CN108557053A - A kind of telescopic device of unmanned plane horn - Google Patents
A kind of telescopic device of unmanned plane horn Download PDFInfo
- Publication number
- CN108557053A CN108557053A CN201810111219.7A CN201810111219A CN108557053A CN 108557053 A CN108557053 A CN 108557053A CN 201810111219 A CN201810111219 A CN 201810111219A CN 108557053 A CN108557053 A CN 108557053A
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- 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.)
- Pending
Links
- 230000003139 buffering effect Effects 0.000 claims description 10
- 238000007789 sealing Methods 0.000 claims description 9
- 238000003780 insertion Methods 0.000 abstract description 19
- 230000037431 insertion Effects 0.000 abstract description 19
- 230000000694 effects Effects 0.000 abstract description 9
- 229910001220 stainless steel Inorganic materials 0.000 description 4
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 241000233855 Orchidaceae Species 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Classifications
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Actuator (AREA)
Abstract
The invention discloses a kind of telescopic devices of unmanned plane horn,Its structure includes unmanned plane body,Unmanned plane circulator,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 circulator,A kind of telescopic device of unmanned plane horn of the present invention,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 present invention is a kind of telescopic device of unmanned plane horn, belongs to telescopic device technical field.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and is provided for oneself
The not manned aircraft that presetting apparatus manipulates, 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 endoporus 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 sets that there are one blind holes, 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 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.
Invention content
In view of the deficienciess of the prior art, it is an object of the present invention to provide a kind of telescopic device of unmanned plane horn, with solution
Certainly the flexibility of prior art unmanned plane horn is poor, during being flown, since the problem of wind speed is easy to influence nobody
The problem of machine harmony.
To achieve the goals above, the present invention is to realize by the following technical solutions：A kind of unmanned plane horn is stretched
Compression apparatus, structure include unmanned plane body, unmanned plane circulator, unmanned plane blade, rotation axis fixed block, rotation axis, stretch
Arm link block, telescopic arm, support leg, camera, status indicator lamp, unmanned plane Rotary Connection block, the unmanned plane rotatable connection
Block insertion is installed in unmanned plane circulator, and the unmanned plane Rotary Connection block is integrated with unmanned plane body, described
Unmanned plane blade is connect with rotation axis fixed block, and the rotation axis fixed block is mutually welded with rotation axis, and the camera is located at shape
The lower section of state indicator light, the telescopic arm include that piston rod, sealing ring, buffering connect flow controller, telescopic arm shell, cushion collar, method
Orchid, the check valve with air vent, piston cylinder, oil inlet and outlet, the piston rod insertion are installed in telescopic arm shell, the piston
Bar is connected with sealing ring, and buffering is equipped in the telescopic arm shell and connects flow controller, the cushion collar is connected with piston cylinder, institute
It states flange insertion to be installed in telescopic arm shell, oil inlet and outlet is equipped in the telescopic arm shell, it is described with the unidirectional of air vent
Valve insertion is installed in telescopic arm shell.
Further, the telescopic arm insertion is installed in unmanned plane circulator.
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, has the effects that anticorrosion.
Further, the telescopic arm is made of ferritic stainless steel, has the effects that water vapor.
Advantageous effect
A kind of telescopic device of unmanned plane horn of the present invention, structure is equipped with telescopic arm, continuously defeated by oil inlet and outlet
Enter pressure oil, when the pressure of oil is enough to overcome all loads on piston rod, piston is continuously moved to another chamber with speed, living
Stopper 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 outside telescopic arm
Shell can play the role of protecting inner body that can effectively adjust the length of horn during being flown
The effect of section, so as to change the stability and harmony of unmanned plane during flying.
Description of the drawings
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other feature of the invention,
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 present invention；
Fig. 2 is the structural schematic diagram of the inside of telescopic arm of the present invention.
In figure：Unmanned plane body -1, unmanned plane circulator -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 implementation mode
To make the technical means, the creative features, the aims and the efficiencies achieved by the present invention be easy to understand, with reference to
Specific implementation mode, the present invention is further explained.
It please refers to Fig.1, Fig. 2, the present invention provides a kind of telescopic device technical solution of unmanned plane horn：Its structure includes nothing
Man-machine body 1, unmanned plane blade 3, rotation axis fixed block 4, rotation axis 5, telescopic arm link block 6, stretches unmanned plane circulator 2
Arm 7, support leg 8, camera 9, status indicator lamp 10, unmanned plane Rotary Connection block 11, the unmanned plane Rotary Connection block 11 are embedding
Enter to be installed in unmanned plane circulator 2, the unmanned plane Rotary Connection block 11 is integrated with unmanned plane body 1, described
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 9
In the lower section of status indicator lamp 10, the telescopic arm 7 connects flow controller 703 including piston rod 701, sealing ring 702, buffering, stretches
Arm shell 704, cushion collar 705, flange 706, the check valve 707 with air vent, piston cylinder 708, oil inlet and outlet 709, the work
The insertion of stopper rod 1 is installed in telescopic arm shell 704, and the piston rod 701 is connected with sealing ring 702, the telescopic arm shell
It is equipped with buffering in 704 and connects flow controller 703, the cushion collar 705 is connected with piston cylinder 708, and the insertion of the flange 706 is installed on
In telescopic arm shell 704, oil inlet and outlet 709 is equipped in the telescopic arm shell 704, the check valve 707 with air vent is embedding
Enter to be installed in telescopic arm shell 704, the insertion of the telescopic arm 7 is installed in unmanned plane circulator 2, and the rotation axis 5 is embedded in
It is installed in telescopic arm link block 6, the insertion of telescopic arm shell 704 is installed in telescopic arm link block 6, the support leg 8
Upper surface and the lower surface of unmanned plane body 1 mutually weld, the support leg 8 is formed using stainless steel, with anti-corrosion
The effects that erosion, the telescopic arm 7 are made of ferritic stainless steel, have the effects that water vapor.
Often there are one indicator lights on a kind of key switch of 10 household lamp of status indicator lamp described in this patent, this
The Resistance Maximum of indicator light keeps the electric current in circuit minimum, to making the voltage in night electrical appliance that rated voltage be not achieved and
Cannot be bright, under normal circumstances there are one capacitance in this indicator light, the unmanned plane blade 3 is also slide plate machine, vane machine, cares for name
Think justice, be that gas compression is realized 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
As the same, 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.
Present invention solution prior art unmanned plane horn flexibility is poor, during being flown, due to wind speed
Problem is easy the problem of influencing unmanned plane harmony, and the present invention is combined with each other by above-mentioned component, and structure is equipped with telescopic arm,
By oil inlet and outlet, continuously input pressure is oily, and when the pressure of oil is enough to overcome all loads on piston rod, piston is with speed
Degree is continuously moved to another chamber, and piston rod does work to the external world, and vice versa, and piston rod insertion is installed on piston cylinder, enables to
Telescopic arm is flexible, then telescopic arm shell can play the role of protecting inner body can be effective during being flown
The effect that is adjusted of the length to horn, it is specific as follows so as to change the stability and harmony of unmanned plane during flying
It is described:
The telescopic arm 7 connects flow controller 703, telescopic arm shell 704, buffering including piston rod 701, sealing ring 702, buffering
Set 705, flange 706, the check valve 707 with air vent, piston cylinder 708, oil inlet and outlet 709, the insertion of the piston rod 1 are installed on
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 is connect
Flow controller 703, the cushion collar 705 are connected with piston cylinder 708, and the insertion of the 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 above shows and describes the basic principles and main features of the present invention and the advantages of the present invention, for this field skill
For art personnel, it is clear that invention is not limited to the details of the above exemplary embodiments, and without departing substantially from the present invention spirit or
In the case of essential characteristic, the present invention can be realized in other specific forms.Therefore, in all respects, should all incite somebody to action
Embodiment regards exemplary as, and is non-limiting, the scope of the present invention by appended claims rather than on state
Bright restriction, it is intended that including all changes that come within the meaning and range of equivalency of the claims in the present invention
It is interior.Any reference signs in the claims should not be construed as limiting the involved claims.
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 embodiment being appreciated 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)
Embedded to be installed in unmanned plane circulator (2), 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), the piston rod (1) is embedded to be installed in telescopic arm shell (704), institute
It states piston rod (701) with sealing ring (702) to be connected, 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 the flange (706) is embedded to be installed in telescopic arm shell (704),
Oil inlet and outlet (709) is equipped in the telescopic arm shell (704), embedded be installed on of the check valve (707) with air vent is stretched
In contracting 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 circulator (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) embedded to be 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 |
|---|---|---|---|
| CN201810111219.7A CN108557053A (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 |
|---|---|---|---|
| CN201810111219.7A CN108557053A (en) | 2018-02-05 | 2018-02-05 | A kind of telescopic device of unmanned plane horn |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108557053A true CN108557053A (en) | 2018-09-21 |
Family
ID=63532218
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810111219.7A Pending CN108557053A (en) | 2018-02-05 | 2018-02-05 | A kind of telescopic device of unmanned plane horn |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108557053A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109278974A (en) * | 2018-10-31 | 2019-01-29 | 上海歌尔泰克机器人有限公司 | Horn structure and unmanned plane |
| US20220332410A1 (en) * | 2021-04-19 | 2022-10-20 | Hyundai Motor Company | Fail safety apparatus of air mobility |
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| CN208102308U (en) * | 2018-02-05 | 2018-11-16 | 季叶兰 | A kind of telescopic device of unmanned plane horn |
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2018
- 2018-02-05 CN CN201810111219.7A patent/CN108557053A/en active Pending
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109278974A (en) * | 2018-10-31 | 2019-01-29 | 上海歌尔泰克机器人有限公司 | Horn structure and unmanned plane |
| US20220332410A1 (en) * | 2021-04-19 | 2022-10-20 | Hyundai Motor Company | Fail safety apparatus of air mobility |
| US11787530B2 (en) * | 2021-04-19 | 2023-10-17 | Hyundai Motor Company | Fail safety apparatus of air mobility |
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Application publication date: 20180921 |