CN106563272A - Novel flight system with high operability - Google Patents
Novel flight system with high operability Download PDFInfo
- Publication number
- CN106563272A CN106563272A CN201510649136.XA CN201510649136A CN106563272A CN 106563272 A CN106563272 A CN 106563272A CN 201510649136 A CN201510649136 A CN 201510649136A CN 106563272 A CN106563272 A CN 106563272A
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- flight system
- strong operability
- new strong
- remote control
- main shaft
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Abstract
The invention discloses a novel flight system with high operability. According to a method, an air blowing seam distributed in an unfolding direction is formed in a position near a front edge flowing separation point of the upper surface of a control surface, and the air blowing is performed in the tangent line direction; therefore on one hand, the control surface flowing separation can be eliminated, and the aerodynamic force of the control surface is improved; and on the other hand, the counter-acting force generated by air blowing is used for providing additional operation moment for an airplane. The control technology has the advantages that the operation characteristics of an aircraft can be obviously improved; and important application values are realized on the development of a near spacecraft.
Description
Technical field
The present invention relates to a kind of electronic toy, more particularly to a kind of flight system of new strong operability.
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 the flight system of new strong operability shorter, and motor mechanomotive force has certain limitation, it is not powerful enough.
Therefore, a kind of flight time length of our demands, the flight system of the new strong operability 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 flight system of the new strong operability strong with super remote endurance, powerful, mobility.
To solve the above problems, the flight system of the new strong operability that the present invention is provided includes a kind of flight system of new strong operability, the flight system of the new strong operability 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 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.
Used as one embodiment, the flight system of the new strong operability also includes the fuel tank for providing oil plant for miniature oil-burning machine and the noise reduction device being installed on the electromotor.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 flight system of the new strong operability also includes balanced component, and the balanced component includes being installed on the gimbal lever on main shaft top and being arranged at the balance blade at the gimbal lever two ends.It is more safe and reliable that the balanced component makes the flight system of new strong operability fly.
As further embodiment, the flight system of the new strong operability 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 the flight system of new strong operability 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, the flight system of the new strong operability of the present invention drives aircraft flight by miniature oil-burning machine, therefore the flight system of the new strong operability of the present invention has the flight system of the strong new strong operability of super remote endurance, powerful, mobility.
To make the present invention easier to understand, the flight system of the new strong operability 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 flight system of the new strong operability 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 flight system of the new strong operability 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 electromotor 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 flight system of the new strong operability also includes the fuel tank for providing oil plant for miniature oil-burning machine and the noise reduction device being installed on the electromotor.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 propeller that is arranged on foot piece.
The flight system of the new strong operability also includes balanced component, and the balanced component includes the gimbal lever being installed on main shaft and the balance blade for being arranged at the gimbal lever two ends.It is more steady safe and reliable that the balanced component makes the flight system of new strong operability fly.
The flight system of the new strong operability 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 the flight system of new strong operability 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 flight system of the new strong operability of the present invention drives the flight system of new strong operability 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 has the flight system of the strong new strong operability 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 flight system of new strong operability, 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 electromotor, the main shaft of the engine gear being installed on the electromotor and the engine gear connection, the main screw being fixed on the main shaft, and the electromotor is miniature oil-burning machine.
2. the flight system of new strong operability as claimed in claim 1, it is characterised in that：Remote control clutch is connected between the engine gear and main shaft.
3. the flight system of new strong operability 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. the flight system of new strong operability 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. the flight system of new strong operability as claimed in claim 1, it is characterised in that：It also includes the noise reduction device being installed on the electromotor.
6. the flight system of new strong operability as claimed in claim 1, it is characterised in that：It also includes balanced component, and the balanced component includes being installed on the gimbal lever on main shaft top and being arranged at the balance blade at the gimbal lever two ends.
7. the flight system of new strong operability 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. the flight system of new strong operability 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. the flight system of new strong operability 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 |
|---|---|---|---|
| CN201510649136.XA CN106563272A (en) | 2015-10-09 | 2015-10-09 | Novel flight system with high operability |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510649136.XA CN106563272A (en) | 2015-10-09 | 2015-10-09 | Novel flight system with high operability |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106563272A true CN106563272A (en) | 2017-04-19 |
Family
ID=58506038
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510649136.XA Withdrawn CN106563272A (en) | 2015-10-09 | 2015-10-09 | Novel flight system with high operability |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106563272A (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20020111117A1 (en) * | 2001-02-09 | 2002-08-15 | Heng-Chun Ho | Toy car camera system and rear vision mirrors |
| CN201070541Y (en) * | 2007-07-02 | 2008-06-11 | 罗之洪 | Model airplane |
| CN204337750U (en) * | 2014-10-25 | 2015-05-20 | 马铿钧 | High sensitivity aircraft |
| CN106492473A (en) * | 2015-09-03 | 2017-03-15 | 马铿杰 | The strong flight system of novel operating |
-
2015
- 2015-10-09 CN CN201510649136.XA patent/CN106563272A/en not_active Withdrawn
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20020111117A1 (en) * | 2001-02-09 | 2002-08-15 | Heng-Chun Ho | Toy car camera system and rear vision mirrors |
| CN201070541Y (en) * | 2007-07-02 | 2008-06-11 | 罗之洪 | Model airplane |
| CN204337750U (en) * | 2014-10-25 | 2015-05-20 | 马铿钧 | High sensitivity aircraft |
| CN106492473A (en) * | 2015-09-03 | 2017-03-15 | 马铿杰 | The strong flight system of novel operating |
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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: 20170419 |
|
| WW01 | Invention patent application withdrawn after publication | ||
| DD01 | Delivery of document by public notice |
Addressee: Ma Kengjie Document name: Notification of Approving Refund |
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| DD01 | Delivery of document by public notice |