經濟部中央揉準局貝工消費合作社印製 A7 ___B7___五、發明説明（1 ) 本發明是有關一種保護目標物之方法，尤指船體，其 發射放射線，特別是指红外線，以防止飛彈之攻擊，此飛 彈配備有聰明自動導向彈頭，尤指具掃描、影像，相關能 力及/或頻譜濾波自動導向之彈頭，尤其是紅外線自動導向 彈頭，其中受攻擊之目標物從發射器上發射一燃燒投射機 構，該投射機構可點火而發出紅外線，其紅外線發射能力 優於原受攻擊目標物，此物體可在導向彈頭之導向區附近 點火並分散，因此形成假目標物雲。 此一方法中物體，如S-船艦（SIC)在某種環境下可受到 充分之保護，以防止受到配備有红外線導向彈頭之飛彈攻 擊，此方法乃基於德國專利申請案34 21 734 A1,及歐洲 專利0 240 819 B1。該文應用下列方法開發導向彈頭的功 能，該導向彈頭含光學裝置，其有相當大的開孔角度（在捜 尋剛開始時），通常其範圍距物體為約10到15公里，因此例 如可覆蓋的捜尋區域在方位角（azimuth)方向約3000至5000 公尺，在佃角（elevation)方向約300至500公尺。辨識物體 後，在飛彈持績飛行期間，自動彈向彈頭鎖住物體，因此 稱之為”鎖定（lock-on)”。此時，自動導向彈頭之光學裝置 的視角在方位角及佃角方向大大地消除。在5到8公里的範 圍内，通常可確定目標物鎖定。此時由自動導向彈頭之搜 尋窗口所覆蓋的區域，其方位角方向約100公尺，且仰角方 向約50公尺。當飛彈持缠飛行直至撞擊之前此區域漸次縮 小。然後在距目標物中心40至50公尺處，約船體上方20至 3〇公尺處，形成红外線靶體雲以分散飛彈之鎖定能力，但 此時靶體雲仍為红外線自動導向彈頭的光學裝置之視角之 已消除角度所補獲。因此靶體雲的紅外線輻射能力必需甚 (請先閲讀背面之注意事項再填寫本頁)Printed by A7 ___B7___ of the Shellfish Consumer Cooperative of the Central Bureau of the Ministry of Economic Affairs. 5. Description of the Invention (1) The present invention relates to a method for protecting a target, especially a hull, which emits radiation, especially infrared rays, to prevent missiles. Attack, this missile is equipped with a smart auto-guided warhead, especially a warhead with scanning, imaging, related capabilities and / or spectral filtering auto-direction, especially an infrared auto-guided warhead, in which the attacked target is launched from the launcher. Combustion projection mechanism. The projection mechanism can ignite and emit infrared rays. Its infrared emission ability is better than the original target. This object can ignite and disperse near the guide area of the guide warhead, thus forming a cloud of fake targets. In this method, objects such as S-ships (SIC) can be fully protected under certain circumstances from being attacked by missiles equipped with infrared-guided warheads. This method is based on German patent application 34 21 734 A1, and European patent 0 240 819 B1. This article uses the following methods to develop the function of a guide warhead. The guide warhead contains an optical device, which has a relatively large opening angle (at the beginning of the search), and usually has a range of about 10 to 15 kilometers from the object. The search area covered is about 3000 to 5000 meters in the azimuth direction and about 300 to 500 meters in the elevation direction. After the object is identified, during the missile's sustained flight, it automatically locks the object towards the warhead, so it is called “lock-on”. At this time, the angle of view of the optical device that automatically guides the warhead is largely eliminated in the azimuth and corner directions. Within a range of 5 to 8 km, the target can usually be determined to be locked. At this time, the area covered by the search window of the automatic guided warhead has an azimuth direction of about 100 meters and an elevation angle of about 50 meters. This area gradually shrinks as the missile flies until it strikes. Then at a distance of 40 to 50 meters from the center of the target, about 20 to 30 meters above the hull, an infrared target cloud was formed to disperse the missile's locking ability, but at this time, the target cloud was still an infrared automatic guided warhead. The angle of view of the optical device is supplemented by the eliminated angle. Therefore, the infrared radiation of the target cloud must be very strong (please read the precautions on the back before filling this page)
本紙張尺度適用中國國家標準（CNS ) A4規格（210X297公釐） 經濟部中央標準局貝工消費合作杜印装 396133 A7 B7 五、發明説明（2 ) 高於實際物體。 但是傳統方法的缺點為移轉效應中，於靶體雲發射及 點火期間並沒有保護能力。因此在點火位置及有效位置期 間建立一空間距離，在此距離内對於自動導向飛彈彈頭視 域内之靶體定位存在急迫性需求，待別是在鎖定之後的誘 使情狀中，否則無法實現必需之移轉效應。 德國專利申請案33 26 884 C2中提出一方法，該方法 為在點火後的一段短時間内，投射體發展出一熱噴蓀，而 達成紅外線範圍内的遮蔽效應。因此，此為一種遮蔽方法 或一雲蓀幕方法，在此方法中自動彈向彈頭（可鎖定目標物 者）無法導向目標物。 在德國專利258 538及德國申請案10 96 805及34 21 734 A1中提出一種殼體，可在飛行的有效紅外線範圍内發 射能量，但是在其間無法看到自動導向飛彈之移轉效應。 因此，本案之目的偽提出一種有效改進靶體的方法， 而使得鎖定目攘物的自動導向飛彈可從目標物中移轉至靶 體。 在此改進方法中，一發射機構定位在投射體上，當投 射體發射時啓動此放射機構，此放射機構從對應的往後之 靶體上放射能量，在發射之後至靶體，待別是紅外線靶體 建立之前，此放射機構發射能量。 因此可假設此放射機構持纊放射能量。 本發明中的放射機構依時脈形式放射。 本發明亦提供一投射體，此投射體依一暫時的空間移 轉發射，且啓動相對應的放射機構且隨後點火，而致投射 機構發散而成為一串連績的新靶髏雲，持別是紅外線靶體 本紙張尺度適用中國國家標準（CNS ) A4規格（210X297公釐） I. ^^1· m 1^1 n HI In ι^ϋ. In In m ,/n. (請先閲讀背面之注意事項再填寫本頁) 經濟部中央標準局員工消费合作社印装 396133 at B7 五、發明説明（3 ) 雲，此靶體雲乃是從前一靶體雲中發展出來，這些導體雲 由相對於自動導向飛彈的能量發射尾端連接。 本發明的發射機構包含一煙火製造組件，例如氣體産 生器、一發光組件或一火箭引擎。 本發明係基於一項驚人的認知，卽持缠決定性地改進 已知方法的防禦效禦，其中暫時性的靶機，其照射受保護 但為自動導向彈頭所辨識的目標物，當投射體發射時（由馬 上要啓動的放射機構産生），該靶體産生於物體的半側面。 由此開始，該自動導向彈頭不再看到目標物，而是看到暫 時性的靶機。當投射體移離受保護之目標物時，自動導向 彈頭追傾暫性靶體，因此移離受保護之目標物的半側面， 且可信賴地移向後者，即靶體，但靶體雲位在自動導向彈 頭的外側時，例如由於錯誤定位，因此可使自動導向撣頭 偏移。所以可得到防衛条統的簡化，此時在發射之後馬上 産生保護效應。 由參考下列附圖可對本發明能有更詳盡的瞭解。 圖一為本發明之序列，其顯示自動導向彈頭接近目標 rfl . 物。 如圖所示，一配備红外線自動導向彈頭的導引飛彈FK ，此飛彈定位船艦S上，首先沿箸飛行路徑F1接近船艦S。 當飛彈FK已鎖定船艦S時，一投射體從一位置WK1發射，其 方向指向靶體SZ,其沿著受保護船艦S之前的發射路徑SB發 射。一與迫蹤彈頭相似的持績熱放射之火箭引擎隨著投射 體的發射在位置WK1處點火，結果在位置WK1的投射體發射 時，船艦S已發射飛彈FK的紅外線自動導向彈頭。所以投射 體（SIC)FK己瞄準投射體位置WK1,然後從F1至F2、F3、F4 本紙張尺度適用中國國家標準（CNS ) A4規格（210 X 297公釐） (請先閲讀背面之注意事項再填寫本頁)This paper size is in accordance with Chinese National Standard (CNS) A4 (210X297 mm). The Central Bureau of Standards of the Ministry of Economic Affairs, Shellfish Consumer Cooperative, Du printed 396133 A7 B7 5. Description of the invention (2) Higher than the actual object. However, the disadvantage of the traditional method is that in the transfer effect, there is no protection ability during the target cloud launch and ignition. Therefore, a space distance is established during the ignition position and the effective position. Within this distance, there is an urgent need for the positioning of the target body within the sight of the automatic guided missile warhead, and it is in the inducement situation after the lock, otherwise the necessary can not be achieved. Transfer effect. A method is proposed in German patent application 33 26 884 C2. This method develops a thermal spray for a short period of time after ignition, thereby achieving a shielding effect in the infrared range. Therefore, this is a shielding method or a cloud curtain method, in which the warhead (the target that can lock the target) cannot be directed to the target automatically. In German patent 258 538 and German application 10 96 805 and 34 21 734 A1, a shell is proposed, which can emit energy in the effective infrared range of flight, but the transfer effect of the automatic guided missile cannot be seen in between. Therefore, the purpose of this case is to propose a method for effectively improving the target, so that the automatic guided missile that locks the target can be transferred from the target to the target. In this improved method, a launching mechanism is positioned on the projection body, and the radiation mechanism is activated when the projection body launches. This radiation mechanism radiates energy from the corresponding backward target, and after the launch, it reaches the target. Before the infrared target is established, this radiation mechanism emits energy. Therefore, it can be assumed that this radiation mechanism holds radon radiation energy. The radiation mechanism in the present invention emits radiation in a clock form. The present invention also provides a projection body. The projection body is fired according to a temporary space transfer, and the corresponding radiation mechanism is activated and subsequently ignited. As a result, the projection mechanism diverges and becomes a series of new target cross-clouds. It is an infrared target. The size of this paper is applicable to the Chinese National Standard (CNS) A4 specification (210X297 mm). I. ^^ 1 · m 1 ^ 1 n HI In ι ^ ϋ. In In m, / n. (Please read the back first Please note this page before filling in) This page is printed by the Consumer Cooperatives of the Central Standards Bureau of the Ministry of Economic Affairs 396133 at B7 V. Description of the invention (3) The cloud, this target cloud is developed from the previous target cloud. Connected to the tail end of the energy launch of the automatic guided missile. The launching mechanism of the present invention includes a pyrotechnic manufacturing component such as a gas generator, a light emitting component, or a rocket engine. The present invention is based on an astonishing cognition, and the defensive decisive improvement of the known method is decisive, in which a temporary target machine irradiates a protected target that is recognized by an automatic guided warhead when the projectile launches Time (produced by the radiation mechanism to be activated soon), the target is generated on the side of the object. From this point on, the automatic guided warhead no longer saw the target, but instead saw a temporary target. When the projectile moves away from the protected target, it automatically guides the warhead to chase the temporary target, so it moves away from the half side of the protected target and can reliably move to the latter, the target, but the target cloud When it is located outside the automatic guided bullet, for example, the automatic guided hoe can be offset due to incorrect positioning. Therefore, the simplification of the defense system can be obtained, and the protection effect is generated immediately after the launch. A more complete understanding of the present invention can be obtained by referring to the following drawings. Figure 1 shows the sequence of the present invention, which shows that the automatic guided warhead approaches the target rfl. As shown in the figure, a guided missile FK equipped with an infrared automatic guided warhead is positioned on the ship S, and first approaches the ship S along the flight path F1. When the missile FK has locked the ship S, a projectile is fired from a position WK1, its direction is directed at the target SZ, and it is fired along the launch path SB before the protected ship S. A rocket engine with sustained thermal radiation similar to the tracking warhead fired at the position WK1 with the launch of the projectile. As a result, when the projectile at the position WK1 was launched, the ship S had fired the infrared infrared guided warhead of the missile FK. Therefore, the projection body (SIC) FK has aimed at the position of the projection body WK1, and then from F1 to F2, F3, F4 This paper size applies the Chinese National Standard (CNS) A4 specification (210 X 297 mm) (Please read the precautions on the back first (Fill in this page again)
、1T 396133 經濟部中央標準局員工消费合作社印製 A7 B7 五、發明説明（4 ) 及F5持鑛改變飛行路徑，而投射體持壤沿著向靶體位置SZ (投射體位置W5 )的方向中的飛行方向WB,通過位置WK2、WK3 及WK4,且然後形成靶體SZ,此處飛彈FK撞擊靶體。 上文中已説明本發明値別及組合持擻，附圖及申請專 利範圍可限定本發明不同實施例。 本紙張尺度適用中國國家標準（CNS ) A4規格（210X 297公釐） (請先閲讀背面之注意事項再填寫本頁)1T 396133 Printed by A7 B7 of the Consumer Cooperatives of the Central Standards Bureau of the Ministry of Economic Affairs 5. Description of the Invention (4) and F5 Mine change the flight path, while the projectile holds the soil in the direction toward the target position SZ (projection position W5) The flight direction WB in the middle passes through the positions WK2, WK3 and WK4, and then forms the target body SZ, where the missile FK hits the target body. The invention has been described above in terms of different types and combinations, the drawings and the scope of the patent application can define different embodiments of the invention. This paper size applies to China National Standard (CNS) A4 (210X 297 mm) (Please read the precautions on the back before filling this page)