CN106606874A - Novel aircraft power system - Google Patents
Novel aircraft power system Download PDFInfo
- Publication number
- CN106606874A CN106606874A CN201510705744.8A CN201510705744A CN106606874A CN 106606874 A CN106606874 A CN 106606874A CN 201510705744 A CN201510705744 A CN 201510705744A CN 106606874 A CN106606874 A CN 106606874A
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- CN
- China
- Prior art keywords
- dynamical system
- engine
- novel
- remote control
- novel aircrafts
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- 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.)
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Links
- 238000005183 dynamical system Methods 0.000 claims description 36
- 238000005516 engineering process Methods 0.000 abstract description 2
- 238000007664 blowing Methods 0.000 abstract 3
- 238000000034 method Methods 0.000 abstract 1
- 238000000926 separation method Methods 0.000 abstract 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 229910052782 aluminium Inorganic materials 0.000 description 3
- 239000002828 fuel tank Substances 0.000 description 3
- 239000003921 oil Substances 0.000 description 3
- 239000000295 fuel oil Substances 0.000 description 2
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000004146 energy storage Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
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- Toys (AREA)
Abstract
The invention discloses a novel aircraft power system for improving a maneuvering characteristic of the aircraft. According to a method, an air blowing seams which are distributed in an unfolding direction are formed in positions, close to flowing separating points, on the front edge of the upper surface of a control plane, and air blowing is performed in a cutting line direction, so that flowing separation on the control plane is eliminated, and aerodynamic force of the control plane is improved; in addition, extra maneuvering moment is provided for an air plane through counter acting force generated by air blowing; and therefore, by virtue of the control technology, the maneuvering characteristic of the aircraft can be obviously improved, and the novel aircraft power system is of significant application value to the development of a near space aircraft.
Description
Technical field
The present invention relates to a kind of electronic toy, more particularly to a kind of novel aircrafts dynamical 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 novel aircrafts dynamical 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 novel aircrafts dynamical 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 novel aircrafts dynamical system strong with super remote endurance, powerful, mobility.
To solve the above problems, the novel aircrafts dynamical system that the present invention is provided includes a kind of novel aircrafts dynamical system, the novel aircrafts dynamical 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 engine, the engine gear being installed on the engine, the main shaft being connected with the engine gear, the main screw being fixed on the main shaft, the engine is miniature oil-burning machine.
Used as one embodiment, the novel aircrafts dynamical system also includes the fuel tank for providing oil plant for miniature oil-burning machine and the noise reduction device being installed on the engine.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 novel aircrafts dynamical system also includes balanced component, and the balanced component includes being installed on the balancing pole on main shaft top and being arranged at the balance blade at the balancing pole two ends.The balanced component makes the flight of novel aircrafts dynamical system more safe and reliable.
As further embodiment, the novel aircrafts dynamical system also includes 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 novel aircrafts dynamical 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, novel aircrafts dynamical system of the invention drives aircraft flight by miniature oil-burning machine, therefore the novel aircrafts dynamical system of the present invention has the strong novel aircrafts dynamical system of super remote endurance, powerful, mobility.
To make the present invention easier to understand, the novel aircrafts dynamical system of the present invention is expanded on further below in conjunction with accompanying drawing.
Description of the drawings
Fig. 1 is the schematic diagram of the novel aircrafts dynamical 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 novel aircrafts dynamical system of the present embodiment includes 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 engine 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 novel aircrafts dynamical system also includes the fuel tank for providing oil plant for miniature oil-burning machine and the noise reduction device being installed on the engine.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 screw that is arranged on foot piece.
The novel aircrafts dynamical system also includes balanced component, and the balanced component includes the balancing pole being installed on main shaft and the balance blade for being arranged at the balancing pole two ends.The balanced component makes the flight of novel aircrafts dynamical system more steady safe and reliable.
The novel aircrafts dynamical system also includes 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 novel aircrafts dynamical 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 novel aircrafts dynamical system of the present invention drives novel aircrafts dynamical systems to fly by miniature oil-burning machine, improves genemotor because of battery energy storage is less, be short of power situation.Therefore the present invention is with the strong novel aircrafts dynamical 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 novel aircrafts dynamical 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 engine, the main shaft of the engine gear being installed on the engine and the engine gear connection, the main screw being fixed on the main shaft, and the engine is miniature oil-burning machine.
2. novel aircrafts dynamical system as claimed in claim 1, it is characterised in that：Remote control clutch is connected between the engine gear and main shaft.
3. novel aircrafts dynamical system as claimed in claim 2, 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. novel aircrafts dynamical system as claimed in claim 3, it is characterised in that：Fan is additionally provided between the remote control clutch rotating disk and main shaft.
5. novel aircrafts dynamical system as claimed in claim 1, it is characterised in that：It also includes the noise reduction device being installed on the engine.
6. novel aircrafts dynamical system as claimed in claim 1, it is characterised in that：It also includes balanced component, and the balanced component includes being installed on the balancing pole on main shaft top and being arranged at the balance blade at the balancing pole two ends.
7. novel aircrafts dynamical system as claimed in claim 1, 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. novel aircrafts dynamical system as claimed in claim 7, it is characterised in that：It also includes the battery for providing electric energy for the control board, steering wheel.
9. novel aircrafts dynamical system as claimed in claim 8, 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.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510705744.8A CN106606874A (en) | 2015-10-23 | 2015-10-23 | Novel aircraft power system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510705744.8A CN106606874A (en) | 2015-10-23 | 2015-10-23 | Novel aircraft power system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106606874A true CN106606874A (en) | 2017-05-03 |
Family
ID=58615374
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510705744.8A Withdrawn CN106606874A (en) | 2015-10-23 | 2015-10-23 | Novel aircraft power system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106606874A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3745699A (en) * | 1971-10-25 | 1973-07-17 | Mabuchi Motor Co | Device for automatically lowering and landing an electric model plane |
| CN201085932Y (en) * | 2007-09-18 | 2008-07-16 | 深圳市艾特航模有限公司 | Direct drive control plane steering mechanism of miniature motor |
| CN202961879U (en) * | 2012-12-05 | 2013-06-05 | 龚伟明 | Inflating type remote control airplane |
| CN106466527A (en) * | 2015-08-21 | 2017-03-01 | 许美兰 | The new complex controll rudder face based on aerodynamic force and direct force |
| CN106552432A (en) * | 2015-09-28 | 2017-04-05 | 许孙 | The system for effectively improving flying power |
-
2015
- 2015-10-23 CN CN201510705744.8A patent/CN106606874A/en not_active Withdrawn
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3745699A (en) * | 1971-10-25 | 1973-07-17 | Mabuchi Motor Co | Device for automatically lowering and landing an electric model plane |
| CN201085932Y (en) * | 2007-09-18 | 2008-07-16 | 深圳市艾特航模有限公司 | Direct drive control plane steering mechanism of miniature motor |
| CN202961879U (en) * | 2012-12-05 | 2013-06-05 | 龚伟明 | Inflating type remote control airplane |
| CN106466527A (en) * | 2015-08-21 | 2017-03-01 | 许美兰 | The new complex controll rudder face based on aerodynamic force and direct force |
| CN106552432A (en) * | 2015-09-28 | 2017-04-05 | 许孙 | The system for effectively improving flying power |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 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 |
Application publication date: 20170503 |
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| WW01 | Invention patent application withdrawn after publication |