CN106466529A - Gyroplane break-in control device - Google Patents

Gyroplane break-in control device Download PDF

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Publication number
CN106466529A
CN106466529A CN201510519757.6A CN201510519757A CN106466529A CN 106466529 A CN106466529 A CN 106466529A CN 201510519757 A CN201510519757 A CN 201510519757A CN 106466529 A CN106466529 A CN 106466529A
Authority
CN
China
Prior art keywords
gyroplane
break
control device
main shaft
electromotor
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.)
Pending
Application number
CN201510519757.6A
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Chinese (zh)
Inventor
许美兰
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
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 CN201510519757.6A priority Critical patent/CN106466529A/en
Publication of CN106466529A publication Critical patent/CN106466529A/en
Pending legal-status Critical Current

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Abstract

The invention discloses a kind of gyroplane break-in control device, this gyroplane break-in control device includes main frame, Shang Gai, landing gear, Power Component and control board, described Power Component includes electromotor, the engine gear being installed on this electromotor main shaft being connected with this engine gear, the main screw being fixed on this main shaft, and described electromotor is miniature oil-burning machine.The present invention has the strong gyroplane break-in control device of super remote endurance, powerful, mobility.

Description

Gyroplane break-in control device
Technical field
The present invention relates to a kind of electronic toy, more particularly, to a kind of gyroplane break-in control device.
Background technology
Aircraft has been increasingly becoming the toy of people's fashion.Existing aircraft to be all driven with electric motor, is so typically necessary offer battery, but existing battery electric quantity amount of storage is extremely limited.Lead to the follow-on mission time of gyroplane break-in control device shorter, and motor mechanomotive force has certain limitation, not powerful.
Therefore, the gyroplane break-in control device of a kind of our demands flight time length, powerful.
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 to have the strong gyroplane break-in control device of super remote endurance, powerful, mobility.
For solving the above problems, the gyroplane break-in control device that the present invention provides includes a kind of gyroplane break-in control device, this gyroplane break-in control device includes main frame, it is connected to the upper lid in front of main frame, it is connected to the empennage at main frame rear, support the landing gear of this main frame, it is arranged at the Power Component on described main frame, and external signal can be received and the control board of described Power Component can be controlled according to external signal, described Power Component includes electromotor, it is installed on the engine gear on this electromotor, the main shaft being connected with this engine gear, it is fixed on the main screw on this main shaft, described electromotor is miniature oil-burning machine.
As an embodiment, described gyroplane break-in control device also includes providing the fuel tank of oil plant for miniature oil-burning machine and is installed on the noise reduction device on described electromotor.This noise reduction device avoids because of the too big impact environment of miniature oil-burning machine noise.
As another embodiment, between described engine gear and main shaft, it is connected with remote control clutch.Described remote control clutch includes the remote control clutch lower cover being connected with engine gear and this remote control clutch lower cover bearing being connected, the power output friction plate connecting this bearing, the remote control clutch rotating disk connecting this power output friction plate.It is additionally provided with fan, this fan can prevent miniature oil-burning machine heating from causing temperature too high between described remote control clutch rotating disk and main shaft.
As another embodiment, described gyroplane break-in control device also includes balanced component, and this balanced component includes being installed on the gimbal lever on main shaft top and the balance blade being arranged at this gimbal lever two ends.It is more safe and reliable that this balanced component makes gyroplane break-in control device fly.
As further embodiment, described gyroplane break-in control device also includes steering assembly and H type fixed mount, pitch that this steering assembly includes being installed on main shaft, steering wheel, the pull bar connecting described steering wheel and pitch, turning sleeve and the connecting rod being connected this turning sleeve and pitch, this steering assembly efficiently controls gyroplane break-in control device and flexibly turns to.It also includes the battery for described control board, steering wheel offer electric energy.Described H type fixed mount is used for installing battery, control board.
Compared with prior art, the gyroplane break-in control device of the present invention drives aircraft flight by miniature oil-burning machine, and the gyroplane break-in control device of the therefore present invention has the strong gyroplane break-in control device of super remote endurance, powerful, mobility.
The gyroplane break-in control device of the present invention for making the present invention easier to understand, is expanded on further below in conjunction with accompanying drawing.
Brief description
Fig. 1 is the schematic diagram of the gyroplane break-in control device 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 gyroplane break-in control device of the present embodiment includes main frame 1, the upper lid 2 being connected to main frame 1 front, the empennage 3 being connected to main frame 1 rear, the landing gear 4 supporting this main frame 1, the Power Component 5 being arranged on described main frame 1, can receive external signal and can control the control board 6 of described Power Component 5 according to external signal.Described main frame 1 is made by special material plate, and it passes through all component of the fixing whole model of an airplane of each fixture.
Described Power Component 5 includes miniature oil-burning machine, the engine gear being installed on this electromotor main shaft being connected with this engine gear, the main screw being fixed on this main shaft.
Remote control clutch is connected with described engine gear.Described remote control clutch includes the remote control clutch lower cover being connected with engine gear and this remote control clutch lower cover bearing being connected, the power output friction plate connecting this bearing, the remote control clutch rotating disk connecting this power output friction plate.It is additionally provided between described remote control clutch rotating disk and main shaft and be sequentially provided with fan, unilateral bearing, start-up rod joint and output sleeve.Described fan can prevent miniature oil-burning machine heating from causing temperature too high.
Described gyroplane break-in control device also includes providing the fuel tank of oil plant for miniature oil-burning machine and is installed on the noise reduction device on described electromotor.This noise reduction device avoids because of the too big impact environment of miniature oil-burning machine noise.Described fuel tank includes the casing of oil bunkering, the first briquetting, the second briquetting, flexible rubber hose and aluminum pipe.Described casing is provided with an opening, and flexible rubber hose is fixedly installed in this opening for described first briquetting and the second briquetting, and this flexible rubber hose is used for sealing this opening, makes the fuel oil in casing occur without leakage.It is designed with through hole, described aluminum pipe is hollow pipe, this aluminum pipe is connected through this through hole with casing, for providing fuel oil to miniature oil-burning machine on described first briquetting, the second briquetting, flexible rubber hose.
Described empennage 3 is included the foot piece being connected with main frame 1 and and is arranged at the tail propeller on foot piece.
Described gyroplane break-in control device also includes balanced component, and this balanced component includes the gimbal lever being installed on main shaft and the balance blade being arranged at this gimbal lever two ends.It is more steadily safe and reliable that this balanced component makes gyroplane break-in control device fly.
Described gyroplane break-in control device also includes steering assembly 0 and H type fixed mount, pitch that this steering assembly includes being installed on main shaft, steering wheel, the pull bar connecting described steering wheel and pitch, turning sleeve and the connecting rod being connected this turning sleeve and pitch, this steering assembly efficiently controls gyroplane break-in control device and flexibly turns to.It also includes the battery for described control board, steering wheel offer electric energy.Described H type fixed mount is used for installing battery, control board.
The gyroplane break-in control device of the present invention drives the flight of gyroplane break-in control device by miniature oil-burning machine, improves genemotor because of battery energy storage is less, be short of power situation.Therefore the present invention has the strong gyroplane break-in control device of super remote endurance, powerful, mobility.
Above disclosed be only presently preferred embodiments of the present invention, certainly the interest field of the present invention, the equivalent variations therefore made according to scope of the present invention patent can not be limited with this, still belong to the scope that the present invention is covered.

Claims (9)

1. a kind of gyroplane break-in control device it is characterised in that:It includes main frame, Shang Gai, landing gear, Power Component and control board, described upper lid is placed in main frame top, described landing gear is placed in main frame bottom, described Power Component and control board are arranged on inside main frame, described Power Component includes electromotor, the engine gear being installed on this electromotor main shaft being connected with this engine gear, the main screw being fixed on this main shaft, and described electromotor is miniature oil-burning machine.
2. gyroplane break-in control device as claimed in claim 1 it is characterised in that:It is connected with remote control clutch between described engine gear and main shaft.
3. gyroplane break-in control device as claimed in claim 2 it is characterised in that:Described remote control clutch includes the remote control clutch lower cover being connected with engine gear and this remote control clutch lower cover bearing being connected, the power output friction plate connecting this bearing, the remote control clutch rotating disk connecting this power output friction plate.
4. gyroplane break-in control device as claimed in claim 3 it is characterised in that:It is additionally provided with fan between described remote control clutch rotating disk and main shaft.
5. gyroplane break-in control device as claimed in claim 1 it is characterised in that:It also includes the noise reduction device being installed on described electromotor.
6. gyroplane break-in control device as claimed in claim 1 it is characterised in that:It also includes balanced component, and this balanced component includes being installed on the gimbal lever on main shaft top and the balance blade being arranged at this gimbal lever two ends.
7. gyroplane break-in control device as claimed in claim 1 it is characterised in that:It also includes steering assembly, pitch that this steering assembly includes being installed on main shaft, steering wheel, the pull bar connecting described steering wheel and pitch, turning sleeve and the connecting rod being connected this turning sleeve and pitch.
8. gyroplane break-in control device as claimed in claim 7 it is characterised in that:It also includes the battery for described control board, steering wheel offer electric energy.
9. gyroplane break-in control device as claimed in claim 8 it is characterised in that:It also includes the H type fixed mount being arranged on main frame, and described battery, control board are installed on this H type fixed mount.
CN201510519757.6A 2015-08-21 2015-08-21 Gyroplane break-in control device Pending CN106466529A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510519757.6A CN106466529A (en) 2015-08-21 2015-08-21 Gyroplane break-in control device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510519757.6A CN106466529A (en) 2015-08-21 2015-08-21 Gyroplane break-in control device

Publications (1)

Publication Number Publication Date
CN106466529A true CN106466529A (en) 2017-03-01

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510519757.6A Pending CN106466529A (en) 2015-08-21 2015-08-21 Gyroplane break-in control device

Country Status (1)

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CN (1) CN106466529A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106552428A (en) * 2015-09-25 2017-04-05 郑华耀 Gear drive model plane

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106552428A (en) * 2015-09-25 2017-04-05 郑华耀 Gear drive model plane

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Application publication date: 20170301