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CN107554808A - A kind of anti-lost four-axle aircraft - Google Patents

A kind of anti-lost four-axle aircraft Download PDF

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Publication number
CN107554808A
CN107554808A CN201710783203.6A CN201710783203A CN107554808A CN 107554808 A CN107554808 A CN 107554808A CN 201710783203 A CN201710783203 A CN 201710783203A CN 107554808 A CN107554808 A CN 107554808A
Authority
CN
China
Prior art keywords
lost
master control
pedestal
control borad
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Withdrawn
Application number
CN201710783203.6A
Other languages
Chinese (zh)
Inventor
林海
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Foshan Jiayun Aviation Technology Co. Ltd.
Original Assignee
Foshan Flying Technology Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Foshan Flying Technology Co Ltd filed Critical Foshan Flying Technology Co Ltd
Priority to CN201710783203.6A priority Critical patent/CN107554808A/en
Publication of CN107554808A publication Critical patent/CN107554808A/en
Withdrawn legal-status Critical Current

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Abstract

A kind of anti-lost four-axle aircraft, 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 anti-lost four-axle aircraft, master control borad is installed in the upper surface of the central area of pedestal, 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 anti-lost four-axle aircraft is lost in the place that operator can't see or is not manipulated using remote control.A kind of anti-lost four-axle aircraft of the present invention, simple in construction, cost is cheaply more many than the aircraft with GPS location instrument, can be that vast consuming public receive.

Description

A kind of anti-lost four-axle aircraft
Technical field
A kind of anti-lost four-axle aircraft, it is related to vehicle technology field, more particularly to a kind of anti-lost 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.
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 anti-lost four-axle aircraft.
A kind of anti-lost four-axle aircraft, including it is propeller, motor, support, pedestal, battery, master control borad, phonetic machine, distant Control device, undercarriage.Described four corners of pedestal are each connected to support, and motor, spiral are provided with the end upper surface of support Oar is arranged on above motor.Undercarriage is arranged on the lower surface of pedestal, and battery is arranged on the lower surface in base central region, is anti- Lose four-axle aircraft and power supply is provided, master control borad is installed above the central area of pedestal, also has power supply inside master control borad Switching mechanism, phonetic machine are arranged on master control borad upper surface, and phonetic machine is connected with wire with the power switching mechanism inside master control borad Connect.
A kind of anti-lost four-axle aircraft is performed such anti-lost work:Prevent when operator holds remote control manipulation When losing four-axle aircraft, phonetic machine no power;When remote control control does not live anti-lost four-axle aircraft or anti-lost four axle flies Row device fly to operator it is invisible local when, the power sector in master control borad plays a role so that phonetic machine is powered, at this moment Phonetic machine will send the sound, can just operator is heard sound when operator finds nearby, it is known that it declines to ground Point, so as to realize loss prevention function.
A kind of anti-lost four-axle aircraft of the present invention, simple in construction, cost is cheaper than the aircraft with GPS location instrument very It is more, can be that vast consumer group is well-established.
Brief description of the drawings
Fig. 1 is a kind of structural representation of anti-lost four-axle aircraft of the present invention;Fig. 2 is a kind of anti-lost four axle of the invention The schematic front view of aircraft.
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.
Embodiment
The present invention is illustrated below in conjunction with the accompanying drawings:A kind of anti-lost four-axle aircraft, including propeller 1, motor 2nd, support 3, pedestal 4, battery 5, master control borad 6, phonetic machine 7, remote control 8, undercarriage 9.
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 Anti-lost four-axle aircraft provides power supply, master control borad 6 is installed with the upper surface of the central area of pedestal 4, the inside of master control borad 6 is also There is power switching mechanism, phonetic machine 7 is arranged on the upper surface of master control borad 6, and phonetic machine 7 is turned with wire and the power supply inside master control borad 6 Converting mechanism is connected.
A kind of anti-lost four-axle aircraft is performed such anti-lost work:Manipulated when operator holds remote control 8 During anti-lost four-axle aircraft, the no power of phonetic machine 7;When remote control 8 loses control of anti-lost four-axle aircraft or anti-lost four Axle aircraft fly to operator it is invisible local when, the power sector in master control borad 6 plays a role so that phonetic machine 7 is logical Electricity, at this moment phonetic machine 7 will send the sound, when operator find nearby when can just operator is heard sound, it is known that It declines place, so as to realize loss prevention function.

Claims (2)

  1. A kind of 1. anti-lost four-axle aircraft, mainly including propeller(1), motor(2), support(3), pedestal(4), battery(5)、 Master control borad(6), phonetic machine(7), remote control(8), undercarriage(9), it is characterised in that:Pedestal(4)Four corners are 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, fly for anti-lost four axle Row device provides power supply, in pedestal(4)The upper surface of central area master control borad is installed(6), master control borad(6)There is power supply inside Switching mechanism, phonetic machine(7)Installed in master control borad(6)Upper surface, phonetic machine(7)With wire and master control borad(6)Internal power supply Switching mechanism is connected.
  2. A kind of 2. anti-lost four-axle aircraft according to claim 1, it is characterised in that:When operator holds remote control (8)When manipulating anti-lost four-axle aircraft, phonetic machine(7)No power;Work as remote control(8)Lose control of anti-lost four-axle aircraft Or anti-lost four-axle aircraft fly to operator it is invisible local when, master control borad(6)Interior power sector plays a role, and makes Obtain phonetic machine(7)It is powered, at this moment phonetic machine(7)The sound will be sent.
CN201710783203.6A 2017-09-03 2017-09-03 A kind of anti-lost four-axle aircraft Withdrawn CN107554808A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710783203.6A CN107554808A (en) 2017-09-03 2017-09-03 A kind of anti-lost four-axle aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710783203.6A CN107554808A (en) 2017-09-03 2017-09-03 A kind of anti-lost four-axle aircraft

Publications (1)

Publication Number Publication Date
CN107554808A true CN107554808A (en) 2018-01-09

Family

ID=60978855

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710783203.6A Withdrawn CN107554808A (en) 2017-09-03 2017-09-03 A kind of anti-lost four-axle aircraft

Country Status (1)

Country Link
CN (1) CN107554808A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109573028A (en) * 2018-12-12 2019-04-05 深圳市道通智能航空技术有限公司 A kind of auxiliary unmanned plane method for retrieving, device and unmanned plane

Citations (3)

* Cited by examiner, † Cited by third party
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
CN107084721A (en) * 2013-07-05 2017-08-22 深圳市大疆创新科技有限公司 The device for retrieving and method of unmanned vehicle

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107084721A (en) * 2013-07-05 2017-08-22 深圳市大疆创新科技有限公司 The device for retrieving and method of unmanned vehicle
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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109573028A (en) * 2018-12-12 2019-04-05 深圳市道通智能航空技术有限公司 A kind of auxiliary unmanned plane method for retrieving, device and unmanned plane

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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: 20181024

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: 20180109