CN210583656U

CN210583656U - Landing rocket

Info

Publication number: CN210583656U
Application number: CN201921134148.9U
Authority: CN
Inventors: 秦燕北
Original assignee: Ace Light & Electronic Tech Ningbo Co ltd
Current assignee: Essen (Ningbo) Intelligent Technology Co.,Ltd.
Priority date: 2019-07-18
Filing date: 2019-07-18
Publication date: 2020-05-22
Anticipated expiration: 2029-07-18
Also published as: US20210016194A1

Abstract

The utility model provides a landing cabin rocket, belonging to the technical field of toy rockets, comprising a rocket body; the bin shell comprises two hollow half shells, the edges of the two half shells are mutually attached and enclosed to form an accommodating cavity, the upper ends of the two half shells are respectively hinged with the lower end of the arrow body, and the two half shells can rotate relatively to open or close the accommodating cavity; the umbrella cloth is contained in the containing cavity in a compressed mode. The utility model has the advantage of being convenient for draw in the parachute.

Description

Landing rocket

Technical Field

The utility model belongs to the technical field of the toy, a landing cabin rocket is related to.

Background

At present, some entertainment rockets with strong interestingness exist in the market, help children to know the structure and the working principle of the rocket, and improve the interest of the children in science and technology.

For example, a chinese patent with application No. 201620475758.5 discloses a rocket toy with an ejection mechanism, which comprises a rocket model and an ejection base, wherein the ejection base is provided with a cover body, the top of the cover body is provided with a vertically arranged launch canister, the launch canister is communicated with the cover body, the side wall of the cover body is provided with a switch door and a power switch, the rocket model is placed on the ejection mechanism arranged in the cover body through the switch door, and the ejection mechanism is used for ejecting the rocket model out of the launch canister when the power switch is powered on; the parachute is arranged at the upper end of the rocket model and is opened when the rocket model falls down, and the parachute is used for reducing the falling speed of the rocket model.

However, the releasing and furling structure of the parachute is relatively complex, and after the rocket is recovered, children can hardly install the parachute back again, so that the parachute is inconvenient for the children to use.

Disclosure of Invention

The utility model aims at solving the problems in the prior art, and provides a landing cabin rocket convenient for furling a parachute.

The purpose of the utility model can be realized by the following technical proposal: a landing bay rocket, comprising:

an arrow body;

the bin shell comprises two hollow half shells, the edges of the two half shells are mutually attached and enclosed to form an accommodating cavity, the upper ends of the two half shells are respectively hinged with the lower end of the arrow body, and the two half shells can rotate relatively to open or close the accommodating cavity;

the umbrella cloth is contained in the containing cavity in a compressed mode.

As a further improvement of the present invention, the pressing portion extends downward from the half shell, and the pressing portions of the two half shells are disposed opposite to each other.

As a further improvement of the present invention, the two pressing portions are engaged with each other in a concave-convex manner.

As a further improvement of the utility model, the umbrella cloth is provided with a connecting strip, and the connecting strip is connected with the inner side of one of the pressing parts.

As a further improvement, the arrow body includes that the arrow body is located arrow body upper end with the cover to the arrow body, and half articulated the installing in arrow body lower extreme of casing, the arrow head tip is the setting of sphere form.

As a further improvement of the utility model, the arrow is made of soft materials.

As a further improvement of the utility model, arrow body downwardly extending has the articulated portion that two intervals set up, and every half casing upwards extends has connecting portion, and connecting portion upwards imbeds between two articulated portions and articulated with the arrow body.

As a further improvement of the utility model, the arrow body outwards extends has trip and a plurality of circumference to arrange the arrow wing.

As a further improvement of the utility model, a light-emitting component is installed in the arrow body.

As a further improvement, light-emitting component is including the mount pad of embedding arrow point lower extreme, and mount pad downwardly extending has holding ring, support column, reference column, and between arrow point embedding arrow point and the holding ring, the holding ring inboard inlays and is equipped with the control panel, fixes a position and passes the control panel, and the support column supports the control panel downwards and links firmly with the control panel, and battery and vibration sensor are installed to the control panel upside, and the light source is installed to the control panel, and battery, vibration sensor, light source are connected with the control panel electricity respectively.

Based on the technical scheme, the embodiment of the utility model provides a can produce following technological effect at least:

1. when the two half shells rotate relatively to be opened, the umbrella cloth can be folded and then placed into one of the half shells, then the two half shells are closed by hands and pressed, at the moment, the umbrella cloth is compressed, the hands are released until the rocket is ejected, and in the flying process of the rocket, the umbrella cloth is not subjected to external pressure any more to prop the two half shells, and then the umbrella cloth is gradually released under the action of airflow to form a parachute, so that the rocket is cushioned, and the rocket is prevented from being damaged due to direct collision between the rocket and the ground. The structure of folding the umbrella cloth by the two half shells is convenient for children to operate by hands, and has better entertainment and education effects, simple structure and low manufacturing cost.

2. Through setting up and pressing the portion, children's accessible two fingers press from both sides tight two half shells to the ejection operation of follow-up rocket is convenient for.

3. Through the concave-convex matching of the edges of the two pressing parts, the two half shells can be positioned for being closed more tightly, and the operation is simpler and more convenient.

Drawings

Fig. 1 is a perspective view of a preferred embodiment of the present invention.

Fig. 2 is a usage status diagram of a preferred embodiment of the present invention.

Fig. 3 is a cross-sectional view of a preferred embodiment of the present invention.

Fig. 4 is a view showing an installation structure of the light emitting module.

In the figure, 100, arrow body; 110. an arrow body; 111. a hinge portion; 112. a hook is clamped; 113. an arrow wing; 120. an arrow;

200. a bin shell; 210. a half shell; 211. a pressing part; 212. a connecting portion; 220. an accommodating chamber;

300. umbrella cloth; 310. a connecting strip;

400. a light emitting assembly; 410. a mounting seat; 411. a positioning ring; 412. a support pillar; 413. a positioning column; 420. a control panel; 430. a battery; 440. a vibration sensor; 450. a light source.

Detailed Description

The following are specific embodiments of the present invention and the accompanying drawings are used to further describe the technical solution of the present invention, but the present invention is not limited to these embodiments.

As shown in fig. 1 to 4, the landing rocket comprises a rocket body 100, a rocket shell 200 and umbrella cloth 300, wherein the rocket shell 200 is formed by an upper circular table and a lower circular table which are attached to each other to form a landing rocket outer contour, which is similar to a flying saucer in shape, so that the landing rocket has a scientific sense and a better appearance effect.

The cartridge case 200 includes two hollow half cases 210, edges of the two half cases 210 are attached to each other and enclose to form a closed accommodating cavity 220, upper ends of the two half cases 210 are respectively hinged to a lower end of the arrow body 100, the two half cases 210 can relatively rotate to open or close the accommodating cavity 220, and the umbrella cloth 300 is compressed and accommodated in the accommodating cavity 220.

When the two half shells 210 are rotated and opened relatively, the umbrella cloth 300 can be folded and then placed into one of the half shells 210, then the two half shells 210 are closed and pressed by hands, at the moment, the umbrella cloth 300 is compressed, the hands are released until the rocket is ejected, during the flight of the rocket, the umbrella cloth 300 is not subjected to external pressure any more to unfold the two half shells 210, and then the umbrella cloth 300 is gradually released under the action of air flow to form a parachute, so that the rocket is cushioned to prevent the rocket from being damaged due to direct collision with the ground. The structure of folding the umbrella cloth 300 by the two half shells 210 is convenient for children to operate by hands, and has better entertainment and education effects, simple structure and low manufacturing cost.

The half shells 210 have pressing portions 211 extending downward, the pressing portions 211 of the two half shells 210 are disposed opposite to each other, and edges of the two pressing portions 211 are attached to each other. By providing the pressing portion 211, a child can clamp the two half shells 210 by two fingers, so as to facilitate the subsequent rocket launching operation.

The edges of the two pressing portions 211 are in concave-convex fit, so that the two half shells 210 can be positioned for being closed, the two half shells 210 are closed more tightly, and the operation is simpler and more convenient. Accordingly, the edges of the two half shells 210 may also be configured to engage in a snap fit to provide a detent to improve closure.

The umbrella cloth 300 is provided with the connecting strip 310, the connecting strip 310 is connected with the inner side of one pressing part 211, the connecting strip 310 is used for ensuring that the umbrella cloth 300 cannot be separated from a rocket, and is connected with the pressing part 211, so that the space between the two pressing parts 211 can be fully utilized, and meanwhile, the phenomenon that the compression and expansion effects are influenced by wrapping the connecting strip 310 when the umbrella cloth 300 is folded is avoided.

The rocket body 100 comprises a rocket body 110 and an arrow 120 sleeved on the upper end of the rocket body 110, the rocket body 110 extends outwards to form a hook 112 and three rocket wings 113 which are circumferentially and uniformly distributed, the hook 112 can be used for hooking the whole rocket body 100 on a rubber band so as to launch the rocket, and the rocket wings 113 can ensure stable posture of the rocket body 110 during flying.

The end part of the arrow 120 is arranged in a spherical shape, so that the injury force of the rocket when accidentally injuring people is reduced, and the safety is better; arrow 120 is made by soft materials such as rubber, polyurethane to further reduce rocket's nociceptive power, is more fit for children's amusement.

The arrow body extends downwards to form two hinge parts 111 which are arranged at intervals, each half shell 210 extends upwards to form a connecting part 212, and the connecting part 212 is embedded between the two hinge parts 111 upwards and is hinged with the arrow body. The two hinges 111 effectively prevent the housing halves 210 from rocking and allow for easier alignment and closure between the two housing halves 210.

In order to further improve entertainment, the light emitting assembly 400 is installed in the arrow body 110, and specifically includes an installation seat 410 embedded in the lower end of the arrow 120, a positioning ring 411, three supporting columns 412 arranged in a triangular shape and two positioning columns 413 extend downwards from the installation seat 410, the arrow body 110 is embedded between the arrow 120 and the positioning ring 411, a control board 420 is embedded inside the positioning ring 411 and positioned to penetrate through the control board 420, the supporting column 412 abuts against the control board 420 downwards and is fixedly bonded with the control board 420, a battery 430 and a vibration sensor 440 are installed on the upper side of the control board 420, a light source 450 is installed on the control board 420, and the battery 430, the vibration sensor 440 and the light source 450 are respectively and.

The shock generated when the rocket is launched causes the vibration sensor 440 to be triggered, so that the control board 420 controls the light source 450 to emit light for a period of time, for example, 60 seconds, and the light penetrates through the rocket body 110 to cause the rocket body 110 to illuminate, so that the rocket can fly and emit light at the same time, thereby achieving better entertainment effect and attracting children.

When this light emitting component 400 installs, control panel 420, light source 450, battery 430, vibration sensor 440 of pre-installation an organic whole wholly passes two reference columns 413, with location embedding holding ring 411, and through three support column 412 with control panel 420 location and a horizontal plane on the bonding link firmly, then with mount pad 410 embedding arrow head 120 lower extreme, again with arrow body 110 upper end embedding arrow head 120 and holding ring 411 between form interference fit with relatively fixed, push down mount pad 410 simultaneously, make light emitting component 400 monolithic stationary, this structure easy dismounting, and connect reliably, be convenient for mass production.

Wherein, the outer edge of the control board 420 is attached to the positioning ring 411 to form a closed space, so that the electrical stability is better.

The specific embodiments described herein are merely illustrative of the spirit of the invention. Various modifications, additions and substitutions for the specific embodiments described herein may be made by those skilled in the art without departing from the spirit of the invention or exceeding the scope of the invention as defined in the accompanying claims.

Claims

1. A landing bay rocket, comprising:

an arrow body;

the umbrella cloth is contained in the containing cavity in a compressed mode.

2. A landing bay rocket as claimed in claim 1, wherein: the half shells extend downwards to form pressing parts, and the pressing parts of the two half shells are arranged oppositely.

3. A landing bay rocket as claimed in claim 2, wherein: the edges of the two pressing parts are in concave-convex fit.

4. A landing bay rocket as claimed in claim 1, wherein: the umbrella cloth is provided with a connecting strip, and the connecting strip is connected with the inner side of one pressing part.

5. A landing bay rocket as claimed in claim 1, wherein: the arrow body includes the arrow body and locates the arrow of arrow body upper end with the cover, and half articulated the installing in arrow body lower extreme of casing, the arrow head tip is the setting of sphere form.

6. A landing bay rocket as claimed in claim 5, wherein: the arrows are made of soft material.

7. A landing bay rocket as claimed in claim 5, wherein: the arrow body downwardly extends to form two hinge parts which are arranged at intervals, each half shell upwardly extends to form a connecting part, and the connecting part is upwardly embedded between the two hinge parts and is hinged with the arrow body.

8. A landing bay rocket as claimed in claim 5, wherein: the arrow body outwards extends has trip and a plurality of arrow wing of circumference arrangement.

9. A landing bay rocket as claimed in claim 5, wherein: and a light-emitting component is arranged in the arrow body.

10. A landing bay rocket as claimed in claim 9, wherein: light emitting component is including the mount pad of embedding arrow head lower extreme, and mount pad downwardly extending has holding ring, support column, reference column, and between arrow body embedding arrow head and the holding ring, the holding ring inboard inlays and is equipped with the control panel, fixes a position and passes the control panel, and the support column supports the control panel downwards and links firmly with the control panel, and battery and vibration sensor are installed to the control panel upside, and the light source is installed to the control panel, and battery, vibration sensor, light source are connected with the control panel electricity respectively.