CN107685870A - A kind of four-axle aircraft with damper - Google Patents
A kind of four-axle aircraft with damper Download PDFInfo
- Publication number
- CN107685870A CN107685870A CN201710783208.9A CN201710783208A CN107685870A CN 107685870 A CN107685870 A CN 107685870A CN 201710783208 A CN201710783208 A CN 201710783208A CN 107685870 A CN107685870 A CN 107685870A
- Authority
- CN
- China
- Prior art keywords
- damper
- master control
- control borad
- pedestal
- axle aircraft
- 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.)
- Withdrawn
Links
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 19
- 230000004888 barrier function Effects 0.000 claims description 2
- 230000003139 buffering effect Effects 0.000 claims 1
- 238000005516 engineering process Methods 0.000 abstract description 5
- 239000006096 absorbing agent Substances 0.000 abstract 1
- 230000035939 shock Effects 0.000 abstract 1
- 230000002265 prevention Effects 0.000 description 2
- 241000196324 Embryophyta Species 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
Classifications
-
- 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
- B64D47/02—Arrangements or adaptations of signal or lighting devices
- B64D47/06—Arrangements or adaptations of signal or lighting devices for indicating aircraft presence
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
Abstract
A kind of four-axle aircraft with damper, it is related to vehicle technology field, including propeller, motor, support, pedestal, battery, master control borad, phonetic machine, remote control, undercarriage.Four corners of pedestal are each connected to support, and motor is provided with the end upper surface of support, and propeller is arranged on above motor.Undercarriage is arranged on the lower surface of pedestal, battery is arranged on the lower surface in base central region, power supply is provided for the four-axle aircraft with damper, damper is arranged on pedestal, master control borad is arranged on damper, there is power switching mechanism inside master control borad, phonetic machine is arranged on master control borad upper surface, and phonetic machine is connected with wire with the power switching mechanism inside master control borad.Phonetic machine can send the sound when the four-axle aircraft with damper is lost in the place that operator can't see or is not manipulated using remote control.The mounting shock absorber on pedestal, damper can be that master control borad and phonetic machine carry out cushioning effect.
Description
Technical field
A kind of four-axle aircraft with damper, is related to vehicle technology field, more particularly to it is a kind of with damper four
Axle aircraft.
Background technology
With the progress of science and technology, aircraft this respect has obtained great development, has also been obtained in life extensively
Application, such as four-axle aircraft receives pursuing for vast model plane hobby person.But the four-axle aircraft of in the market makes
User manipulate when, it is more likely that occur it is out of control or manipulation technology it is not really up to the mark so as to cause four-axle aircraft lose ask
Topic, and it is all that some have weeds or more woody place mostly to lose place so that operator is difficult to find.In the market
Also there are some four-axle aircrafts with GPS location instrument, but this kind of four-axle aircraft cost is higher, regular player is consumed not
Rise.It is fragile and common four-axle aircraft is intolerant to falling.
The content of the invention
The purpose of the present invention is to overcome the shortcomings of above-mentioned four-axle aircraft, there is provided a kind of four-axle aircraft with damper.
A kind of four-axle aircraft with damper, including propeller, motor, support, pedestal, battery, master control borad, voice
Machine, remote control, undercarriage, damper.Described four corners of pedestal are each connected to support, are installed in the end upper surface of support
There is motor, propeller is arranged on above motor.Undercarriage is arranged on the lower surface of pedestal, and battery is arranged on base central region
Lower surface, power supply is provided for the four-axle aircraft with damper, damper is arranged on pedestal, and master control borad is arranged on damper
On, there is power switching mechanism inside master control borad, phonetic machine is arranged on master control borad upper surface, in phonetic machine wire and master control borad
The power switching mechanism in portion is connected.
A kind of four-axle aircraft with damper is performed such anti-lost work：When operator holds remote control behaviour
When controlling the four-axle aircraft with damper, phonetic machine no power；When remote control control do not live the four-axle aircraft with damper or
Four-axle aircraft with damper fly to operator it is invisible local when, the power sector in master control borad plays a role, and makes
Obtain phonetic machine to be powered, at this moment phonetic machine will send the sound, can just hear operator when operator finds nearby
Sound, it is known that it declines place, so as to realize loss prevention function.
A kind of four-axle aircraft with damper of the present invention, simple in construction, cost is cheaper than the aircraft with GPS location instrument
A lot, it can be that vast consumer group is well-established, and damper is installed, barrier is struck in the four-axle aircraft with damper
When hindering thing, damper can be that master control borad and phonetic machine carry out cushioning effect.
Brief description of the drawings
Fig. 1 is a kind of structural representation of the four-axle aircraft with damper of the present invention；Fig. 2 is a kind of band damping of the invention
The schematic front view of the four-axle aircraft of device.
In figure, including 1- propellers, 2- motors, 3- supports, 4- pedestals, 5- batteries, 6- master control borads, 7- phonetic machines, 8- distant
Control device, 9- undercarriages, 10- dampers.
Embodiment
The present invention is illustrated below in conjunction with the accompanying drawings：A kind of four-axle aircraft with damper, including propeller 1,
Motor 2, support 3, pedestal 4, battery 5, master control borad 6, phonetic machine 7, remote control 8, undercarriage 9, damper 10.
4 four corners of pedestal are each connected to support 3, are provided with motor 2 in the end upper surface of support 3, propeller 1 is pacified
Above motor 2.Undercarriage 9 is arranged on the lower surface of pedestal 4, and battery 5 is arranged on the lower surface of the central area of pedestal 4, is
Four-axle aircraft with damper provides power supply, and damper 10 is arranged on pedestal 4, and master control borad 6 is arranged on damper 10, main
Control the inside of plate 6 and also have power switching mechanism, phonetic machine 7 is arranged on the upper surface of master control borad 6, and phonetic machine 7 is with wire and master control borad 6
The power switching mechanism in portion is connected.
A kind of four-axle aircraft with damper is performed such anti-lost work：When operator holds remote control 8
When manipulating the four-axle aircraft with damper, the no power of phonetic machine 7；When remote control 8 loses control of the four axles flight with damper
Device or four-axle aircraft with damper fly to operator it is invisible local when, the power sector in master control borad 6, which plays, to be made
With so that phonetic machine 7 is powered, and at this moment phonetic machine 7 will send the sound, can just make manipulation people when operator finds nearby
Member hears sound, it is known that it declines place, so as to realize loss prevention function.
Claims (2)
- A kind of 1. four-axle aircraft with damper, mainly including propeller（1）, motor（2）, support（3）, pedestal（4）, battery （5）, master control borad（6）, phonetic machine（7）, remote control（8）, undercarriage（9）, damper（10）, it is characterised in that：Pedestal（4）Four Corner is each connected to support（3）, in support（3）End upper surface motor is installed（2）, propeller（1）Installed in motor （2）Top；Undercarriage（9）Installed in pedestal（4）Lower surface, battery（5）Installed in pedestal（4）The lower surface of central area, Power supply is provided for the four-axle aircraft with damper.
- A kind of 2. four-axle aircraft with damper according to claim 1, it is characterised in that：Damper（10）It is arranged on Pedestal（4）On, master control borad（6）Installed in damper（10）On, master control borad（6）There is power switching mechanism, phonetic machine in inside（7） Installed in master control borad（6）Upper surface, phonetic machine（7）With wire and master control borad（6）Internal power switching mechanism is connected, in band When the four-axle aircraft of damper strikes barrier, damper（10）It can be master control borad（6）And phonetic machine（7）Enter row buffering Effect.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710783208.9A CN107685870A (en) | 2017-09-03 | 2017-09-03 | A kind of four-axle aircraft with damper |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710783208.9A CN107685870A (en) | 2017-09-03 | 2017-09-03 | A kind of four-axle aircraft with damper |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107685870A true CN107685870A (en) | 2018-02-13 |
Family
ID=61155896
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710783208.9A Withdrawn CN107685870A (en) | 2017-09-03 | 2017-09-03 | A kind of four-axle aircraft with damper |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107685870A (en) |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204197292U (en) * | 2014-08-07 | 2015-03-11 | 金卫红 | A kind of Multi-axis aircraft |
| CN106347643A (en) * | 2016-11-02 | 2017-01-25 | 王宇飞 | Automatic protection system for unmanned plane |
| CN106828928A (en) * | 2016-12-29 | 2017-06-13 | 合肥旋极智能科技有限公司 | A kind of unmanned plane search and rescue system based on Internet of Things |
-
2017
- 2017-09-03 CN CN201710783208.9A patent/CN107685870A/en not_active Withdrawn
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204197292U (en) * | 2014-08-07 | 2015-03-11 | 金卫红 | A kind of Multi-axis aircraft |
| CN106347643A (en) * | 2016-11-02 | 2017-01-25 | 王宇飞 | Automatic protection system for unmanned plane |
| CN106828928A (en) * | 2016-12-29 | 2017-06-13 | 合肥旋极智能科技有限公司 | A kind of unmanned plane search and rescue system based on Internet of Things |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| TA01 | Transfer of patent application right | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20181025 Address after: 528000 201L two (1 / two) of Feng Jie street, Chao'an Road, Zu Miao street, Chancheng District, Guangdong, China (residence declaration) Applicant after: Foshan Jiayun Aviation Technology Co. Ltd. Address before: 528000 201Q two (1 / two) of Feng Jie street, Chao'an Road, Zu Miao street, Chancheng District, Guangdong, China (residence declaration) Applicant before: Foshan flying Technology Co., Ltd. |
|
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20180213 |