kind of telescopic device of unmanned plane horn Download PDFInfo
- Publication number
- CN208102308U CN208102308U CN201820189701.8U CN201820189701U CN208102308U CN 208102308 U CN208102308 U CN 208102308U CN 201820189701 U CN201820189701 U CN 201820189701U CN 208102308 U CN208102308 U CN 208102308U
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- telescopic arm
- telescopic
- rotation axis
- piston rod
- 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.)
- Expired - Fee Related
Links
Landscapes
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Abstract
The utility model discloses a kind of telescopic devices of unmanned plane horn,Its structure includes unmanned plane body,Unmanned plane rotator,Unmanned plane blade,Rotation axis fixed block,Rotation axis,Telescopic arm link block,Telescopic arm,Support leg,Camera,Status indicator lamp,Unmanned plane Rotary Connection block,The insertion of unmanned plane Rotary Connection block is installed in unmanned plane rotator,A kind of telescopic device of unmanned plane horn of the utility model,Structure is equipped with telescopic arm,By oil inlet and outlet, continuously input pressure is oily,When the pressure of oil is enough to overcome all loads on piston rod,Piston is continuously moved to another chamber with speed,Piston rod does work to the external world,Vice versa,Piston rod insertion is installed on piston cylinder,Enable to telescopic arm flexible,Then telescopic arm shell can play the role of protecting inner body,During being flown,The effect that effectively length of horn can be adjusted,So as to change the stability and harmony of unmanned plane during flying.
Description
Technical field
The utility model is a kind of telescopic device of unmanned plane horn, belongs to telescopic device technical field.
Background technique
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, is using radio robot and to provide for oneself
The not manned aircraft of presetting apparatus manipulation, or fully or intermittently automatically operated by car-mounted computer, with someone
It driving an airplane and compares, unmanned plane is often more suitable for the task of those too " slow-witted, dirty or dangerous ", and unmanned plane presses application field,
Can be divided into it is military with it is civilian, military aspect, unmanned plane is divided into reconnaissance plane and target drone.
Prior art discloses application No. is：201720036410.0 a kind of scalable horn of unmanned plane, including first
Horn, the second horn, spring and positioning pin, first horn are tubular structure, and the inner hole of first horn is equipped with interior spiral shell
Line, the side of first horn are equipped with multiple through-holes arranged side by side, and the shape of second horn is cylinder, and described the
The outer surface of two horns is equipped with external screw thread, and the side of second horn is equipped with a blind hole, and the spring and positioning pin are located at
In the blind hole, the spring is located at the bottom of the blind hole, and the outer end face of the positioning pin is bulb, and second horn is logical
The internal screw thread for crossing the external screw thread and first horn is spirally connected, and the upper end of the positioning pin withstands on the bottom of the through-hole, still
The prior art unmanned plane horn flexibility is poor, during being flown, since the problem of wind speed is easy to influence nobody
Machine harmony.
Utility model content
In view of the deficienciess of the prior art, the utility model aim is to provide a kind of telescopic device of unmanned plane horn,
It is poor to solve prior art unmanned plane horn flexibility, during being flown, it is easy the problem of due to wind speed to influence
The problem of unmanned plane harmony.
To achieve the goals above, the utility model is to realize by the following technical solutions：A kind of unmanned plane horn
Telescopic device, structure include unmanned plane body, unmanned plane rotator, unmanned plane blade, rotation axis fixed block, rotation axis,
Telescopic arm link block, telescopic arm, support leg, camera, status indicator lamp, unmanned plane Rotary Connection block, the unmanned plane rotation
Link block insertion is installed in unmanned plane rotator, and the unmanned plane Rotary Connection block is integrated with unmanned plane body,
The unmanned plane blade is connect with rotation axis fixed block, and the rotation axis fixed block is mutually welded with rotation axis, the camera position
In the lower section of status indicator lamp, the telescopic arm includes that piston rod, sealing ring, buffering connect flow controller, telescopic arm shell, buffering
Set, flange, the check valve with air vent, piston cylinder, oil inlet and outlet, the piston rod insertion are installed in telescopic arm shell, institute
It states piston rod to be connected with sealing ring, buffering is equipped in the telescopic arm shell and connects flow controller, the cushion collar and piston cylinder phase
Connection, the flange insertion are installed in telescopic arm shell, and oil inlet and outlet, the band air vent are equipped in the telescopic arm shell
Check valve insertion be installed in telescopic arm shell.
Further, the telescopic arm insertion is installed in unmanned plane rotator.
Further, the rotation axis insertion is installed in telescopic arm link block.
Further, the telescopic arm shell insertion is installed in telescopic arm link block.
Further, the upper surface of the support leg and the lower surface of unmanned plane body are mutually welded.
Further, the support leg is formed using stainless steel material, has the effects that anticorrosion.
Further, the telescopic arm is made of ferritic stainless steel, has the effects that water vapor.
Beneficial effect
A kind of telescopic device of unmanned plane horn of the utility model, structure is equipped with telescopic arm, continuous by oil inlet and outlet
Ground input pressure oil, when the pressure of oil is enough to overcome all loads on piston rod, piston is continuously transported to another chamber with speed
Dynamic, piston rod does work to the external world, and vice versa, and piston rod insertion is installed on piston cylinder, enables to telescopic arm flexible, then stretches
Arm shell can play the role of protect inner body, during being flown, can effectively to the length of horn into
The effect that row is adjusted, so as to change the stability and harmony of unmanned plane during flying.
Detailed description of the invention
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other spies of the utility model
Sign, objects and advantages will become more apparent upon：
Fig. 1 is a kind of structural schematic diagram of the telescopic device of unmanned plane horn of the utility model；
Fig. 2 is the structural schematic diagram of the inside of the utility model telescopic arm.
In figure：Unmanned plane body -1, unmanned plane rotator -2, unmanned plane blade -3, rotation axis fixed block -4, rotation axis -
5, telescopic arm link block -6, telescopic arm -7, support leg -8, camera -9, status indicator lamp -10, unmanned plane Rotary Connection block -
11, piston rod -701, sealing ring -702, buffering connect flow controller -703, telescopic arm shell -704, cushion collar -705, flange -706,
Check valve -707, piston cylinder -708, oil inlet and outlet -709 with air vent.
Specific embodiment
To be easy to understand the technical means, creative features, achievement of purpose, and effectiveness of the utility model, below
In conjunction with specific embodiment, the utility model is further described.
Fig. 1, Fig. 2 are please referred to, the utility model provides a kind of telescopic device technical solution of unmanned plane horn：Its structure packet
Include unmanned plane body 1, unmanned plane rotator 2, unmanned plane blade 3, rotation axis fixed block 4, rotation axis 5, telescopic arm link block 6,
Telescopic arm 7, support leg 8, camera 9, status indicator lamp 10, unmanned plane Rotary Connection block 11, the unmanned plane Rotary Connection block
11 insertions are installed in unmanned plane rotator 2, and the unmanned plane Rotary Connection block 11 is integrated with unmanned plane body 1,
The unmanned plane blade 3 is connect with rotation axis fixed block 4, and the rotation axis fixed block 4 is welded with 5 phase of rotation axis, the camera shooting
First 9 be located at status indicator lamp 10 lower section, the telescopic arm 7 include piston rod 701, sealing ring 702, buffering connect flow controller 703,
Telescopic arm shell 704, cushion collar 705, flange 706, the check valve 707 with air vent, piston cylinder 708, oil inlet and outlet 709, institute
It states the insertion of piston rod 701 to be installed in telescopic arm shell 704, the piston rod 701 is connected with sealing ring 702, described flexible
It is equipped with buffering in arm shell 704 and connects flow controller 703, the cushion collar 705 is connected with piston cylinder 708, and the flange 706 is embedded in
It is installed in telescopic arm shell 704, is equipped with oil inlet and outlet 709, the check valve with air vent in the telescopic arm shell 704
707 insertions are installed in telescopic arm shell 704, and the insertion of telescopic arm 7 is installed in unmanned plane rotator 2, the rotation axis 5
Insertion is installed in telescopic arm link block 6, and the insertion of telescopic arm shell 704 is installed in telescopic arm link block 6, the support
The upper surface of foot 8 and the lower surface of unmanned plane body 1 are mutually welded, and the support leg 8 is formed using stainless steel material, are had anti-
The effects of corrosion, the telescopic arm 7 are made of ferritic stainless steel, have the effects that water vapor.
Often there is an indicator light on a kind of key switch of 10 household lamp of status indicator lamp described in this patent, it is this
The Resistance Maximum of indicator light keeps the electric current in circuit minimum, thus make voltage rating is not achieved in the voltage of night electrical appliance and
Cannot be bright, there is a capacitor in this indicator light under normal circumstances, the unmanned plane blade 3 is also slide plate machine, vane machine, cares for name
Think justice, be to realize gas compression by moving blade, will finally realize that mechanical energy is converted to a kind of compressor of wind energy.It belongs to
In one kind of positive displacement compressor.
It is carrying out in use, cylinder barrel is fixed, by oil inlet and outlet 709, continuously input pressure is oily, when the pressure of oil is enough
When overcoming all loads on piston rod 701, piston is continuously moved to another chamber with speed, and piston rod does work to the external world, on the contrary
, the insertion of piston rod 701 is installed on piston cylinder 708, enables to telescopic arm flexible, then telescopic arm shell 704 can play
Protect the effect of inner body.
The utility model solution prior art unmanned plane horn flexibility is poor, during being flown, due to wind
The problem of speed is easy the problem of influencing unmanned plane harmony, and the utility model is combined with each other by above-mentioned component, is set in structure
There is telescopic arm, by oil inlet and outlet, continuously input pressure is oily, when the pressure of oil is enough to overcome all loads on piston rod,
Piston is continuously moved to another chamber with speed, and piston rod does work to the external world, and vice versa, and piston rod insertion is installed on piston cylinder,
Enable to telescopic arm flexible, then telescopic arm shell can play the role of protecting inner body, during being flown,
The effect that effectively length of horn can be adjusted, so as to change the stability and harmony of unmanned plane during flying,
It is described in detail below:
The telescopic arm 7 connects flow controller 703, telescopic arm shell 704, buffering including piston rod 701, sealing ring 702, buffering
Cover 705, flange 706, the check valve 707 with air vent, piston cylinder 708, oil inlet and outlet 709, the insertion of piston rod 701 installation
In in telescopic arm shell 704, the piston rod 701 is connected with sealing ring 702, is equipped with buffering in the telescopic arm shell 704
Flow controller 703 is connect, the cushion collar 705 is connected with piston cylinder 708, and the insertion of flange 706 is installed on telescopic arm shell 704
It is interior, oil inlet and outlet 709 is equipped in the telescopic arm shell 704, the insertion of check valve 707 with air vent is installed on telescopic arm
In shell 704.
The basic principles and main features of the present invention and the advantages of the present invention have been shown and described above, for
For those skilled in the art, it is clear that the present invention is not limited to the details of the above exemplary embodiments, and without departing substantially from this
In the case where the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by institute
Attached claim rather than above description limit, it is intended that will fall within the meaning and scope of the equivalent elements of the claims
All changes are embraced therein.It should not treat any reference in the claims as limiting related right
It is required that.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiments being understood that.
Claims (5)
1. a kind of telescopic device of unmanned plane horn, it is characterised in that：Its structure includes unmanned plane body (1), unmanned plane rotation
Device (2), unmanned plane blade (3), rotation axis fixed block (4), rotation axis (5), telescopic arm link block (6), telescopic arm (7), support
Foot (8), camera (9), status indicator lamp (10), unmanned plane Rotary Connection block (11), the unmanned plane Rotary Connection block (11)
Insertion is installed in unmanned plane rotator (2), and the unmanned plane Rotary Connection block (11) is integrated knot with unmanned plane body (1)
Structure, the unmanned plane blade (3) connect with rotation axis fixed block (4), and the rotation axis fixed block (4) is mutually welded with rotation axis (5)
It connects, the camera (9) is located at the lower section of status indicator lamp (10), and the telescopic arm (7) includes piston rod (701), sealing ring
(702), buffering connect flow controller (703), telescopic arm shell (704), cushion collar (705), flange (706), with the unidirectional of air vent
Valve (707), piston cylinder (708), oil inlet and outlet (709), piston rod (701) insertion are installed in telescopic arm shell (704),
The piston rod (701) is connected with sealing ring (702), and buffering is equipped in the telescopic arm shell (704) and connects flow controller
(703), the cushion collar (705) is connected with piston cylinder (708), and flange (706) insertion is installed on telescopic arm shell
(704) in, oil inlet and outlet (709) are equipped in the telescopic arm shell (704), check valve (707) insertion with air vent
It is installed in telescopic arm shell (704).
2. a kind of telescopic device of unmanned plane horn according to claim 1, it is characterised in that：The telescopic arm (7) is embedding
Enter to be installed in unmanned plane rotator (2).
3. a kind of telescopic device of unmanned plane horn according to claim 1, it is characterised in that：The rotation axis (5) is embedding
Enter to be installed in telescopic arm link block (6).
4. a kind of telescopic device of unmanned plane horn according to claim 1, it is characterised in that：The telescopic arm shell
(704) insertion is installed in telescopic arm link block (6).
5. a kind of telescopic device of unmanned plane horn according to claim 1, it is characterised in that：The support leg (8)
Upper surface and the lower surface of unmanned plane body (1) are mutually welded.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820189701.8U CN208102308U (en) | 2018-02-05 | 2018-02-05 | A kind of telescopic device of unmanned plane horn |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820189701.8U CN208102308U (en) | 2018-02-05 | 2018-02-05 | A kind of telescopic device of unmanned plane horn |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208102308U true CN208102308U (en) | 2018-11-16 |
Family
ID=64128204
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820189701.8U Expired - Fee Related CN208102308U (en) | 2018-02-05 | 2018-02-05 | A kind of telescopic device of unmanned plane horn |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208102308U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108557053A (en) * | 2018-02-05 | 2018-09-21 | 叶哲企 | A kind of telescopic device of unmanned plane horn |
-
2018
- 2018-02-05 CN CN201820189701.8U patent/CN208102308U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108557053A (en) * | 2018-02-05 | 2018-09-21 | 叶哲企 | A kind of telescopic device of unmanned plane horn |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN208360489U (en) | A kind of retractable unmanned plane undercarriage | |
| CN208102308U (en) | A kind of telescopic device of unmanned plane horn | |
| CN108557053A (en) | A kind of telescopic device of unmanned plane horn | |
| CN209258403U (en) | A kind of multifunctional fire-fighting unmanned helicopter | |
| CN108583893A (en) | A kind of intelligent plant protection drone that the cruising ability being conveniently replaceable battery is strong | |
| CN206789975U (en) | Can carry the device of combustible removing is carried out on unmanned plane | |
| CN107161316A (en) | A kind of replaceable horn connect-disconnect structure of unmanned plane | |
| CN206017928U (en) | A kind of breather valve | |
| CN203783680U (en) | Biaxial rotating type oil absorption ventilation device for aerobatics | |
| CN206476119U (en) | It is a kind of from rotor plant protection unmanned plane | |
| CN207795936U (en) | A kind of pistol two-man act structure | |
| CN105620773A (en) | Two-way ventilation device for universal airplane wing fuel tank ventilation system | |
| CN207060393U (en) | A kind of horn, frame and unmanned plane | |
| CN107165761B (en) | A kind of igniter for automobile with concealed apex angle termination | |
| CN209298362U (en) | A kind of New-style electrical wire connector | |
| CN208793117U (en) | A kind of intelligent engine structure | |
| CN206645008U (en) | Depopulated helicopter rotor head with built-in fixing axle | |
| CN206860703U (en) | A kind of spline pair for preventing accidental separation | |
| CN207162255U (en) | A kind of unmanned remotely controlled submersible vehicle lighting module | |
| CN209233676U (en) | A kind of motor enclosed seat | |
| CN209487995U (en) | A kind of waterproof distribution box | |
| CN107906105A (en) | A kind of high sealing quick-release bolt for airframe | |
| CN109990073A (en) | A kind of automobile gearbox seal structure for casing | |
| CN203416504U (en) | Printed circuit board (PCB) group and light-emitting diode (LED) light fixture | |
| CN109159898A (en) | A kind of unmanned plane sprayed insecticide |
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: 20181116 Termination date: 20190205 |