CN104436686A - Front bumper device for aero-model helicopter - Google Patents

Front bumper device for aero-model helicopter Download PDF

Info

Publication number
CN104436686A
CN104436686A CN201410741641.2A CN201410741641A CN104436686A CN 104436686 A CN104436686 A CN 104436686A CN 201410741641 A CN201410741641 A CN 201410741641A CN 104436686 A CN104436686 A CN 104436686A
Authority
CN
China
Prior art keywords
solar cell
fixedly connected
helicopter
warning lamp
crash
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.)
Granted
Application number
CN201410741641.2A
Other languages
Chinese (zh)
Other versions
CN104436686B (en
Inventor
张立
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.)
Zhejiang Plastic China Technology Co.,Ltd.
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CN201410741641.2A priority Critical patent/CN104436686B/en
Publication of CN104436686A publication Critical patent/CN104436686A/en
Application granted granted Critical
Publication of CN104436686B publication Critical patent/CN104436686B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Toys (AREA)

Abstract

The invention relates to a front bumper device for a aero-model helicopter. The device comprises an anti-collision bracket connected with the front end of a helicopter fuselage by a bolt. Both ends of the anti-collision bracket are fixedly connected with warning lamps for illuminating at night; the top ends of the warning lamps are fixedly connected with protective covers for promoting safety; the upper surface of the anti-collision bracket is fixedly connected with a solar cell for supplying power to the warning lamps and charging a fuselage storage battery; a control device which is provided with a built-in light sensor and is used for controlling the warning lamps to work at night is arranged on the upper surface of the solar cell; the control device is electrically connected with the solar cell. The front bumper device for the aero-model helicopter, which is disclosed by the invention, is provided with the anti-collision warning lamps, a light control switch and the solar cell, so that safety and cruising power of a helicopter are greatly promoted.

Description

A kind of front guard frame for helicopter model
Technical field
The present invention relates to a kind of front guard frame for helicopter model.
Background technology
Common helicopter model fuselage does not have anti-collision device; helicopter model break down or maloperation time; be easy to cause fuselage breakage because clash into or scrap; very dangerous; and common safeties structure is simple; cannot provide warning at night, solar recharging and auxiliary collision prevention function, function is very single.
Summary of the invention
The technical problem to be solved in the present invention is: for solving above-mentioned Problems existing, provides a kind of front guard frame for helicopter model, and solving pure helicopter model plane does not have multi-functional front security anti-collision device, causes the problem that fuselage security is poor.
The technical solution adopted for the present invention to solve the technical problems is: a kind of front guard frame for helicopter model, comprise crash-proof bracket bolted with helicopter fuselage front end, crash-proof bracket two ends are fixedly connected with the warning lamp for night illumination, warning lamp top is fixedly connected with the protective cover for promoting security, crash-proof bracket upper surface is fixedly connected with for being powered to warning lamp and the solar cell of fuselage charge in batteries, solar cell upper surface is provided with the control device that built in light line sensor is being worked at night for controlling warning lamp, control device is electrically connected with solar cell.
Further, disconnected of crash-proof bracket is fixedly connected with the reflecting piece for promoting security.
Further, protective cover is translucent protective cover.
The invention has the beneficial effects as follows, of the present inventionly on the front guard frame of helicopter model, be provided with accident alarming light, light gauge tap and solar cell, greatly promote security and the flying power of helicopter.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the present invention is further described.
Fig. 1 is decomposition texture schematic diagram of the present invention.
Fig. 2 is structural representation of the present invention.
1. crash-proof brackets, 2. warning lamp, 3. protective cover, 4. solar cell, 5. control device, 6. reflecting piece in figure.
Detailed description of the invention
In conjunction with the accompanying drawings, the present invention is further detailed explanation.These accompanying drawings are the schematic diagram of simplification, only basic structure of the present invention are described in a schematic way, and therefore it only shows the formation relevant with the present invention.
A kind of front guard frame for helicopter model as depicted in figs. 1 and 2, comprise the bolted crash-proof bracket 1 with helicopter fuselage front end, crash-proof bracket 1 two ends are fixedly connected with the warning lamp 2 for night illumination, warning lamp 2 top is fixedly connected with the protective cover 3 for promoting security, crash-proof bracket 1 upper surface is fixedly connected with for being powered and the solar cell 4 of fuselage charge in batteries to warning lamp 2, solar cell 4 upper surface is provided with the control device 5 that built in light line sensor is being worked at night for controlling warning lamp 2, control device 5 is electrically connected with solar cell 4, further, disconnected of crash-proof bracket 1 is fixedly connected with the reflecting piece 6 for promoting security, further, protective cover 3 is translucent protective cover, of the present inventionly on the front guard frame of helicopter model, be provided with accident alarming light 2, light gauge tap and solar cell 4, greatly promote security and the flying power of helicopter.
People are when operating helicopter model, control device 5 on helicopter model is strong and weak by light sensor induction sunlight, when sunlight is more weak, automatically open warning lamp 2, prevent people from not seeing helicopter model on ground, cause maloperation, when light is stronger, automatically close warning lamp 2, thus energy-conserving and environment-protective, also give the storage battery power supply in fuselage simultaneously by solar cell 4, thus promote voyage.
With above-mentioned according to desirable embodiment of the present invention for enlightenment, by above-mentioned description, relevant staff in the scope not departing from this invention technological thought, can carry out various change and amendment completely.The technical scope of this invention is not limited to the content on description, must determine its technical scope according to right.

Claims (3)

1. the front guard frame for helicopter model, comprise and the bolted crash-proof bracket in helicopter fuselage front end (1), it is characterized in that: described crash-proof bracket (1) two ends are fixedly connected with the warning lamp (2) for night illumination, described warning lamp (2) top is fixedly connected with the protective cover (3) for promoting security, described crash-proof bracket (1) upper surface is fixedly connected with for warning lamp (2) power supply and the solar cell (4) of fuselage charge in batteries, described solar cell (4) upper surface is provided with built in light line sensor for controlling warning lamp (2) in the control device of working at night (5), described control device (5) is electrically connected with solar cell (4).
2. the front guard frame for helicopter model according to claim 1, is characterized in that: disconnected described of crash-proof bracket (1) is fixedly connected with reflecting piece (6).
3. the front guard frame for helicopter model according to claim 1, is characterized in that: described protective cover (3) is translucent protective cover.
CN201410741641.2A 2014-12-09 2014-12-09 Front bumper device for aero-model helicopter Active CN104436686B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410741641.2A CN104436686B (en) 2014-12-09 2014-12-09 Front bumper device for aero-model helicopter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410741641.2A CN104436686B (en) 2014-12-09 2014-12-09 Front bumper device for aero-model helicopter

Publications (2)

Publication Number Publication Date
CN104436686A true CN104436686A (en) 2015-03-25
CN104436686B CN104436686B (en) 2017-01-18

Family

ID=52883906

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410741641.2A Active CN104436686B (en) 2014-12-09 2014-12-09 Front bumper device for aero-model helicopter

Country Status (1)

Country Link
CN (1) CN104436686B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108888970A (en) * 2018-09-18 2018-11-27 高岩 A kind of fixed-wing model plane convenient for landing training

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3798834A (en) * 1973-03-21 1974-03-26 Samuel Alfred Flying disc having impact protected electric signaling device therein
JPH0833772A (en) * 1994-07-22 1996-02-06 Sato Kensetsu Kogyo Kk Wireless control small airplane
US20050227582A1 (en) * 2004-01-16 2005-10-13 Kloos Wade M Composite model construction and method
CN201161112Y (en) * 2008-02-17 2008-12-10 广东高乐玩具股份有限公司 Bidirectional security protection positioning device for airplane toy
CN201342243Y (en) * 2009-01-16 2009-11-11 程美爱 Catapult plane model
CN102743882A (en) * 2012-07-30 2012-10-24 无锡同春新能源科技有限公司 Lighting bamboo dragonfly using solar photovoltaic generation as supply power
CN202538353U (en) * 2012-03-30 2012-11-21 林齐晓 Anti-collision device for model plane
CN203060813U (en) * 2011-12-06 2013-07-17 余昕 Entertainment device
CN203591594U (en) * 2013-10-16 2014-05-14 张宁 Drop-resistant remote-controlled airplane

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3798834A (en) * 1973-03-21 1974-03-26 Samuel Alfred Flying disc having impact protected electric signaling device therein
JPH0833772A (en) * 1994-07-22 1996-02-06 Sato Kensetsu Kogyo Kk Wireless control small airplane
US20050227582A1 (en) * 2004-01-16 2005-10-13 Kloos Wade M Composite model construction and method
CN201161112Y (en) * 2008-02-17 2008-12-10 广东高乐玩具股份有限公司 Bidirectional security protection positioning device for airplane toy
CN201342243Y (en) * 2009-01-16 2009-11-11 程美爱 Catapult plane model
CN203060813U (en) * 2011-12-06 2013-07-17 余昕 Entertainment device
CN202538353U (en) * 2012-03-30 2012-11-21 林齐晓 Anti-collision device for model plane
CN102743882A (en) * 2012-07-30 2012-10-24 无锡同春新能源科技有限公司 Lighting bamboo dragonfly using solar photovoltaic generation as supply power
CN203591594U (en) * 2013-10-16 2014-05-14 张宁 Drop-resistant remote-controlled airplane

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108888970A (en) * 2018-09-18 2018-11-27 高岩 A kind of fixed-wing model plane convenient for landing training
CN108888970B (en) * 2018-09-18 2023-10-27 高岩 Fixed wing model aeroplane and model ship convenient to take off and land training

Also Published As

Publication number Publication date
CN104436686B (en) 2017-01-18

Similar Documents

Publication Publication Date Title
CN104436686A (en) Front bumper device for aero-model helicopter
CN204748537U (en) Solar car safety hammer with illumination and alarm function
CN204674527U (en) Multi-functional broken window life saving emergency hammer
CN203805836U (en) Multifunctional emergency hammer
CN202647549U (en) Secure garmenture lighting system
CN204149839U (en) Solar energy magnetic half body car clothing
CN205815072U (en) There is the safety slip snow slab of generating function
CN201119453Y (en) Solar illumination caution protective helmet
CN210127423U (en) Warning device for expressway
KR20130005194U (en) Light bar integrated with tripod
CN204070710U (en) A kind of photosensitive safety cap
CN204409719U (en) The solar powered multi-functional helmet of riding
CN204126723U (en) There is the mobile energy resource supply equipment of tenminal block safety protection
CN203209785U (en) Sawing machine with infrared detection function
CN202907878U (en) Safety helmet for warning mine accident
CN203353766U (en) Novel multi-directional lighting safety helmet
CN104047714A (en) Mobile energy supply device with amphenol connector safety protection function
CN204309693U (en) A kind of multi-purpose vehicle(MPV) safety appliance depositing declaration form
CN204207160U (en) A kind of wear-type safety cap with safety distinguishing apparatus for building
CN103646499A (en) A station platform direction board
CN205512579U (en) Power construction helmet
CN203180004U (en) Lithium battery for electromobile
CN203372178U (en) Multifunctional automobile emergency hammer
CN203087672U (en) Helmet
CN202834798U (en) Multifunctional field emergent flashlight

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
C41 Transfer of patent application or patent right or utility model
CB03 Change of inventor or designer information

Inventor after: Li Jian

Inventor before: Zhang Li

COR Change of bibliographic data
TA01 Transfer of patent application right

Effective date of registration: 20161019

Address after: 241000 room six, building 1, 1501 Changjiang Bay, Shanxi Road, Jinghu District, Wuhu, Anhui

Applicant after: Li Jian

Address before: Pearl City Road 233000 Anhui Longzihu district city of Bengbu province No. 31 shipping technical school

Applicant before: Zhang Li

C14 Grant of patent or utility model
GR01 Patent grant
TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20180112

Address after: 400147 Chongqing city Yubei District Longxi street new irrigation Road No. 18 building 11 Ambassador city 24-11

Patentee after: Chongqing view Intellectual Property Service Co.,Ltd.

Address before: 241000 room six, building 1, 1501 Changjiang Bay, Shanxi Road, Jinghu District, Wuhu, Anhui

Patentee before: Li Jian

TR01 Transfer of patent right

Effective date of registration: 20190225

Address after: 401120 Chongqing Yubei District Longxi Street Jinlong Road 259 Finance and Information City International 4 1-6

Patentee after: Chongqing Haoting Zhongtuo Environmental Technology Co.,Ltd.

Address before: 400147 Guobin Town, 18 Xinji Avenue, Longxi Street, Yubei District, Chongqing City, 11 blocks, 24-11

Patentee before: Chongqing view Intellectual Property Service Co.,Ltd.

TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20201207

Address after: 313000 Jiuguan town Beigang village Beigang, Nanxun District, Huzhou City, Zhejiang Province

Patentee after: Zhejiang Plastic China Technology Co.,Ltd.

Address before: 401120 Chongqing Yubei District Longxi Street Jinlong Road 259 Finance and Information City International 4 1-6

Patentee before: Chongqing Haoting Zhongtuo Environmental Technology Co.,Ltd.

TR01 Transfer of patent right
EE01 Entry into force of recordation of patent licensing contract

Application publication date: 20150325

Assignee: Huzhou amber New Material Co.,Ltd.

Assignor: Zhejiang Plastic China Technology Co.,Ltd.

Contract record no.: X2021330000165

Denomination of invention: A front safety device for helicopter model

Granted publication date: 20170118

License type: Common License

Record date: 20210828

EE01 Entry into force of recordation of patent licensing contract
PE01 Entry into force of the registration of the contract for pledge of patent right

Denomination of invention: A front safety device for helicopter models

Granted publication date: 20170118

Pledgee: Nanxun Zhejiang rural commercial bank Limited by Share Ltd. old branch branch

Pledgor: Zhejiang Plastic China Technology Co.,Ltd.

Registration number: Y2024330000860

PE01 Entry into force of the registration of the contract for pledge of patent right