1292029 玫、發明說明 (發明說钥應敘明：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）1292029 Rose, invention description (invention said that the key should be stated: the technical field, prior art, content, implementation and drawings of the invention)
【發明所屬^^技術領域；J 發明領域 本舍明係有關於軍火以及火斋。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 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。 1292029 玖、發明說明 依據本發明之一態樣，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； 多數個管狀圓形物，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屬合； 閉合元件，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 10 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。 該閉合元件係為一適當地夾在相鄰管狀體部分之間的 1292029 # 91135201號專利申請案發明說明書修正頁96年4月 玖、發明說明 閉合壁構件。各個閉合壁構件可延伸並與該炮身密封地嚆 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。 5 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 轴向擠壓成為與該炮身有效的密封嚅合。對於低壓的施加 10 ’此類對於造成與該炮身緊密封嚆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 该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。 15 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，該等圓形物可包括與鄰 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 20分，其可向外延伸與任一相鄰之套疊圓形物部分中成為密 封喷a，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 封喷合。 1292029. 第91135201號專利申請案發明說明書修正頁96年4月 玖、發明說明 各個夾在中間的閉合壁構件亦可排列以對推進燃料充 填物壓力反應而抵住該閉合之前置面以密封抵住該後端圓 形物的端面以防止在該鄰接之後圓形物内之充填物的吹漏 燃燒。此反應性密封亦可發生在該圓形物的緊鄰端面部分 5 之間及/或該前置圓形物與閉合壁構件之間。 4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 開口之前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 2〇 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： 一開放端之管狀體，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喃合； 1292029 第91135201號專利申請案發明說明書修正頁96年4月 玖、發明說明 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的炮身閉合； 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，例示本發明之典型具 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 弟5圖仍為本發明之另一形式之一部分的概略說明。 20 【資施方式】 較佳實施例之詳細說明 在第1A至1D圖中所示的實施例中，該炮身總成1〇 具有多數個圓形物11，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 1292029 玖、發明說明 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 一炮身閉合構件14，該炮身閉合構件14配置於各相鄰管 5狀體13a ' 13b、13c及13d之間並使其彼此分隔開，該管 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，該推進燃料充填物丨“係維持於個別 之炮身閉合構件l4a # 14b間之一後端管狀體⑽的内部 在孩貝施例中，另一推進燃料充填物15d係包含於該炮[Technical field of invention]; Field of invention The present invention relates to arms and fire fasting. The present invention is particularly, but not exclusively, applied to a body assembly having a plurality of circular bodies and an optional combustible propellant fuel that is not axially stacked, the flammable propellant fuel system being axially stacked thereon The gun body is used to continuously advance the round objects through the muzzle of the gun body. Such a body assembly will be hereinafter, in the type described, reference to 0 10 [Prior Art] BACKGROUND OF THE INVENTION The present invention relates to artillery assemblies for arms and firearms, particularly of the type described, such as early It is described in the International Patent Application No. PCT/AU94/00124 and PCT/AU96/00459 filed by the present inventors. 15 However, tubular rounds are known to be limited to certain applications such as supersonic transmitters, but the Applicant does not know that any tubular rounds are suitable for stacking with alternative flammable propellant fuel fillers in the body. In particular, no tubular rounds are suitable for the body assembly of the type described. 20 SUMMARY OF THE INVENTION The present invention contemplates providing a body assembly for electronically controlled munitions and firearms, particularly of the type described, which is suitable for igniting tubular round objects and is provided for A tubular shape for this purpose. 1292029 A description of the invention provides a body assembly of the type described, comprising: a body having a muzzle; a plurality of tubular circular members axially stacked The body of the gun is arranged in rows 5 to be in effective sealing with the body; a closure member is inserted between the tubular circles for between the tubular bodies Generating an effective gun body closure; and an optional flammable propellant fuel filled in each of the rounds and flammable for propelling an adjacent front circular 10 through the muzzle of the gun body and The combined closure element. Preferably, the tubular circles are stacked in abutting relationship, although they may be spaced apart by the propellant fuel. Preferably, each of the circular bodies includes a tubular body having a closure element bonded to at least its rear end. The closure element can act to close the forward end of the rear end circular. Optionally, individual closure elements can be used for the front and rear ends of each of the rounds to provide closure of the rear end to disable ignition of the fill therein, allowing the leading round to exit the cannon The body is burning effectively. The closure element can be disposed from the tubular body to be discarded or secured to the front tubular body. The tubular circular shape can be mounted by aerodynamic means to have the desired flight characteristics. When the tubular body is used with a disposable closure element, the pattern of the inner surface of the tubular body acts to maintain the axial alignment of the circular body along the direction of the flight path. Optionally, the tubular body can be weighted by weighting one end to make it heavier than the other end. The closure element is suitably clamped between adjacent tubular body portions. 1292029 #91135201 Patent Application Disclosure Manuscript, April 1996 玖, Invention Description Closed wall member. Each of the closure wall members can extend and sealingly engage the body. Optionally, the tubular circular body can have an outer end wall portion that abuts or is placed adjacent to each other, and the closed wall member is sandwiched between the inner end wall portions. 5 In the previous arrangement, the closure wall member can be sandwiched between the end faces of adjacent tubular figures. The closed wall member can be a type that is invariant in an operational state. Optionally, the peripheral portion of the closure wall member is formed to extend outwardly between adjacent tubular circles, and the axial compression applied by the end faces becomes an effective sealing engagement with the body. For the application of low pressure 10 ′ such deformation is not unavoidable for causing a tight seal with the gun body. The end faces of the adjacent tubular circular objects may extend radially to the gun body, or the end faces of the adjacent tubular circular objects may form respective complementary wedge-shaped surfaces on the peripheral portion of the sandwiching closed wall members. Hehe. The tubular bodies of adjacent circular objects may overlap each other to provide a stack of twists between adjacent circular objects. For this purpose, the circular objects may include an outer end wall portion that partially overlaps an inner end wall of an adjacent circular object, and the closed wall member may be sandwiched within a complementary end wall of the nested circle between. If desired, the nested portion of the adjacent circular object may include a thin-walled portion 20 that extends outwardly from any adjacent set of circular portions to form a sealed spray a to prevent advancement. The fuel leaks out into the gun body or blows into the adjacent propellant fuel fill. Optionally, the outward extension may be an outer telescoping portion to enhance the sealing of the ignited circular object with the body of the gun. 1292029. Patent Application No. 91,135,201, the disclosure of the specification of the invention, April 1996, the invention discloses that the respective closed wall members sandwiched in the middle may also be arranged to resist the pressure reaction of the propellant fuel filler against the closed front surface to seal The end face of the rear end round is pressed against the blow-by combustion of the fill within the round after the abutment. This reactive seal can also occur between the immediately adjacent end face portions 5 of the circular body and/or between the front circular member and the closed wall member. 4 Propelling the fuel filling can be as described in our previous international application. To this end, each of the selective flammable propellant fuel fillers can include an electrically activated detonator coupled to a pair of spaced apart annular contacts that extend around and through the circular object The gun body is in contact with the electrical contacts of each of the 10 and is suitably combined with the electronic control unit. The closure element can be integral with the circular object and can include a movable wall section or an extendable wall that can be forwardly in a closed position and in a posture that substantially conforms to the barrel. When in the closed position, the wall segments can exert a force on the combustion of the propellant fuel fill at a forward end to maintain or enhance the closing effect of the closure member. Before loading into the body, prepare appropriate circular objects for propelling the fuel filler, if desired, by continuously loading a circular tubular body having an open front end, The open end of the circular tubular body is closed after the propellant fuel fill is filled, which may be obtained by individual operation or by placing the next circular tubular body at a position. In another aspect, the invention is a circular object that can be fired from a body assembly of an munition or firearm, the circular body comprising: an open end tubular body adapted to be loaded into the body The body of one of the assemblies is used to effectively seal the body with the body; 1292029 Patent Application No. 91135201, the amendment to the specification of the invention, April 1996, the invention discloses a closed wall member suitable for insertion into the tubular body and Between a tubular body adjacent to the circular object for creating an effective body closure between the circular objects; and an optional flammable propellant fuel filler located within the tubular body of the adjacent circular body The propellant fuel filler is flammable for advancing the tubular body of the circular body through the muzzle of the gun body. BRIEF DESCRIPTION OF THE DRAWINGS In order to make the present invention easy to understand and practice, the exemplary embodiments of the present invention will be described with reference to the drawings, wherein: FIGS. 1A to 1D schematically illustrate one form of the present invention and its mode of operation. Part 2A to 2D schematically illustrate a portion of another embodiment of the present invention and its mode of operation; 15 Figure 3 is a perspective view illustrating the embodiment shown in Figures 2A through 2D A circular shape; Figure 4 schematically illustrates a portion of another form of the invention; and Figure 5 is still a schematic illustration of one portion of another form of the invention. 20] The detailed description of the preferred embodiment In the embodiment shown in FIGS. 1A to 1D, the gun body assembly 1 has a plurality of circular bodies 11 which are axially oriented. Adjacent relationships are stacked within the body of the gun, and the circular objects are adapted to be ignited by electrons or otherwise ignited in accordance with the instructions of the invention, as described in the inventor's earlier international application. Known by technology. Each of the circular bodies 11 includes a tubular body 13 which is coupled with a body closing member 14 which is disposed between adjacent pipe-like bodies 13a' 13b, 13c and 13d and Separate from each other, the tubular body 13 is combined with the propellant fuel filler 15 arranged behind the closure member 14. For example, the propellant fuel filler "is maintained inside the rear end tubular body (10) of one of the individual body closing members l4a #14b. In the case of the child, another propellant fuel filler 15d is included in the gun.
10身、％成/0 # -後延伸部16，用以推進最後之管狀體H 在第1A圖中可見到各個管狀體13之前環狀端向 内且向後延伸以形成_局部圓錐端面19。該局部圓錐端面 與一互補的局部圓錐表面22配合，該局部圓錐表面22大 約形成於該炮身閉合構件14之外表後端周圍的部分，如第 15 1B圖所不。另_互補的局部圓錐的前置面u大約形成於 該閉合構件14的外表邊緣，如第lc圖所示。該另_互補 的局4圓錐的河置面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之壁27之形 狀的後端部分26。 夕 20 /將可見到該壁27向内縮回，而該管狀體13的其餘部 刀:為口疋的官狀部分，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。 ;^第1B圖所示之從該炮身之該管狀體13的點燃期間 口亥縮回壁部分26係由該閉合構件24所抓住。如第lc 10 1292029 第91135201號專利申請案發明說明書修正頁％年4月 玖、發明說明 圖所述，在飛行期間該閉合構件14從該管狀體13拋出， 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可藉螺釘、銷接、膠合、衝 5模或其他所需者來固著至該管狀體13。 使用時，該炮身總成1〇係與該圓形物丨丨堆疊，其中 個中空管狀體13a係為前置發射體。當前置的推進燃料 充填物15a在下一個相鄰管狀體13b内點燃時，所造成的 亂體壓力將對包圍著已點燃的推進燃料充填物之前置端以 1〇及後端的閉合構件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12推 進。同時該氣體壓力將迫使該後端閉合構件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。 15 此排列將把該後端主體13b之前置環狀端18插入至該 丈〇身12使之成也、封銜接，並且把該閉合構件1 插入使之 與該部分圓錐端面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圖所不之中空體13b，其可藉由在下一個後端體i3c 20中之推進燃料15b的點火而從該炮身總成1〇推進。 在第2A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提供有向外會合的閉合節33，該節33係緊靠或重疊 以形成该官狀體31各自的閉合件。當該圓形物3〇係沿著 11 1292029 91135201號專利申請案發明說明書修正頁％年4月 玖、發明說明 紀身36的長度來配置時，這些節％提供一個互相緊鄰 之中心陷入部分3 5。 節33的較佳型式係如第3圖所示一相對成對的節，當 置於炮身36之中時，該節33係置於具有緊靠之端壁39的 5 主體延伸部38之間。 該前置節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 圓形物30，如第2A圖内部分所示。此作用可供形成下一 個丽置圓形物30與在該炮身中實質上為管狀的體31，該 10主體由一串閉合節33僅在其後端關閉，該壁節33向後分 叉以&仏卩曰入部分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3〇之該前置的節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 15 ，該前置的節33將打開使燃燒氣體的壓力在該前置主體 31之後端之節33的後端面接觸，且因此從炮身36推進該 主體。在此作用中，下一個主體則準備點燃。 該等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 2〇 錐形的閉合件。 右為所欲，後端的閉合郎3 3可藉由極接元件3 2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 ，這些郎3 3可供飛行或穩定該本體31之飛行的發射件， 12 1292029 發明說明書修正頁96年4月 第91135201號專利申請案 玫、發明說明 或若有必要可使其旋轉。 5 10 可去由推動該前置本體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-個圓形物的前置端，以及藉由下一個圓形物中之 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^中，該炮相合構件14係可自由浮動且為一抛 ” k V才层炮身發射可藉由該管狀圓形物的旋轉而 或在氣行期間藉由空氣壓力而分離。藉由該抛棄段 ’該圓形物用於從飛機發射或用㈣合進入的飛彈，如船 隻自我防禦的領域，等等相當長排㈣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 «亥主體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。 2〇 #圓形物堆疊於-炮身中時，其係彼此接觸，且明確 地落在其預期的位置上。實際上，該圓形物利用其為發射 體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，故只顯示最後的二圓形物42及43 13 1292029 第91135201说專利申請案發明說明書修正頁％年*月 玖、發明說明 刖置圓形物(未表示)已從該炮身發射。可見到在此實 施例中，圓形物42及43連同該後端圓形物43的外前置端 部44係為堆疊的，其中該圓形物43係沿伸至中圓形物43 之内後端部45。 所有鳊面邻为係圓錐形，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％為鄰接之關係。該閉合壁面 構件包含括-亦具有一部分圓錐狀之端面54的周圍部分 52在此貝施例中，該套疊壁面部分44及係相對較長 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£力對著包含已點燃之推進燃料之中間圓形物Μ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 b前置圓形物離去期間，壓力係以此作用在後端圓形物^之 前置端47及49上，且迫使中間發射體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。 〇 内面48及49亦與閉合壁面構件50之周圍部分52楔 合為岔封嚅合，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之外部前置端部分料緊 密屬合使得炮身41之洩漏降至最低。 14 1292029^ 第91135201號專利申請案發明說明書修正頁96年4月 玖、發明說明 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 1〇例，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 提供更鬲私度的軋動結構，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_以上的圓形物 20。將可見到的是各炮身閉合件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腫徑 ^觸以及與該炮身或前置環狀端楔合炮身閉合件成為密封 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 15 第91135201號專利申請案發明說明書修正頁96年4月 玖、發明說明 為嚅合的擴張。 此楔合可由維持相對陡峭的楔合角度來獲得，此係有 效地藉由該閉合件之向後移動停止於在密閉於該閉合件及 該管狀圓形物之間的一點來提供前置端的停止，但須在該 5管狀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 物之後端的閉合壁以及用於保護該圓形物中之推進燃料的 軟填料閉合件或其相似物。 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、或如突破防禦設施 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。 【圖式簡單說明】 16 1292029 玖、發明說明 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； 5 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 【圖式之主要元件代表符號表】 10炮身總成 11圓形物 12炮身 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 25 15a推進燃料充填物 15b推進燃料充填物 15c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 後端部分 27 壁 3 0圓形物 17 1292029 玖 、發明說明 31 管狀主體部分 25 50 32 才區接兀件 51 33 Λ-/Γ 即 52 35 陷入部分 53 36 炮身 54 37 推進燃料 30 55 38 主體延伸部 56 39 端壁 57 40 炮身總成 58 41 炮身 59 42 圓形物 35 60 43 圓形物 61 44 前置端部 62 45 後端部 63 46 外端面部分 64 47 外端面部分 40 48 内端面 49 内端面 閉合壁面構件 前置端 周圍部分 彈簧接點 端面 引子 推進燃料充填物 接觸環 接觸環 彈簧接點 炮身總成 圓形物 内壁 環狀外圍部分 炮身 18 2010 body, %/0# - rear extension 16 for advancing the last tubular body H. The annular end is extended inwardly and rearwardly to form a partial conical end face 19 before the respective tubular body 13 is visible in Fig. 1A. The partial conical end face cooperates with a complementary partial conical surface 22 which is formed approximately at a portion around the rear end of the outer portion of the body closure member 14, as shown in Fig. 15B. The front face u of the other complementary partial cone is formed approximately at the outer edge of the closure member 14, as shown in Figure lc. The other complementary -4 conical river surface 23 is combined with the retracted surface 24 to provide a recess 25 that receives the rear end portion 26 of the shape of the wall 27 of each tubular body 13. On the eve 20 / it will be seen that the wall 27 is retracted inwardly, while the remaining knife of the tubular body 13 is the official portion of the mouth, but if desired it can be formed into a thin waist tube shape to pass the tubular Body 13. The wall portion 26 of the tubular body 13 from the body of the gun shown in Fig. 1B is caught by the closing member 24. The closure member 14 is ejected from the tubular body 13 during flight as described in the artillery 12, as described in the revised specification page of the patent application No. 91, 135, pp. The twist line causes the rotation of the tubular body 13, or as described in Fig. 1D, to remain with the tubular body 13 during flight. For this purpose, the closure member 14 can be secured to the tubular body 13 by screws, pins, glues, punches or other requirements. In use, the body assembly 1 is stacked with the circular object, and the hollow tubular body 13a is a front emitter. When the current propellant fuel filler 15a is ignited in the next adjacent tubular body 13b, the resulting body pressure will be about the closing member 14a surrounding the front end of the ignited propellant fuel filler at 1 〇 and the rear end, 14b plays a role in both. The action of the gas pressure causes the front closing member 14a and the front body 13a to be pushed by the body 12. At the same time, the gas pressure will force the rear end closure member 14b to axially compress with the rear end body 13b, causing the radial extension of the partial conical end face 19 of the rear end body. 15 This arrangement inserts the front end end 18b of the rear end body 13b into the body 12 to be joined, and the closure member 1 is inserted to seal the portion of the conical end face 19. Ensure that no leaking combustion gases enter the propellant fuel of the next back end fill 15b. Thereafter, the hollow body 13b as shown in Fig. 1B can be advanced from the gun body assembly 1 by the ignition of the propellant fuel 15b in the next rear end body i3c 20. In the embodiment of the body assembly shown in Figures 2A through 2D, each of the circular bodies 30 has a tubular body portion 31 provided with a closed portion 33 that meets outwardly. The segments 33 are abutted or overlapped to form respective closures of the official body 31. When the circular element 3 is configured along the length of the invention manual revision page of the invention of the invention, the length of the invention is as follows: 5. The preferred version of the segment 33 is a relatively paired segment as shown in Fig. 3 which, when placed in the body 36, is placed in the body extension 38 of the body having the end wall 39 abutting between. The front section 33 is opened to be placed along the gun body 36 on the propellant fuel 37 contained within the circle 30. The combustion of the propellant fuel also advances the pre-circle 30, as shown in the interior of Figure 2A. This action serves to form the next sleek circle 30 and the body 31 which is substantially tubular in the body, the body 10 being closed by a series of closure segments 33 only at its rear end, the wall segment 33 being bifurcated backwards Break in section 35 with & as shown in Figure 2B. The trap portion 35 abuts the trap portion 35 formed before the next preceding segment 33 adjacent the rear end circular member 3''. When the next propelling fuel 37 in the next rear end circular body 3 is ignited 15, the front section 33 will open to bring the pressure of the combustion gas into contact at the rear end face of the node 33 at the rear end of the front body 31, and thus The body is advanced from the gun body 36. In this role, the next subject is ready to ignite. The nodes may optionally be a plurality of substantially triangular wall segments having a base disposed about the body 31 and a closure member extending inwardly to form an angle 2 锥形 cone. The right end is desired, the closing lang 3 3 of the rear end can be coupled to the tubular body 31 by the pole connecting member 3 2, and the wall section is opened immediately after leaving the gun body due to air pressure, as shown in FIG. 2D. Shown. If desired, these langs 3 3 can be used to fly or stabilize the launching of the flight of the body 31, 12 1292029, the specification of the invention, the patent application No. 91135201, April 1996, the invention description or, if necessary, Rotate. 5 10 The high pressure caused by the propellant fuel combustion of the front body 31 is applied to the rear portion of the rear end circular body, and is pressed against the front end of the circular object. And by the ignition seal of the propellant fuel in the next circle to resist unwanted airflow, thus ensuring that the fire gas continues to operate at the desired rate of emission. ^ In the ^, the gun-engaging member 14 is freely floatable and is a throw" k V layer gun body emission can be separated by the rotation of the tubular circle or during air travel by air pressure. From the abandonment section, the circular object is used for missiles that are launched from or with (4), such as the field of self-defense of the ship, etc., which can have improved aerodynamic performance when the long row (four) is combined. In some applications, it may be advantageous to secure the closure member 14 to the tubular body 31. For example, a closed circular object may be fired by a plurality of cannons 15 against a buried mine. This circular object then digs the soil. Into the main body 31 and remove it from the mine position. 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 circular object thus has the potential to provide an improved tool for exposing and/or ineffectively burying the mine. 2〇#When the round objects are stacked in the gun body, they are in contact with each other and fall clearly in their intended position. Above. In fact, the circle It uses an ammunition box which is several times the size of the emitter itself. The body assembly 4 shown in Fig. 4 indicates that the body of the cut-out part is displayed at the front end or the grabbing end, so only the last two circles are displayed. Shapes 42 and 43 13 1292029 Patent No. 91,135,201, the disclosure of the specification of the invention of the patent application, % year * month, invention description, the circular object (not shown) has been emitted from the gun body. It can be seen that in this embodiment, the circle The shapes 42 and 43 are stacked together with the outer front end portion 44 of the rear end circular member 43, wherein the circular body 43 extends along the inner rear end portion 45 of the middle circular object 43. Adjacent to the conical shape, each of the complementary outer end portions 46 and 47 abut one end, and the inner end faces 48 and 49 terminate in a spaced relationship with each other and are in abutting relationship with the closed wall member %. The closed wall member includes The peripheral portion 52, which also has a portion of the conical end surface 54, in this embodiment, the telescoping wall portion 44 is relatively long 10 and one of the two forms a hermetic fit in the other. Do not place a circular object (not shown) during use during launch, propelling fuel The force acts against the closed wall member 5G containing the intermediate circular object of the ignited propellant fuel. This is the complementary inner end surface portion 49 opposite the rear end circular member 43, such that the end surface of the wall member 50 54. During the departure of the b front circular object, the pressure acts on the front end ends 47 and 49 of the rear end, and forces the intermediate emitter 42 outwardly and inwardly to the rear end surface. The wedged front outer surface 47 creates a seal between them. The outward pressure also expands the front end 51 of the rear end circular portion 43 to the outer end portion 44 to engage the body 41. The inner faces 48 and 49 are also wedged with the peripheral portion 52 of the closed wall member 50 to prevent the rear end circular member 43 from leaking due to the combustion of the propellant fuel. Further, the propulsion fuel pressure will tend to expand the inner rear end portion 45 of the intermediate circular member 42 to closely engage the outer front end portion of the rear end circular member 43 to minimize leakage of the body 41. 14 1292029^ Patent Application No. 91135201, the disclosure of the specification of the invention, April 1996, the description of the invention, as described, 'a primer 55 is located within each of the selectively combustible propellant fuel fillers 56, and along the circle The positive and negative collector loop contacts 57 and 58 spaced around the outside of the shapes 42 and 43 are connected. The body 41 is provided with spring contacts 53 and 59 that extend into corresponding positions in the body to create a contact with the contact rings 5 57 and 58. A suitable electronic controller is provided for actuating the primer and burning the propellant fuel fill 56. As shown in Fig. 3, these peripheral contacts 57 and 58 are suitable for use in all of the illustrated circular objects. The barrel assembly 6 shown in Fig. 5 is similar to the embodiment shown in Fig. 4, except that the circular object 61 and the annular peripheral portion 63 provided in the barrel 64 are reversed. That is, in the embodiment of Fig. 4, the circular members 42 and 43 have an inner wall which is reduced inwardly, and the inner wall 62 of the circular body 61 has a fixed diameter from the head to the tail and then expands outward. It is believed that this arrangement will provide a more sturdy rolling structure, but has a lower seal than the embodiment of Figure 4. Industrial Applicability The can body assembly and the tubular round of the present invention can be used on small arms, but it is conceivable that they would be more suitable for a circular object 20 having a diameter of 2 〇 or more. It will be seen that each of the body closure members can engage the annular end of the adjacent tubular circular body by forcing the annular end outwardly to contact the swollen path of the body and the body. Or the front annular end wedge body seal closure becomes a seal fit or by forming the closure member into a tight seal with the inner end wedge of the partial cone of the tubular circle without significant The front end is made into the fifteenth of April, the invention is described in the specification of the invention. This wedging can be obtained by maintaining a relatively steep wedge angle, which effectively stops the stop of the front end by the rearward movement of the closure member at a point sealed between the closure member and the tubular circular object. However, it must be before the radial extension of the front end of the 5 tubular circular object. Optionally, the front end is sufficiently strong to resist outward deployment by the influence of the wedge force from the propulsion of the front circular. This sealing action is more suitable for low pressure, low muzzle speed applications. When the stacked circular objects 10 are provided at the original position within a can body, the circular objects can also be supplied from a single ammunition cartridge to a weapon by conventional means. To this end, a circle may include a closed wall adapted to be secured to the rear end of the circle and a soft filler closure or the like for protecting the propellant fuel in the circle. The can body assembly of the present invention utilizing an open tubular body can also be ignited from a subsurface location, such as from a ship, submarine, or concealed land base such as a breakout defense facility. For example, submarines can use such gun assemblies to perform self-defense, subsurface mine damage or anti-torped or missile activities. It is to be understood that the above-described embodiments are merely exemplified in the present invention, and modifications and variations that become apparent to those skilled in the art will be deemed to fall within the scope of the following claims. The main scope and field of the invention are presented. BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1A to 1D schematically illustrate a part of one form of the present invention and its operation mode; FIGS. 2A to 2D schematically illustrate another embodiment of the present invention and its operation mode. Part 3; 5 is a perspective view illustrating a circular object of the embodiment shown in Figures 2A to 2D; Figure 4 is a schematic view showing a portion of another form of the present invention; Figure 5 is still a schematic illustration of a portion of another form of the invention. 10 [Main component representative symbol table of the drawing] 10 Gun body assembly 11 circular body 12 gun body 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 Closure member 14d closure member 15 propelling fuel filler 25 15a propelling fuel filler 15b propelling fuel filler 15c propelling fuel filler 15d propelling fuel filler 16 extension 30 18 annular end 19 conical end surface 22 conical surface 23 front surface 24 Retraction surface 35 25 recess 26 rear end portion 27 wall 3 0 round object 17 1292029 玖, invention description 31 tubular body portion 25 50 32 区 兀 51 51 33 Λ-/Γ ie 52 35 immersed part 53 36 cannon Body 54 37 Propulsion fuel 30 55 38 Body extension 56 39 End wall 57 40 Gun body assembly 58 41 Gun body 59 42 Round 35 60 43 Round object 61 44 Front end 62 45 Rear end 63 46 Outside End face portion 64 47 Outer end face portion 40 48 Inner end face 49 Inner end face Closed wall member Front portion of the front end of the spring contact end Leading propulsion Fuel filling contact ring Contact ring spring Point barrel cartridge was circular inner wall peripheral portion of the annular barrel 1820