CN203400502U - Water rocket launching frame - Google Patents
Water rocket launching frame Download PDFInfo
- Publication number
- CN203400502U CN203400502U CN201320424425.6U CN201320424425U CN203400502U CN 203400502 U CN203400502 U CN 203400502U CN 201320424425 U CN201320424425 U CN 201320424425U CN 203400502 U CN203400502 U CN 203400502U
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- water rocket
- grid
- rocket launching
- launching
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Abstract
The utility model relates to a water rocket launching frame, and belongs to the technical field of intelligence-benefiting type game devices. The water rocket launching frame comprises a launching frame body and a launching device, wherein the launching frame body comprises two sliding rails, a support and a base, the support is perpendicularly and fixedly connected with the front middle portions of the sliding rails, the base is arranged at the bottom end of the support and connected with an adjusting screw for the support, and the launching device comprises a spraying handle, a spraying rubber plug, a spraying opening fixing frame, a spraying opening pin fixed gate, a gas-pressure meter, an inflation valve, a vent valve, an inflation opening and an exhaust port. The launching device is installed on the tail of the sliding rails. Compared with the prior art, the water rocket launching frame has the remarkable advantages of being reasonable in structural design and strong in intelligence-benefiting performance, having certain technological contents, and having rapidity, safety, high efficiency, practicability and enjoyment.
Description
Technical field
The utility model relates to a kind of water rocket launching rack, belongs to intelligent developing type game device technical field.
Background technology
Conventional water rocket launching game device, generally adopts the explosive force principle of firecracker to launch, not too safe, easily occurs personnel's injury accident; Adopt in addition in addition mechanical elastic ejection mechanism to launch, ejection force is little, and range is not far, and emission rate is not high, lacks certain interest and intelligence.
Utility model content
Technical problem to be solved in the utility model is to overcome existing above-mentioned deficiency in prior art, and a kind of intelligent developing type water rocket launching rack of reasonable in design is provided.
The utility model solves the problems of the technologies described above adopted technical scheme: this water rocket launching rack, comprise launcher and emitter, it is characterized in that: described launcher comprises two slide rails, a support and a base, vertical being fixedly connected with of middle front part of support and slide rail, the bottom that base is positioned at support is connected with adjusting screw with support; Described emitter comprises injection handle, sprays plug, jet fixed mount, jet pin fixed grid, air gauge, charge valve, air bleeding valve, inflation inlet, exhaust outlet, and described emitter is arranged on the afterbody of slide rail.
Jet pin fixed grid described in the utility model comprises hole grid and hinge, and the middle part of hole grid has bottleneck hole, and hole grid are connected with hinge with screw, and hinge is connected with jet fixed mount with holding screw.
The angle on slide rail described in the utility model and ground is 30-60 degree.
The angle on slide rail described in the utility model and ground is 45 degree.
The utlity model has: rapidity, utilize pairing page grid to open principle quick, that resistance distance is short, hinge grid mechanism is used for to the water rocket launching quick startup of moment; Security, is equipped with air gauge on launcher, before transmitting, rocket body is locked by hinge grid, and water rocket can be filled with maximum safe air pressure, has both guaranteed that rocket body can mistakenly not launched, and also guarantees that rocket body can not explode because of hyperinflation; High efficiency, during rocket body transmitting, hinge grid opening speed is fast, resistance is little, be subject to force-stroke short, so hinge grid mechanism is minimum to the consumption of potential energy when rocket body is launched, used after pairing page grid, stress balance during rocket body transmitting, guarantees that the emission angle of rocket body can not change; Practicality, this device is drawn materials easily, makes simply, and effect is fine, is applicable to numerous students in middle and primary schools and makes, and improves manipulative ability.
The utility model compared with prior art, has following positive effect: reasonable in design, intelligence is strong, has certain scientific and technological content, has rapidity, security, high efficiency, practicality and interest.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Fig. 2 is the plan structure schematic diagram of Fig. 1.
Fig. 3 is hinge grid structural representations.
Fig. 4 is that the present embodiment is used view.
In figure: 1 launcher, 11 slide rails, 12 supports, 13 bases, 14 adjust screw, 2 emitters, and 21 spray handle, 22 jet fixed mounts, 23 jet pin fixed grids, 231 hole grid, 232 hinges, 233 bottleneck holes, 234 screws, 235 holding screws, 24 air gauges, 25 charge valves, 26 air bleeding valves, 27 inflation inlets, 28 exhaust outlets, 29 spray plug, 3 extreme misery rocket bodies.
The specific embodiment
Below in conjunction with accompanying drawing and by embodiment, the utility model is described in further detail.
Embodiment:
Referring to Fig. 1～Fig. 4, the present embodiment comprises launcher 1 and emitter 2, launcher 1 comprises two slide rails 11, support 12 and a base 13, vertical being fixedly connected with of middle front part of support 12 and slide rail 11, and the bottom that base 13 is positioned at support 12 is adjusted screws 14 with support 12 use and is connected; Emitter 2 comprises injection handle 21, sprays plug 29, jet fixed mount 22, jet pin fixed grid 23, air gauge 24, charge valve 25, air bleeding valve 26, inflation inlet 27, exhaust outlet 28, and described emitter 2 is arranged on the afterbody of slide rail 11; Jet pin fixed grid 23 comprises hole grid 231 and hinge 232, and the middle part of hole grid 231 has bottleneck 233 holes, and grid 231 use screws 234 in hole are connected with hinge 232, and hinge 232 use holding screws 235 are connected with jet fixed mount 22; Slide rail 11 is 30-60 degree with the angle on ground; As preferably, slide rail 11 is 45 degree with the angle on ground.
The running of water rocket launching rack below:
First 1 of launcher is regulated to the mutual positional distance of support 12 and base 13 on the ground by adjusting screw 14, adjust the angle on slide rail 11 and ground, be preferably 45 degree;
Then by 3 of extreme misery rocket bodies on two slide rails 11 of launcher 1, open and spray handle 21, the hinge 232 of jet pin fixed grid 23 is opened, the tail end of extreme misery rocket body 3 is through hole grid 231, then hinge 232 closes, close and spray handle 21, now the tail end of rocket body is fixed by bottleneck hole 233 pins in hole grid 231;
Emitter preparation: connect source of the gas at inflation inlet 27, open charge valve 25, close air bleeding valve 26 simultaneously, when air gauge 24 demonstrations are filled with maximum safe air pressure, close charge valve 25;
Transmitting: open and spray handle 21, jet pin fixed grid 23 is opened fast, extreme misery rocket body 3 moment transmitted at high speed;
Transmitting is finished can open air bleeding valve 26, from exhaust outlet 28, discharges remaining air and water droplet.
The feature of the utlity model has is:
1 rapidity: utilize pairing page grid to open principle quick, that resistance distance is short, hinge grid mechanism is used for to the water rocket launching quick startup of moment;
2 securities: air gauge is housed on launcher, and before transmitting, rocket body is locked by hinge grid, and water rocket can be filled with maximum safe air pressure, has both guaranteed that rocket body can mistakenly not launched, and also guarantees that rocket body can not explode because of hyperinflation;
3 high efficiency: during rocket body transmitting, hinge grid opening speed is fast, resistance is little, is subject to force-stroke short, so hinge grid mechanism is minimum to the consumption of potential energy when rocket body is launched, used after pairing page grid, stress balance during rocket body transmitting, guarantees that the emission angle of rocket body can not change;
4 practicality: this device is drawn materials easily, make simply, and effect is fine, are applicable to numerous students in middle and primary schools and make, and improve manipulative ability.
The utility model is also applicable to launch under water extreme misery rocket body.
In addition, it should be noted that, the specific embodiment described in this description, as long as the undeclared concrete shape of its part and size, this part can be any shape and size that adapt with its structure; Meanwhile, the title that part is got also can be different.All equivalence or simple change of doing according to described structure, feature and the principle of the utility model patent design, are included in the protection domain of the utility model patent.
Claims (4)
1. a water rocket launching rack, comprise launcher and emitter, it is characterized in that: described launcher comprises two slide rails, a support and a base, vertical being fixedly connected with of middle front part of support and slide rail, the bottom that base is positioned at support is connected with adjusting screw with support; Described emitter comprises injection handle, sprays plug, jet fixed mount, jet pin fixed grid, air gauge, charge valve, air bleeding valve, inflation inlet, exhaust outlet, and described emitter is arranged on the afterbody of slide rail.
2. water rocket launching rack according to claim 1, is characterized in that: described jet pin fixed grid comprises hole grid and hinge, and the middle part of hole grid has bottleneck hole, and hole grid are connected with hinge with screw, and hinge is connected with jet fixed mount with holding screw.
3. water rocket launching rack according to claim 1, is characterized in that: described slide rail and the angle on ground are 30-60 degree.
4. water rocket launching rack according to claim 3, is characterized in that: described slide rail and the angle on ground are 45 degree.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320424425.6U CN203400502U (en) | 2013-07-17 | 2013-07-17 | Water rocket launching frame |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320424425.6U CN203400502U (en) | 2013-07-17 | 2013-07-17 | Water rocket launching frame |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203400502U true CN203400502U (en) | 2014-01-22 |
Family
ID=49936445
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320424425.6U Expired - Fee Related CN203400502U (en) | 2013-07-17 | 2013-07-17 | Water rocket launching frame |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203400502U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI558449B (en) * | 2014-04-10 | 2016-11-21 | Univ Hsiuping Sci & Tech | Water rocket with automatic filling system and wind direction detection device |
| TWI566815B (en) * | 2014-04-10 | 2017-01-21 | With automatic water filling system to detect wind speed and wind direction cum means of rocket |
-
2013
- 2013-07-17 CN CN201320424425.6U patent/CN203400502U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI558449B (en) * | 2014-04-10 | 2016-11-21 | Univ Hsiuping Sci & Tech | Water rocket with automatic filling system and wind direction detection device |
| TWI566815B (en) * | 2014-04-10 | 2017-01-21 | With automatic water filling system to detect wind speed and wind direction cum means of rocket |
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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: 20140122 Termination date: 20140717 |
|
| EXPY | Termination of patent right or utility model |