CN106823404A - The strong flight system of mobility - Google Patents
The strong flight system of mobility Download PDFInfo
- Publication number
- CN106823404A CN106823404A CN201510887347.7A CN201510887347A CN106823404A CN 106823404 A CN106823404 A CN 106823404A CN 201510887347 A CN201510887347 A CN 201510887347A CN 106823404 A CN106823404 A CN 106823404A
- Authority
- CN
- China
- Prior art keywords
- gear
- mobility
- flight system
- power source
- strong
- 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
Classifications
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H27/00—Toy aircraft; Other flying toys
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H31/00—Gearing for toys
- A63H31/08—Gear-control mechanisms; Gears for imparting a reciprocating motion
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- Toys (AREA)
Abstract
A kind of strong flight system of mobility of the present invention, including main body framework, caudal directions control device, landing mechanism, driving source mechanism and integrated remote control device, included the power of described power source in described driving source mechanism while passing to the The gear deceleration clutch of front propeller and rear screw shaft；The present invention realizes a power source and drives double oars or many oars to rotate simultaneously, the strong flight system of the mobility weight of itself is greatly reduced, so as to improve the mobility and endurance of the strong flight system of mobility.
Description
Technical field
The present invention relates to a kind of electronic toy, more particularly, the present invention relates to a kind of strong flight system of mobility.
Background technology
As the requirement of people's flight system strong to mobility is improved constantly, often require that the strong flight system of mobility has good flying quality, the interest of the strong flight system of mobility is manipulated to increase, it is the weight of the strong flight system of mobility that the flying quality of the flight system strong to mobility is far-reaching, the strong flight system of coaxial double oar mobility is typically all to complete power supply by two power sources, it is also required to two sets of actuating units, this flight system for making mobility strong considerably increases weight, therefore the weight for mitigating the strong flight system of mobility turns into industry urgent problem.
The content of the invention
The technical problems to be solved by the invention are directed to the defect existing for above-mentioned prior art and provide can mitigate the strong flight system own wt of mobility, and the strong flight system of the mobility of reduces cost is capable of again.
Solving the technical scheme that is used of present invention problem is：A kind of strong flight system of mobility includes main body framework, caudal directions control device is connected with main body framework rear, with the landing mechanism that main body framework lower section is connected to support the main body framework, the driving source mechanism being arranged in the main body framework and the integrated remote control device that external control signal can be received, described driving source mechanism includes power source, axle sleeve, through the power transmission shaft of the axle sleeve, it is arranged at the front propeller on power transmission shaft, the rear screw shaft that is arranged on axle sleeve and by the power of described power source while passing to the The gear deceleration clutch of front propeller and rear screw shaft.
The beneficial effects of the present invention are：The power driving source of the strong flight system of mobility passes to front propeller and rear screw shaft simultaneously by The gear deceleration clutch, front propeller and rear screw shaft is set to reversely rotate simultaneously, the present invention is realized a power source drives double oars to rotate simultaneously, greatly reduces the strong flight system of the mobility weight and manufacturing cost of itself.
As the preferred embodiment of the strong flight system of mobility of the present invention, described The gear deceleration clutch includes the power source gear being fixed on power source output shaft, the driving gear on described axle sleeve is engaged and is fixed on the power source gear, the driving gear has planet internal ring gear, at least one planetary gear engaged with driving gear planet internal ring gear, the central gear for being engaged with described planetary gear and being fixed on power transmission shaft.
As mobility of the present invention another preferred embodiment of strong flight system, it also includes dynamic balancer, described dynamic balancer includes balancing pole connector, balancing pole and is arranged at the balance weight at balancing pole two ends, described dynamic balancer is arranged on the upper end of power transmission shaft by balancing pole connector, balance its whole body during the strong flight system flight of the dynamic balancer mobility, make the strong flight system of mobility more can safety and steady fly.
As the strong flight system further embodiment of mobility of the present invention, it also includes steering assembly, described steering assembly includes the connecting rod of pitch on the axle sleeve, steering wheel, connection steering wheel and pitch, pitch leading truck and is connected the connecting rod of the pitch leading truck and pitch, and the steering assembly efficiently controls the strong flight system of mobility and flexibly turns to.
Below in conjunction with drawings and Examples, technical scheme is described in further detail.
Brief description of the drawings
Fig. 1 is the explosive view of the strong flight system of the mobility 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 strong flight system of mobility of the present invention includes the landing mechanism 3 that the caudal directions control device 2 that main body framework 1 and main body framework rear connect and main body framework bottom be connected to support the main body framework, the driving source mechanism 4 being arranged in the main body framework 1, can receive external control signal integrated remote control device 5 and provide the battery 6 of electric energy for consuming parts in main body framework.
Described driving source mechanism 4 includes power source, axle sleeve, the power transmission shaft through the axle sleeve, front propeller, rear screw shaft, power source gear, driving gear, planetary gear, central gear.Front propeller is pressed from both sides by front vane and is arranged on power transmission shaft, rear screw shaft is pressed from both sides by rear blade and is arranged on axle sleeve, power source gear is installed on described power source output shaft, described driving gear is engaged with power source gear and is fixed on described axle sleeve, driving gear has planet internal ring gear, there are three planetary gears engaged with driving gear planet internal ring gear, described central gear is engaged and is fixed on power transmission shaft with three planetary gears, central gear is provided with planet carrier, and three planetary gear bearings are mutually in 120 degree of positioning planet carriers.Certainly, planetary gear can be one or more in other embodiments.Power transmission shaft lower end is positioned on the bearing block of main body framework by bearing, and axle sleeve upper end is provided with bearing block, and the bearing on power transmission shaft is arranged in bearing block.Power source drive is arranged on the power source gear on power source output shaft, the driving gear that drive is engaged with power source gear, the rotation of driving gear rotates axle sleeve, so that the rear screw shaft rotation being fixed on axle sleeve, and drive the three planetary gears rotation engaged with driving gear planet internal ring gear, three planetary gears rotarily drive central gear rotation, central gear rotation rotates power transmission shaft, so that the front propeller being fixed on power transmission shaft is rotated with the direction opposite with rear screw shaft, it has been achieved in that a power source drives front propeller and rear screw shaft by gear drive while rotating in the opposite direction simultaneously, eliminate a power source and its transmission device, greatly reduce the strong flight system of the mobility weight of itself, so as to improve the flying quality of the strong flight system of mobility and cost-effective.
The strong flight system of the mobility also includes dynamic balancer, the dynamic balancer includes balancing pole connector, balancing pole and is arranged at the balance weight at balancing pole two ends, balancing pole is arranged on the upper end of power transmission shaft by balancing pole connector, the dynamic balancer makes to balance its whole body during the strong flight system flight of mobility, make the strong flight system of mobility more can safety and steady fly.
The strong flight system of described mobility also includes steering assembly, the steering assembly includes the connecting rod of pitch on the axle sleeve, steering wheel, connection steering wheel and pitch, pitch leading truck and is connected the connecting rod of the pitch leading truck and pitch, and the steering assembly efficiently controls model plane and flexibly turns to.
The caudal directions control device includes the tailstock being connected with main body framework, the tail propeller being arranged on tailstock and the tail power source for driving the tail propeller.
Finally should be noted that; the above embodiments are merely illustrative of the technical solutions of the present invention rather than limiting the scope of the invention; although being explained in detail to the present invention with reference to preferred embodiment; but it will be understood by those within the art that; technical scheme can be modified or equivalent, without deviating from the spirit and scope of technical solution of the present invention.
Claims (4)
1. the strong flight system of a kind of mobility, it is characterised in that：Including main body framework, caudal directions control device, landing mechanism, driving source mechanism and integrated remote control device, the caudal directions control device is connected to the main body framework rear portion, the landing mechanism is connected to below the main body framework, the driving source mechanism and integrated remote control device are arranged on inside the main body framework, described driving source mechanism includes power source, axle sleeve, through the power transmission shaft of the axle sleeve, the front propeller being arranged on power transmission shaft and the rear screw shaft being arranged on axle sleeve, and the power of described power source is passed to the The gear deceleration clutch of front propeller and rear screw shaft simultaneously.
2. the strong flight system of mobility as claimed in claim 1, it is characterised in that：Described The gear deceleration clutch includes the power source gear being fixed on power source output shaft, the driving gear on described axle sleeve is engaged and is fixed on the power source gear, the driving gear has planet internal ring gear, at least one planetary gear engaged with driving gear planet internal ring gear, the central gear for being engaged with described planetary gear and being fixed on power transmission shaft.
3. the strong flight system of mobility as claimed in claim 2, it is characterised in that：Planet carrier is fixed with described central gear, described planetary gear is positioned on the planet carrier.
4. the strong flight system of mobility as claimed in claim 1, it is characterised in that：It also includes dynamic balancer, and described dynamic balancer includes balancing pole connector, balancing pole and is arranged at the balance weight at balancing pole two ends, and described dynamic balancer is arranged on the upper end of power transmission shaft by balancing pole connector.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510887347.7A CN106823404A (en) | 2015-12-05 | 2015-12-05 | The strong flight system of mobility |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510887347.7A CN106823404A (en) | 2015-12-05 | 2015-12-05 | The strong flight system of mobility |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106823404A true CN106823404A (en) | 2017-06-13 |
Family
ID=59150504
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510887347.7A Pending CN106823404A (en) | 2015-12-05 | 2015-12-05 | The strong flight system of mobility |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106823404A (en) |
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2015
- 2015-12-05 CN CN201510887347.7A patent/CN106823404A/en active Pending
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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: 20170613 |