CN204973061U - Conveniently change motor aircraft - Google Patents
Conveniently change motor aircraft Download PDFInfo
- Publication number
- CN204973061U CN204973061U CN201520694389.4U CN201520694389U CN204973061U CN 204973061 U CN204973061 U CN 204973061U CN 201520694389 U CN201520694389 U CN 201520694389U CN 204973061 U CN204973061 U CN 204973061U
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- CN
- China
- Prior art keywords
- motor
- wing arm
- opening
- wing
- aircraft
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- Expired - Fee Related
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Abstract
The utility model discloses a conveniently change motor aircraft, it includes the fuselage, this fuselage has three at least wing arms, the not end of each wing arm is equipped with vane actuated mechanism, vane actuated mechanism includes the motor, drive gear and rotor, drive gear through the pivot setting on wing arm, the rotor sets up in the pivot, the position that the motor corresponds drive gear is through planting the truss setting in wing arm, and through drive tooth and transmission gear meshing, be equipped with on the wing arm and let the exerted opening of motor, and be equipped with on this opening and dismantle the lid with its confined, the utility model has the advantages of reasonable design, ingeniously being equipped with the opening on wing arm, when the motor goes wrong, can carrying out the quick replacement motor through this opening and continue to play, process, convenient and fast are changed to effective the simplification, and motor adoption level sets up the structure, and overall structure is simple, compact, reduces the vane actuated mechanism volume, is favorable to outward appearance various design, and is interesting high for the person of playing provides more enjoyment, does benefit to extensive popularization.
Description
Technical field
The utility model relates to toy technique field, is specifically related to one and is convenient for changing motor aircraft.
Background technology
Toy aircraft is a kind of toy that children and numerous airplane hobbyists like, sends instruction to realize the landing of aircraft, acceleration and deceleration and direction controlling etc. by wireless control system to aircraft.
The toy aircraft of selling on the market is varied, and it has different design concepts separately, makes every effort to the instructions for use that can reach different user, and great majority are with its lively moulding, changeable flight function, have captured increasing consumption market.Existing toy aircraft generally can both complete the flare maneuvers such as advance, retrogressing, turning, and therefore, existing toy aircraft has certain interest.
But the motor of existing toy aircraft is fragile, requires frequent maintenance and replacement; Usual replacing operation toy aircraft all will be taken apart, troublesome poeration, changes make troubles to motor.
Utility model content
For above-mentioned deficiency, the purpose of this utility model is, provides a kind of smart structural design, rationally, what be convenient for changing motor is convenient for changing motor aircraft.
For achieving the above object, technical scheme provided by the utility model is:
One is convenient for changing motor aircraft, it comprises fuselage, this fuselage has at least three wing arms, the end of each wing arm is provided with rotor mechanism, described rotor mechanism comprises motor, travelling gear and rotor, described travelling gear is arranged on wing arm by rotating shaft, and the upper end of this rotating shaft is stretched out wing arm and is formed an installation portion, described rotor is arranged on this installation portion, the position of the corresponding travelling gear of described motor is arranged in wing arm by insertion slot frame, and the driving shaft of this motor is provided with the driving gear be meshed with this travelling gear, described wing arm is provided with the opening allowing motor expose, and on this opening, be provided with the dismounting lid that can be closed.
Improve as one of the present utility model, described motor is horizontally set in wing arm.
Improve as one of the present utility model, described dismounting lid is screwed on described wing arm, is provided with motor baffle plate in this dismounting lid.
Improve as one of the present utility model, the quantity of described wing arm is four, is symmetricly set on described fuselage.
The beneficial effects of the utility model are: the utility model reasonable in design, ingeniously on wing arm, are provided with opening, when motor goes wrong, can carry out quick-replaceable motor continue to play by this opening, effectively simplify and change operation, convenient and swift; And motor employing is horizontally disposed with structure, overall structure is simple, compact, reduces rotor mechanism volume, is conducive to outward appearance design, for player provides more enjoyment, interesting high, is beneficial to extensive popularization.
Below in conjunction with accompanying drawing and embodiment, the utility model is further illustrated.
Accompanying drawing explanation
Fig. 1 is perspective view one of the present utility model.
Fig. 2 is perspective view two of the present utility model.
Fig. 3 is the decomposition texture schematic diagram one of rotor mechanism in the utility model.
Fig. 4 is the decomposition texture schematic diagram two of rotor mechanism in the utility model.
Detailed description of the invention
See Fig. 1, Fig. 2, Fig. 3 and Fig. 4, the one that the present embodiment provides is convenient for changing motor aircraft, it comprises fuselage 1, this fuselage 1 has at least three wing arms 2, the end of each wing arm 2 is provided with rotor mechanism 3, described rotor mechanism 3 comprises motor 31, travelling gear 32 and rotor 33, described travelling gear 32 is arranged on wing arm 2 by rotating shaft, and the upper end of this rotating shaft is stretched out wing arm 2 and is formed an installation portion, described rotor 33 is arranged on this installation portion, the position of the corresponding travelling gear 32 of described motor 31 is arranged in wing arm 2 by plant truss 34, and the driving shaft of this motor 31 is provided with the driving gear 35 be meshed with this travelling gear 32, described wing arm 2 is provided with the opening 21 allowing motor 31 expose, and on this opening 21, be provided with the dismounting lid 22 that can be closed.Concrete, described dismounting lid 22 is screwed on described wing arm 2, is provided with motor baffle plate 23 in this dismounting lid 22.When dismounting lid 22 covers on opening 21, motor baffle plate 23 just top is pressed in the breech face of motor 31, and good stability, avoids motor 31 to be shifted.
In the present embodiment, the quantity of described wing arm 2 is four, is symmetricly set on described fuselage 1.In other embodiment, the quantity of this wing arm 2 can be three, six or more.
Preferably, described motor 31 is horizontally set in wing arm 2, and motor 31 adopts and is horizontally disposed with structure, and overall structure is simple, compact, reduces rotor mechanism 3 volume, is conducive to outward appearance design.
When need change motor 31, see Fig. 3 and Fig. 4, turn on the screw on dismounting lid 22, and then open opening 21 motor 31 is exposed, then with hand, this motor 31 is pulled out from plant truss 34, then new motor is inserted plant truss 34, and cover dismounting lid 22, namely complete and change motor object, effectively simplify and change operation, convenient and swift.
The announcement of book and instruction according to the above description, the utility model those skilled in the art can also change above-mentioned embodiment and revise.Therefore, the utility model is not limited to detailed description of the invention disclosed and described above, also should fall in the protection domain of claim of the present utility model modifications and changes more of the present utility model.In addition, although employ some specific terms in this description, these terms just for convenience of description, do not form any restriction to the utility model.As described in the utility model above-described embodiment, adopt structure same or analogous with it and other aircraft obtained, all in the utility model protection domain.
Claims (4)
1. one kind is convenient for changing motor aircraft, it comprises fuselage, this fuselage has at least three wing arms, the end of each wing arm is provided with rotor mechanism, it is characterized in that, described rotor mechanism comprises motor, travelling gear and rotor, described travelling gear is arranged on wing arm by rotating shaft, and the upper end of this rotating shaft is stretched out wing arm and is formed an installation portion, described rotor is arranged on this installation portion, the position of the corresponding travelling gear of described motor is arranged in wing arm by insertion slot frame, and the driving shaft of this motor is provided with the driving gear be meshed with this travelling gear, described wing arm is provided with the opening allowing motor expose, and on this opening, be provided with the dismounting lid that can be closed.
2. be according to claim 1ly convenient for changing motor aircraft, it is characterized in that: described motor is horizontally set in wing arm.
3. be according to claim 1 and 2ly convenient for changing motor aircraft, it is characterized in that: described dismounting lid is screwed on described wing arm, is provided with motor baffle plate in this dismounting lid.
4. be according to claim 1ly convenient for changing motor aircraft, it is characterized in that: the quantity of described wing arm is four, is symmetricly set on described fuselage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520694389.4U CN204973061U (en) | 2015-09-10 | 2015-09-10 | Conveniently change motor aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520694389.4U CN204973061U (en) | 2015-09-10 | 2015-09-10 | Conveniently change motor aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204973061U true CN204973061U (en) | 2016-01-20 |
Family
ID=55107481
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520694389.4U Expired - Fee Related CN204973061U (en) | 2015-09-10 | 2015-09-10 | Conveniently change motor aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204973061U (en) |
-
2015
- 2015-09-10 CN CN201520694389.4U patent/CN204973061U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160120 Termination date: 20170910 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |