TW573114B - Launching device capable of continuously accelerating a carrier by continuous detonation - Google Patents

Launching device capable of continuously accelerating a carrier by continuous detonation Download PDF

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Publication number
TW573114B
TW573114B TW91124480A TW91124480A TW573114B TW 573114 B TW573114 B TW 573114B TW 91124480 A TW91124480 A TW 91124480A TW 91124480 A TW91124480 A TW 91124480A TW 573114 B TW573114 B TW 573114B
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Taiwan
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carrier
gunpowder
hole
scope
filling
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TW91124480A
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Chinese (zh)
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Ke-Yin Yan
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Ke-Yin Yan
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573114 五、發明說明(1) 發明背景: 本發明係一種發射裝置,尤指一種藉連續引爆火藥, 以令載體連續加速,並以極高速度發射出去之發射裝置。 先前技藝 按, 「大砲」 之爆炸威 為令砲彈 年來,許 發所謂之 不僅可作 可作為一 體,透過 有效減少 及製作火 在較低之 域之願景 二次 均在「長 次世界大 「V 3砲」 外,其砲 爆炸室間 傳統上 ’均係 力,以 能被發 多國家 「長程 為攻擊 種載體 該發射 研發及 箭所需 成本及 ,用以 藉引爆 令砲管 射出去 之國防 火砲發 性武器 之發射 裝置, 製作火 之相關 較短之 發射砲 砲管内 内之砲 ,順利 單位及 射器」 ,攻擊 裝置, 直接射 箭所需 科學及 時間内 彈之火 所填裝 彈受力 擊中遠 軍火製 ,期待 遠距離 以將攜 入地球 之龐大 技術人 ,即可 砲發射 之火藥 而發射 距離外 造商一 此種長 外之敵 帶有人 軌道, 成本, 才不足 快速實 器,即 包,產 出去。 之目標 直積極 程火砲 方目標 造衛星 如此, 亦可彌 之問題 現探索 俗稱之 生強大 然而, 物,多 研究開 發射器 物,更 之載 不僅可 補研發 ,令其 太空領 世界大戰及嗣後之冷戰期間,世界上有許多國 程火砲發射器」上投入極多之人力及經費,^ 一 戰期間之德國為例,曾秘密研發出一種所謂之 ,該種長程火砲發射器上除設有一大口栌= 管管壁外沿其軸向,接設有複數個爆炸室,L = 相隔一定間距,各該爆炸室係與砲管内金、目郴 叩日逆通,573114 V. Description of the invention (1) Background of the invention: The present invention is a launching device, especially a launching device that continuously detonates gunpowder to continuously accelerate the carrier and launch it at a very high speed. According to previous techniques, the explosive power of the "Cannon" has made the shells for years. Xu Fa's so-called not only can be used as a whole, but by effectively reducing and making fire in the lower field, the vision is twice in the "Long Times World Great" V In addition to the "three guns", the artillery explosion chambers have traditionally been all tied to each other, and the cost of research and development and arrows required to launch the long-range as a carrier for multi-country attacks and the cost of defense for detonating the gun tube Artillery fire weapon launching device, making fire related short firing guns inside the barrel of the gun, smooth units and launchers ", attacking devices, direct firing arrows required for scientific and time-fired bomb loading force Hitting the long-range munitions system, and looking forward to the long-distance to bring the huge technical personnel brought into the earth, can fire the gunpowder and launch the range from a foreign manufacturer. Such a long-term enemy has a human orbit. The cost is not enough for a fast implement, that is, Package, output goes. The target is directly aimed at the artillery side. The goal is to build a satellite like this. It can also be explored. The problem is now known as the powerful life. However, more research and launching of launching objects, and the load can not only supplement research and development, make its space-leading world war and future During the Cold War, there were many national artillery launchers in the world. "Many people and funds were invested in it. ^ In Germany during the First World War, for example, a so-called, long-range artillery launcher was secretly developed.栌 = there are several explosion chambers along the axial direction of the outer wall of the tube, L = a certain distance from each other, each of the explosion chambers is in reverse communication with the gold and the eye of the barrel,

第5頁 573114 五、發明說明(2) 其内不僅填裝 形成一定失角 移動後,可藉 砲管内逐漸加 一作法,雖曾 射出去,並以 國,但該發射 砲管内高速移 僅對砲彈產生 藥,而造成無 彈在砲管内逐 準性並不良好 有火藥及引信,且與砲管中心軸沿砲口方向 ,俾在引爆砲官内之火藥包,令砲彈向砲口 依序引爆各該爆炸室之火藥,令砲彈得以在 速,並以極高之速度,自砲口發射出去,此 令,達140公斤之砲彈,由14〇釐米之大砲發 ,南之速度’射向遠在約丨6 5公里處外之英 器不僅結構複雜,製作成本昂貴,且砲彈在 動時,砲彈前方所形成之高溫壓縮空氣,不 極大之阻力,且易預先引爆各該爆炸室之火 法精準引爆各該爆炸室之火藥,故無法令砲 漸加速,達到預定之速度,故其穩定性及精 另,自1 9 6 0年代以後,美國太空總署(NASA)亦展開了 一項名為HARP之高空研究計劃(即High AUitudePage 5 573114 V. Description of the invention (2) Not only can it be filled to form a certain missing angle movement, it can be gradually added to the gun barrel. Although it has been fired and used in the country, the high-speed movement in the firing barrel is only suitable for Cannonballs generate powder, which results in poor accuracy in the gun barrel. There are gunpowder and fuze, and along the muzzle of the gun's center axis, it is detonated in the gunner's gunpowder package, so that the shells are ordered towards the muzzle. Detonating the gunpowder in each of the explosion chambers allowed the shells to speed up and fire from the muzzle at a very high speed. This order, a shell of 140 kilograms was fired from a 14 cm cannon and was fired toward the south. British vessels far away from about 6.5 kilometers are not only complicated in structure and expensive to produce, but also the high-temperature compressed air formed in front of the shell when the shell is moving, does not have great resistance, and it is easy to detonate the fire of each explosion chamber in advance. Since the explosives of each explosion chamber were precisely detonated by law, the artillery could not be gradually accelerated to reach the predetermined speed, so its stability and precision were improved. Since the 1960s, NASA also launched a project Altitude called HARP Study plan (ie High AUitude

Research Project),此一計劃之目的,係在研究發 -種可將攜帶有小型人造衛星之載體,利用大跑直接發射 至距離地球表面約1 8 〇公里外之地球執道,丨9 9 2年間, 國太空總署在勞倫斯利弗莫實驗室(L〇wrence Livermae、 Laboratory)進行的一項高空研究計劃中,根據不列公 式,發現砲彈之速度永遠無法超越砲管内空氣被推送之 度: & (v, rms)2 = 3RT/M ’其中(ν’ rms)為氣體分子速度之均方根 (root-mean-SqUare value),r為理想氣體常數,了為絕對Research Project), the purpose of this project is to research and develop a kind of carrier that can carry small artificial satellites, and use it to launch directly to the earth, about 1 800 kilometers away from the surface of the earth, 9 9 2 During the year, in a high-altitude research program conducted by the National Space Administration at Lawrence Livermae and Laboratory, it was found that the speed of the shell could never exceed the degree that the air in the barrel was pushed: & (v, rms) 2 = 3RT / M 'where (ν' rms) is the root-mean-SqUare value of the molecular velocity of the gas, r is the ideal gas constant, and is absolute

573114 ,發明說明(3) 浪度’Μ為空氣分子之所旦 空氣分子之質量Μ,否=里故,除非能有效降低砲管内 度,因此,曾使用氫、1 ’難以有效提昇砲彈之發射速 空氣分子之質量Μ,人妁.、、、砲官内之空氣,以降低砲管内 度,該項研究計劃所可「在砲管内達到更高之移動速 斤之砲彈’以每秒約3二° 長程大砲」,曾將重達5公 至於,其它國穿^ 速度發射出去。 國,亦相繼進行Puf國、英國、巾國及伊拉克…等 劃之詳細内容為何工;:,研究計劃’峨其研究計 射器,均係利用砲管作:砲發設計出之長程火砲發 基本結構與傳統大砲雷 二-:發射裝置’其 一 ^ „ 退之地方’必需增加其砲管長度及:?丨 ί,此;卜,t t射器不僅結構龐大複雜,且製作成本昂 貝二 :Η匕種傳統結構之火砲發射器,《限於砲管 内氣體之排放速度及砲彈前方壓縮空氣之阻力大盆 彈在砲口之速度始終無法如預期加速至一極高之理想速 度。 發明綱要: 有鑑於前述傳統結構之發射器,結構龐大複雜,製 成本昂貴’且受限於砲管内氣體阻力,令其砲彈之砲口迷 度無法加速至理想速度之缺點’發明人經過長久研究,、炊 於開發設計出本發明之一種「可藉連續引爆以令載體連二 加速之發射裝置」。 ’573114, description of the invention (3) The wave length 'M is the mass M of air molecules, no = reason, unless it can effectively reduce the gun's internal degree. Therefore, it has been difficult to effectively improve the launch of the shell with hydrogen. The mass M of the fast-air molecules, the air inside the gunner, to reduce the gun's internal degree, the research project "can achieve a higher moving speed of the shell in the gun's gun at about 3 per second. "Two-degree long-range artillery", once weighed up to 5 meters, and other countries fired out at a speed of ^. China, has also carried out the details of the plans of Puf, Britain, India and Iraq ...:, the research plan 'Eqi research projectiles, all use gun barrels as: long-range artillery fire designed Basic structure and traditional artillery mine II: The launching device 'one ^ „retreat place' must increase the length of its barrel and:? 丨 ί, this; bu, tt launcher not only has a huge and complicated structure, but also costs Angbe II : The traditional artillery launcher of the dagger type, "Limited to the speed of gas discharge in the barrel and the resistance of the compressed air in front of the shell, the velocity of the large shell at the muzzle has not been able to accelerate to an extremely high ideal speed as expected. Outline of the invention: In view of the above-mentioned traditional structure of the launcher, the structure is huge and complicated, and it is expensive to manufacture. 'It is limited by the gas resistance in the barrel, which makes it impossible to accelerate the muzzle of its shell to the desired speed.' After long research, the inventor In the development of the invention, a "launching device capable of accelerating the carrier by two successive detonations" was developed. ’

第7頁 573114Page 7 573114

本發明之一 置包括一載體, 住策听裝置 孔之大小 體之底部 緣係與該 該座體上 及引信, 套設於該 上之一第 啟動該第 孔内爆燃 向加速移 恰可令 並開設 貫穿孔 ’其側 相鄰填 柱體上 一填裝 一填裝 ,並對 動0 目的,係在提供一 該載體之中央部位 該載體被套設於該 有一槽孔’其大小 ,該火藥填 開設有複數 相銜接 面依序 裝孔間 ,並停 孔位置 孔内之 該載體 並保持一預 駐在最接近 ,恰位於該 引信,引爆 產生推力, 设有一貫穿孔,該貫穿 火藥填裝柱體上,該载 係大於該貫穿孔,且上 裝柱體之一端係固定至 個填裝孔,供填裝火藥 定間隙,俾當該載體被 該座體位置時,該柱體 載體底部之槽孔内,故 火藥時,火藥可在該槽 令其沿該柱體之另端方 本發明之另一目的,係在該載體依序位移至後續之該 ^填裝孔位置,且該等後續填裝孔恰位於該槽孔内時,可 ^依序啟動其中之引信,引爆火藥,即可令該載體連續加 、’並以極高之速度發射出去。 本發明之又一目的,係在用以啟動各該引信之啟動元 牛’可為一機械式、電子式或光電式之啟動元件,各該啟 動元件在感應到該載體位移至各該填裝孔位置時,可觸發 該弓丨信,以在各該填裝孔恰位於該載體之槽孔内時,引爆 火藥,對該載體產生連續加速之推力。 為便於 貴審查委員能對本發明之形狀、構造及裝置 之目的、特徵及功效,有更進一步之認識與瞭解,茲舉若One aspect of the present invention includes a carrier, the bottom edge of the large and small body of the hearing device hole is connected to the base and the fuze, and the first edge of the hole in the first hole is activated to accelerate the explosion. And a through-hole is opened to fill and fill one of the adjacent pillars on its side, and the action is to provide a central part of the carrier. The carrier is sheathed in the slot. Its size is the size of the gunpowder. A plurality of connecting surfaces are sequentially installed in the hole, and the carrier in the hole is stopped and the carrier stays closest to it, which is located exactly on the fuze and detonates to generate thrust. A through hole is provided, and the penetrating charge packing column is provided. On the body, the load is larger than the through-hole, and one end of the upper post is fixed to a filling hole for filling the powder to set a gap. When the carrier is positioned by the base, the bottom of the carrier of the post is fixed. In the slot, when the gunpowder is in charge, the gunpowder can make it along the other end of the cylinder in the slot. Another object of the present invention is to sequentially shift the carrier to the subsequent filling hole position, and Subsequent filling holes are located exactly in this slot Within, the sequential startup ^ wherein the fuse, detonating powder, enabling the carrier to continuously add, "and at the high speed is emitted. Another object of the present invention is that the starting element used to start each of the fuzes may be a mechanical, electronic, or optoelectronic starting element. Each of the starting elements senses the displacement of the carrier to the filling. When the hole is located, the bow can be triggered so that when each of the filling holes is located in the slot of the carrier, the gunpowder is detonated, and a continuous acceleration thrust is generated on the carrier. In order for your reviewers to have a further understanding and understanding of the shape, structure, and device's purpose, features, and functions of the present invention,

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干實施例配合圖示,詳細說明如下·· 詳細說明: 本發明係了種「可藉連續引爆以令載體連續加速之發 射裝置」,請參閱第1圖所示,該發射裝置包括一載體 1〇 : 一火藥填裝柱體20及一座體50 ;在第i圖中,該載體 1 0係一沿圓周方向對稱之錐狀體,惟本發明在實際實施 時,並不侷限於此,該載體10可為其它沿圓周方向對稱之 載體^,該載體10之中央部位設有一貫穿孔u,該貫穿孔 11在第1圖中,係呈方形,,准本發明在實際實施時,並不 侷限於此,該貫穿孔i i可為其它形狀,其大小恰可令該載 體10滑動地套設於該火藥填裝柱體20上,該載體10之底部 並開設有了槽孔12,該槽孔12之大小係大於該貫穿孔u, 且其上緣係與該貫穿孔丨丨相銜接;該火藥填裝柱體2〇係一 呈,條狀之柱體20,在第1圖中所示之該柱體2〇,係配合 該二穿孔11,而為一呈方形斷面之柱體2〇,惟本發明在實 際實施時,並不侷限於此,可配合該貫穿孔丨丨之形狀,被 設計成其它斷面形狀,該柱體20之一端係固定至該座體50 上,其上至少一個以上之側面,沿該柱體20之另端方向, 依序開认有複數個填裝孔2 1,供填裝火藥2 2及引信2 3 ,相 郴之該等填裝孔2 1間並保持一預定之間隙,俾當該載體工〇 被套設於該柱體20上,並停駐在最接近該座體5〇位置時, 該柱體20上最接近該座體5〇之一第一填裝孔21 i位置,恰 位於該載體1〇底部之槽孔12内。The dry embodiment is illustrated in detail with the following details: The detailed description: The present invention is a "launch device capable of continuously accelerating the carrier by continuous detonation". Please refer to FIG. 1, which includes a carrier 1 〇: A gunpowder fills the pillar 20 and the base 50; in the figure i, the carrier 10 is a cone-shaped body symmetrical in the circumferential direction. However, in actual implementation, the present invention is not limited to this. The carrier 10 may be other carriers symmetrical in the circumferential direction. A central portion of the carrier 10 is provided with a through hole u. The through hole 11 is square in the first figure. In practice, the present invention does not Limited to this, the through hole ii may have other shapes, and its size is just enough to allow the carrier 10 to be slidably sleeved on the gunpowder filling cylinder 20, and a slot 12 is formed at the bottom of the carrier 10, and the slot The size of the hole 12 is larger than the through-hole u, and its upper edge is connected to the through-hole 丨 丨; the gunpowder filling column 20 is a strip-shaped column 20, as shown in FIG. The cylinder 20 shown in the figure is a cylinder 2 with a square cross-section in combination with the two perforations 11. 〇 However, the present invention is not limited to this in actual implementation. The shape of the through hole 丨 丨 can be designed into other cross-sectional shapes. One end of the pillar 20 is fixed to the base 50. At least one or more side surfaces, along the direction of the other end of the column 20, are sequentially identified as having a plurality of filling holes 21 for filling gunpowder 2 2 and fuze 2 3, and the corresponding filling holes 2 1 and maintain a predetermined gap, when the carrier is placed on the pillar 20 and stopped at a position closest to the seat 50, the pillar 20 is closest to the seat 50. A first filling hole 21 i is located in the slot 12 at the bottom of the carrier 10.

573114573114

因此’當啟動該第一填裝孔211内所安裝之引信23, 引爆其中之火藥22時,火藥22可在該槽孔12内爆燃,並對 該載體10產生推力,令其沿該柱體20之另端方向加速移 動。在本發明中,由於該座體5〇可藉至少一個以上之連接 元件51,穩固定地定位於地面或其它固定物上,或令該座 體50。地面或其它固定物連接成一體,以在引爆火藥μ發 射該載體10時,使該載體10及固定其上之該火藥填裝柱體 2 0,仍能準確地定位在地面或其它固定物上,而不致產生 劇烈晃動。 由以上所述之結構,可清楚得知,當啟動該第一填裝 孔211内所安裝之引信23,引爆火藥22,令該載體1〇沿該 柱體20之另端方向加速移動時,由於該載體1〇係在一開放 空間中移動,故無需承受如傳統砲管内之壓縮空氣所造成 之強大阻力,而火藥2 2在該槽孔1 2内爆燃,所產生之強大 推力’則可令該載體1 〇如同火箭般,沿該柱體2 〇之另端方 向快速移動。基於此一發射原理,俟該載體丨〇被位移至後 續之一第二填裝孔2 1 2位置,且該第二填裝孔2丨2恰位於該 槽孔12内時,啟動第二填裝孔212内所安裝之引信23,引 爆火藥2 2 ’令其在該槽孔1 2内爆燃,以對該載體1 〇產生加 速移動之推力。同理,當該載體1 〇依序位移至後續之該等 填裝孔2 1位置’且該等後續填裝孔2 1恰位於該槽孔1 2内 時,依序啟動其中之引信23,引爆火藥22,即^令該載體 10被連續加速,而以極高之速度發射出去。 在本發明中,用以啟動引信23以引爆火藥22之元件,Therefore, when the fuze 23 installed in the first filling hole 211 is activated and the gunpowder 22 is detonated, the gunpowder 22 can deflagrate in the slot 12 and generate a thrust force to the carrier 10 so that it runs along the cylinder. The other end of 20 accelerates. In the present invention, since the base body 50 can be stably fixed on the ground or other fixed objects by the at least one connection element 51, or the base body 50 can be fixed. The ground or other fixtures are connected to form a whole, so that when the powder 10 is detonated by the gunpowder μ, the carrier 10 and the gunpowder filling cylinder 20 fixed on it can still be accurately positioned on the ground or other fixtures. Without violent shaking. From the structure described above, it is clear that when the fuze 23 installed in the first filling hole 211 is activated, the powder 22 is detonated, and the carrier 10 is accelerated to move in the direction of the other end of the pillar 20, Because the carrier 10 moves in an open space, it does not need to withstand the strong resistance caused by the compressed air in the traditional gun barrel, and the explosive force of the gunpowder 22 deflagration in the slot 12 can generate a strong thrust. Make the carrier 10 move rapidly like a rocket along the other end of the cylinder 20. Based on this launching principle, the carrier is moved to one of the subsequent second filling holes 2 1 2 and the second filling hole 2 is located in the slot 12 to start the second filling. The fuze 23 installed in the mounting hole 212 detonates the gunpowder 2 2 ′ to cause it to deflagrate in the slot 12 to generate a thrust to accelerate the carrier 10. Similarly, when the carrier 10 is sequentially displaced to the subsequent filling holes 21 1 ′ and the subsequent filling holes 21 are located in the slot holes 12 in sequence, the fuze 23 is sequentially activated. Detonating the gunpowder 22 causes the carrier 10 to be continuously accelerated and fired at a very high speed. In the present invention, the element for activating the fuze 23 to detonate the gunpowder 22,

第10頁 五、發明說明(?) i;係::式、電子式或光電式之啟動元件’無論該啟動 到該载體?“何種方式觸發引信23,其主要目的均係在感應 孔21内之引^9移至各該填裝孔21位置時,可啟動該等填裝 孔12内日士 以在各該填裝孔21恰位於該載體之槽 m二引爆火藥22,對該載體1〇產生連續加速之推 件3。為ί :月之一最佳實施例中,兹以一機械式之啟動元 率作ΓΓ月,參閱第2及3圖所示,該弓1信23與火 狀怜可:乍成一體,形成一火藥&,該火藥包之大小及形 了肷入各該填裝孔21内,且其任一端上設有一 id:該啟動元件3°上並設有一摯動桿31,該㈣ 鼓入各該填裝孔21時’恰可凸露於各該 =?外,且其與該火藥包相連接之夾 載=之移動方向…,當該載體10位 = 孔21時’該載體10之貫穿孔"前緣將觸碰該下—個 該啟動元件3°上之摯動桿31,並令其向該填裝^ 内擠壓’以觸發引信23,引爆該火藥22。在 U2」 最佳實施例中,該啟動元件30亦可設在各該填裴孔2 緣,該啟動元件30之該摯動桿31可在該火藥包兮 填裝孔2 1時,凸露於各該填裝孔2丨外,且其與 以 21孔緣相連接之夾角,恰面對於該載體丨〇之移= 此’當該載體1()之貫穿仙前緣觸碰到該摯 時:: 令其向該填裝孔21内擠壓,以觸發引信23,引爆該=藥將 據上所述,本發明之發射裂置,不僅具備結構簡單、 573114 五、發明說明(8) 點’且由於其載體y無f承受如傳 ,、鱼痒所產生之強大阻力,故在依序引爆火藥 '、績對該載體1 0進行加速後,可輕易令該載體1 0於較 短的:务射行程内,達到極高之發射速度。 此外’在本發明之又一最佳實施例中,本發明所述及 之、體10 ’可視實際之需要,被設計成不同之形狀及大 ^ ,在其貝穿孔11周緣規劃出一定大小之容置空間4 0, 多閱第f圖所示,倘該發射裝置係被用以發射小型人造衛 星,則該容置空間4〇必須足以容納一小型人 該小型衛星所需之機構及控制元件(圖中未示),若= 射裝置係被用以發射砲彈,則該容置空間4〇必須足以^ 載之炸藥及引信(圖中未示),如此,當該載體;〇 被本發明之發射裝置以極高之速度發射至地球軌道或遠方 之目標物時’即可藉由控制該容置空間40内所安裝之栌制 :件,在地球執道上開啟小型人造衛星,或工 物位置觸發引信,引爆炸藥,完成所欲達成之任務。心 按’以上所述’僅為本發明最佳之具體實施例,惟本 :明之構造特徵並不侷限於此,凡任何熟悉該項技蓺者在 請之變化或修飾’應“蓋在 573114 圖式簡單說明 圖示說明: 第1圖係本發明之立體透視圖; 第2圖係本發明之一最佳實施例中具有局部剖面之立 體透視圖; 第3圖係第2圖所示該最佳實施例中之剖面示意圖; 第4圖係本發明之又一最佳實施例之剖面示意圖。 主要元件編號: 載體 .........10 火藥填裝柱體.........20 座體 .........5 0 貫穿孔 11 槽孔 .........12 填裝孔 21 火藥 .........2 2 引信 23 第一填裝孔.........211第二填裝孔 .........212 容置空間 .........40 連接元件 51 啟動元件 .........30 摯動桿 31Page 10 V. Description of the invention (?) I; Department of :: type, electronic or optoelectronic type starting element 'whatever is activated to the carrier?' "How to trigger the fuze 23, the main purpose of which is the induction hole When the guide ^ 9 in 21 is moved to the position of each of the filling holes 21, the Japanese inside the filling holes 12 can be activated to detonate the gunpowder 22 at each of the filling holes 21 exactly in the slot m of the carrier. The carrier 10 generates a continuously accelerating pusher 3. For one of the best embodiments, a mechanical start-up rate is used as ΓΓmonth, as shown in Figures 2 and 3, the bow 1 letter 23 Pity with the fire: at first, form a gunpowder & the size and shape of the gunpowder are inserted into each of the filling holes 21, and an id is provided on either end of the gun: the starting element is 3 ° above the A moving rod 31 is provided, and when the drum bulges into each of the filling holes 21, it can just be exposed out of each of the openings, and the direction of movement of the clip load = connected to the gunpowder ..., when the carrier 10th place = hole 21 'the through hole of the carrier 10' will touch the leading rod 31 on the next 3 ° of the starting element and make it squeeze into the filling ^ Fuze 23 is used to detonate the gunpowder 22. In the preferred embodiment of U2 ", the activation element 30 may also be provided at each edge of the filling hole 2, and the actuating rod 31 of the activation element 30 may be enclosed in the gunpowder. When the filling hole 21 is filled, it protrudes outside each of the filling holes 2 丨, and its angle connected with the edge of the 21 hole is exactly the same as the movement of the carrier 丨 〇 = this' When the carrier 1 () When you touch the heart through the front edge of the fairy: :: make it squeeze into the filling hole 21 to trigger the fuse 23 and detonate the = medicine will be based on the above, the firing split of the present invention not only has a simple structure 573114 V. Description of the invention (8) Point 'and because its carrier y has no f resistance, such as transmission, strong resistance caused by fish itch, so in order to detonate gunpowder', Ji accelerated the carrier 10, can Easily make the carrier 10 reach a very high launch speed within a short: mission range. In addition, in another preferred embodiment of the present invention, the body 10 described in the present invention can be designed in different shapes and sizes according to actual needs, and a certain size is planned on the 11th periphery of the perforation. Receiving space 40, read more in Figure f. If the launch device is used to launch a small artificial satellite, the accommodating space 40 must be sufficient to accommodate a small person with the mechanism and control elements required for the small satellite (Not shown in the figure), if the firing device is used to launch a shell, the containing space 40 must be sufficient to carry explosives and fuzes (not shown in the figure), so when the carrier is; When the launching device launches to the earth orbit or a distant target at a very high speed, it is possible to control the built-in: pieces in the accommodation space 40 to open a small artificial satellite on the earth ’s path, or a work object. The position triggers a fuze, detonates the explosive, and completes the desired task. The word "above" is only the best specific embodiment of the present invention, but the structural features of the present invention are not limited to this. Any changes or modifications that are familiar to the person skilled in the art should be covered by 573114. The drawings are briefly illustrated and illustrated: FIG. 1 is a perspective perspective view of the present invention; FIG. 2 is a perspective perspective view with a partial cross-section in a preferred embodiment of the present invention; and FIG. 3 is a perspective view of FIG. A schematic cross-sectional view of the preferred embodiment; FIG. 4 is a schematic cross-sectional view of another preferred embodiment of the present invention. The main component number: the carrier ......... 10 gunpowder filling column ... ..... 20 base body ......... 5 0 through hole 11 slotted hole ......... 12 filling hole 21 gunpowder ......... 2 2 Fuze 23 First filling hole ......... 211 Second filling hole ......... 212 Receiving space ......... 40 Connecting element 51 Starting element ......... 30 Actuator 31

第13頁Page 13

Claims (1)

573114 六、申請專利範圍 置 I、一種可藉連續引爆以令載體連續加速之發射裝 包括: 座,’係穩固定地定位於地面或其它固定物上; 面 一火藥填裝柱體,該火藥填裝柱體係一呈長條狀之柱 ^ 了端係固定至該座體上,其上至少一個以上之側 沿,柱體之另端方向,依序開設有複數個填裝孔,供 土、裝火藥及引信,相鄰填裝孔間並保持一預定間隙; 載體,泫載體之中央部位設有一貫穿孔,其大小恰 y令該載體滑動地套設於該火藥填裝柱體上,該載體之底 =1開設有一槽孔,該槽孔之大小係大於該貫穿孔,且宜 =係與該貫穿孔相銜接,當該載體被套設於該柱體上, 二二駐在取接近該座體位置時,該柱體上最接近該座體之 一第一填裝孔位置,恰位於該載體底部之槽孔内 =’士當啟?該第—填裳孔内所安裝之引信,引爆其 Λ之八:晗’纟樂可在該槽孔内爆燃,並對該載體產生推 力,令其沿該柱體之另端方向加生推 置,且該等後續填裝孔恰位於 ϊ序啟動其中之引信,引爆火藥,即可令該 載體被連項加速,以極高之速度發射出去。 2、 如申請專利範圍第1 g 俨、查择4邙夕恭私姑班 、斤述之可藉連續引爆以令載 ,連續加速之發射裝置,其中該載 : 方向對稱之錐狀體。 「办』兩/口 a周 3、 如申請專利範圍第丨項所述之 體連續加速之發射裝置,其中該载體在^連、,只引爆以々載 -、曱請專利範圍 叹有一定大小且密閉之容置空間,供容納所欲承載之物 件’並在該載體被發射至遠方預定位置時,可啟動該物 件。 以 4 +、如申請專利範圍第i項所述之可藉連續引爆以令載 運績加速之發射裝置,其中該座體尚可藉至少一個以上 連接元件’將其穩固定地定位於地面或其它固定物上。 5、 如申請專利範圍第i項所述之可藉連續引爆以令載 —=、·.只加速之發射裝置,其中該座體尚可與地面 疋物連接成一體。 八 6、 如申請專利範圍第丨項所述之可藉連續引爆以令載 、,,貝加速之發射裝置,其中該引信與火藥可製作成一 填裝SC ::火藥包’該火藥包之大小及形狀恰可嵌入各該 7、 如申請專利範圍項所述之可 體連續加速之發射梦罢甘士 A勺虹私Γ 爆7載 動該該載體位移至各該填裝孔位置時1以啟 槽孔内時U ?引信’以在各該填裝孔恰位於該載體之 8 / 引,火藥,對該載體產生連續加速之推力。 _如申請專利範圍第7項所述之可藉連續引燋u人藝 =續:速;發射裝置,其中該啟動元件係設 包被礙入各包括一擎ϊ桿,該擎動桿在該火藥 盥該火藥包ίί時’恰可凸露於各該填裝孔外,且其 ’、9 /如申:奎接之夹角,恰面對於該載體之移動方向。 节h專利範圍第7項所述之可藉連續引爆以令載 573114 六、申請專利範圍 體 連續加速之發射裝置,其中該啟動元件係^在久· 孔之孔緣,該啟動元件包括一擎勤丨曰 、X 該填裴 藥包被嵌入各該填裝孔時,]+ 該摯動椁可在該火 各該填裝孔孔緣相連接之爽露於各該填裝孔外,且其與 向。 ’恰面對於該載體之移動^573114 Sixth, the scope of the patent application I. A launching device that can be continuously detonated to continuously accelerate the carrier includes: a seat, 'fixed and fixedly positioned on the ground or other fixed objects; a gunpowder filling the cylinder, the gunpowder The packing column system is a long column. The end system is fixed to the base body. At least one side edge of the packing column is on the other end of the column. A plurality of packing holes are sequentially opened for the soil. 1. Loading gunpowder and fuze, and maintaining a predetermined gap between adjacent filling holes; the carrier, the carrier is provided with a through hole in the central portion, the size of which is such that the carrier is slidably sleeved on the gunpowder filling cylinder, The bottom of the carrier = 1 is provided with a slot, the size of the slot is larger than the through hole, and it should be connected with the through hole. When the carrier is nested on the pillar, two or two will stay close to the through hole. At the position of the seat, the position of the first filling hole on the pillar closest to the seat is located in the slot at the bottom of the carrier = 'Shidangqi? The fuze installed in the first-filled hole detonates its eighth: 晗 '纟 乐 can deflagrate in the slot and generate thrust on the carrier, causing it to push in the direction of the other end of the cylinder And the subsequent filling holes are located in the sequence to activate the fuze and detonate the gunpowder, the carrier can be accelerated by successive items and fired at a very high speed. 2. If the scope of the patent application is 1g 俨, check 4 邙 xi Gong's private aunt class, it can be described as a launching device that can be continuously detonated to make the load and continuously accelerated, where the load is a cone with a symmetrical direction. "Do" two / mouth a week 3, as described in the scope of the application for the scope of the patent application of the continuous acceleration of the launch device, where the carrier ^ Li, only detonated to carry a load-, please ask the patent scope to a certain extent A large and enclosed storage space for accommodating the object to be carried 'and the object can be activated when the carrier is launched to a predetermined location in the distance. 4 +, as described in item i of the scope of patent application, can be borrowed continuously A launching device that detonates to accelerate the carrying performance, wherein the base body can still be fixedly fixed on the ground or other fixed objects by at least one or more connecting elements. 5. It may be as described in item i of the scope of patent application. Continuous detonation to make the load — =, .... Only acceleration launching device, in which the base body can still be connected to the ground object as a whole. 8 6. As described in the scope of the patent application, the continuous detonation can be used to make the load. 、,, Shell accelerated launching device, where the fuze and gunpowder can be made into a filled SC :: gunpowder packet 'The size and shape of the gunpowder packet can be embedded in each of the 7, as described in the scope of the patent application accelerate Fire the dream striker A spoonful of rainbow private Γ Burst 7 to move the carrier to the position of each of the filling holes 1 to open the slot when U? Fuze 'so that each of the filling holes is located exactly 8 of the carrier / Induction, gunpowder, which generates continuous acceleration thrust to the carrier. _ As described in item 7 of the scope of patent application, continuous induction can be used. 人人 艺 = Continued: speed; launching device, in which the starting element is blocked by the package. Each of them includes an engine lever, and the engine lever may just be exposed outside each of the filling holes when the gunpowder and the gunpowder package are lit, and its', 9 / Rushen: Kui Jie's included angle, just The direction of movement of the carrier is described in Section 7 of the patent scope. The launching device can be continuously detonated to enable the load to be 573114. 6. The patent application scope of the launching device is continuously accelerated, wherein the starting element is a hole in the long hole. The starting element includes an engine, X, and X when the filling pack is embedded in each of the filling holes.] + The motion can be exposed at the edge of each filling hole of the fire. Each of the filling holes is outside, and it faces in the same direction. 'Just the movement of the carrier ^
TW91124480A 2002-10-23 2002-10-23 Launching device capable of continuously accelerating a carrier by continuous detonation TW573114B (en)

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