CN204337750U - High sensitivity aircraft - Google Patents
High sensitivity aircraft Download PDFInfo
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- CN204337750U CN204337750U CN201420627051.2U CN201420627051U CN204337750U CN 204337750 U CN204337750 U CN 204337750U CN 201420627051 U CN201420627051 U CN 201420627051U CN 204337750 U CN204337750 U CN 204337750U
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- aircraft
- power source
- high sensitivity
- skeleton
- line shaft
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Abstract
The utility model discloses a kind of high sensitivity aircraft, this high sensitivity aircraft comprises skeleton, support the lower carriage of this skeleton, be arranged at the energy device on described skeleton, and can external signal be received and can according to external signal control described energy device integrated chip it comprise skeleton, support the lower carriage of this skeleton, be arranged at the energy device on described skeleton, and can external signal be received and the integrated chip of described energy device can be controlled according to external signal, described energy device comprises power source, be installed on the power source gear on this power source, the line shaft be connected with this power source gear, be fixed on the air propeller on this line shaft, described power source is internal combustion engine, high sensitivity aircraft of the present utility model has the advantage that the duration is long, horsepower is sufficient.
Description
Technical field
The utility model relates to a kind of electronic toy, particularly relates to a kind of high sensitivity aircraft.
Background technology
Aircraft has become the toy of people's fashion day by day.Existing aircraft all drives with electric power source, and general so all needs provides battery, but existing battery electric quantity memory space is extremely limited.Cause the follow-on mission time of high sensitivity aircraft shorter, and electric-powered driving source have certain limitation, powerful not.
Therefore, the high sensitivity aircraft that our demand a kind of duration is long, horsepower is sufficient.
Summary of the invention
Based on the deficiencies in the prior art, problem to be solved in the utility model is to provide the high sensitivity aircraft that a kind of duration is long, horsepower is sufficient.
For solving the problem, the high sensitivity aircraft that the utility model provides comprises a kind of high sensitivity aircraft, this high sensitivity aircraft comprises skeleton, be connected to the head-shield in skeleton front, be connected to the empennage at skeleton rear, support the lower carriage of this skeleton, be arranged at the energy device on described skeleton, and can external signal be received and the integrated chip of described energy device can be controlled according to external signal, described energy device comprises power source, be installed on the power source gear on this power source, the line shaft be connected with this power source gear, be fixed on the air propeller on this line shaft, described power source is internal combustion engine.
As an embodiment, described high sensitivity aircraft also comprises the noise absorber for internal combustion engine provides the fuel tank of fuel and is installed on described power source.This noise absorber is avoided affecting environment because engine noise is too large.
As another embodiment, between described power source gear and line shaft, be connected with clutching device.Described clutching device comprises the clutching device housing be connected with power source gear, the bearing be connected with this clutching device housing, connects the clutch disc of this bearing, connects the spill spin block of this clutch disc.Also be provided with cooling device between described spill spin block and line shaft, this cooling device can prevent internal combustion engine from generating heat and causing temperature too high.
As another embodiment, described high sensitivity aircraft also comprises gravity's center control device, and this gravity's center control device comprises the rod and be arranged at the block of weighing and considering in order to uphold justice at these excellent two ends of weighing and considering in order to uphold justice of weighing and considering in order to uphold justice being installed on line shaft top.This gravity's center control device makes high sensitivity aircraft flight more safe and reliable.
As another embodiment, described high sensitivity aircraft also comprises steering assembly and T-shaped fixed mount, this steering assembly comprises the pitch be installed on line shaft, steering wheel, the pull bar of the described steering wheel of connection and pitch, turning sleeve and is connected the connecting rod of this turning sleeve and pitch, and this steering assembly effectively controls high sensitivity aircraft and turns to flexibly.It also comprises for described integrated chip, steering wheel provide the battery of electric energy.Described T-shaped fixed mount is for installing battery, integrated chip.
Compared with prior art, high sensitivity aircraft of the present utility model, by internal combustion engine drive high sensitivity aircraft flight, changes electric-powered source because of the situation that battery energy storage is less, be short of power.Therefore high sensitivity aircraft of the present utility model has the beneficial effect that the duration is long, horsepower is sufficient.
For making the utility model easier to understand, set forth high sensitivity aircraft of the present utility model further below in conjunction with accompanying drawing.
Accompanying drawing explanation
Fig. 1 is the structural representation of the high sensitivity aircraft of the utility model preferred embodiment.
Fig. 2 is the explosive view of Fig. 1.
Fig. 3 is the connection diagram of described power source, clutching device and cooling device.
Fig. 4 is the structural representation of described fuel tank.
Detailed description of the invention
With reference now to accompanying drawing, preferred embodiment of the present utility model is described.
With reference to figure 1, Fig. 2, the high sensitivity aircraft of the present embodiment comprises skeleton 10, is connected to the head-shield 20 in skeleton 10 front, is connected to the empennage 30 at skeleton 10 rear, supports the lower carriage 40 of this skeleton 10, the energy device 50 be 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 figure 2, Fig. 3, described energy device 50 comprises internal combustion engine 51, the power source gear 52 be installed on this power source 51, the line shaft 53 be connected with this power source gear 52, the air propeller 54 be fixed on this line shaft 53.
Described power source gear 52 is connected with clutching device 55.Described clutching device 55 comprises the clutching device housing 551 be connected with power source gear 52, the bearing 552 be 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.Also be provided with between described spill spin block 554 and line shaft 53 and be provided with cooling device 56, unilateral bearing 58, start-up rod joint 59 and output sleeve 501 successively.Described cooling device 56 can prevent internal combustion engine 51 from generating heat and causing temperature too high.
With reference to figure 1, Fig. 4, described high sensitivity aircraft also comprises the noise absorber 90 for internal combustion engine 51 provides the fuel tank 57 of fuel and is installed on described power source 51.This noise absorber 90 is avoided affecting environment because internal combustion engine 51 noise is too large.Described fuel tank 57 comprises casing 571, first briquetting 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, for sealing this opening, makes the fuel in casing 571 not occur leaking.Described first briquetting 572, second briquetting 573, flexible rubber hose 574 are all provided with through hole, and described aluminum pipe 575 is hollow pipe, and this aluminum pipe 575 is connected with casing 571 through this through hole, provides fuel for internal combustion engine 51.
With reference to figure 1, Fig. 2, described empennage 30 comprises the foot piece 31 that is connected with skeleton 10 and and the tail screw 32 that is arranged on foot piece 31.
Continue with reference to figure 1, described high sensitivity aircraft also comprises gravity's center control device 70, and this gravity's center control device 70 comprises being installed on, and line shaft 53 weighs and consider in order to uphold justice excellent 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.This gravity's center control device 70 makes high sensitivity aircraft flight more steadily safe and reliable.
Described high sensitivity aircraft also comprises steering assembly 80 and T-shaped fixed mount 110, this steering assembly 80 comprises the pitch 81 be installed on line shaft 53, steering wheel 82, the pull bar 83 connecting described steering wheel 82 and pitch 81, turning sleeve 84 and is connected the connecting rod 85 of this turning sleeve 84 and pitch 81, and this steering assembly 80 effectively controls high sensitivity aircraft and turns to flexibly.It also comprises for described integrated chip 60, steering wheel 82 provide the battery 100 of electric energy.Described L-type 110 fixed mount is for installing battery 100, integrated chip 60.
High sensitivity aircraft of the present utility model, by internal combustion engine drive high sensitivity aircraft flight, improves electric-powered source because of the situation that battery energy storage is less, be short of power.Therefore high sensitivity aircraft of the present utility model has the beneficial effect that the duration is long, horsepower is sufficient.
Above disclosedly be only preferred embodiment of the present utility model, certainly can not limit the interest field of the utility model with this, therefore according to the equivalent variations that the utility model claim is done, still belong to the scope that the utility model is contained.
Claims (7)
1. a high sensitivity aircraft, it is characterized in that: it comprises skeleton, supports the lower carriage of this skeleton, is arranged at the energy device on described skeleton and can receives external signal and can control the integrated chip of described energy device according to external signal, described energy device comprises power source, the power source gear be installed on this power source, the line shaft be connected with this power source gear, the air propeller be fixed on this line shaft, and described power source is internal combustion engine.
2. high sensitivity aircraft as claimed in claim 1, is characterized in that: be connected with clutching device between described power source gear and line shaft.
3. high sensitivity aircraft as claimed in claim 2, it is characterized in that: described clutching device comprises the clutching device housing be connected with power source gear, the bearing be connected with this clutching device housing, connects the clutch disc of this bearing, connects the spill spin block of this clutch disc, is also provided with cooling device between described spill spin block and line shaft.
4. high sensitivity aircraft as claimed in claim 1, is characterized in that: it also comprises the noise absorber be installed on described power source.
5. high sensitivity aircraft as claimed in claim 1, is characterized in that: it also comprises gravity's center control device, and this gravity's center control device comprises the rod and be arranged at the block of weighing and considering in order to uphold justice at these excellent two ends of weighing and considering in order to uphold justice of weighing and considering in order to uphold justice being installed on line shaft top.
6. high sensitivity aircraft as claimed in claim 1, it is characterized in that: it also comprises steering assembly, this steering assembly comprises the pitch be installed on line shaft, steering wheel, the pull bar of the described steering wheel of connection and pitch, turning sleeve and is connected the connecting rod of this turning sleeve and pitch.
7. high sensitivity aircraft as claimed in claim 6, it is characterized in that: it also comprises the T-shaped fixed mount be arranged on skeleton, described integrated chip is installed on this T-shaped fixed mount.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420627051.2U CN204337750U (en) | 2014-10-25 | 2014-10-25 | High sensitivity aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420627051.2U CN204337750U (en) | 2014-10-25 | 2014-10-25 | High sensitivity aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204337750U true CN204337750U (en) | 2015-05-20 |
Family
ID=53221054
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420627051.2U Expired - Fee Related CN204337750U (en) | 2014-10-25 | 2014-10-25 | High sensitivity aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204337750U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106563272A (en) * | 2015-10-09 | 2017-04-19 | 马铿杰 | Novel flight system with high operability |
| CN106672228A (en) * | 2015-11-07 | 2017-05-17 | 马铿杰 | Multi-blade rotor tandem type aircraft |
| CN106669186A (en) * | 2015-11-07 | 2017-05-17 | 马铿杰 | Large-amplitude motion follow-up type five-degree-of-freedom airworthiness |
-
2014
- 2014-10-25 CN CN201420627051.2U patent/CN204337750U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106563272A (en) * | 2015-10-09 | 2017-04-19 | 马铿杰 | Novel flight system with high operability |
| CN106672228A (en) * | 2015-11-07 | 2017-05-17 | 马铿杰 | Multi-blade rotor tandem type aircraft |
| CN106669186A (en) * | 2015-11-07 | 2017-05-17 | 马铿杰 | Large-amplitude motion follow-up type five-degree-of-freedom airworthiness |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150520 Termination date: 20151025 |
|
| EXPY | Termination of patent right or utility model |