CN105797401A - Propeller impact protector and model airplane provided with propeller impact protector - Google Patents
Propeller impact protector and model airplane provided with propeller impact protector Download PDFInfo
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- CN105797401A CN105797401A CN201410856184.1A CN201410856184A CN105797401A CN 105797401 A CN105797401 A CN 105797401A CN 201410856184 A CN201410856184 A CN 201410856184A CN 105797401 A CN105797401 A CN 105797401A
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- propeller
- protector
- model
- power source
- impact protector
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Abstract
The invention discloses a propeller impact protector and a model airplane provided with the propeller impact protector. The propeller impact protector and the model airplane provided with the propeller impact protector comprise a skeleton, a lower bracket for supporting the skeleton, energy equipment which is arranged on the skeleton and an integrated chip which is capable of receiving external signals and is capable of controlling the energy equipment in accordance with the external signals. The propeller impact protector and the model airplane provided with the propeller impact protector disclosed by the invention have the advantages of long duration and strong power.
Description
Technical field
The present invention relates to a kind of electronic toy, particularly relate to a kind of propeller impact protector and the model of an airplane containing described propeller protector.
Background technology
Aircraft has been increasingly becoming the toy of people's fashion.Existing aircraft is all driven with electric power source, is so typically necessary offer battery, but existing battery electric quantity amount of storage is extremely limited.Cause that the lasting persistent period of propeller impact protector and the model of an airplane containing described propeller protector is shorter, and electric-powered driving source has certain limitation, powerful not.
Therefore, our demand a kind of persistent period length, horsepower foot propeller impact protector and containing the model of an airplane of described propeller protector.
Summary of the invention
Based on the deficiencies in the prior art, problem to be solved by this invention be to provide a kind of persistent period length, horsepower foot propeller impact protector and containing the model of an airplane of described propeller protector.
For solving the problems referred to above, propeller impact protector provided by the invention and the model of an airplane containing described propeller protector include a kind of propeller impact protector and the model of an airplane containing described propeller protector, this propeller impact protector and the model of an airplane containing described propeller protector include skeleton, it is connected to the head-shield in skeleton front, it is connected to the empennage at skeleton rear, support the lower carriage of this skeleton, it is arranged at the energy device on described skeleton, and external signal can be received and the integrated chip of described energy device can be controlled according to external signal, described energy device includes power source, it is installed on the power source gear on this power source, the line shaft being connected with this power source gear, it is fixed on the air propeller on this line shaft, described power source is internal combustion engine.
Also include providing the fuel tank of fuel for internal combustion engine and being installed on the noise absorber on described power source as an embodiment, described propeller impact protector and the model of an airplane containing described propeller protector.This noise absorber is avoided affecting environment because engine noise is too big.
As another embodiment, between described power source gear and line shaft, it is connected with clutching device.The bearing that the clutching device housing that described clutching device includes being connected with power source gear is connected with this clutching device housing, the clutch disc connecting this bearing, connect the spill spin block of this clutch disc.Being additionally provided with chiller between described spill spin block and line shaft, this chiller is possible to prevent internal combustion engine heating to cause temperature too high.
As another embodiment, described propeller impact protector and the model of an airplane containing described propeller protector also include gravity's center control device, and this gravity's center control device includes being installed on the rod and be arranged at the block of weighing and considering in order to uphold justice at these rod two ends of weighing and considering in order to uphold justice of weighing and considering in order to uphold justice on line shaft top.This gravity's center control device makes propeller impact protector and the flight of the model of an airplane containing described propeller protector more safe and reliable.
As further embodiment; described propeller impact protector and the model of an airplane containing described propeller protector also include steering assembly and T-shaped fixed mount; this steering assembly includes the pitch, steering wheel, the described steering wheel of connection and the pull bar of pitch, turning sleeve and the connecting rod being connected this turning sleeve and pitch that are installed on line shaft, and this steering assembly efficiently controls propeller impact protector and the model of an airplane containing described propeller protector flexibly turns to.It also includes the battery for described integrated chip, steering wheel offer electric energy.Described T-shaped fixed mount is used for installing battery, integrated chip.
Compared with prior art; the propeller impact protector of the present invention and the model of an airplane containing described propeller protector drive propeller impact protector and the model of an airplane containing described propeller protector to fly by internal combustion engine, change electric-powered source because of battery energy storage is less, be short of power situation.Therefore the propeller impact protector of the present invention and the model of an airplane containing described propeller protector have the beneficial effect of persistent period length, horsepower foot.
For making the present invention easier to understand, the propeller impact protector of the present invention and the model of an airplane containing described propeller protector are expanded on further below in conjunction with accompanying drawing.
Accompanying drawing explanation
Fig. 1 is propeller impact protector and the structural representation of the model of an airplane containing described propeller protector of a preferred embodiment of the present invention.
Fig. 2 is the explosive view of Fig. 1.
Fig. 3 is the connection diagram of described power source, clutching device and chiller.
Fig. 4 is the structural representation of described fuel tank.
Detailed description of the invention
With reference now to accompanying drawing, the preferred embodiments of the present invention are described.
With reference to Fig. 1, Fig. 2, the propeller impact protector of the present embodiment and the model of an airplane containing described propeller protector include skeleton 10, be connected to the head-shield 20 in skeleton 10 front, be connected to the empennage 30 at skeleton 10 rear, support the lower carriage 40 of this skeleton 10, the energy device 50 being arranged on described skeleton 10, can receive external signal and can control the integrated chip 60 of described energy device 50 according to external signal.Described skeleton 10 is made by special material plate, and it fixes all component of the whole model of an airplane by each fixture.
With reference to Fig. 2, Fig. 3, described energy device 50 includes internal combustion engine 51, the power source gear 52 that is installed on this power source 51 is connected with this power source gear 52 line shaft 53, the air propeller 54 being fixed on this line shaft 53.
Described power source gear 52 is connected with clutching device 55.The bearing 552 that the clutching device housing 551 that described clutching device 55 includes being connected with power source gear 52 is connected with this clutching device housing 551, the clutch disc 553 connecting this bearing 552, the spill spin block 554 that connects this clutch disc 553.It is additionally provided with between described spill spin block 554 and line shaft 53 and is sequentially provided with chiller 56, unilateral bearing 58, start-up rod joint 59 and output sleeve 501.Described chiller 56 is possible to prevent internal combustion engine 51 to generate heat and cause temperature too high.
Also include providing the fuel tank 57 of fuel for internal combustion engine 51 and being installed on the noise absorber 90 on described power source 51 with reference to Fig. 1, Fig. 4, described propeller impact protector and the model of an airplane containing described propeller protector.This noise absorber 90 is avoided affecting environment because internal combustion engine 51 noise is too big.Described fuel tank 57 includes casing the 571, first briquetting the 572, second briquetting 573, flexible rubber hose 574 and the aluminum pipe 575 that charge.Described casing 571 is provided with an opening, and flexible rubber hose 574 is fixedly installed in this opening by described first briquetting 572 and the second briquetting 573, and this flexible rubber hose 574 is used for sealing this opening, makes the fuel in casing 571 occur without leakage.Being designed with through hole on described first briquetting the 572, second briquetting 573, flexible rubber hose 574, described aluminum pipe 575 is hollow pipe, and this aluminum pipe 575 is connected through this through hole with casing 571, for providing fuel to internal combustion engine 51.
With reference to Fig. 1, Fig. 2, described empennage 30 includes the foot piece 31 that is connected with skeleton 10 and and the tail propeller 32 that is arranged on foot piece 31.
With continued reference to Fig. 1; described propeller impact protector and also include gravity's center control device 70 containing the model of an airplane of described propeller protector, this gravity's center control device 70 includes being installed on the rod 71 and be arranged at the block 72 of weighing and considering in order to uphold justice at these excellent 71 two ends of weighing and considering in order to uphold justice of weighing and considering in order to uphold justice on line shaft 53.This gravity's center control device 70 makes propeller impact protector and the flight of the model of an airplane containing described propeller protector more steadily safe and reliable.
Described propeller impact protector and the model of an airplane containing described propeller protector also include steering assembly 80 and T-shaped fixed mount 110; pitch 81, steering wheel 82 that this steering assembly 80 includes being installed on line shaft 53, connecting described steering wheel 82 and the pull bar 83 of pitch 81, turning sleeve 84 and the connecting rod 85 being connected this turning sleeve 84 and pitch 81, this steering assembly 80 efficiently controls propeller impact protector and the model of an airplane containing described propeller protector flexibly turns to.Its battery 100 also including providing electric energy for described integrated chip 60, steering wheel 82.Described L-type 110 fixed mount is used for installing battery 100, integrated chip 60.
The propeller impact protector of the present invention and the model of an airplane containing described propeller protector drive propeller impact protector and the model of an airplane containing described propeller protector to fly by internal combustion engine, improve electric-powered source because of battery energy storage is less, be short of power situation.Therefore the propeller impact protector of the present invention and the model of an airplane containing described propeller protector have the beneficial effect of persistent period length, horsepower foot.
Above disclosed it is only presently preferred embodiments of the present invention, certainly can not limit the interest field of the present invention, the equivalent variations therefore made according to the present patent application the scope of the claims with this, still belong to the scope that the present invention contains.
Claims (7)
1. a propeller impact protector and the model of an airplane containing described propeller protector; it is characterized in that: it includes skeleton, support the lower carriage of this skeleton, the energy device that is arranged on described skeleton and can receive external signal and can control the integrated chip of described energy device according to external signal; line shaft that the power source gear that described energy device includes power source, be installed on this power source is connected with this power source gear, the air propeller being fixed on this line shaft, described power source is internal combustion engine.
2. propeller impact protector as claimed in claim 1 and the model of an airplane containing described propeller protector, it is characterised in that: it is connected with clutching device between described power source gear and line shaft.
3. propeller impact protector as claimed in claim 3 and the model of an airplane containing described propeller protector; it is characterized in that: the bearing that the clutching device housing that described clutching device includes being connected with power source gear is connected with this clutching device housing, the clutch disc connecting this bearing, connect the spill spin block of this clutch disc, between described spill spin block and line shaft, be additionally provided with chiller.
4. propeller impact protector as claimed in claim 1 and the model of an airplane containing described propeller protector, it is characterised in that: it also includes the noise absorber being installed on described power source.
5. propeller impact protector as claimed in claim 1 and the model of an airplane containing described propeller protector; it is characterized in that: it also includes gravity's center control device, this gravity's center control device includes being installed on the rod and be arranged at the block of weighing and considering in order to uphold justice at these rod two ends of weighing and considering in order to uphold justice of weighing and considering in order to uphold justice on line shaft top.
6. propeller impact protector as claimed in claim 1 and the model of an airplane containing described propeller protector; it is characterized in that: it also includes steering assembly, this steering assembly includes the pitch, steering wheel, the described steering wheel of connection and the pull bar of pitch, turning sleeve and the connecting rod being connected this turning sleeve and pitch that are installed on line shaft.
7. propeller impact protector as claimed in claim 6 and the model of an airplane containing described propeller protector, it is characterised in that: it also includes the T-shaped fixed mount being arranged on skeleton, and described integrated chip is installed on this T-shaped fixed mount.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410856184.1A CN105797401A (en) | 2014-12-31 | 2014-12-31 | Propeller impact protector and model airplane provided with propeller impact protector |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410856184.1A CN105797401A (en) | 2014-12-31 | 2014-12-31 | Propeller impact protector and model airplane provided with propeller impact protector |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105797401A true CN105797401A (en) | 2016-07-27 |
Family
ID=56465144
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410856184.1A Pending CN105797401A (en) | 2014-12-31 | 2014-12-31 | Propeller impact protector and model airplane provided with propeller impact protector |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105797401A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2301243Y (en) * | 1997-03-25 | 1998-12-23 | 朱健民 | Controlled motor-driven model aeroplane |
| CN201070541Y (en) * | 2007-07-02 | 2008-06-11 | 罗之洪 | Model airplane |
| CN101219283A (en) * | 2007-11-26 | 2008-07-16 | 罗之洪 | Model airplane |
| CN202491920U (en) * | 2011-11-25 | 2012-10-17 | 成铁芳 | Remote control airplane with propeller protection function |
| CN104015923A (en) * | 2014-06-25 | 2014-09-03 | 杨雅茹 | Helicopter with adjustable empennage attitude |
-
2014
- 2014-12-31 CN CN201410856184.1A patent/CN105797401A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2301243Y (en) * | 1997-03-25 | 1998-12-23 | 朱健民 | Controlled motor-driven model aeroplane |
| CN201070541Y (en) * | 2007-07-02 | 2008-06-11 | 罗之洪 | Model airplane |
| CN101219283A (en) * | 2007-11-26 | 2008-07-16 | 罗之洪 | Model airplane |
| CN202491920U (en) * | 2011-11-25 | 2012-10-17 | 成铁芳 | Remote control airplane with propeller protection function |
| CN104015923A (en) * | 2014-06-25 | 2014-09-03 | 杨雅茹 | Helicopter with adjustable empennage attitude |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
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| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20160727 |