TWM282273U - Device for launching a mini rocket - Google Patents

Device for launching a mini rocket Download PDF

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Publication number
TWM282273U
TWM282273U TW94208312U TW94208312U TWM282273U TW M282273 U TWM282273 U TW M282273U TW 94208312 U TW94208312 U TW 94208312U TW 94208312 U TW94208312 U TW 94208312U TW M282273 U TWM282273 U TW M282273U
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Taiwan
Prior art keywords
rocket
launcher
miniature
launching
conductive
Prior art date
Application number
TW94208312U
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Chinese (zh)
Inventor
Yung-Chiang Ting
Yu-Chao Shen
Jyun-Yuan Su
De-Yang Chen
Sung-Yi Chung
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Far East College
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Priority to TW94208312U priority Critical patent/TWM282273U/en
Publication of TWM282273U publication Critical patent/TWM282273U/en

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Description

M282273 八、新型說明: 【新型所屬之技術領域】 本創作係關於一種微型火箭發射裝置,尤指一種利用 私解方式產生之可燃氣體做為逑你化微型水火箭之發射推 力,而可用以驗證具科學教育性之電解實驗,且兼具娱樂 性,達致一寓教於樂目的之裝置者。 、’、 【先前技術】 按,近幾年來,國内外校園中常見一種「水火箭」的 競賽活動,這種結合環保意識、科技教育、益智娛樂的活 動,乃是目前相當盛行的親子休閒活自,連大人們也會為 之著迷,而這種水火箭的環保設計,主要是以寶特瓶:材 料,而利用牛頓第三定律「作用力與反作用力」之原理, 猎空氣壓力及水作為動力,用以將這種環保火箭發射升 空,簡單來說,就是於寶特瓶内灌入空氣,形成氣壓大於 大氣壓力之壓縮空氣,復於寶特瓶之喷氣閥打開時,以壓 縮空氣推動瓶内加入的適量水,如此,運用動量守恆,當 水流高速向外衝出,產生更強之反作用力,而能推動水火 前升空飛得更快,之後,升空後之水火箭再以本身之慣性 力置持續飛行,復經受地心引力及空氣阻力之影響而速度 漸緩慢,終而呈一拋物線路徑墜落地面。 而上述簡單的水火箭製作,即涉及了多項的物理概 念’其包括有動量守恆定理、牛頓第三定律及拋物線理論, M282273 藉此,學生透過活動的實踐,乃更能體會其中的科學原理。 然而,科學領域中相關定律、原理的印證,以校園為 例,以往多只是單純於課堂、實驗室藉由實驗獲得,1今 係有更多人投入教育性與娛樂性兼具之教具研發領域中, 身為教育者之申請人亦是不遺餘力的投注心力於此,遂有 本創作之產生。 【新型内容】 • »上,本創作之目的即在於提供一種微型火箭發射裝 置,其所欲解決之問題係為考量昔日所見之寶特瓶水火 箭,其體積較大,且射程遠’以發射火箭之安全性來說, 較適合年齡較長的學童,而其解決問題之技術取向乃是著 .眼於迷你化之設計,而且藉由這樣迷你化的微型火箭設 •計,使其亦得結合另一科學基礎之原理印證,而發展出一 更具教學功能之教具,更進一步的,這樣的教具也能衍生 鲁成一種寓教於樂之玩具;具體來說: 本創作所欲解決之問題即在於·· 1·昔日寶特瓶環保水火箭體積較大、射程遠,安全性較 不佳。 2·昔日水火箭包含之科學理論印證早已周知,知識教導 限於此。 本創作解決問題之技術手段即在於: 1 ·水火箭採迷你化之微型設計。 M282273 ▲ 卜結合了利用電解作用而產生可職體之原理印 證。 本創作對照先前技術之功效即在於: 1.柄作使収加安全、有趣,適合更小學童的教學 樂。 、 2·科學教育之基礎原理印證更加廣泛。 而本創作進-步之實施手段則為: • Μ用-電解單元結合一充填座與配合一發射單元組成 微型火箭之發射震置,以供迷你化之微型火箭可實施發 身二其中,電解單元包含一裂電解液之容器,容器具有二 W棒及-導官,導管得穿接於前述充填座,及以一供電 •件經導電線相接於導電棒,發射單元為以—發射架設於一 ‘發射台上,且包含一發射器,發射器具有一發射桿與一點 火端,而微型火箭則具有一中空腔室與一閥口,而可套於 _充填座内之導官,或另套於發射桿之點火端,藉之,經電 解單元電解產生之可燃氣體可充填於微型火箭含水之中空 月工至中,以予集氣排水,復微型火箭可内含少量水再套於 發射夯,以藉點火端引燃中空腔室内之可燃氣體,而產生 瞬門九、炸之推力,進而排出微型火箭中之少量水做為發射 動力’使微型火箭逕予射出者。 【實施方式】 首先參閱第一、二圖所示,本創作之微型火箭發射裝 M282273 置’其=射裝置為利用—電解單元結合—充填座⑵與配合 务射單凡而成,其進一步之具體實施例設計為·· 該電解單s係包含—裝電解液之封閉容器⑴,且該容 器⑴以-蓋體⑴)與—盒體⑽組成具有氣密性之封: 空間’且該容器⑴上具有二導電棒(13)、(⑷及一導管 ⑽’該導管⑽之外㈣段得穿接於前述充填座⑵,及 以一供電件⑶經導電線(31)相接於該導電棒⑽、(⑷, 其中,該供電件⑶可為—電池,該導電線(3ι) —端接於電 池之正負極’另端則具有夾體(32)夾於該導電棒(⑻、 (14); •該發射單元係以—發射架⑷設於—發射台⑸上,及包 =一發射器(6) ’該發射器⑻具有—發射桿⑽與一點火 端(62),實際運用上’該發射器⑻得為—電子點火之 搶; ” 多韻型火箭⑺係具有_中空腔室⑺)與—閥口⑺), 可,套於前述充填座⑵内之導管⑽,或者’套於前述發 射為(6)發射桿(61)之點火端(62)。 错由上述裝置之設計’如第三、四圖所示,於微型火箭 ⑺之/空腔室⑺)中裝填足量的水,復套於充填座⑵内 =¥吕(15) ’其經電解單元之電解作用,裝有電解液之容 _)内卩此產生可燃氣體而經導管(15)充填於微型火箭 ⑺含水之中空腔室⑺)中,其間,中空腔室⑽内之狀態 M282273 便會形成集氣(可燃氣體)排水之現象,之後,再取下該中 空腔至(71)内含少量水與較多可燃氣體之微型火箭(7 ),以 將微型火箭(7)再套於發射器(6)之發射桿(61)【如第五圖 所示】,如此,則當欲發射微型火箭(7)時,只要藉由發射 為(6)既有之點火線路,使其點火端(62)引燃微型火箭(?) 中空腔室(71)内之可燃氣體,其便能產生瞬間之爆炸推 力,進而排出微型火箭(7)中之少量水,形成一股發射動 _力’使微型火箭(7 )能夠快速順利發射出去。 以上,本創作即是參照當前的具體實施例加以描述,應 足令本技術領域中的通識者能了解以上的實施例,惟,上 述實施例僅是用來說明本創作,在未脫離本創作精神的情 .況下,所稱通識者應還可作出各種等效的變化和修改,因 •此,只要在本創作的實質範疇内對上述實施例之變化、修 飾,理應都將落於本創作之申請專利範圍内,特申明之。 • 【圖式簡單說明】 第一圖係本創作可行實施例之結構示意圖(一)。 .第二圖係本創作可行實施例之結構示意圖(二)。 第二圖係本創作可行實施例操作電解充氣之立體視圖。 第四圖係本創作可行實施例操作電解充氣之剖視圖。 第五圖係本創作可行實施例發射安裝之立體視圖。 【主要元件符號說明】 (11)蓋體 " (1) 容器 M282273 (12) 盒體 (13) (14) 導電棒 (15) (2) 充填座 (3) (31) 導電線 (32) (4) 發射架 (5) (6) 發射器 (61) (62) 點火端 (7) (71) 中空腔室 (72) 導電棒 導管 供電件 夾體 發射台 發射桿 微型火箭 閥口M282273 8. Description of the new type: [Technical field to which the new type belongs] This creation is about a micro-rocket launcher, especially a flammable gas generated by a private solution as a launch thrust for a micro-water rocket. It can be used to verify Electrolytic experiments with scientific education, and both entertainment, to achieve a device for teaching and fun. [Previous technology] According to recent years, a "water rocket" competition has been common in domestic and foreign campuses. This combination of environmental awareness, science and technology education, education and entertainment is a very popular parent-child leisure. Even the adults will be fascinated by the living, and the environmental design of this water rocket is mainly based on the special bottle: material, and uses the principle of Newton's third law "force and reaction force" to hunt air pressure and Water is used as the power to launch this environmentally friendly rocket into the air. In simple terms, air is filled into the bottle to form compressed air with a pressure greater than atmospheric pressure. When the jet valve of the bottle is opened, Compressed air pushes the right amount of water into the bottle. In this way, the conservation of momentum is used. When the water flow rushes out at high speed, it generates a stronger reaction force, which can promote the water to fly faster before the fire and then the water after the lift. The rocket continued to fly with its own inertial force, and gradually slowed down under the influence of gravity and air resistance, eventually falling into the ground in a parabolic path. The above-mentioned simple water rocket production involves a number of physical concepts, including the conservation of momentum theory, Newton's third law, and the parabolic theory. With this, students can better understand the scientific principles through the practice of activities. However, the corroboration of related laws and principles in the field of science. Take campus as an example. In the past, it was only obtained through experiments in the classroom and laboratory. More people in the department are now engaged in the development of educational and entertainment teaching aids. However, the applicant as an educator has spared no effort in betting on this, and thus has created this creation. [New content] • »The above, the purpose of this creation is to provide a miniature rocket launcher. The problem to be solved is to consider the Pote bottle water rocket seen in the past. It has a large volume and a long range. In terms of the safety of the rocket, it is more suitable for older school children, and its technical orientation to solve problems is focused on miniaturized design, and with such miniaturized miniature rocket design, it also makes it Combined with the proof of another scientific foundation principle, a teaching tool with more teaching functions has been developed. Furthermore, such teaching tools can also be derived into a kind of educational toy; specifically: The problem lies in ... 1. The old environmental protection water rocket of Baote bottle was large in size, long in range, and inferior in safety. 2. The scientific theories contained in the water rockets of the past have been well known, and the teaching of knowledge is limited to this. The technical means to solve the problem in this creation are: 1. Miniature miniature design of water rocket. M282273 ▲ Combined with the principle of using electrolysis to produce a jobable body. The effects of this creation compared with the prior art are: 1. Handle makes the collection safe, fun, and suitable for the teaching pleasure of more elementary school children. 2. The basic principles of science education are more extensive. The implementation methods of this creation are as follows: • The M-electrolysis unit combines a filling base and a launch unit to form a launcher for a miniature rocket, so that a miniaturized miniature rocket can implement the second launch. Among them, electrolysis The unit contains a cracked electrolyte container. The container has two W rods and-guides. The conduit must be connected to the aforementioned filling base, and a power supply is connected to the conductive rods through conductive wires. On a 'launch pad' and containing a launcher, the launcher has a launch rod and an ignition end, while the miniature rocket has a hollow chamber and a valve port, which can be placed on the guide in the filling seat, or Another set is on the firing end of the launching rod. By this, the combustible gas produced by the electrolysis unit can be filled into the water containing micro-rocket to work in the air to collect gas and drain. The micro-rocket can contain a small amount of water and then set it on The launch ram is used to ignite the combustible gas in the hollow cavity by the ignition end to generate the thrust of instantaneous door IX and explosion, and then discharge a small amount of water in the miniature rocket as the launching power to make the miniature rocket pass to the shooter. [Embodiment] First, referring to the first and second figures, the miniature rocket launcher M282273 of this creation is set with a shooting device that uses a combination of electrolytic unit-filling seat and matching shooting, and further The specific embodiment is designed as follows: The electrolytic cell s is a sealed container 装 containing an electrolyte, and the container ⑴ is covered with a lid ⑴) and a box ⑽ is formed into a hermetically sealed seal: a space 'and the container There are two conductive rods (13), (1) and a conduit ('the outside of the conduit') can be connected to the aforementioned filling seat (5), and a power supply component (3) is connected to the conductor through a conductive wire (31). Rods ⑽, (⑷, where the power supply member ⑶ may be-a battery, the conductive wire (3ι)-terminated at the positive and negative electrodes of the battery, and the other end has a clip body (32) sandwiched between the conductive rod (⑻, ( 14); • The launching unit is set on a launching stand 发射 and a launcher (6) 'The launcher ⑻ has a launching pole ⑽ and an ignition end (62), practical use On 'the launcher won't be-electronic ignition grab; "polyphonic rocket system has _ hollow Chamber ⑺) and —valve port ⑺), can be sheathed in the conduit ⑽ in the aforementioned filling seat ⑵, or 'covered in the ignition end (62) of the aforementioned launcher (6) launch rod (61). Design 'As shown in the third and fourth figures, fill a sufficient amount of water in the miniature rocket ⑺ / cavity ⑺) and set it in the filling seat == ¥ LV (15)' It is electrolyzed by the electrolytic unit In the container with the electrolyte _), a flammable gas is generated and filled in the miniature rocket ⑺ water-containing hollow chamber 微型) via the duct (15), during which the state M282273 in the hollow chamber ⑽ will form a gas collection. (Flammable gas) drainage phenomenon, after that, remove the hollow cavity to (71) a miniature rocket (7) containing a small amount of water and more combustible gas, so as to put the miniature rocket (7) on the launcher (6) ) (61) [as shown in the fifth figure], so, when you want to launch a miniature rocket (7), as long as it is fired by the existing ignition circuit of (6), its ignition end (62) Ignite the flammable gas in the hollow chamber (71) of the miniature rocket (?), Which can produce an instant explosive thrust, and further A small amount of water in the miniature rocket (7) forms a launching force to enable the miniature rocket (7) to launch quickly and smoothly. Above, this creation is described with reference to the current specific embodiment. A generalist in the technical field can understand the above embodiments. However, the above embodiments are only used to explain the creation. Without departing from the spirit of the creation, the so-called generalist should be able to make various other things. Therefore, as long as the above embodiments are changed and modified within the essential scope of this creation, they should all fall within the scope of the patent application for this creation, and hereby declare it. • [Schematic description The first diagram is a schematic diagram of the structure of the feasible embodiment of the creation (1). The second diagram is the schematic diagram of the structure of the feasible embodiment of the creation (2). The second figure is a three-dimensional view of the electrolytic aeration operation in this feasible embodiment. The fourth figure is a cross-sectional view of the electrolytic aeration operation of this feasible embodiment. The fifth figure is a perspective view of the launch installation of the feasible embodiment of the present invention. [Description of main component symbols] (11) Lid " (1) Container M282273 (12) Box (13) (14) Conductive rod (15) (2) Filling base (3) (31) Conductive wire (32) (4) Launcher (5) (6) Launcher (61) (62) Ignition end (7) (71) Hollow chamber (72) Conductor rod conduit power supply clip launch pad launcher miniature rocket valve port

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Claims (1)

M282273 九、申請專利範圍: 為利用一電解單 以供微型火箭實 1. 一㈣敎箭發射裝置,其發射裝置 元結合-充填座與配合_發射單元而成, 施發射,其中: 、,早兀包合-裝電解液之封閉容器,該容器具有二 導電棒及:導管,該導管之外伸管段得穿接於前述充: 座及以供電件經導電線相接於該導電棒; 、 該發射單it為以—發射架設於—發射台上,及包含—發 s ’ aim具有_發射桿與—點火端; 該微型火箭係具有一中办脒 、,甲工腔至與一閥口,可供套於前述 填座内之導管,或套於前述發射器之點火端。 .2.如中請專·則1項所述之微型火箭發射裂置,其 -中該容n由-蓋體與盒體組成’並具有—氣密性。〃 /·如申請專利範圍第1項所述之微型火箭發射裝置,其 ,中。亥ί、電件可為一電池,該導電線一端接於電池之正負 極,另端具有夾體夾於前述導電棒。 4·如申請專利範圍第1項所述之微型火箭發射裝置,其 中忒發射器得為一電子點火之點火搶。M282273 9. Scope of patent application: In order to use an electrolysis unit for miniature rockets. 1. An arrow launching device, the launching device is a combination of a filling base and a launching unit, which is used for launching, of which: ,, early A closed container containing an electrolytic solution, the container has two conductive rods and a conduit, and the extended pipe section of the conduit must be connected to the aforementioned charging base and the conductive rod connected to the conductive rod through conductive wires; The launcher it consists of a launcher mounted on a launch pad, and a launcher including a launcher and an ignition end; the miniature rocket system has a central office, a cavity and a valve port. , Can be used to cover the catheter inside the filling seat, or the ignition end of the transmitter. .2. The micro-rocket firing split as described in item 1 of the Chinese patent, where the capacity n is composed of a cover body and a box body and has air-tightness. 〃 / · The miniature rocket launcher as described in item 1 of the scope of patent application, where, The electric component may be a battery. One end of the conductive wire is connected to the positive and negative electrodes of the battery, and the other end has a clip to clamp the aforementioned conductive rod. 4. The micro-rocket launching device as described in item 1 of the scope of the patent application, in which the plutonium launcher can be an electronic ignition ignition.
TW94208312U 2005-05-23 2005-05-23 Device for launching a mini rocket TWM282273U (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111653174A (en) * 2020-05-26 2020-09-11 南京航空航天大学 Rocket model stable control demonstration device applied to science popularization education

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111653174A (en) * 2020-05-26 2020-09-11 南京航空航天大学 Rocket model stable control demonstration device applied to science popularization education

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