CN106563277A - Model airplane having integration control system - Google Patents

Model airplane having integration control system Download PDF

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Publication number
CN106563277A
CN106563277A CN201510649134.0A CN201510649134A CN106563277A CN 106563277 A CN106563277 A CN 106563277A CN 201510649134 A CN201510649134 A CN 201510649134A CN 106563277 A CN106563277 A CN 106563277A
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CN
China
Prior art keywords
control system
model plane
integrated control
main shaft
main frame
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Withdrawn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
CN201510649134.0A
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Chinese (zh)
Inventor
马铿杰
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.)
Individual
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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 CN201510649134.0A priority Critical patent/CN106563277A/en
Publication of CN106563277A publication Critical patent/CN106563277A/en
Withdrawn legal-status Critical Current

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Abstract

The invention discloses a model airplane having an integration control system. The model airplane comprises a main frame, an upper cover, a landing device, a power assembly and a control circuit board. The power assembly consists of an engine, an engine gear installed at the engine, a main shaft connected with the engine gear, and a main propeller fixed at the main shaft. The engine is a miniature oil-fired engine. The model airplane has advantages of high endurance, powerful power, and good maneuvering performance.

Description

Model plane with integrated control system
Technical field
The present invention relates to a kind of electronic toy, more particularly to a kind of model plane with integrated control system.
Background technology
Aircraft has been increasingly becoming the toy of people's fashion.Existing aircraft is all driven with electric motor, is so typically necessary offer battery, but existing battery electric quantity amount of storage is extremely limited.Cause the follow-on mission time of the model plane with integrated control system shorter, and motor mechanomotive force has certain limitation, it is not powerful enough.
Therefore, a kind of flight time length of our demands, the model plane with integrated control system of powerful.
The content of the invention
Based on the deficiencies in the prior art, problem to be solved by this invention is to provide a kind of model plane with integrated control system strong with super remote endurance, powerful, mobility.
To solve the above problems, the model plane with integrated control system that the present invention is provided include a kind of model plane with integrated control system, should have the model plane of integrated control system includes main frame, the upper lid being connected in front of main frame, it is connected to the empennage at main frame rear, support the landing gear of the main frame, the Power Component being arranged on the main frame, and external signal can be received and the control board of the Power Component can be controlled according to external signal, the Power Component includes electromotor, the engine gear being installed on the electromotor, the main shaft being connected with the engine gear, the main screw being fixed on the main shaft, the electromotor is miniature oil-burning machine.
Used as one embodiment, the model plane with integrated control system also include the fuel tank for providing oil plant for miniature oil-burning machine and the noise reduction device being installed on the electromotor.The noise reduction device is avoided because of the too big impact environment of miniature oil-burning machine noise.
As another embodiment, remote control clutch is connected between the engine gear and main shaft.The remote control clutch includes the bearing of the remote control clutch lower cover being connected with engine gear and remote control clutch lower cover connection, connects the power output friction plate of the bearing, connects the remote control clutch rotating disk of the power output friction plate.Fan is additionally provided between the remote control clutch rotating disk and main shaft, the fan can prevent miniature oil-burning machine from generating heat and causing temperature too high.
Used as another embodiment, the model plane with integrated control system also include balanced component, and the balanced component includes being installed on the gimbal lever on main shaft top and being arranged at the balance blade at the gimbal lever two ends.It is more safe and reliable that the balanced component makes the model plane with integrated control system fly.
As further embodiment; the model plane with integrated control system also include steering assembly and H type fixed mounts; the steering assembly includes the pitch being installed on main shaft, steering wheel, connect the steering wheel and pitch pull bar, turning sleeve and it is connected the connecting rod of the turning sleeve and pitch, the steering assembly efficiently controls the model plane with integrated control system and flexibly turns to.It also includes the battery for providing electric energy for the control board, steering wheel.The H types fixed mount is used to install battery, control board.
Compared with prior art, the model plane with integrated control system of the present invention drive aircraft flight by miniature oil-burning machine, therefore the model plane with integrated control system of the present invention have the strong model plane with integrated control system of super remote endurance, powerful, mobility.
To make the present invention easier to understand, the model plane with integrated control system of the present invention are expanded on further below in conjunction with accompanying drawing.
Description of the drawings
Fig. 1 is the schematic diagram of the model plane with integrated control system of a preferred embodiment of the present invention.
Specific embodiment
With reference now to Description of Drawings the preferred embodiments of the present invention,.
With reference to Fig. 1, the model plane with integrated control system of the present embodiment include main frame 1, the upper lid 2 that is connected to the front of main frame 1, the empennage 3 for being connected to the rear of main frame 1, the landing gear 4 for supporting the main frame 1, the Power Component 5 being arranged on the main frame 1, can receive external signal and the control board 6 of the Power Component 5 can be controlled according to external signal.The main frame 1 is made by special material plate, and it passes through all component that each fixture fixes the whole model of an airplane.
The Power Component 5 includes miniature oil-burning machine, the main shaft of the engine gear being installed on the electromotor and the engine gear connection, the main screw being fixed on the main shaft.
Remote control clutch is connected with the engine gear.The remote control clutch includes the bearing of the remote control clutch lower cover being connected with engine gear and remote control clutch lower cover connection, connects the power output friction plate of the bearing, connects the remote control clutch rotating disk of the power output friction plate.It is additionally provided between the remote control clutch rotating disk and main shaft and is sequentially provided with fan, unilateral bearing, start-up rod joint and output sleeve.The fan can prevent miniature oil-burning machine from generating heat and causing temperature too high.
The model plane with integrated control system also include the fuel tank for providing oil plant for miniature oil-burning machine and the noise reduction device being installed on the electromotor.The noise reduction device is avoided because of the too big impact environment of miniature oil-burning machine noise.The fuel tank includes casing, the first briquetting, the second briquetting, flexible rubber hose and the aluminum pipe of oil bunkering.The casing is provided with an opening, and first briquetting and the second briquetting are fixedly installed on flexible rubber hose in the opening, and the flexible rubber hose is used to seal the opening, makes the fuel oil in casing occur without leakage.Through hole is designed with first briquetting, the second briquetting, flexible rubber hose, the aluminum pipe is hollow pipe, and the aluminum pipe is connected through the through hole with casing, for providing fuel oil to miniature oil-burning machine.
The empennage 3 includes the foot piece being connected with main frame 1 and and the tail propeller that is arranged on foot piece.
The model plane with integrated control system also include balanced component, and the balanced component includes the gimbal lever being installed on main shaft and the balance blade for being arranged at the gimbal lever two ends.It is more steady safe and reliable that the balanced component makes the model plane with integrated control system fly.
The model plane with integrated control system also include steering assembly 0 and H type fixed mounts; the steering assembly includes the pitch being installed on main shaft, steering wheel, connect the steering wheel and pitch pull bar, turning sleeve and it is connected the connecting rod of the turning sleeve and pitch, the steering assembly efficiently controls the model plane with integrated control system and flexibly turns to.It also includes the battery for providing electric energy for the control board, steering wheel.The H types fixed mount is used to install battery, control board.
The model plane with integrated control system of the present invention drive the model plane with integrated control system to fly by miniature oil-burning machine, improve genemotor because of battery energy storage is less, be short of power situation.Therefore the present invention is with the strong model plane with integrated control system of super remote endurance, powerful, mobility.
Above disclosed is only presently preferred embodiments of the present invention, can not limit the interest field of the present invention, therefore the equivalent variations made according to scope of the present invention patent with this certainly, still belongs to the scope that the present invention is covered.

Claims (9)

1. a kind of model plane with integrated control system, it is characterised in that:It includes main frame, upper lid, landing gear, Power Component and control board, the upper lid is placed in main frame top, the landing gear is placed in main frame bottom, the Power Component and control board are arranged on inside main frame, the Power Component includes electromotor, the main shaft of the engine gear being installed on the electromotor and the engine gear connection, the main screw being fixed on the main shaft, and the electromotor is miniature oil-burning machine.
2. there are as claimed in claim 1 the model plane of integrated control system, it is characterised in that:Remote control clutch is connected between the engine gear and main shaft.
3. there are as claimed in claim 2 the model plane of integrated control system, it is characterised in that:The remote control clutch includes the bearing of the remote control clutch lower cover being connected with engine gear and remote control clutch lower cover connection, connects the power output friction plate of the bearing, connects the remote control clutch rotating disk of the power output friction plate.
4. there are as claimed in claim 3 the model plane of integrated control system, it is characterised in that:Fan is additionally provided between the remote control clutch rotating disk and main shaft.
5. there are as claimed in claim 1 the model plane of integrated control system, it is characterised in that:It also includes the noise reduction device being installed on the electromotor.
6. there are as claimed in claim 1 the model plane of integrated control system, it is characterised in that:It also includes balanced component, and the balanced component includes being installed on the gimbal lever on main shaft top and being arranged at the balance blade at the gimbal lever two ends.
7. there are as claimed in claim 1 the model plane of integrated control system, it is characterised in that:It also includes steering assembly, and the steering assembly includes the pitch being installed on main shaft, steering wheel, the pull bar that connects the steering wheel and pitch, turning sleeve and be connected the connecting rod of the turning sleeve and pitch.
8. there are as claimed in claim 7 the model plane of integrated control system, it is characterised in that:It also includes the battery for providing electric energy for the control board, steering wheel.
9. there are as claimed in claim 8 the model plane of integrated control system, it is characterised in that:It also includes the H type fixed mounts being arranged on main frame, and the battery, control board are installed on the H type fixed mounts.
CN201510649134.0A 2015-10-09 2015-10-09 Model airplane having integration control system Withdrawn CN106563277A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510649134.0A CN106563277A (en) 2015-10-09 2015-10-09 Model airplane having integration control system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510649134.0A CN106563277A (en) 2015-10-09 2015-10-09 Model airplane having integration control system

Publications (1)

Publication Number Publication Date
CN106563277A true CN106563277A (en) 2017-04-19

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CN201510649134.0A Withdrawn CN106563277A (en) 2015-10-09 2015-10-09 Model airplane having integration control system

Country Status (1)

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CN (1) CN106563277A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106606880A (en) * 2015-10-23 2017-05-03 许美兰 A model airplane with a micro-fuel oil machine

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2444446A (en) * 2008-01-03 2008-06-04 Silverlit Toys Manufactory Ltd Integrated remote control and storage housing for remote control helicopter.
CN201565139U (en) * 2009-11-12 2010-09-01 陈立光 Novel toy helicopter
CN106492478A (en) * 2015-09-03 2017-03-15 马铿杰 There are the model plane of integrated control system

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2444446A (en) * 2008-01-03 2008-06-04 Silverlit Toys Manufactory Ltd Integrated remote control and storage housing for remote control helicopter.
CN201565139U (en) * 2009-11-12 2010-09-01 陈立光 Novel toy helicopter
CN106492478A (en) * 2015-09-03 2017-03-15 马铿杰 There are the model plane of integrated control system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106606880A (en) * 2015-10-23 2017-05-03 许美兰 A model airplane with a micro-fuel oil machine

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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: 20170419

DD01 Delivery of document by public notice
DD01 Delivery of document by public notice

Addressee: Ma Kengjie

Document name: Notification of Approving Refund