CN210356035U

CN210356035U - Sucking disc missile

Info

Publication number: CN210356035U
Application number: CN201920715591.9U
Authority: CN
Inventors: 廖昱森
Original assignee: Individual
Current assignee: Individual
Priority date: 2019-05-17
Filing date: 2019-05-17
Publication date: 2020-04-21
Anticipated expiration: 2029-05-17

Abstract

The utility model discloses a sucker missile, which is characterized in that the missile comprises a missile main body, wherein the front end of the missile main body is provided with a sucker for adsorbing and fixing the missile main body on a smooth plane, the bottom surface of the concave inner part of the sucker is provided with a raised limiting lug, and the limiting lug is made of soft plastic and is used for preventing the sucker from being completely adsorbed and fixed on the smooth plane; the tail end of the rear end of the missile main body is provided with a missile wing, and the missile main body adopts a streamline design structure with a large front end and a small rear end. The missile wing is provided with three pieces. Three missile wings are along tail end periphery interval one hundred twenty degrees settings the beneficial effects of the utility model reside in that: the sucking disc adsorbs fixedly, prevents that the missile from hurting other people when using, reduces the potential safety hazard, avoids the emergence of incident. The design of spacing lug is favorable to when the sucking disc is fixed the missile main part on smooth plane, and the user takes off the sucking disc from smooth plane after still being convenient for use.

Description

Sucking disc missile

Technical Field

The utility model relates to a toy field especially relates to a sucking disc missile.

Background

A flying toy is a common one in the field of toys. However, the front ends of many flying toys are generally designed to be relatively sharp arrow-shaped, and are easy to stab others in actual use, thereby causing safety accidents. Therefore, the applicant firstly provides a safer suction cup missile to solve the potential safety hazard.

SUMMERY OF THE UTILITY MODEL

Based on this, the utility model provides a sucking disc missile, the sucking disc adsorbs fixedly, prevents that the missile from hurting other people when using time stamp, reduces the potential safety hazard, avoids the emergence of incident. The design of spacing lug is favorable to when the sucking disc is fixed the missile main part on smooth plane, and the user takes off the sucking disc from smooth plane after still being convenient for use.

In order to realize the utility model discloses a purpose, the utility model discloses a following technical scheme:

a sucking disc missile is characterized by comprising a missile main body, wherein a sucking disc for adsorbing and fixing the missile main body on a smooth plane is arranged at the front end of the missile main body, a raised limiting lug is arranged on the concave bottom surface of the sucking disc, the limiting lug is made of soft plastic and is used for preventing the sucking disc from being completely adsorbed and fixed on the smooth plane, and the sucking disc is conveniently separated from the smooth plane; the tail end of the rear end of the missile main body is provided with a missile wing, and the missile main body adopts a streamline design structure with a large front end and a small rear end.

Preferably, the bottom surface of the suction cup is made of gel.

Preferably, the missile wing is provided with three parts.

Preferably, the three missile wings are arranged along the outer periphery of the tail end at intervals of one hundred twenty degrees.

The beneficial effects of the utility model reside in that: the sucking disc adsorbs fixedly, prevents that the missile from hurting other people when using, reduces the potential safety hazard, avoids the emergence of incident. The design of spacing lug is favorable to when the sucking disc is fixed the missile main part on smooth plane, and the user takes off the sucking disc from smooth plane after still being convenient for use.

Drawings

Fig. 1 is a schematic structural diagram of the present invention.

Fig. 2 is a schematic view of the bottom structure of the suction cup of the present invention.

In the figure: 1-missile main body, 2-sucker, 3-tail end, 4-missile wing and 21-limit bump.

Detailed Description

In order to facilitate understanding of the present invention, the present invention will be described more fully hereinafter with reference to the accompanying drawings. The preferred embodiments of the present invention are shown in the drawings. The invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete.

It will be understood that when an element is referred to as being "secured to" another element, it can be directly on the other element or intervening elements may also be present. When an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present. In contrast, when an element is referred to as being "directly on" another element, there are no intervening elements present. As used herein, the terms "vertical," "horizontal," "left," "right," and the like are for illustrative purposes only and do not represent the only embodiments, and as used herein, the terms "upper," "lower," "left," "right," "front," "rear," and the like are used in a positional relationship with reference to the drawings.

Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. The terminology used herein in the description of the invention is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. As used herein, the term "and/or" includes any and all combinations of one or more of the associated listed items.

The technical solution of the present patent will be described in further detail with reference to the following embodiments.

As shown in the figure, the sucking disc missile is characterized by comprising a missile main body 1, wherein a sucking disc 2 for adsorbing and fixing the missile main body 1 on a smooth plane is arranged at the front end of the missile main body 1, a raised limiting lug 21 is arranged on the concave bottom surface of the sucking disc 2, and the limiting lug 21 is made of soft plastic and is used for preventing the sucking disc 2 from being completely adsorbed and fixed on the smooth plane, so that the sucking disc 2 is conveniently separated from the smooth plane; the missile is characterized in that a missile wing 4 is mounted on the tail end 3 of the rear end of the missile main body 1, and the missile main body 1 is of a streamline design structure with a large front end and a small rear end.

The bottom surface of the suction cup 2 is made of gel.

The missile wing 4 is provided with three pieces.

The three missile wings 4 are arranged along the outer circumference of the tail end 3 at intervals of one hundred twenty degrees.

In the above-described manufacturing process of the missile body 1, the weight of the front end of the missile body 1 is greater than the weight of the rear end, and the weight of the rear end of the missile body 1 is prevented from being greater, thereby greatly changing the path of the movement of the missile body 1.

The beneficial effects of the utility model reside in that: the sucker 2 is fixed in an adsorption mode, so that the flying bomb is prevented from hurting other people when being used, potential safety hazards are reduced, and safety accidents are avoided. The design of spacing lug 21 is favorable to when sucking disc 2 fixes missile main part 1 on smooth plane, and the user of still being convenient for after the use takes off sucking disc 2 from smooth plane.

The above embodiments are only used for illustrating the present invention, and not for limiting the present invention, and those skilled in the relevant technical field can make various changes and modifications without departing from the spirit and scope of the present invention, so that all equivalent technical solutions also belong to the scope of the present invention, and the protection scope of the present invention should be defined by the claims.

Claims

1. A sucking disc missile is characterized by comprising a missile main body, wherein a sucking disc for sucking and fixing the missile main body on a smooth plane is arranged at the front end of the missile main body, a raised limiting lug is arranged on the concave bottom surface of the sucking disc, and the limiting lug is made of soft plastic and is used for preventing the sucking disc from being completely sucked and fixed on the smooth plane; the tail end of the rear end of the missile main body is provided with a missile wing, and the missile main body adopts a streamline design structure with a large front end and a small rear end.

2. The suction cup projectile as defined in claim 1, wherein said suction cup bottom surface is made of gel.

3. The suction cup missile of claim 1, wherein the missile wing has three pieces.

4. The suction cup missile of claim 3, wherein the three missile wings are arranged at one hundred twenty degrees intervals along the outer circumference of the tail end.