CN107298167A - A kind of anti-vibration unmanned plane - Google Patents
A kind of anti-vibration unmanned plane Download PDFInfo
- Publication number
- CN107298167A CN107298167A CN201710569877.6A CN201710569877A CN107298167A CN 107298167 A CN107298167 A CN 107298167A CN 201710569877 A CN201710569877 A CN 201710569877A CN 107298167 A CN107298167 A CN 107298167A
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- CN
- China
- Prior art keywords
- unmanned plane
- plane body
- remote sensing
- baffle
- receiving platform
- 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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- 238000013016 damping Methods 0.000 claims abstract description 23
- 230000006698 induction Effects 0.000 claims abstract description 16
- 238000003780 insertion Methods 0.000 claims abstract description 13
- 230000037431 insertion Effects 0.000 claims abstract description 13
- 238000003466 welding Methods 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 10
- 230000004888 barrier function Effects 0.000 abstract description 6
- 238000012545 processing Methods 0.000 abstract description 4
- 238000007689 inspection Methods 0.000 abstract description 2
- 238000005516 engineering process Methods 0.000 description 7
- 238000013461 design Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000002159 abnormal effect Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000005183 dynamical system Methods 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 230000010365 information processing Effects 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/06—Helicopters with single rotor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Measurement Of Velocity Or Position Using Acoustic Or Ultrasonic Waves (AREA)
Abstract
The invention discloses a kind of anti-vibration unmanned plane, including unmanned plane body and remote sensing receiving platform, the side of the unmanned plane body is provided with screw and baffle-box, and the screw is closely welded with unmanned plane body, and baffle-box insertion is arranged in unmanned plane body, baffle-box is provided with the inside of the screw, and the baffle-box insertion is arranged in unmanned plane body, pass through the cushioning effect with damping spring, can avoid not in time handling flight information progress causes unmanned plane normally to fly to be forced to land and the problem of the vibrations that are subject to are larger, and utilize the antidetonation induction effect of damping induction rod, unmanned plane is set to obtain further protection, be conducive to the safe handling of unmanned plane, and utilize minisize pick-up head, realize the quality of image, the quick inspection of flight reappearance and the quick processing of data, by being provided with supersonic generator, the distance of unmanned plane and barrier can be judged by ultrasonic wave.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, specially a kind of anti-vibration unmanned plane.
Background technology
Unmanned plane industry is new high-tech industry, is related to sensor technology, the communication technology, the information processing technology, intelligence control
Technology processed and weapon and dynamical system technology etc..Empirically, hollow long endurance, the market of Altitude Long Endurance Unmanned Air Vehicle are needed
Total amount is asked to account for about the 60% of unmanned plane overall market demand.Xinda security represent that it is intelligence, aerospace electron, Hong Douhang to have an optimistic view of match
Listed company's After-market performance empty, that unmanned plane development is engaged in into winged integrated, Shandong ore deposit machine etc., in similar disaster monitoring, nothing
It is man-machine that there is irreplaceable effect.Even include the investigation of some explosive incidents, can also be played a role using unmanned plane, nothing
The history of man-machine application is very long, the history for having decades in the world, also has the not short time in China.Remote sensing fields although
There is the application of unmanned plane, but unmanned plane is not greatly developed.
Current anti-vibration unmanned plane, due to handling not in time flight information, so as to cause unmanned plane can not be just
Normal flight, or even landing can be forced, and the vibrations being subject to during landing are larger, so as to cause the damage of unmanned plane
It is bad, and without provided with supersonic generator, it is impossible to the distance of unmanned plane and barrier is judged by ultrasonic wave, when distance is less than
During setpoint distance, cause the flight of unmanned plane dangerous.
So, how to design a kind of anti-vibration unmanned plane, the problem of currently being solved as us.
The content of the invention
It is right not in time to solve to propose in above-mentioned background technology it is an object of the invention to provide a kind of anti-vibration unmanned plane
Flight information is handled, so as to cause the damage of unmanned plane, it is impossible to judge unmanned plane and barrier by ultrasonic wave
Apart from the problem of.
To achieve the above object, the present invention provides following technical scheme：A kind of anti-vibration unmanned plane, including unmanned plane body
With remote sensing receiving platform, the side of the unmanned plane body is provided with screw and baffle-box, and the screw and nobody
Machine body is closely welded, and baffle-box insertion is arranged in unmanned plane body, and buffering is provided with the inside of the screw
Case, and the baffle-box insertion be arranged in unmanned plane body, the surface of the baffle-box is provided with spiral support bar and spiral
Oar, and the spiral support bar is through being arranged in propeller, the downside of the spiral support bar provided with supersonic generator and
Minisize pick-up head, the both sides of the minisize pick-up head are provided with overall framework, and the overall framework passes through with unmanned plane body
Screw is fixedly connected, and the inside of the unmanned plane body is provided with antidetonation cushion course, and antidetonation cushion course insertion is arranged on nothing
In man-machine body, the outer surface of the antidetonation cushion course is provided with adapted lamp and supersonic generator, and the supersonic generator
It is flexibly connected with unmanned plane body, one end of the unmanned plane body is provided with remote sensing receiving platform, the top of the remote sensing receiving platform
Portion is provided with signal receiver, and the remote sensing receiving platform is connected with unmanned plane body by signal receiver signal, described distant
The side of sense receiving platform is provided with information analysis instrument and remote sensing bar, and described information analyzer and remote sensing bar with remote sensing receiving platform
It is fixedly connected.
Further, the end of the screw is provided with lightning protection device, and the lightning protection device is through being arranged in screw.
Further, the bottom of the overall framework is provided with damping spring, and the damping spring and the overall frame
Frame is flexibly connected.
Further, the positive lower end of the unmanned plane body be provided with damping induction rod, and the damping induction rod with it is described
Unmanned plane body is fixedly connected.
Further, the lightning protection device is provided with four, and the lightning protection device is electrically connected with the unmanned plane body.
Further, the surface of the remote sensing receiving platform is provided with display screen and button, and the display screen and button are embedding
Enter to be arranged in the remote sensing receiving platform.
Compared with prior art, the beneficial effects of the invention are as follows：This kind of anti-vibration unmanned plane, by with damping spring
Cushioning effect, can avoid not in time to flight information progress processing cause unmanned plane can not normally fly be forced landing and by
The problem of vibrations arrived are larger, and using the antidetonation induction effect of damping induction rod, unmanned plane is obtained further protection,
Be conducive to the safe handling of unmanned plane, and utilize minisize pick-up head, realize the quality of image, the quick inspection of flight reappearance and data
Quick processing, by being provided with supersonic generator, the distance of unmanned plane and barrier can be judged by ultrasonic wave, when away from
During from less than setpoint distance, the warning light on remote sensing receiving platform is lighted, and reaches early warning effect, while having used baffle-box and antidetonation
Cushion course, when being conducive to the unmanned plane to encounter barrier, can play cushioning effect, protect unmanned plane internal structure, unmanned plane
Sophisticated design and strict control, with wide variety of prospect.
Brief description of the drawings
Fig. 1 is the overall structure diagram of the present invention；
Fig. 2 is the partial structural diagram of remote sensing receiving platform of the present invention；
In figure：1- unmanned plane bodies；2- screws；3- overall frameworks；4- damping springs；5- adapted lamps；6- ultrasonic waves occur
Device；7- minisize pick-up heads；8- damping induction rods；9- antidetonation cushion courses；10- spiral support bars；11- propellers；12- baffle-boxs；
13- lightning protection devices；14- remote sensing receiving platforms；15- signal receivers；16- information analysis instrument；17- remote sensing bars.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation is described, it is clear that described embodiment is only a part of embodiment of the invention, rather than whole embodiments.It is based on
Embodiment in the present invention, it is every other that those of ordinary skill in the art are obtained under the premise of creative work is not made
Embodiment, belongs to the scope of protection of the invention.
Fig. 1-2 is referred to, the present invention provides technical scheme：A kind of anti-vibration unmanned plane, including unmanned plane body 1 and remote sensing
Receiving platform 14, the side of the unmanned plane body 1 is provided with screw 2 and baffle-box 12, and the screw 2 and nobody
Machine body 1 is closely welded, and the insertion of baffle-box 12 is arranged in unmanned plane body 1, and the inner side of the screw 2 is provided with
Baffle-box 2, and the baffle-box 2 insertion be arranged in unmanned plane body 1, the surface of the baffle-box 2 is provided with spiral support
Bar 10 and propeller 11, and the spiral support bar 10 is through being arranged in propeller 11, the downside of the spiral support bar 10
Provided with supersonic generator 6 and minisize pick-up head 7, the both sides of the minisize pick-up head 7 are provided with overall framework 3, and described total
Body framework 3 is screwed with unmanned plane body 1 and is connected, and the inside of the unmanned plane body 1 is provided with antidetonation cushion course 9, and
The insertion of antidetonation cushion course 9 is arranged in unmanned plane body 1, and the outer surface of the antidetonation cushion course 9 is provided with the He of adapted lamp 5
Supersonic generator 6, and the supersonic generator 6 is flexibly connected with unmanned plane body 1, one end of the unmanned plane body 1
Remote sensing receiving platform 14 is installed, the top of the remote sensing receiving platform 14 is provided with signal receiver 15, and the remote sensing receiving platform
14 are connected with unmanned plane body 1 by the signal of signal receiver 15, and the side of the remote sensing receiving platform 14 is provided with information analysis
Instrument 16 and remote sensing bar 17, and described information analyzer 16 and remote sensing bar 17 be fixedly connected with remote sensing receiving platform 14.
Further, the end of the screw 2 is provided with lightning protection device 13, and the lightning protection device 13 is through being arranged on screw
In 2, with lightning protection effect, be conducive to the flight of unmanned plane safety.
Further, the bottom of the overall framework 3 is provided with damping spring 4, and the damping spring 4 and the totality
Framework 3 is flexibly connected, water-tight corrosion-proof antidetonation, effectively increases unmanned machine aided drop boot efficiency and reliability.
Further, the positive lower end of the unmanned plane body 1 is provided with damping induction rod 8, and the damping induction rod 8 and institute
State unmanned plane body 1 to be fixedly connected, using the antidetonation induction effect of damping induction rod 8, unmanned plane is obtained further protection.
Further, the lightning protection device 13 is provided with four, and the lightning protection device 13 electrically connects with the unmanned plane body 1
Connect, improve the security used.
Further, the surface of the remote sensing receiving platform 14 is provided with display screen and button, and the display screen and button
Insertion is arranged in the remote sensing receiving platform 14, is easy to the control for carrying out unmanned plane, is controlled with good fine setting performance and essence
Performance；Operation principle：This kind of anti-vibration unmanned plane, first, is installed to the bottom of overall framework 3, together by damping spring 4 by screw
When damping induction rod 8 is punctured into the central part of the downside of unmanned plane body 1, and by signal receiver 15 by remote sensing receiving platform 14
Connected, unmanned plane body 1 can be opened now with unmanned plane body 1, then to use propeller 11 and screw 2 to enter
Row flight, now carries out the overall monitor work of flight environment of vehicle, then using supersonic generator 6 using minisize pick-up head 7
Send ultrasonic wave to judge the distance of unmanned plane and barrier, while reducing the gas being subject in flight using baffle-box 12
Pressure, then carries out the processing of unmanned plane during flying information by information analysis instrument 16, when the detection of supersonic generator 6 has abnormal
Warning light on remote sensing receiving platform 14 is lighted, and unmanned plane body 1 now is carried out into forced landing, and then utilizes damping spring 4
To reduce the pressure being subject in landing, finally, by the antidetonation induction effect of damping induction rod 8, unmanned plane is allowed to obtain further
Protection.
Although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of changes, modification can be carried out to these embodiments, replace without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (6)
1. a kind of anti-vibration unmanned plane, including unmanned plane body（1）With remote sensing receiving platform（14）, it is characterised in that：It is described nobody
Machine body（1）Side screw is installed（2）And baffle-box（12）, and the screw（2）With unmanned plane body（1）
Close welding, and baffle-box（12）Insertion is arranged on unmanned plane body（1）In, the screw（2）Inner side be provided with
Baffle-box（2）, and the baffle-box（2）Insertion is arranged on unmanned plane body（1）In, the baffle-box（2）Surface be provided with
Spiral support bar（10）And propeller（11）, and the spiral support bar（10）Through being arranged on propeller（11）In, the spiral shell
Circumflex branch strut（10）Downside be provided with supersonic generator（6）And minisize pick-up head（7）, the minisize pick-up head（7）Both sides
Overall framework is installed（3）, and the overall framework（3）With unmanned plane body（1）It is screwed connection, the unmanned plane
Body（1）Inside be provided with antidetonation cushion course（9）, and the antidetonation cushion course（9）Insertion is arranged on unmanned plane body（1）It is interior,
The antidetonation cushion course（9）Outer surface be provided with adapted lamp（5）And supersonic generator（6）, and the supersonic generator
（6）With unmanned plane body（1）It is flexibly connected, the unmanned plane body（1）One end remote sensing receiving platform is installed（14）, it is described distant
Feel receiving platform（14）Top be provided with signal receiver（15）, and the remote sensing receiving platform（14）With unmanned plane body（1）It is logical
Cross signal receiver（15）Signal is connected, the remote sensing receiving platform（14）Side information analysis instrument is installed（16）With remote sensing bar
（17）, and described information analyzer（16）With remote sensing bar（17）With remote sensing receiving platform（14）It is fixedly connected.
2. a kind of anti-vibration unmanned plane according to claim 1, it is characterised in that：The screw（2）End set
There is lightning protection device（13）, and the lightning protection device（13）Through being arranged on screw（2）In.
3. a kind of anti-vibration unmanned plane according to claim 1, it is characterised in that：The overall framework（3）Bottom peace
Equipped with damping spring（4）, and the damping spring（4）With the overall framework（3）It is flexibly connected.
4. a kind of anti-vibration unmanned plane according to claim 1, it is characterised in that：The unmanned plane body（1）Just under
End is provided with damping induction rod（8）, and the damping induction rod（8）With the unmanned plane body（1）It is fixedly connected.
5. a kind of anti-vibration unmanned plane according to claim 1, it is characterised in that：The lightning protection device（13）It is provided with four
It is individual, and the lightning protection device（13）With the unmanned plane body（1）It is electrically connected with.
6. a kind of anti-vibration unmanned plane according to claim 1, it is characterised in that：The remote sensing receiving platform（14）Surface
Display screen and button are provided with, and the display screen and button insertion are arranged on the remote sensing receiving platform（14）In.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710569877.6A CN107298167A (en) | 2017-07-13 | 2017-07-13 | A kind of anti-vibration unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710569877.6A CN107298167A (en) | 2017-07-13 | 2017-07-13 | A kind of anti-vibration unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107298167A true CN107298167A (en) | 2017-10-27 |
Family
ID=60132692
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710569877.6A Withdrawn CN107298167A (en) | 2017-07-13 | 2017-07-13 | A kind of anti-vibration unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107298167A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108033008A (en) * | 2017-12-15 | 2018-05-15 | 佛山市神风航空科技有限公司 | One kind is herded with bionic mechanical bird and its flight control method |
| CN112373701A (en) * | 2020-11-12 | 2021-02-19 | 河南大学 | Petroleum pipeline detects four rotor unmanned aerial vehicle with 5G instant messaging |
-
2017
- 2017-07-13 CN CN201710569877.6A patent/CN107298167A/en not_active Withdrawn
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108033008A (en) * | 2017-12-15 | 2018-05-15 | 佛山市神风航空科技有限公司 | One kind is herded with bionic mechanical bird and its flight control method |
| CN112373701A (en) * | 2020-11-12 | 2021-02-19 | 河南大学 | Petroleum pipeline detects four rotor unmanned aerial vehicle with 5G instant messaging |
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|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20171027 |