200409900 玖、發明說明 (發明說明應敘明：發明所屬之技術領域、先前技術、內容、實施方式及圖式簡單說明） I：發明戶斤屬之技術領域3 發明領域 本發明係有關於軍火以及火器。本發明為特別但非專 用於炮身總成的應用，該炮身總成具有多數個圓形物以及 5 不連接之可選擇之可燃性推進燃料，該可燃性推進燃料係 軸向地堆疊在該炮身内用以連續地推進該等圓形物通過該 炮身的炮口。此等炮身總成將在下文中以”該所述類型”提 及0 10 【先前技術】 發明背景 本發明有關於軍火及火器之炮身總成，特別是該所述 類型，如早期由本發明者提出之國際專利申請案 PCT/AU94/00124 以及 PCT/AU96/00459 中所述。 15 然而管狀圓形物已知限定在某些如超音速發射器的限 定應用，但該申請人並不知道有任何管狀圓形物適合於與 可選擇之可燃性推進燃料充填物堆疊於炮身内，特別是無 任何管狀圓形物適合該所述類型的炮身總成。 20 【發明内容】 本發明希望提供用於電子控制之軍火及火器的炮身總 成，特別是該所述類型，該等炮身總成係適合於點燃管狀 的圓形物，並提供用於此一目的之管狀圓形物。 0續次頁（發明說明頁不敷使用時，請註記並使用續頁) 200409900 玖、發明說明 發明說明，續頁 依據本發明之-態樣，係提供一種該所述類型之炮身 總成，包括： 一炮身’具有一炮口； 夕數個g狀圓形物，其軸向地堆疊於該炮身中且經排 5列使之與該炮身有效的密封嗡合； 閉口元件，係插入於該等管狀圓形物之間，用以在該 等管狀圓形物的兩者之間產生有效的炮身閉合；以及 一可選擇之可燃性推進燃料，充填於每一圓形物且為 可燃性的’用以經由該炮身的炮口推進一鄰接的前置圓形 ίο 物及所結合的閉合元件。 儘管可由推進燃料所間隔開，該等管狀圓形物較佳仍 以鄰接的關係堆疊。較佳為各個圓形物包括一管狀體，該 管狀體具有至少與其後端所結合之一閉合元件。 該閉合元件可作用以閉合該後端圓形物的前置端。任 15擇地，個別的閉合元件可用於各個圓形物的前置端及後端 ，以提供後端的閉合使在其中之該充填物的點燃無效，可 使推進該前導端圓形物離開炮身的燃燒有效。 該閉合元件可經排列由該管狀體拋棄或固定至該前置 管狀體。該管狀圓形物可藉由航空動力學的方式來安裝以 20具有所欲的飛行特性。當該管狀體隨著一可拋棄的閉合元· 件一起使用時，該管狀體内面的型式，可作用於順著該飛 行路徑的方向來維持該圓形物的軸向對準。任擇地，該管 狀體可由加重一端使其重於另一端來增加重量。 该閉合元件係為一適當地夾在相鄰管狀體部分之間的 0續次頁（發明說明頁不敷使用時，請註記並使用續頁） 玖、發明說明 發明說明續頁 閉合壁構件。各個閉合壁構件可延伸並與該炮身密封地嚅 合。任擇地，該管狀圓形物可具有彼此緊靠或置於相鄰之 互補的外端壁部分，且該閉合壁構件被夾在内端壁部分之 間。 在之前的排列中，該閉合壁構件可夾在相鄰之管狀圓 形物的端面之間。該閉合壁構件係可為在操作狀態下不變 形的一種型態。任擇地，該該閉合壁構件的周邊部分經形 成使之在相鄰的管狀圓形物之間向外延伸，藉由端面所施 的軸向擠壓成為與該炮身有效的密封嚅合。對於低壓的施 加，此類對於造成與該炮身緊密封嚅合的變形並非無法避 免的。 該等鄰接的管狀圓形物之端面可徑向延伸至炮身，或 該等相鄰管狀圓形物之端面可在該夾著之閉合壁構件的周 邊部分上形成各自互補之楔型表面的嚅合。 鄰接之圓形物的管狀體可彼此重疊以在相鄰圓形物之 間提供一套疊的嚅合。為此目的，該圓形物可包括與鄰接 之圓形物的内端壁部分重疊的外端壁部分，且該閉合壁構 件可被夾在該套疊圓形物之内互補端壁面之間。 若為所欲’鄰接之圓形物的套疊部分可包括一薄壁部 分，其可向外延伸與任一相鄰之套疊圓形物部分中成為密 封喃δ，使之避免推進燃料的漏出而進入炮身内或是吹漏 至該鄰接的推進燃料充填物内。任擇地，此該向外的延伸 可為外表套疊的部分以加強被點燃的圓形物與該炮身的密 封嗜合。 0續次頁（發明說明頁不敷使用時，請註記並使用續頁） 200409900 玖、發明說明 發明說明，續頁 各個夾在中間的閉合壁構件亦可經排列由對著其前面 之推進燃料充填物壓力的反作用，以密封該後端圓形物的 端面，防止在該鄰接之後圓形物内之充填物的吹漏燃燒。 此反作用密封亦可發生在該圓形物的緊鄰端面部分之間及 5 /或該前面的圓形物與閉合壁構件之間。 該推進燃料充填物的燃燒可如吾人先前的國際申請案 中所述。為此目的，各個選擇性可燃性推進燃料充填物可 包括一電啟動引爆器，該引爆器連接至一對間隔的環狀接 點，該等接點延伸至該圓形物周圍且與通過該炮身而伸出 10 之各個的電接點接觸並且適當地與電子控制元件結合。 該閉合元件可與該圓形物整合，且可包括可移動的壁 節或可延伸的壁，該等閉合元件可一閉合姿態向前為一開 放姿態且為與炮身實質上相符的姿態。當在該閉合姿態時 ，該等壁節可對一前置端之推進燃料充填物的燃燒行反作 15用力來維持或是加強該閉合元件的閉合效果。 在裝載入該炮身之前，先準備有其推進燃料充填物之 適當的各個圓形物，若為所欲，可藉由連續地裝載具有一 開口之則置端的圓形管狀體來裝載，該圓形管狀體的開口 端在推進燃料充填物充填後閉合，其可為個別操作或放入 20下一個圓形管狀體所在之位置而得。 在另一態樣，本發明係屬於一種圓形物，其可從軍火 或火器的炮身總成發射，該圓形物包括： 一開放端之官狀體，適合用以載入至該炮身總成之一 的炮身内，用以與該炮身有效密封嚙合； 0續次頁（發明說明頁不敷使用時，請註記並使用續頁） 200409900 玖、發明說明 發明說明續頁 一閉合壁構件，適合插入至該管狀體及一鄰近圓形物 的管狀體之間，用以在圓形物之間產生有效炮的身閉合； 以及 一可選擇之可燃性推進燃料充填物，位於該相鄰圓形 5 物之管狀體内，該推進燃料充填物係具可燃性以用於推進 該圓形物的管狀體通過該炮身之炮口處。 圖式簡單說明 為了使本發明易於了解並施行，例示本發明之典型罝 10 體實施例之所附圖式將作為參考，其中： 第1A至1D圖概略地說明本發明與其操作模式之一形 式的一部分； 第2A至2D圖概略地說明本發明與其操作模式之另一 具體實施例的一部份； 15 第3圖係一透視圖，說明在第2A至2D圖中所示之實 施例的一圓形物； 第4圖概略說明本發明另一種形式的一部份；以及 第5圖仍為本發明之另一形式之一部分的概略說明。 20 【實施方式】 較佳實施例之詳細說明 在第1A i 1D圖中所示的實施例中，該炮身總成 具有多數個圓形物U，該圓形物u以軸向鄰接的關係堆 疊於該炮身内，並且使這些圓形物適以經電子點燃或是依 0續次頁（發明說明頁不敷使用時，請註記並使用續苜） 9 一 玖、發明說明 發明說明續頁 序以其他方式點燃，如在該發明人之早期國際申請案中所 述或習知技術已知者。 各個圓形物11包含一管狀體13，該管狀體13結合有 一炮身閉合構# 14 ’該炮身閉合構件14配置於各相鄰管 狀體13a 13b、13C及i3d之間並使其彼此分隔開，該管 10 15 狀體13且與排列在_閉合構件14之後的—推進燃料充填 物15相結合。例如，該推進燃料充填物…係維持於個別 之炮身閉合構件14a與14b間之一後端管狀體现的内部 。在該實_中’另—推進燃料充料15d係包含於該炮 身總成10的-後延伸部16，用以推進最後之管狀體咖。 牡乐1A圖中可見到各個200409900 发明, description of the invention (the description of the invention should state: the technical field, prior art, content, embodiments, and drawings of the invention) I: the technical field of the inventor 3 Field of the invention The present invention relates to arms and firearm. The present invention is a special, but not exclusively, application for a gun body assembly having a plurality of rounds and 5 non-connectable alternative combustible propulsion fuels which are axially stacked on The gun body is used to continuously propel the round objects through the muzzle of the gun body. These artillery body assemblies will be referred to hereinafter as "the type" 0 10 [PRIOR ART] BACKGROUND OF THE INVENTION The present invention relates to artillery body assemblies for arms and firearms, and in particular the type described, as described earlier by the present invention International patent applications PCT / AU94 / 00124 and PCT / AU96 / 00459 filed by the author. 15 However, tubular rounds are known to be limited to certain limited applications such as supersonic launchers, but the applicant is not aware of any tubular rounds that are suitable for stacking within the gun body with an optional combustible fuel charge , Especially without any tubular round body suitable for this type of gun body assembly. [Summary of the Invention] The present invention hopes to provide gun body assemblies for electronically controlled arms and firearms, in particular of the type described, such gun body assemblies are suitable for igniting tubular round objects and provide for A tubular round object for this purpose. 0 Continued pages (Please note and use the continuation page when the invention description page is insufficient.) 200409900 玖 The invention description, the continuation page is based on the aspect of the present invention, which provides a gun body assembly of the type described. Including: a gun body 'with a muzzle; several g-shaped circular objects, which are axially stacked in the gun body and arranged in 5 rows to effectively seal and hum with the gun body; Is inserted between the tubular circular objects to produce an effective gun body closure between the tubular circular objects; and an optional flammable propulsion fuel is filled in each circular It is flammable and is used to propel an adjacent front circular object and the combined closing element through the muzzle of the gun body. Although spaced by the propulsion fuel, the tubular rounds are preferably still stacked in a contiguous relationship. Preferably each circular object comprises a tubular body having at least one closure element coupled to its rear end. The closing element is operable to close the leading end of the rear end round. Optionally, individual closing elements can be used for the front and rear ends of each round to provide closing of the back end to invalidate the ignition of the filling therein, and to advance the leading end round off the gun. The body burns effectively. The closure element may be arranged to be discarded from the tubular body or fixed to the front tubular body. The circular tube can be installed by aerodynamics to have the desired flight characteristics. When the tubular body is used with a disposable closure element, the inner shape of the tubular body can be used to maintain the axial alignment of the circular object along the direction of the flight path. Alternatively, the tubular body may be increased in weight by weighting one end so that it is heavier than the other end. This closing element is a 0-sequence page that is properly sandwiched between adjacent tubular body parts (note that the invention description page is insufficient, please note and use the continuation page) 发明 Description of the invention Description of the invention Continuation page Closed wall member. Each closed wall member may extend and sealably engage the gun body. Alternatively, the tubular rounds may have complementary outer end wall portions abutting or placed adjacent to each other, and the closed wall member is sandwiched between the inner end wall portions. In the previous arrangement, the closed wall member could be sandwiched between the end faces of adjacent tubular rounds. The closed wall member may be a type that does not deform in an operating state. Optionally, the peripheral portion of the closed wall member is formed so as to extend outward between adjacent tubular circular objects, and is axially squeezed by the end face to form an effective seal with the gun body. . For the application of low pressure, this type of deformation is not inevitable to cause a tight seal with the gun body. The end faces of the adjacent tubular circular members may extend radially to the gun body, or the end faces of the adjacent tubular circular members may form respective complementary wedge-shaped surfaces on the peripheral portion of the sandwiched closed wall member. Mingle. The tubular bodies of adjacent circles may overlap each other to provide a set of overlapping joints between adjacent circles. For this purpose, the circle may include an outer end wall portion overlapping an inner end wall portion of an adjacent circle, and the closed wall member may be sandwiched between complementary end wall surfaces within the nested circle. . If the nested part of the circular object is desired, it may include a thin-walled part, which can be extended outward to become a seal δ in any adjacent nested circular part, so as to prevent the fuel from advancing. It leaks into the gun body or blows into the adjacent propulsion fuel charge. Optionally, this outward extension may be a telescoped part to enhance the sealing attachment of the ignited round object to the gun body. 0 Continued pages (Please note and use the continuation pages when the invention description page is not enough.) 200409900 玖, description of the invention description, the closed-wall members sandwiched between the continuation pages can also be arranged by the propulsion fuel facing the front. The reaction of the pressure of the filling material seals the end surface of the rear round object and prevents the burning of the filling material in the round object after the abutment. This reaction sealing may also occur between the immediately adjacent end portions of the circle and / or between the front circle and the closed wall member. The combustion of this propulsion fuel charge may be as described in my previous international application. To this end, each of the selectively flammable propulsion fuel fillers may include an electrically activated detonator connected to a pair of spaced-apart annular contacts that extend around the circle and pass through the The electrical contacts of each gun projecting out of the 10 are in contact and are suitably combined with electronic control elements. The closure element may be integrated with the circular object, and may include movable wall sections or extendable walls. The closure elements may have a closed posture forward to an open posture and a posture substantially consistent with the gun body. When in the closed attitude, the wall sections can react to the combustion of the propulsion fuel charge at a forward end 15 to maintain or enhance the closing effect of the closing element. Before loading the gun body, prepare appropriate rounds for its fuel advancement, if desired, by continuously loading a round tubular body with an open end, The open end of the circular tubular body is closed after the fuel filler is filled, and it can be obtained by individual operation or by placing the position of the next circular tubular body. In another aspect, the invention belongs to a circular object that can be launched from a gun body assembly of a munition or firearm. The circular object includes: an open-ended official body suitable for loading into the gun The inside of the gun body, which is one of the body assemblies, is used for effective sealing engagement with the gun body; 0 Continued pages (When the description page of the invention is insufficient, please note and use the continued page) 200409900 A wall member adapted to be inserted between the tubular body and a tubular body adjacent to the circular object to generate an effective gun body closure between the circular objects; and an optional flammable propulsion fuel filler located at the The propulsion fuel filling is flammable for the tubular body of the adjacent circular five objects to pass through the muzzle of the gun body. Brief Description of the Drawings In order to make the present invention easy to understand and implement, the drawings illustrating a typical embodiment of the present invention will be referred to, in which: Figures 1A to 1D schematically illustrate one form of the present invention and its operation mode Figures 2A to 2D schematically illustrate a part of another specific embodiment of the present invention and its operation mode; 15 Figure 3 is a perspective view illustrating the embodiment shown in Figures 2A to 2D A circular object; FIG. 4 schematically illustrates a part of another form of the present invention; and FIG. 5 is still a schematic description of a part of another form of the present invention. 20 [Embodiment] Detailed description of the preferred embodiment In the embodiment shown in Figures 1A i 1D, the gun body assembly has a plurality of circular objects U, and the circular objects u are axially adjacent to each other. Stack in the gun body, and make these rounds suitable for electronic ignition or follow the 0 pages (if the description page is not enough, please note and use the alfalfa) 9 I. Description of the invention Continued page The sequence is ignited in other ways, as described in the inventor's earlier international applications or known in the art. Each circular object 11 includes a tubular body 13 combined with a gun body closing structure # 14 'The gun body closing member 14 is disposed between each adjacent tubular body 13a 13b, 13C, and i3d and separates them from each other. Separately, the tube 10 15 is shaped like a body 13 and is combined with a propulsion fuel filler 15 arranged behind the closing member 14. For example, the propulsion fuel charge ... is maintained inside the tubular-shaped interior of one of the rear ends of the individual gun body closing members 14a and 14b. In this embodiment, the other-propelled fuel charge 15d is included in the rear extension 16 of the gun body assembly 10 to propel the final tubular body coffee. You can see each
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J*rfq A ^ ,MV 内且向後延伸以形成—局部圓錐端面19。該局部圓錐端面 與-互補的局部圓錐表面22配合，該局部圓錐表面22大 約形成於該炮相合構件14之外表後端厢的部分，如第 :B圖所示。另一互補的局部圓錐的前置面23大約形成於 該閉合構件14的外表邊緣，如第lc @所示1另—互補 的局部圓錐的前置面23係與-縮回面24結合以提供一凹 處25 ’該凹處25收納了各個管狀體13之互補形 壁26 〇 2〇 將可見到該後端壁26向内縮回，而該管狀體13的其 餘部分係為固定的管狀部分，然而若為所欲，其可形成為 一細腰管形狀以通過該管狀體13。 ” 如第1B圖所示之從該炮身之該管狀體13的點燃期間 ，該縮回壁部分26係由該閉合構件24所抓住。'曰 _次頁(画說明頁不敷使鱗，請_並使麵頁） 10〆 5 玖、發明說明 Γ翻說 圖所述’在飛行期間該閉合構件14從該管狀 原因在於炮身12内所提供的膛線導致該管狀體13的旋轉 ’或如第1D圖所述，在飛行期間與該管狀體13保持在一 起。為此目的，該閉合構件14可藉螺針、鎖接、朦合、衝 模或其他所需者來固著至該管狀體13。 10 使用時，該炮身總成10係與該圓形物u堆疊，其中 一個中空管㈣i3a係為前置發射器。當前置的推進燃料 純物15a在下-個相鄰管狀體⑶内點燃時，所造成的 乱體堡力將對包圍著已點燃的推進燃料充填物之前置端以 及後端的閉合構件14a、14b兩者之中作用。該氣體壓力的 作用造成前置閉合構件14a與該前置體13a由該炮身_ 進。同時該氣體壓力將迫使該後端閉合構彳14b與該後端 體13b —起成為軸向壓縮，致使該後端體之部分圓錐端面 19的徑向延伸。 此排列將把該後端主體13b之前置環狀端18插入至該 炮身12使之成密封銜接，並且把該閉合構件丨仆插入使之 與忒部分圓錐端面19成密封銜接，確保沒有任何漏出的燃 燒氣體進入下一個後端充填物15b的推進燃料中。之後如 第1B圖所示之中空體13b，其可藉由在下一個後端體nc 20中之推進燃料15b的點火而從該炮身總成1〇推進。 在弟2 A圖至第2D圖所示之炮身總成的具體實施例中 ’各個圓形物30皆具有一管狀體部分31，該管狀主體部 分31提供有向外會合的壁節33，該壁節33係緊靠或重疊 以形成該管狀體31的各自閉合。當該圓形物3〇係沿著一 0續次頁（發明說明頁不敷使用時，請註記並使用續頁） 11 玖、發明說明 炮身36的長度來配置時 之中心陷入部分35。 發明說明續頁 這些壁節33提供一個互相緊鄰 "卩的k佳型式係如第3圖所示_相對成對的節， 虽置於炮身36之中時，該壁節33係置於具有緊靠之端壁 39的主體延伸部38之間。 忒刖置壁即33打開以沿著炮身36置於包含在該圓形 物30之内的推進燃料37上。推進燃料的燃燒也推進該前 置圓幵/物30 ’如帛2A 1|内部分所示。此作用可供形成下 個刚置圓形物3G與在該炮身中實質上為管狀的體3 i， 該主體由-串閉合的壁節33僅在其後端關閉，該壁節％ 向後分叉以提供-陷入部分35，如第2B圖所示。該陷入 部分35緊靠下一個鄰接後端圓形物3〇之該向分又的壁節 33之前所形成的陷入部分35。 當下一個鄰接後端圓形物3〇中的推進燃料37點火時 ，該前置壁節33將打開使燃燒氣體的壓力在該前置主體 31之後知之壁郎33的後端面接觸，且因此從炮身推進 該主體。在此作用中，下一個主體則準備點燃。 該壁節係可任擇為多數個實質上為三角形的壁節，其 具有配置在該主體31周圍的基部以及向内延伸以形成一角 錐形的閉合。 若為所欲，後端的閉合壁節33可藉由樞接元件32結 合至該管狀本體31，由於空氣壓力通過該管狀本體31，該 壁節在離開炮身之後隨即打開，如第2D圖所示。若為所 欲，這些壁節33可供飛行或穩定該本體31之飛行的發射 0續次頁（發明說明頁不敷使用時，請註記並使用續頁） 12 20040990° 玖、發明說明 發明說明，續頁 件’或若有必要可使其旋轉。 由上述可知，由推動該前置本體31之推進燃料燃燒所 造成的高壓，係作用於後端圓形物的後部，對其施壓使之 靠緊下一個圓形物的前置端，以及藉由下一個圓形物中之 5推進燃料的點火密封以抵抗不欲的氣流，因此確保該火氣 以所欲的發射速率來持續操作。 在操作中，5亥炮身閉合構件1 4係可自由浮動且為一拋 棄段，若從一步搶炮身發射可藉由該管狀圓形物的旋轉而 分離，或在飛行期間藉由空氣壓力而分離。藉由該拋棄段 10 ，該圓形物用於從飛機發射或用於嚅合進入的飛彈，如船 隻自我防禦的領域，等等相當長排的嚅合時，可具有改善 的氣體動力學表現。 然而，在某些應用上，將該閉合構件14固定至管狀 主體31上可能優點。例如，經閉合的圓形物可由許多炮身 15發射來燃對抗一埋藏的地雷。此一圓形物接著將泥土挖進 孩主體31中並且將其從該地雷位置拿開。由於該圓形物上 之圓形物的動態衝擊，其效果可為泥土之一般干擾的額外 作用。從多炮身所發射的多圓形物因此具有提供使埋藏的 地雷曝露及/或是無效之改良工具的潛力。 '〇 當圓形物堆疊於一炮身中時，其係彼此接觸，且明確 地洛在其預期的位置上。實際上，該圓形物利用其為發射 器本身數倍的一彈藥盒。 第4圖所示之炮身總成4〇中表示在其前置端或搶口顯 示切掉部分的炮身4卜故只顯示最後的二圓形物42及43 S?4 0續次頁（發明說明頁不敷使用時，請註記並使用續頁） 13〆 玖、發明說明 發明說明續頁 月J置圓形物（未表示）已從該炮身發射。可見到在此實 ②例中乂，圓形物42及43連同該後端圓形物43的外前置端 P 44係為堆豐的，其中該圓形物Μ係沿伸至中圓形物 之内後端部45。 所有^面部分係圓錐形，各自與互補的外端面部分46 及47彼此末端鄰接’且該内端面48及49係以彼此間隔的 關係終止並與閉合壁面構件5〇為鄰接之關係。 該閉合壁面 構件包含括一亦具有一部分圓錐狀之端面％的周圍部分 52。在此實施例中，該套疊壁面部分44及45係相對較長 10且兩者之一在另一之中形成係為密閉配合。 在别置圓形物（未表示）之發射期間的使用中，推進燃 料的壓力對著包含已點燃之推進燃料之中間圓形物42的閉 合壁面構件5G作用。此係為對著後端圓形物43之互補内 端表面部分49 ’使得壁面構件50之末端表面54推進。在 15刖置圓形物離去期間，壓力係以此作用在後端圓形物43之 前置端47及49上，且迫使中間發射器42向外及向内將後 端表面46楔合前置外部表面47造成它們之間的密封。該 向外的壓力亦擴張後端圓形物43之前置外部末端部分44 的前置端51使之與炮身41嚅合。 20 内面48及49亦與閉合壁面構件5〇之周圍部分％模 合為密封嚷合，避免後端圓形物43因推進燃料的燃燒而漏 氣。再者，推進燃料壓力將傾向於擴張中間圓形物42之内 部後端部分45而與後端圓形物43之外部前置端部分44緊 密嚅合使得炮身41之洩漏降至最低。 0續次頁（發明說明頁不敷使用時，請註記並使用續頁） 14 200409900 玖、發明說明 發明說明，續頁 如所述，一引子55係位於各具選擇性之可燃的推進燃 料充填物56之内，且與沿著圓形物42及43之外部周圍隔 開的正負集電環狀接點57及58相連。該炮身41提供有伸 入炮身内之對應位置的彈簧接點53及59 ,產生與接觸環 5 57及58各有一接點。 適當的電子控制器供作為啟動該引子以及燃燒推進燃 料充填物56。如第3圖所示，這些周圍接點57及58係適 合利用在所有例示的圓形物。 第5圖所示之炮身總成6〇係類似於第4圖所示的實施 10例’差別在於炮身64内所提供之圓形物61以及環狀外圍 部分63為顛倒的。那是在第4圖實施例中，圓形物42及 43具有一向内縮減的内壁，而圓形物61的内壁62從頭到 尾的大部分長度為固定直徑接著向外擴張。相信此安排將 提供更兩程度的氣動結構，但是相較第4圖的實施例有較 15 低的密封。 工業應用 本發明之炮身總成及管狀圓形物可用於小型武器上， 但可想像的是它們將更適合於直徑為2〇mm以上的圓形物 。將可見到的是各炮身閉合可與鄰接之管狀圓形物之前置 環狀端配合，藉由迫使該環狀端向外使之與炮身的孔接觸 以及與該炮身或前置環狀端楔合炮身閉成為密封嚅合，或 者藉由使該閉合構件與該管狀圓形物的部分圓錐之内端楔 合成為緊密密封而無明顯之與該炮身之前置端成為嚅合的 0續次頁（發明說明頁不敷使用時，請註記並使用續頁） 15 200409900 玖、發明說明 發明說明續頁 擴張。 此楔合可由維持相對陡峭的楔合角度來獲得，此係有 效地藉由該壁合之向後移動停止於在密閉於該閉合及該管 狀圓形物之間的一點來提供前置端的停止，但須在該管狀 5 圓形物的前置端徑向發生擴張之前。任擇地，該前置端可 充份堅固形成，在藉由來自於前置圓形物之推進力之楔合 作用的影響下以抵抗向外展開。此一密封作用係更適合於 低壓力、低炮口速度的應用。 當所述為在一炮身内原位置處所提供的堆疊的圓形物 10 時，該圓形物亦可以常見的手段分別從一外部彈藥盒供應 至一武器。為此目的，一圓形物可包括 適合固定於該圓 形物之閉合壁以及用於保護該圓形物中之推進燃料的軟 填料閉合或其相似物。 本發明之利用開放式之管狀圓形物的炮身總成亦可用 15於從水面下的位置，如從船艦、潛艇、或如突破防紫設施 的隱藏式陸地基地，予以點燃。例如，潛艇可利用此類炮 身總成來行自我防禦、水面下水雷破壞或是反魚雷或飛彈 活動。 當然，將可瞭解的是上述僅為本發明所例示的實施例 2〇 ’且對於熟悉此技術者而言’變得顯而易知的修飾及變化 將視為落入以下申請專利範圍中所提出之本發明的主要範 圍及領域。 【囷式簡單說明】 0續次頁（翻國頁不雖用時，請註記並删續頁) 16 200409900 玖、發明說明 發明說明續頁 第1A至1D圖概略地說明本發明與其操作模式之一形 式的一部分； 第2A至2D圖概略地說明本發明與其操作模式之另一 具體實施例的一部份； 第3圖係一透視圖，說明在第2A至2D圖中所示之實 施例的一圓形物； 第4圖概略說明本發明另一種形式的一部份；以及 第5圖仍為本發明之另一形式之一部分的概略說明。 10 【囷式之主要元件代表符號表】 10炮身總成 25 15a推進燃料充填物 11圓形物 15b推進燃料充填物 12炮身 15c推進燃料充填物 13管狀體 15 13a管狀體 13b管狀體 13c管狀體 13d管狀體 14 閉合構件 20 14a閉合構件 14b閉合構件 14c閉合構件 14d閉合構件 15 推進燃料充填物 15d推進燃料充填物 16 ♦延伸部 30 18*環狀端 19·圓錐端面 22*圓錐表面 23 ♦前置面 24 *縮回面 35 25 *凹處 26·後端壁 3(L·圓形物 31 ·管狀主體部分 0續次頁（發明說明頁不敷使用時，請註記並使用續頁) 200409900 玖 32* 33 ♦ 35， 36, 37 ♦ 38* 39* 40. 41 * 42* 43 * 44 ♦ 45 ♦ 46* 47 * 48* 、發明說明 發明說明 才區接兀件 50·閉合壁面構件 壁節 51+前置端 陷入部分 52·周圍部分 炮身 53*彈簧接點 推進燃料 54*端面 主體延伸部 55*引子 端壁 56«推進燃料充填物 炮身總成 57«接觸環 炮身 58*接觸環 圓形物 59*彈簧接點 圓形物 6Cl·炮身總成 前置端部 6L·圓形物 後端部 62·内壁 外端面部分 63·環狀外圍部分 外端面部分 64*炮身 内端面 49 *内端面^ η · 4 ^ 71A. J * rfq A ^, MV extends inward and backward to form a partial conical end face 19. The local conical end surface cooperates with a -complementary local conical surface 22, which is formed approximately at the outer rear end of the gun joint member 14, as shown in Fig.: B. Another complementary partial conical front surface 23 is formed approximately at the outer edge of the closing member 14 as shown in lc @ 1 1—The complementary partial conical front surface 23 is combined with the retracted surface 24 to provide A recess 25 'This recess 25 houses the complementary wall 26 of each tubular body 13 and it will be seen that the rear wall 26 retracts inward, while the rest of the tubular body 13 is a fixed tubular portion However, if desired, it can be formed into a thin waist tube shape to pass through the tubular body 13. As shown in Figure 1B, during the ignition of the tubular body 13 from the gun body, the retracted wall portion 26 is grasped by the closing member 24. ' Please make the page) 10〆5 玖, the description of the invention Γ said that the 'close member 14 from the tube during flight is caused by the rifling provided in the gun body 12 causing the tube 13 to rotate' Or as shown in Figure 1D, held together with the tubular body 13 during flight. To this end, the closure member 14 may be secured to the by means of a screw pin, a lock, a closure, a die or other required. Tubular body 13. 10 In use, the gun body assembly 10 series is stacked with the circular object u, one of which is a hollow tube ㈣i3a is a front launcher. The current propulsion fuel pure 15a is under the next adjacent tube When it is ignited in the body ⑶, the resulting chaotic force will act on the closed members 14a, 14b that surround the front end and the rear end of the ignited propulsion fuel filling. The effect of this gas pressure causes the front The closing member 14a and the front body 13a are advanced by the gun body. At the same time, the gas pressure will force The rear-end closed structure 彳 14b and the rear-end body 13b together become axial compression, resulting in a radial extension of a part of the conical end face 19 of the rear-end body. This arrangement will place the rear-end body 13b forward of the annular end. 18 is inserted into the gun body 12 so as to form a sealed connection, and the closing member is inserted so as to form a sealed connection with the conical end surface 19 of the cymbal to ensure that no leakage of combustion gas enters the next rear-end filling 15b. In the fuel, as shown in FIG. 1B, the hollow body 13b can then be advanced from the gun body assembly 10 by the ignition of the propulsion fuel 15b in the next rear body nc 20. In FIG. 2A to In the specific embodiment of the gun body assembly shown in FIG. 2D, each circular object 30 has a tubular body portion 31. The tubular body portion 31 is provided with a wall section 33 that meets outward, and the wall section 33 is fastened. Lean or overlap to form the respective closures of the tubular body 31. When the circular object 30 is continued along the next page (the description page of the invention is insufficient, please note and use the continued page) 11 When the length of the body 36 is configured, the center sinks into the portion 35. 发明 说Continuing, these wall sections 33 provide a "k" type system which is next to each other as shown in Fig. 3_ Relatively paired sections. Although placed in the gun body 36, the wall section 33 Leaning against the main body extension 38 of the end wall 39. The set-up wall, ie 33, opens to rest along the gun body 36 on the propulsion fuel 37 contained within the circular body 30. The combustion of the propulsion fuel also advances the The front round 幵 / 物 30 'is shown in the inner part of 帛 2A 1 |. This effect can be used to form the next rigid round 3G and the body 3 i which is substantially tubular in the gun body. The main body consists of- The string closed wall section 33 is closed only at its rear end, and this wall section is bifurcated rearward to provide the sinking section 35, as shown in FIG. 2B. The sinking portion 35 is immediately adjacent to the sinking portion 35 formed immediately before the reciprocating wall portion 33 adjacent to the rear end round 30. When the next propulsion fuel 37 adjacent to the rear end round body 30 is ignited, the front wall section 33 will be opened so that the pressure of the combustion gas comes into contact with the rear end face of the wall man 33 behind the front body 31, and therefore from The gun body propelled the subject. In this role, the next subject is ready to ignite. The wall joint system may optionally be a plurality of substantially triangular wall joints having a base portion arranged around the main body 31 and a closure extending inwardly to form a pyramid. If desired, the closed wall section 33 at the rear end can be coupled to the tubular body 31 by a pivoting element 32. Due to the air pressure passing through the tubular body 31, the wall section opens immediately after leaving the gun body, as shown in FIG. 2D Show. If desired, these wall sections 33 can be used to launch or stabilize the flight of the body 31. 0 Continued pages (Notes on the use of continuation pages are insufficient, please note and use the continuation pages) 12 20040990 ° , Continuations' or rotate it if necessary. From the above, it can be known that the high pressure caused by the combustion of the propelling fuel of the front body 31 acts on the rear part of the rear round object, and presses it against the front end of the next round object, and The ignition seal of the fuel is advanced by 5 of the next round to resist unwanted airflow, thus ensuring that the fire gas continues to operate at the desired emission rate. In operation, the 5 Hai gun body closing member 1 4 is freely floating and is an abandonment segment. If the gun body is fired from one step, it can be separated by the rotation of the tubular circular object, or by air pressure during flight. And separated. With the abandonment section 10, the round object is used for launching from an aircraft or for coupling incoming missiles, such as in the field of self-defense of ships, etc., and can have improved aerodynamic performance when it is coupled in a relatively long row . However, in certain applications, fixing the closure member 14 to the tubular body 31 may be advantageous. For example, a closed circle can be fired by a number of gun bodies 15 to ignite a buried mine. This circular object then digs dirt into the child body 31 and removes it from the mine site. Due to the dynamic impact of the circular object on the circular object, the effect can be an additional effect of the general interference of the soil. The multiple rounds fired from multiple gun bodies therefore have the potential to provide improved tools for exposing and / or ineffective buried mines. '〇 When the rounds are stacked in a gun body, they are in contact with each other and are clearly in their intended position. In effect, the round uses a cartridge that is several times the launcher itself. The gun body assembly 40 shown in FIG. 4 indicates that the cut-out part of the gun body is displayed on its front end or grab. Therefore, only the last two round objects 42 and 43 are displayed. (When the description page of the invention is insufficient, please note and use the continuation page.) 13〆 玖. Description of the invention The continued page of the description of the invention. A circular object (not shown) has been launched from the gun body. It can be seen that in this example ②, the circular objects 42 and 43 together with the outer front end P 44 of the rear circular object 43 are piled, and the circular object M extends along the middle circle.物 内 内 后部 45。 The inner rear end portion 45. All of the face portions are conical, each of which is complementary to the complementary outer end surface portions 46 and 47 at their ends, and the inner end surfaces 48 and 49 terminate in a spaced relationship and abut the closed wall member 50. The closed wall surface member includes a peripheral portion 52 which also has a part of a conical end face%. In this embodiment, the telescoping wall surface portions 44 and 45 are relatively long 10 and one of them forms a tight fit in the other. During use during the launch of a separate circular object (not shown), the pressure of the propulsion fuel acts on the closed wall member 5G of the intermediate circular object 42 containing the ignited propulsion fuel. This is because the complementary inner end surface portion 49 'of the rear end circular object 43 advances the end surface 54 of the wall member 50. During the departure of the 15-shaped circular object, the pressure is applied to the front-mounted ends 47 and 49 of the rear-end circular object 43 and forces the middle launcher 42 to wedge the rear-end surface 46 outwardly and inwardly. The front exterior surface 47 creates a seal between them. This outward pressure also expands the front end 51 of the front-side outer end portion 44 of the rear-end circular object 43 to fit the gun body 41. 20 The inner surfaces 48 and 49 are also molded tightly with the surrounding parts of the closed wall surface member 50 to prevent leakage of air from the rear end 43 due to the combustion of the propulsion fuel. Furthermore, the propulsion fuel pressure will tend to expand the inner rear end portion 45 of the middle circle 42 and closely fit the outer front end portion 44 of the rear circle 43 to minimize the leakage of the gun body 41. 0 Continued pages (please note and use continuation pages when the invention description page is not enough) 14 200409900 玖, description of invention description, continuation page, as mentioned, a primer 55 is located in each of the optional flammable propulsion fuel filling Within the object 56 and connected to the positive and negative collector ring contacts 57 and 58 spaced along the outer periphery of the circular objects 42 and 43. The gun body 41 is provided with spring contacts 53 and 59 projecting into corresponding positions in the gun body, each of which has a contact with the contact ring 5 57 and 58. A suitable electronic controller is provided to actuate the primer and burn the propulsion fuel charge 56. As shown in Fig. 3, these peripheral contacts 57 and 58 are suitable for use in all illustrated circular objects. The gun body assembly 60 shown in Fig. 5 is similar to the embodiment shown in Fig. 10. The difference is that the round 61 provided in the gun body 64 and the ring-shaped peripheral portion 63 are reversed. That is, in the embodiment of Fig. 4, the circular objects 42 and 43 have an inner wall that shrinks inward, and the inner wall 62 of the circular object 61 has a fixed length from the beginning to the end and then expands outward. It is believed that this arrangement will provide a greater degree of aerodynamic construction, but with a lower seal than the embodiment of FIG. 4. Industrial Application The gun body assembly and the tubular round object of the present invention can be used for small arms, but it is conceivable that they will be more suitable for round objects with a diameter of 20 mm or more. It will be seen that each gun body is closed to cooperate with the anterior annular end of the adjacent tubular circular object, by forcing the annular end outward to make contact with the hole of the gun body and with the gun body or front The ring-end wedge gun body is closed to form a tight coupling, or by closing the closure member with the inner end wedge of a part of the circular cone of the tubular circle to form a tight seal without apparently becoming the front end of the gun body. Coupled 0 continuation pages (Notes and use of continuation pages when the invention description page is not enough) 15 200409900 玖. The invention description extension page continues. This wedging can be obtained by maintaining a relatively steep wedging angle, which effectively provides a stop at the leading end by the wall's backward movement stopping at a point enclosed between the closure and the tubular circle, But before the front end of the tubular 5-round body expands radially. Optionally, the leading end may be formed sufficiently firmly to resist outward expansion under the influence of wedging action by the propulsive force from the leading circular object. This sealing effect is more suitable for low pressure and low muzzle speed applications. When the stacked rounds 10 are provided at the original position in a gun body, the rounds can also be supplied to an weapon from an external ammunition box by common means, respectively. For this purpose, a circle may include a closed wall adapted to be fixed to the circle and a soft filler closure or the like for protecting the propulsion fuel in the circle. The gun body assembly using the open tubular round object of the present invention can also be used for igniting from a position below the water surface, such as from a ship, a submarine, or a hidden land base such as a breakthrough purple-proof facility. For example, submarines can use such gun body assemblies for self-defense, surface mine damage, or anti-torpedo or missile activities. Of course, it will be understood that the modifications and changes described above, which are merely examples of the present invention, and which become obvious to those skilled in the art, will be deemed to fall within the scope of the following patent applications. The main scope and field of the invention proposed. [Simplified description of the formula] 0 Continued pages (note when the page is not used, please note and delete the continuation page) 16 200409900 玖 Description of the invention Description of the invention Continued pages 1A to 1D Figures schematically illustrate the present invention and its operation mode A part of a form; Figures 2A to 2D schematically illustrate a part of another specific embodiment of the present invention and its operation mode; Figure 3 is a perspective view illustrating the embodiment shown in Figures 2A to 2D FIG. 4 schematically illustrates a part of another form of the present invention; and FIG. 5 is still a schematic description of another part of the form of the present invention. 10 [Representative symbols for main components of the style] 10 gun body assembly 25 15a propulsion fuel filling 11 round 15b propulsion fuel filling 12 gun body 15c propulsion fuel filling 13 tubular body 15 13a tubular body 13b tubular body 13c Tubular body 13d Tubular body 14 Closing member 20 14a Closing member 14b Closing member 14c Closing member 14d Closing member 15 Propulsion fuel filling 15d Propulsion fuel filling 16 ♦ Extension 30 18 * Ring end 19 · Conical end surface 22 * Conical surface 23 ♦ Front face 24 * Retracted face 35 25 * Recession 26 · Rear wall 3 (L · Circle 31 · Tubular body part 0 Continued pages (If the description page of the invention is insufficient, please note and use the continued pages ) 200409900 玖 32 * 33 ♦ 35, 36, 37 ♦ 38 * 39 * 40. 41 * 42 * 43 * 44 ♦ 45 ♦ 46 * 47 * 48 *, invention description, invention description, interface member 50, closed wall member Wall section 51 + Front end sinking part 52 · Surrounding part of the gun body 53 * Spring contact propelling fuel 54 * End body extension 55 * Introduction end wall 56``Propulsion fuel filling gun body assembly 57''Contact ring gun body 58 * Contact ring round 59 * Spring contact circle 6Cl-barrel cartridge was front-end portion of the rear end portion thereof a circular 6L · 62 · inner wall of the outer end portion of an outer peripheral annular portion 63 · end surface of the body portion end surface 64 * 49 * gun inner end surface