1248505 九、發明說明： 【發明所屬之技術領域】 本發明有關於一種用於、'空氣軟搶（Air Soft Gun®)夕 或、、軟空氣（Softair®)"形式之武器複製品中修正發射 物飛行軌道的裝置，其中，該等武器複製品能發射直徑約 為6mm非常質輕的塑膠圓球。更精確地說，本發明係有關 於一武器複製品中的發射器所發射之塑膠發射物的飛行軌 道之修正。該發射物飛行執道之修正可同樣在長武器複製 品和小武器複製品的垂直方向和水平方向來進行。 基本上，本發明可應用在彈簧負荷或電力長武器的領 域當中，尤其是，應用在諸如電動來福搶等長武器複製品。 尤其是，本發明可應用在武器複製品，其等發射物係 塑膠材質圓球。本發明同時可裝配在小型武器複製品。 【先前技術】 在武器複製品的領域裡，依據用於成人和/或兒童玩具 製造的目的，各種型式的武器被再製。此等武器複製品一 般係為能發射塑膠發射物（例如，塑膠圓球）而非真正武 =用之圓球或料的武m為如此，該等武器複製品通 常具有若干缺點，該等缺點來自複製品本身的製造。此等 缺：通常係存在發射系統或發射器當中，導致發射物在從 武益離開期間的偏離。例如，在離開武器之際，該等發射 物可能偏向右邊或偏向左邊，甚至向上或向下。此等缺點 實際上是不可避以’且單純是由於的製造上公差所造 1248505 成。此等缺點對來福搶形式的長“㈣ 擾，該等長武器之發射範圍較遠。事…而吕特別困 發射物所涵蓋的距離越長 ：勤應瞭解到：該 顯。 ㈣也仃軌道的偏離越明 並無施加修正於 目前，在大部分的長武器複製品裡 發射物的飛行軌道上。 但是，在現有的武器複製品的 士上你 心 知母了為备中，有用於垂 直向修正發射物飛行軌道的李在 J矛…死畀在。此系統，稱作，，躍起 (HOP UP®)，，系統，其包括一位 卜隹急 、武裔赉射裔内部的橡膠銷 釘’位在發射器中心的輸入和垂直位置。更精確地說，此 橡膠銷釘係位在-垂直轴上，該垂直軸橫過武器發射器的 中心’且位在發射器的上部份。此橡膠銷釘具有保持和定 向該發射物的功能。實際上，此橡膠銷釘或多或少可維持 由發射系系統所發射之發射物在離開武器發射器之前的方 向。該維持發射物在離開發射器之後的飛行方向的作用， 給予該發射物在離開飛行軌道上一旋轉效應。此旋轉效應 繼而造成發射物的上升，亦即，可往上修正該執道。但是， 發射物本身的重量偏移了發射物刻意上升的軌道，此在發 射物離開發射器短暫時間之後，產生一發射物水平軌道。 從上述解釋中可以瞭解到：此躍起系統僅對發射物軌 道做了垂直分量的修正。如果如此，誠如上文所述，該武 器複製品的製造缺點，將可能造成執道之垂直分量和水平 分量上偏離的缺點。 1248505 【發明内容】 本發明的目的在於精確地解決前述系統的缺點。 此目的，本發明提出一種用於修正發射物的飛行軌道之裝 置’其中，該發射物係由一電動長武器中的發射器所發射，、 :匕裝置可修正飛行軌道的垂直分量，甚至其垂直和水平分 量兩者。針對該項用途，依據本發明的裝置包括將兩橡: 錦釘對稱地設置在通過發射器中心之垂直轴的兩側。〃 更明確地5兒，本發明有關於一種用於複製品之發射 發射的發射物之飛行軌道的修正裝置，該裝置包括—第。 =’該鎖釘在發射器當中形成該發射物的一第一保持凸 射-ί t月的特斂在於·其包括一第二銷釘，該銷釘在發 射益當中形成該發射物的一第二保持凸起部；該第一和第 一銷釘對稱地安裝在通過發射器中心的垂直軸之兩側。 較佳地，發射器中的第_ 整的，因而，對該圓球的所右口！： p之高度係可調 佳化該發射精度。… u整白可進打，以便最 【實施方式】 圖1表示一電動長武琴避制口 ^ σ 跃态複製"口（例如，來福搶的複- 口口）中的發射器之一前立丨 <者綿π ϋ σ面硯圖。此電動長武器複製品 —紅¥ 及表0口，係配備有依據本發明的‘ 仃軌道修正裝置。在圖1 5亥武裔I射态的標註有符】 1。该發射器包括：一内表 ,. 才面11和一外表面1 e。此發射 1248505 係沿著其内> & , · 、面11配備有—發射器接頭2。此發射器接頭 糸由一例如是橡膠的彈性材料所構成。 點C代表該發射器的中心，亦即，表示該發射器的幾 :中心’以XX標註的垂直軸和以M標註的 幾何中心C。 為了 4 σ本發明，該發射器1配備有-發射物飛行執 、多正裝置。該裝置包括一第一銷釘3d(右銷釘）和一第二 銷釘3g(左銷釘），其等個別地形成發射器i内部的一第一 凸起部6d和-第二凸起部6g。此等銷釘心仏係對稱 地放置在垂直轴χχ之兩側，水平轴hh上方。在圖工的實 。中”亥等銷釘3d及3g係以相對於垂直軸χχ 一約4〇 。之角度而設置。 用於4等銷釘3d及3g之螺絲，可以橫過該發射器i 本身的方式’導入發射器的内部。同時，該螺絲可以橫過 發射器的支撐件和發射器之本身來被導入。在後者之實施 例中，此能夠讓m放置在武器複製品的搶托附近。 然後’發射者可輕易地調整該等凸起部的高度，同時，持 續地進行對標的之瞄準。 ' 在圖1的具體實施例中’每一銷釘3(1及3g分別包括 -螺絲4d及4g，該等螺絲4(1及4g埋入發射器的接頭2 裡頭’因巾’藉由施加在接頭上的壓力，分別形成凸起部 及6g。在此具體實施例中，該等螺絲切及紅係分別為 一調整鈕5d及5g所操控，該等調整鈕5d及5g能調整埋 入接頭2中的螺絲之高度。因此，調緊或調鬆發射器1中 1248505 的每-螺絲，將造成埋人接帛2中的凸起部體積的增加或 減小。 因此，該等凸起部之高度調整系、统係屬旋轉式的。 換句話說，每-個埋入接頭2中的螺絲之高度調整， 代表每一個凸起部之高度的調整。因此，該等凸起部6d 及可具有相同的兩度，或者具有不同的高度。 當該發射物從發射器往外發射時，每一個此等凸起部 之功能係在於或多或少地保持該發射物。此項保持能讓離 開發射器的發射物之飛行軌道被修正。具有不同凸起部高 度之功能，能讓飛行軌道的水平分量被修正。換句話說， 正因為該等凸起部的存在，所以該飛行軌道的垂直分量可 被修正° !亥等凸起部高度的差異調I ’能促使發射物的飛 行轨道之水平分量被修正’也就是，讓該發射物向左或向 右偏離。事實’當該凸起部具有一低高度時，此將降低 該發射物纟其通道内的效貞，減地，該凸起冑具有較高 的高度時，此將增加該發射物在其通道内的效應。 應該瞭解到：如果該等凸起部6d及6g具有相同的高 度時，也就是說，如果該等銷釘3d，及3g的調整鈕被等量 凋整時，則该發射物的飛行軌道之並不水平地被調整；其 飛行軌道僅在垂直平面上調整。另一方面，如果該等凸起 邛6d，6g具有不同的高度，則此將影響該發射物在水平和 垂直平面上的飛行軌道。 特別地是，如果左凸起部6g高於右凸起部6d時，則 該發射會偏向左邊。相反地，如果右凸起部6d高於左凸 1248505 起部6g，則該發射會偏向右邊。 發身:偏離的範例可參考圖2所示。更明確地說，圖2 代表-標的，其上有三種不同已發射物之彈著痕跡。 °° ★。艮跡T1顯示·该發射物之飛行軌跡僅需要在 垂直分量上做修正。因此，該左右凸起部6d及6g之高产 係相等的。 & 第二彈著痕跡T2為定向於垂直軸XX之右方。此顯示·· 右凸起部6d的高度高於該左凸起部6g之高度。 相反地，該第三彈著痕跡T3係位在垂直轴χχ的左邊。 此顯示：該左凸起部6g係大於右凸起部6d。 因此’圖2係顯示··除了垂直平面之外，一發射物的 飛灯執道亦可在水平平面上做修正，藉由造成該等凸起部 6d及6g的高度被改變。因此，應該瞭解到··整個 ^發^飛行㈣之修正，實際上能讓-發射發射物的武 裔複製品之所有缺點被修正。 一在圖3A中’-側橫剖面視圖表示依據本發明的該裝置 之-第二具體實施例。在此具體實施例中，該調整 =:為8。此銷釘8包括-塑膠材質（例如，橡勝） 的凸出件9,該凸出件9裝載在一彈性帶ι〇上面 帶例如由金屬材質所製成。藉由任何固定方二例 :彈::：或鑽孔，該凸出件9係固定在彈性帶10的末端。 二τ 10以右干長度（例如’其本身長度之—半） 固疋於一例如是金屬的控制桿u上。 破 該發射器1被製作有-孔口 13,以方便該凸出 1248505 通過。因此，該凸出件9方 66 了在孔口 13 ^保持發射者所選定 -位置。因此’該凸出件9在武器的發射器内 起部。此凸起部的古疮叮丄 凸 凸（邛的间度可由連結於彈性帶 所控制。更明確地說，該彈 工制才干11 位处 帶1 〇將凸出件9或多或少地 在上 ^3之中。為達此目的，該彈性帶1G為其固定 射者：=制：11所延伸。因此’當該控制桿11越朝發 1=時 帶10將越延伸，使得更少部份之凸 果 入“ 13之中’這將縮短該凸起部。相反地，如 果该Ui# 11越朝發”支撐件 將越放鬆，使得該凸出件9更完全地進二“，性帶10 丨卞y旯兀王地進入孔口 13之中，因 ，增大了該凸起部。當該控制桿η朝發射器！推送 大程度時，該彈性帶1 〇將放 最 …… 頂靠發射器1的外表面， 使付该凸出件9非常地進入發射 _ 最大古疳μ °的内口 Ρ，這將造成一 最大回度的凸起部，但是不會阻擋到小圓球的發射， 彈性帶的撓性可仍然讓圓球射 ‘"、 1L , 方面’當該控制桿 朝:射者作最大拉近時’該彈性帶！。將處於最 :(如圖3Α所示），這將使得該凸出件9在孔口13内做 隶大的上升，而不形成任何之凸起部。 為了=更該控制桿U的此拉近和推離的操作，該控制 ' Τ包括—槓# 12’例如，該槓桿12可為控制桿u 相對於水平轴HH 一 90。之彎折延伸。在此實施例，如圖3β ::二此損桿12穿過武器外框“中所形成的一長 藉由此槓桿12的拉近和推離，該發射者可直接作用由 1248505 凸出件9所形成之凸起部的高度。此具體實施例能讓一系 =調整該發射器内凸起部之線性高度。此一線性調整具有 此讓發射者更容易量測之優點。事實上，藉由長橢圓形孔 口 15中的槓桿12之觀察，發射者可看到該凸起部的大小， 例如’該凸起部為零、低、中、高和最高及所有中間高度。 一。圖3A和3B顯示一單一凸起部和用於此凸起部高度的 -：-調整系統。當然，應該瞭解到：如同圖2之第一具 體實施例所表示的，依據此第二具體實施例所實施之飛^ 軌道修正裝置可同時包括二對稱之凸起部，每一個凸起部# 之高度可由一獨立控制系統（包括：控制桿、彈性帶 所調整。 不管選擇那一個具體實施例，該飛行軌道修正裝置皆 係放在發射物朝外發射的隨後位置，也就 的入口處。在第-具體實施例中，該凸起部調整系= 置在武器的外部，實際上，似置在發射物被發射的位置。 在第二具體實施例中，該凸起部調整系統具有能夠被運輸 的優點’亦即’其可放置在武器一選擇的地點，例如，靠« 近發射者之位置。 在本發明之一變例中，該飛行軌道修正裝置係不可調 整的，其可配備在簡約型武器複製品上面。在此實施例， 該修正裝置包括兩個位於發射器上部及軸χχ兩側上的凸 起部。此兩凸起部6(1及6g與圖！所表示者相同，除了它 們的高度係不可調整之外。此等凸起部係以橡膠材料之半 圓球形成於發射器1内部表面上面。在此變例中，於旋轉 12 1248505 的有效期間，該圓球係比以單一凸起 實施例被更失_ vu保持该囫球的已知 ：# J 後可略微移向發射轴的左邊戎右 邊。此裝置能縮減 次右 著較佳的群聚效應 連續發射期間該彈 在另外-變例，該等凸起部6行及6g在發 面的位置係可調整的。此變例表示二| 、 置包括-固定例之凸起部，且該修正裝 疋隹表射為I之上的調整鈕16， 6d及^系等距的。該發射器（或包括二、兩凸起二 的該部份）係可自由地旋轉，所以n 之發射益 射器1繞著發射器支推件7來枢轉，°因°此6能使發 部⑼及6g相對於轴χχ來移^ ’可將該等凸起 此發射器部份或整體的 左邊，皆能讓笋射1 不^疋向軸的右邊或 二;=Γ 軌道偏向…右邊或左邊 水丨夕止疾句蛞說5此發射薄夕计Μ 道的水平分量之修正。 D成轉’可進行圓球飛行軌 【圖式簡單說明】 圖1表不依據本路明的^ 施例 。 〜〜仃軌道修正裝置的一具體實 圖2表示一標的，盆盈一· 炎裝置的不同調整，所莽 *據本發明的飛行軌道修 圖3A和3” 乂 該等發射物的撞擊痕跡。 圖3A和3B表不依據 第二具體實施例。 1爪仃執道修正裝置的一 13 1248505 圖4表示依據本發明的該飛行軌道修正裝置的一變 例0 【主要元件符號說明】 C 發射器中心 HH 水平軸 XX 垂直軸 T1 第一彈著痕跡 T2 第二彈著痕跡 T3 第三彈著痕跡 1 武器發射器 1 e 外表面 li 内表面 2 發射器接頭 3d 第一銷釘（右銷釘） 3g 第二銷釘（左銷釘） 4d、 4g 螺絲 5d、 5g 調整鈕 6d 第一凸起部 6g 第二凸起部 7 支撐件 8 調整銷釘 9 凸出件 10 彈性帶1248505 IX. Description of the invention: [Technical field to which the invention pertains] The present invention relates to a correction for a copy of a weapon in the form of 'Air Soft Gun®, Softair®, Softair®" A device for launching a flight orbit, wherein the replica of the weapon is capable of emitting a very lightweight plastic ball having a diameter of about 6 mm. More specifically, the present invention relates to the correction of the flight path of a plastic projectile emitted by a transmitter in a weapon replica. The correction of the missile's flight command can also be made in the vertical and horizontal directions of long weapon replicas and small arms replicas. Basically, the present invention can be applied to the field of spring load or long electric weapons, and in particular, to long weapons replicas such as electric blessings. In particular, the present invention can be applied to a replica of a weapon such as a plastic ball. The invention can also be assembled on small arms replicas. [Prior Art] In the field of weapons replicas, various types of weapons are reworked for the purpose of manufacturing adult and/or children's toys. Such weapons replicas are generally such that they can emit plastic propellants (for example, plastic spheres) rather than the actual ball or material used for such weapons. Such weapons replicas usually have several disadvantages, such shortcomings. From the manufacture of the replica itself. These shortcomings are usually present in the launch system or transmitter, causing the projectile to deviate during its departure from Wuyi. For example, when leaving the weapon, the emissions may be biased to the right or to the left, even up or down. These shortcomings are in fact unavoidable and are simply due to the manufacturing tolerances of 1248505. These shortcomings are long (4) disturbances in the form of the rifle, and the launching range of the long-range weapons is far away. The longer the distance covered by Lu’s particularly sleepy missiles: the diligent should know: the obvious. The more clearly the deviation of the orbit is, the correction is made at present, in the flight orbit of the projectile in most of the long-arm replicas. However, in the existing weapons replicas, you know that the mother is in the middle, and it is used for Vertically correcting the missile's flight orbiting Li in the J spear...dead. This system, called, the hop (HOP UP®), the system, which includes a rubber inside the 隹 、, 武 赉 裔 裔The pin 'is in the input and vertical position of the center of the transmitter. More precisely, the rubber pin is tied to the vertical axis that traverses the center of the weapon launcher and is located in the upper portion of the transmitter. The rubber pin has the function of holding and orienting the emitter. In fact, the rubber pin more or less maintains the direction of the emission emitted by the launch system before exiting the weapon launcher. The sustain emitter exits the launch Device The effect of the direction of flight, giving the projectile a rotational effect on the flight path. This rotation effect in turn causes the launcher to rise, that is, the command can be corrected upwards. However, the weight of the projectile itself is offset. A deliberately rising orbit of the projectile, which produces a horizontal horizon of the projectile after a short time has elapsed from the launcher. It is understood from the above explanation that the hopping system only corrects the vertical component of the projectile orbit. As described above, the manufacturing defects of the weapon replica may cause a disadvantage of deviation between the vertical component and the horizontal component of the obstinence. 1248505 SUMMARY OF THE INVENTION The object of the present invention is to accurately solve the disadvantages of the aforementioned system. OBJECTS OF THE INVENTION The present invention provides a device for correcting a flight path of an object of a project, wherein the object is emitted by an emitter in an electric long weapon, and the device can correct the vertical component of the flight orbit, even vertical. And horizontal components. For this purpose, the device according to the invention comprises two ruins: brocade symmetry Provided on both sides of the vertical axis passing through the center of the emitter. 〃 More specifically, the present invention relates to a correction device for a flight orbit of a launch of a replica, the device comprising -. The pin forms a first retention embossing of the emitter in the emitter - the inclusion of a second pin that forms a second retention projection of the emitter during the transmission benefit The first and first pins are symmetrically mounted on either side of the vertical axis passing through the center of the emitter. Preferably, the first in the emitter, and thus the right port of the sphere!: The height of p can be adjusted to improve the accuracy of the transmission.... u can be put into white, so that the most [implementation] Figure 1 shows an electric long martial arts avoidance mouth ^ σ transcript copy "" (for example, Laifu Grab the complex - one of the emitters in the mouth before the 丨 者 绵 π ϋ σ σ surface map. This electric long weapon replica - red ¥ and table 0 is equipped with a '仃 track correction device according to the present invention. In Figure 5, the mark of the Wuwu I morphism is characterized by 1. The transmitter includes: an inner surface, a face 11 and an outer surface 1 e. This launch 1248505 is equipped with a transmitter connector 2 along its inside >& The transmitter connector is constructed of an elastomeric material such as rubber. Point C represents the center of the emitter, i.e., represents the vertical axis of the emitter: center XX, and the geometric center C labeled M. For the present invention, the transmitter 1 is equipped with a - launcher flight control, multiple positive devices. The apparatus includes a first pin 3d (right pin) and a second pin 3g (left pin) which individually form a first boss portion 6d and a second boss portion 6g inside the emitter i. These pins are placed symmetrically on either side of the vertical axis and above the horizontal axis hh. In the actual work of the map. The "3" and "3g" pins are set at an angle of about 4 inches with respect to the vertical axis. The screws for the 4d pins 3d and 3g can be introduced into the transmitter in a manner transverse to the emitter i itself. At the same time, the screw can be introduced across the support of the launcher and the launcher itself. In the latter embodiment, this allows m to be placed near the grab of the weapon replica. Then the 'transmitter can The height of the raised portions is easily adjusted, and at the same time, the aiming of the target is continuously performed. 'In the specific embodiment of Fig. 1, 'each pin 3 (1 and 3g respectively include - screws 4d and 4g, respectively) 4 (1 and 4g are embedded in the connector 2 of the transmitter, and the protrusions and 6g are respectively formed by the pressure applied to the joint by the towel. In this embodiment, the screw and the red are respectively Controlled by an adjustment knob 5d and 5g, the adjustment knobs 5d and 5g can adjust the height of the screw embedded in the joint 2. Therefore, tightening or loosening each screw of the 1248505 in the transmitter 1 will result in a buried connection. The increase or decrease in the volume of the boss in 帛2. Therefore, the convex The height adjustment system of the part is a rotary type. In other words, the height adjustment of each screw in the buried joint 2 represents the adjustment of the height of each convex portion. Therefore, the convex portions 6d And may have the same two degrees, or have different heights. When the emitter is emitted from the emitter, each of the bosses functions to hold the emitter more or less. The flight path of the projectile leaving the launcher is corrected. The function of the height of the different bosses allows the horizontal component of the flight track to be corrected. In other words, because of the presence of the bosses, the flight track The vertical component can be corrected by the difference in the height of the convex portion such as hai, which can cause the horizontal component of the flight orbit of the projectile to be corrected 'that is, let the projectile deviate to the left or right. When the raised portion has a low height, this will reduce the effect of the projectile within its channel, which, when it has a higher height, will increase the effect of the projectile within its channel. Should understand To: if the raised portions 6d and 6g have the same height, that is, if the pins 3d and 3g of the adjusting buttons are equalized, the flying orbit of the projectile is not horizontal The ground is adjusted; its flight orbit is adjusted only in a vertical plane. On the other hand, if the raised ridges 6d, 6g have different heights, this will affect the flight orbit of the projectile in horizontal and vertical planes. Ground, if the left raised portion 6g is higher than the right raised portion 6d, the emission will be biased to the left. Conversely, if the right raised portion 6d is higher than the left raised 122855 starting portion 6g, the emission will be biased to the right. The departure: an example of deviation can be seen in Figure 2. More specifically, Figure 2 represents the - mark with three different projectiles on it. ° ° ★. Trace T1 shows · the launcher The flight trajectory only needs to be corrected on the vertical component. Therefore, the high-production systems of the left and right boss portions 6d and 6g are equal. & The second impact mark T2 is oriented to the right of the vertical axis XX. This display·· the height of the right convex portion 6d is higher than the height of the left convex portion 6g. Conversely, the third impact mark T3 is located to the left of the vertical axis χχ. This display shows that the left convex portion 6g is larger than the right convex portion 6d. Therefore, Fig. 2 shows that in addition to the vertical plane, the flying lamp of an object can be corrected in the horizontal plane by causing the heights of the projections 6d and 6g to be changed. Therefore, it should be understood that the entire amendment to the flight (4) can actually correct all the shortcomings of the corpusic replica of the launching object. A side cross-sectional view in Fig. 3A shows a second embodiment of the apparatus in accordance with the present invention. In this particular embodiment, the adjustment =: is 8. This pin 8 comprises a projecting member 9 of a plastic material (e.g., rubber) which is loaded on an elastic band ι. The belt is made of, for example, a metal material. The projecting member 9 is fixed to the end of the elastic band 10 by any of the two fixing methods: bomb::: or drilling. The two τ 10 is fixed to a control rod u such as a metal with a right dry length (e.g., a half of its own length). The emitter 1 is made with an orifice 13 to facilitate the passage of the projection 1248505. Therefore, the projection 9 is held at the orifice 13 ^ to maintain the position selected by the emitter. Thus the projection 9 starts in the launcher of the weapon. The convexity of the convex portion of the convex portion (the degree of the ridge can be controlled by the elastic band. More specifically, the elastic system is 11 points with 1 〇 will protrude 9 more or less In the above ^3. For this purpose, the elastic band 1G is its fixed shooter: = system: 11 extension. Therefore 'when the control rod 11 is toward the hair 1 = the band 10 will extend more, making A small part of the convex into the "13" will shorten the raised portion. Conversely, if the Ui #11 is more toward the hair, the support will be more relaxed, so that the protruding member 9 is more completely into the second" , the band 10 丨卞 y 旯兀 旯兀 旯兀 , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , ...... against the outer surface of the emitter 1, so that the projection 9 is very entangled into the inner Ρ of the launch _ max 疳 μ °, which will result in a maximum degree of bulge, but will not block The launch of the small ball, the flexibility of the elastic band can still let the ball shoot '", 1L, the aspect 'when the control rod is facing the maximum of the shooter' Will be at the most: (as shown in Fig. 3A), which will cause the protruding member 9 to make a large rise in the orifice 13 without forming any protrusions. The operation of zooming in and pushing off, the control 'Τ includes - bar # 12', for example, the lever 12 can be bent and extended with respect to the horizontal axis HH - 90. In this embodiment, as shown in Fig. 3β: 2: The length of the damage rod 12 passing through the outer frame of the weapon is “pulled by the lever 12 and the pusher can directly act on the height of the protrusion formed by the 1248505 projecting member 9. This embodiment enables a system to adjust the linear height of the raised portion of the emitter. This linear adjustment has the advantage of making it easier for the emitter to measure. In fact, by the oblong opening 15 The observation of the lever 12 allows the launcher to see the size of the raised portion, such as 'the raised portion is zero, low, medium, high and highest and all intermediate heights. 1. Figures 3A and 3B show a single bump And the -:-adjustment system for the height of the bulge. Of course, it should be understood that: as the first concrete figure of Figure 2 For example, the flying rail correction device implemented according to the second embodiment can simultaneously include two symmetric convex portions, and the height of each convex portion # can be controlled by an independent control system (including: control lever, elasticity) The belt is adjusted. Regardless of which embodiment is selected, the flight path correction device is placed at a subsequent location where the projectile is emitted outwardly, that is, at the entrance. In the first embodiment, the boss adjustment system = placed outside the weapon, in fact, placed where the projectile is fired. In a second embodiment, the boss adjustment system has the advantage of being able to be transported, ie it can be placed in a weapon The location chosen, for example, by « near the launcher's location. In a variation of the invention, the flight path correction device is not adjustable and can be provided on a compact weapon replica. In this embodiment, the correction device includes two projections on the upper portion of the emitter and on both sides of the shaft. The two raised portions 6 (1 and 6g are the same as those shown in Fig. 3 except that their heights are not adjustable. These raised portions are formed on the inner surface of the emitter 1 by a semi-spherical ball of rubber material. In this variant, during the period of rotation 12 1248505, the ball is more lost than the single raised embodiment. The known ball: _ vu can be slightly moved to the left of the launch axis. The device can reduce the secondary right and the better clustering effect during the continuous emission of the bomb in another variant, the positions of the protrusions 6 and 6g in the hair surface are adjustable. This variant represents two | And the protrusions of the fixing example are arranged, and the adjustment knobs 16 , 6d and ^ above the correction device are equidistant. The emitter (or the second or the two protrusions 2) Partially) is free to rotate, so the launching prosthesis 1 of n pivots around the launcher 7 and the 6 can move the hairs (9) and 6g relative to the axis. The protrusions of the emitter part or the left side of the whole can make the bamboo shoots 1 not to the right or the right of the axis; = Γ track bias... The side or the left side of the water 丨 止 止 蛞 蛞 蛞 此 此 此 此 此 此 此 此 此 此 此 此 此 此 此 此 此 此 此 此 此 此 此 此 此 此 此 此 此 此 此 此 此 此 此 此 此 此 此 此^ Example. A specific actual figure 2 of the ~~仃 orbit correction device indicates a different adjustment of the target, the basin-expanding device, and the flying orbit according to the present invention. 3A and 3" 3A and 3B are not according to the second embodiment. 1 13 1248505 of the claw correction device FIG. 4 shows a modification 0 of the flight track correction device according to the present invention. 】 C emitter center HH horizontal axis XX vertical axis T1 first impact mark T2 second impact mark T3 third bullet trace 1 weapon launcher 1 e outer surface li inner surface 2 transmitter joint 3d first pin (right Pin) 3g second pin (left pin) 4d, 4g screw 5d, 5g adjustment button 6d first boss 6g second boss 7 support 8 adjustment pin 9 projection 10 elastic band
14 1248505 11 控制桿 12 槓桿 13 孔口 14 武器外框 15 長圓形孔口 16 調整鈕14 1248505 11 Joystick 12 Lever 13 Hole 14 Weapon frame 15 Oblong aperture 16 Adjustment button