CN106492479A - There is diesel-driven flight system - Google Patents
There is diesel-driven flight system Download PDFInfo
- Publication number
- CN106492479A CN106492479A CN201510559613.3A CN201510559613A CN106492479A CN 106492479 A CN106492479 A CN 106492479A CN 201510559613 A CN201510559613 A CN 201510559613A CN 106492479 A CN106492479 A CN 106492479A
- Authority
- CN
- China
- Prior art keywords
- diesel
- flight system
- driven flight
- main shaft
- remote control
- 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
Links
Landscapes
- Toys (AREA)
Abstract
The invention discloses a kind of have diesel-driven flight system, there should be diesel-driven flight system to include main frame, upper lid, landing gear, Power Component and control board, the Power Component includes the main shaft of electromotor, the engine gear being installed on the electromotor and engine gear connection, the main screw being fixed on the main shaft, and the electromotor is miniature oil-burning machine.The present invention have super remote endurance, powerful, mobility strong with diesel-driven flight system.
Description
Technical field
The present invention relates to a kind of electronic toy, more particularly to a kind of with diesel-driven flight 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 with diesel-driven flight system shorter, and motor mechanomotive force has certain limitation, not powerful enough.
Therefore, a kind of flight time length of our demands, powerful with diesel-driven flight system.
Content of the invention
Be based on the deficiencies in the prior art, problem to be solved by this invention be to provide a kind of with super remote endurance, powerful, mobility strong with diesel-driven flight system.
For solving the above problems, including with diesel-driven flight system that the present invention is provided is a kind of with diesel-driven flight system, there should be diesel-driven flight system to include 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.
As one embodiment, the fuel tank and the noise reduction device being installed on the electromotor for also including providing oil plant for miniature oil-burning machine with diesel-driven flight system.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 between the engine gear and main shaft, is connected with.The remote control clutch include the remote control clutch lower cover being connected with engine gear and the remote control clutch lower cover connection bearing, connect the power output friction plate of the bearing, connect 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 heating and cause temperature too high.
As another embodiment, described also include balanced component with diesel-driven flight system, the balanced component includes the gimbal lever for being installed on main shaft top and the balance blade for being arranged at the gimbal lever two ends.The balanced component makes more safe and reliable with the flight of diesel-driven flight system.
As further embodiment, described also include steering assembly and H type fixed mounts with diesel-driven flight system, the steering assembly includes the pitch being installed on main shaft, steering wheel, the pull bar for connecting the steering wheel and pitch, turning sleeve and is connected the connecting rod of the turning sleeve and pitch, and the steering assembly is efficiently controlled and flexibly turned to diesel-driven flight system.Which also includes the battery for providing electric energy for the control board, steering wheel.The H types fixed mount is used for installing battery, control board.
Compared with prior art, the present invention with diesel-driven flight system by miniature oil-burning machine drive aircraft flight, therefore the present invention with diesel-driven flight system have super remote endurance, powerful, mobility strong with diesel-driven flight system.
For make the present invention easier to understand, below in conjunction with accompanying drawing be expanded on further the present invention with diesel-driven flight system.
Description of the drawings
Schematic diagrams with diesel-driven flight system of the Fig. 1 for 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 present embodiment includes main frame 1, the upper lid 2 being connected in front of main frame 1, the empennage 3 for being connected to 1 rear of main frame, the landing gear 4 for supporting the main frame 1, the Power Component 5 being arranged on the main frame 1, the control board 6 that can be received external signal and can control the Power Component 5 according to external signal with diesel-driven flight system.The main frame 1 is made by special material plate, and which passes through all component that the whole model of an airplane fixed by each fixture.
The Power Component 5 includes the main shaft of miniature oil-burning machine, the engine gear being installed on the electromotor and 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 include the remote control clutch lower cover being connected with engine gear and the remote control clutch lower cover connection bearing, connect the power output friction plate of the bearing, connect 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 heating and cause temperature too high.
The fuel tank and the noise reduction device being installed on the electromotor for also including providing oil plant for miniature oil-burning machine with diesel-driven flight system.The noise reduction device is avoided because of the too big impact environment of miniature oil-burning machine noise.The fuel tank includes the casing of oil bunkering, the first briquetting, the second briquetting, flexible rubber hose and aluminum pipe.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 for sealing the opening, makes the fuel oil in casing occur without leakage.Through hole is designed with first briquetting, the second briquetting, flexible rubber hose, and the aluminum pipe is hollow pipe, and the aluminum pipe is connected through the through hole with casing, for fuel oil being provided 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.
Described also include balanced component with diesel-driven flight system, the balanced component includes the gimbal lever being installed on main shaft and is arranged at the balance blade at the gimbal lever two ends.The balanced component makes more steadily safe and reliable with the flight of diesel-driven flight system.
Described also include steering assembly 0 and H type fixed mounts with diesel-driven flight system, the steering assembly includes the pitch being installed on main shaft, steering wheel, the pull bar for connecting the steering wheel and pitch, turning sleeve and is connected the connecting rod of the turning sleeve and pitch, and the steering assembly is efficiently controlled and flexibly turned to diesel-driven flight system.Which also includes the battery for providing electric energy for the control board, steering wheel.The H types fixed mount is used for installing battery, control board.
Being driven by miniature oil-burning machine with diesel-driven flight system for the present invention has the flight of diesel-driven flight system, improves genemotor because of battery energy storage is less, be short of power situation.Therefore the present invention have super remote endurance, powerful, mobility strong with diesel-driven flight system.
Above disclosed is only presently preferred embodiments of the present invention, can not limit certainly the interest field of the present invention with this, and the equivalent variations that is therefore made according to scope of the present invention patent still belong to the scope covered by the present invention.
Claims (9)
1. a kind of have diesel-driven flight system, it is characterised in that:Which 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 inside main frame, the Power Component includes the main shaft of electromotor, the engine gear being installed on the electromotor and engine gear connection, the main screw being fixed on the main shaft, and the electromotor is miniature oil-burning machine.
2. there is diesel-driven flight system as claimed in claim 1, it is characterised in that:Remote control clutch is connected between the engine gear and main shaft.
3. there is diesel-driven flight system as claimed in claim 2, it is characterised in that:The remote control clutch include the remote control clutch lower cover being connected with engine gear and the remote control clutch lower cover connection bearing, connect the power output friction plate of the bearing, connect the remote control clutch rotating disk of the power output friction plate.
4. there is diesel-driven flight 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. there is diesel-driven flight system as claimed in claim 1, it is characterised in that:Which also includes the noise reduction device being installed on the electromotor.
6. there is diesel-driven flight system as claimed in claim 1, it is characterised in that:Which also includes balanced component, and the balanced component includes the gimbal lever for being installed on main shaft top and the balance blade for being arranged at the gimbal lever two ends.
7. there is diesel-driven flight system as claimed in claim 1, it is characterised in that:Which also includes steering assembly, and the steering assembly includes the pitch being installed on main shaft, steering wheel, the pull bar for connecting the steering wheel and pitch, turning sleeve and is connected the connecting rod of the turning sleeve and pitch.
8. there is diesel-driven flight system as claimed in claim 7, it is characterised in that:Which also includes the battery for providing electric energy for the control board, steering wheel.
9. there is diesel-driven flight system as claimed in claim 8, it is characterised in that:Which also includes that the H type fixed mounts being arranged on main frame, the battery, control board are installed on the H type fixed mounts.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201510559613.3A CN106492479A (en) | 2015-09-03 | 2015-09-03 | There is diesel-driven flight system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201510559613.3A CN106492479A (en) | 2015-09-03 | 2015-09-03 | There is diesel-driven flight system |
Publications (1)
Publication Number | Publication Date |
---|---|
CN106492479A true CN106492479A (en) | 2017-03-15 |
Family
ID=58286683
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201510559613.3A Pending CN106492479A (en) | 2015-09-03 | 2015-09-03 | There is diesel-driven flight system |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN106492479A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106552428A (en) * | 2015-09-25 | 2017-04-05 | 郑华耀 | Gear drive model plane |
-
2015
- 2015-09-03 CN CN201510559613.3A patent/CN106492479A/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106552428A (en) * | 2015-09-25 | 2017-04-05 | 郑华耀 | Gear drive model plane |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN106492478A (en) | There are the model plane of integrated control system | |
CN201385780Y (en) | Novel propeller | |
CN106474746A (en) | Model plane with super remote endurance | |
CN106492473A (en) | The strong flight system of novel operating | |
CN203730715U (en) | Transmission structure adopting multifunctional gear transmission shaft | |
CN204337750U (en) | High sensitivity aircraft | |
CN106492479A (en) | There is diesel-driven flight system | |
CN106466527A (en) | The new complex controll rudder face based on aerodynamic force and direct force | |
CN106552428A (en) | Gear drive model plane | |
CN106540461A (en) | Model plane with integrated chip | |
CN106606871A (en) | Aircraft having flight protection system | |
CN106466529A (en) | Gyroplane break-in control device | |
CN106563277A (en) | Model airplane having integration control system | |
CN201070541Y (en) | Model airplane | |
CN205084407U (en) | Super endurance flying device far away | |
CN106552432A (en) | The system for effectively improving flying power | |
CN106552429A (en) | High transmission efficiency flight instruments | |
CN106606880A (en) | A model airplane with a micro-fuel oil machine | |
CN106563274A (en) | Intelligent model airplane | |
CN106823405A (en) | Miniature oil-burning machine model plane | |
CN101003302A (en) | An aviation aircraft | |
CN106563272A (en) | Novel flight system with high operability | |
CN208070047U (en) | A kind of fixed structure of aircraft accessory casing | |
CN106606874A (en) | Novel aircraft power system | |
CN106823400A (en) | Novel aircrafts dynamical system |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
WD01 | Invention patent application deemed withdrawn after publication | ||
WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170315 |