CN204502398U

CN204502398U - Safe aircraft

Info

Publication number: CN204502398U
Application number: CN201520151966.5U
Authority: CN
Inventors: 杜文龙
Original assignee: Individual
Current assignee: Individual
Priority date: 2015-03-18
Filing date: 2015-03-18
Publication date: 2015-07-29
Anticipated expiration: 2025-03-18

Abstract

The utility model discloses a kind of safe aircraft, it comprises upper plate body, lower body, support pedestal and rotor mechanism, upper and lower plate body is stacked by sequence interval from top to bottom, supporting pedestal is arranged between upper and lower plate body, rotor mechanism is arranged on lower body, and is provided with wind groove on upper and lower plate body, the utility model smart structural design, rationally, by mutually stacked to upper plate body and lower body formation cover type safeguard structure, completely flabellum can be covered, and then do not make the flabellum of aircraft High Rotation Speed when shaking control flight damaged and avoid occurring that flabellum hurts the phenomenon of people or thing, security performance is high, player is allowed to damage flabellum without the need to considering and to hurt people or thing, greatly enrich playing method, for player provides more enjoyment, greatly strengthen interest and playability, player is avoided to produce sensation dry as dust, overall structure is simple in addition, compact, parts are few, make assembling more simple and convenient, be easy to realize, production cost is low, be beneficial to extensive popularization.

Description

Safe aircraft

Technical field

The utility model relates to toy technique field, is specifically related to a kind of safe 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 structure of current existing toy aircraft is comparatively complicated; and owing to designing without safety protection structure; the flabellum of toy aircraft High Rotation Speed when shaking control flight is made often easily to hurt people; also damage flabellum; even casualty accident is caused time serious; cause it recreational low, also lack corresponding enjoyment.

Utility model content

For above-mentioned deficiency, the purpose of this utility model is, provides a kind of smart structural design, rationally, energy available protecting flabellum is not damaged and avoid occurring that flabellum hurts the safe aircraft of people or thing.

For achieving the above object, technical scheme provided by the utility model is:

A kind of safe aircraft, it comprises upper plate body, lower body, support pedestal and rotor mechanism, the sequence interval that described upper plate body and lower body are pressed from top to bottom is stacked, supporting pedestal is arranged between upper plate body and lower body, and upper end is connected with described upper plate body, lower end is connected with described lower body, and described rotor mechanism is arranged on the surface of described lower body towards described upper plate body, and on described upper plate body with lower body, be provided with the wind groove corresponding with this rotor mechanism.

Improve as one of the present utility model, the quantity of described rotor mechanism is four, is symmetricly set on described lower body in the center of circle.

Improve as one of the present utility model, described rotor mechanism comprises CD-ROM drive motor and is arranged on the flabellum in the rotating shaft of this CD-ROM drive motor, and described CD-ROM drive motor is connected with control circuit board, and this control circuit board is arranged on the upper surface center of described upper plate body.

Improve as one of the present utility model, described upper plate body and lower body parallel.

Improve as one of the present utility model, described upper plate body and lower body are square plate body, and four angles are provided with rounding.

The beneficial effects of the utility model are: the utility model smart structural design, rationally, by mutually stacked to upper plate body and lower body formation cover type safeguard structure, completely flabellum can be covered, and then do not make the flabellum of aircraft High Rotation Speed when shaking control flight damaged and avoid occurring that flabellum hurts the phenomenon of people or thing, security performance is high, player is allowed to damage flabellum without the need to considering and to hurt people or thing, greatly enrich playing method, for player provides more enjoyment, greatly strengthen interest and playability, player is avoided to produce sensation dry as dust, overall structure is simple in addition, compact, parts are few, make assembling more simple and convenient, be easy to realize, production cost is low, be 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 of the present utility model.

Fig. 2 is the decomposition texture schematic diagram of Fig. 1.

Detailed description of the invention

See Fig. 1 and Fig. 2, a kind of safe aircraft that the present embodiment provides, it comprises upper plate body 1, lower body 2, supports pedestal 3 and rotor mechanism 4, the sequence interval that described upper plate body 1 and lower body 2 are pressed from top to bottom is stacked, supporting pedestal 3 is arranged between upper plate body 1 and lower body 2, and upper end is connected with described upper plate body 1, lower end is connected with described lower body 2, described rotor mechanism 4 is arranged on the surface of described lower body 2 towards described upper plate body 1, and is provided with the wind groove 11 corresponding with this rotor mechanism 4, wind groove 21 on described upper plate body 1 and lower body 2.

See Fig. 2, the quantity of described rotor mechanism 4 is four, is symmetricly set on described lower body 2 in the center of circle.Concrete, the flabellum 42 that described rotor mechanism 4 comprises CD-ROM drive motor 41 and is arranged in the rotating shaft of this CD-ROM drive motor 41, described CD-ROM drive motor 41 is connected with control circuit board 5, and this control circuit board 5 is arranged on the upper surface center of described upper plate body 1.

Preferably, described upper plate body 1 and lower body 2 parallel.Described upper plate body 1 and lower body 2 are square plate body, and four angles are provided with rounding, avoid occurring that wedge angle hurts people or thing, effectively promote security performance.

The utility model is ingenious to be arranged between upper plate body 1 and lower body 2 by rotor mechanism 4, by upper plate body 1 and lower body 2 mutually stacked formation cover type safeguard structure, completely flabellum 42 can be covered, and then do not make the flabellum 42 of aircraft High Rotation Speed when shaking control flight damaged and avoid occurring that flabellum 42 hurts the phenomenon of people or thing, security performance is high, allow player damage flabellum 42 without the need to considering and to hurt people or thing, greatly enrich playing method, for player provides more enjoyment.

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, adopt other toy same or analogous with it, all in the utility model protection domain.

Claims

1. a safe aircraft, it is characterized in that, it comprises upper plate body, lower body, support pedestal and rotor mechanism, the sequence interval that described upper plate body and lower body are pressed from top to bottom is stacked, support pedestal to be arranged between upper plate body and lower body, and upper end is connected with described upper plate body, lower end is connected with described lower body, described rotor mechanism is arranged on the surface of described lower body towards described upper plate body, and on described upper plate body with lower body, be provided with the wind groove corresponding with this rotor mechanism.

2. safe aircraft according to claim 1, is characterized in that: the quantity of described rotor mechanism is four, is symmetricly set on described lower body in the center of circle.

3. safe aircraft according to claim 1 and 2, it is characterized in that: described rotor mechanism comprises CD-ROM drive motor and is arranged on the flabellum in the rotating shaft of this CD-ROM drive motor, described CD-ROM drive motor is connected with control circuit board, and this control circuit board is arranged on the upper surface center of described upper plate body.

4. safe aircraft according to claim 1, is characterized in that: described upper plate body and lower body parallel.

5. safe aircraft according to claim 1, is characterized in that: described upper plate body and lower body are square plate body, and four angles are provided with rounding.