CN106606871A - Aircraft having flight protection system - Google Patents
Aircraft having flight protection system Download PDFInfo
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- CN106606871A CN106606871A CN201510708350.8A CN201510708350A CN106606871A CN 106606871 A CN106606871 A CN 106606871A CN 201510708350 A CN201510708350 A CN 201510708350A CN 106606871 A CN106606871 A CN 106606871A
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- flight
- aircraft
- protection system
- main shaft
- remote control
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Abstract
The invention discloses an aircraft having a flight protection system. The aircraft having the flight protection system comprises an aircraft body, an upper cover, a landing device, a flight driving mechanism and a flight collision avoidance device. Obstacle voidance can be realized in the flight of an aeromodelling airplane so that the nonstop flight performance of the aeromodelling airplane can be enhanced, the practicality is high and popularization and application are facilitated.
Description
Technical field
The present invention relates to a kind of electronic toy, more particularly to a kind of aircraft with flight protection 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 model plane shorter, and motor mechanomotive force has certain limitation, it is not powerful enough, even if where open, during without other barriers, multi rack aeromodelling airplane flies in the air simultaneously, and still suffering from collision may, a series of troubles are caused, therefore the setting of the anticollision device, collision-prevention device of aeromodelling airplane is very necessary.
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 aircraft with flight protection system strong with super remote endurance, powerful, mobility.
To solve the above problems, the aircraft with flight protection system that the present invention is provided includes a kind of aircraft with flight protection system, should have the aircraft of flight protection system includes fuselage body, the upper lid being connected in front of fuselage body, it is connected to the empennage at fuselage body rear, support the landing gear of the fuselage body, the flight drive mechanism being arranged on the fuselage body, and external signal can be received and the flight collision avoidance device of the flight drive mechanism can be controlled according to external signal, the flight drive mechanism includes electromotor, the engine gear being installed on the electromotor, the main shaft being connected with the engine gear, the forward propeller being fixed on the main shaft, the electromotor is miniature oil-burning machine.
Used as one embodiment, the aircraft with flight protection system 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.
Compared with prior art, the present invention can realize avoidance of the to barrier during aeromodelling airplane flight in the air, improve the follow-on mission performance of aeromodelling airplane, practical, easy to utilize.
To make the present invention easier to understand, the aircraft with flight protection 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 aircraft with flight protection 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 aircraft with flight protection system of the present embodiment includes fuselage body 1, the upper lid 2 that is connected to the front of fuselage body 1, the empennage 3 for being connected to the rear of fuselage body 1, the landing gear 4 for supporting the fuselage body 1, the flight drive mechanism 5 being arranged on the fuselage body 1, can receive external signal and the flight collision avoidance device 6 of the flight drive mechanism 5 can be controlled according to external signal.The fuselage body 1 is made by special material plate, and it passes through all component that each fixture fixes the whole model of an airplane.
The flight drive mechanism 5 includes miniature oil-burning machine, the main shaft of the engine gear being installed on the electromotor and the engine gear connection, the forward propeller 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 aircraft with flight protection system 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 fuselage body 1 and and the tail propeller that is arranged on foot piece.
The aircraft with flight protection system 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.The balanced component makes the aircraft flight with flight protection system more steady safe and reliable.
The aircraft with flight protection system also includes steering assembly 0 and drum fixed mount; 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 aircraft with flight protection system and flexibly turns to.It also includes the battery for providing electric energy for the flight collision avoidance device, steering wheel.The drum fixed mount is used to install battery, flight collision avoidance device.
The aircraft with flight protection system of the present invention drives the aircraft flight with flight protection system 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 aircraft with flight protection 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 (3)
1. a kind of aircraft with flight protection system, it is characterised in that：It includes fuselage body, upper lid, landing gear, empennage, flight drive mechanism and flight collision avoidance device, the upper lid is placed in fuselage body top, the landing gear is placed in fuselage body bottom, the flight drive mechanism and flight collision avoidance device are arranged on inside fuselage body, the flight drive mechanism includes electromotor, the main shaft of the engine gear being installed on the electromotor and the engine gear connection, the forward propeller being fixed on the main shaft, and the electromotor is miniature oil-burning machine；It is connected with remote control clutch 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.
2. there is as claimed in claim 1 the aircraft of flight protection system, it is characterised in that：It also includes noise reduction device and 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.
3. there is as claimed in claim 1 the aircraft of flight protection system, it is characterised in that：It also includes steering assembly and the battery that provides electric energy for the flight collision avoidance device, steering wheel, and the steering assembly includes the pull bar of the pitch being installed on main shaft, steering wheel, the connection steering wheel and pitch, turning sleeve and is connected the connecting rod of the turning sleeve and pitch.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510708350.8A CN106606871A (en) | 2015-10-26 | 2015-10-26 | Aircraft having flight protection system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510708350.8A CN106606871A (en) | 2015-10-26 | 2015-10-26 | Aircraft having flight protection system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106606871A true CN106606871A (en) | 2017-05-03 |
Family
ID=58614525
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510708350.8A Pending CN106606871A (en) | 2015-10-26 | 2015-10-26 | Aircraft having flight protection system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106606871A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106621386A (en) * | 2015-10-29 | 2017-05-10 | 马铿钧 | Novel model airplane avoidance system |
| CN107050884A (en) * | 2017-05-22 | 2017-08-18 | 山东英才学院 | A kind of children use Anti-bump remote-control car |
-
2015
- 2015-10-26 CN CN201510708350.8A patent/CN106606871A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106621386A (en) * | 2015-10-29 | 2017-05-10 | 马铿钧 | Novel model airplane avoidance system |
| CN107050884A (en) * | 2017-05-22 | 2017-08-18 | 山东英才学院 | A kind of children use Anti-bump remote-control car |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170503 |