TWI646301B - Delay fuze structure and control method thereof - Google Patents
Delay fuze structure and control method thereof Download PDFInfo
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- TWI646301B TWI646301B TW107130788A TW107130788A TWI646301B TW I646301 B TWI646301 B TW I646301B TW 107130788 A TW107130788 A TW 107130788A TW 107130788 A TW107130788 A TW 107130788A TW I646301 B TWI646301 B TW I646301B
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- 238000000034 method Methods 0.000 title claims abstract description 18
- 230000009471 action Effects 0.000 claims abstract description 10
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- 239000003990 capacitor Substances 0.000 claims description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000010248 power generation Methods 0.000 description 3
- 238000005474 detonation Methods 0.000 description 2
- 239000002775 capsule Substances 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
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Abstract
本發明係提供一種延時引信結構改良及其控制方法,其係為一種運用於風力驅動之延時引信結構改良及其控制方法,透過拋射時所產生之風力,驅動引信模組作動之延時引信結構改良,該結構係包括一本體、一發電單元、引信模組及一控制單元,透過控制單元設定啟動引信模組所需之條件,當該本體受到拋射作動時,因拋射所產生之氣體進入該本體內,驅動該發電單元產生啟動該引信模組所需之電力,藉以達到控制及啟動延時引信之目的。 The invention provides a structure and a control method for a delay fuze, which is a structure and a control method for a delay fuze applied to a wind drive, and improves the delay fuze structure of the fuze module by driving the wind generated by the ejecting. The structure includes a body, a power generating unit, a fuze module and a control unit, and the conditions required to start the fuze module are set through the control unit. When the body is subjected to the projectile action, the gas generated by the projectile enters the body. In the body, the power generating unit is driven to generate power required to activate the fuze module, thereby achieving the purpose of controlling and starting the delay fuze.
Description
本發明係有關於一種引信結構改良,更詳而言之,尤指一種運用於風力驅動之延時引信結構改良及其控制方法。 The present invention relates to a fuze structure improvement, and more particularly to an improved structure and control method for a delay fuze applied to a wind drive.
請參閱第1圖,係為美國專利第6237495號示意圖,如圖所示,係為拋射體10結構係包括一彈殼11、一彈體12及一鼻錐13,該引信係沿一縱軸A依序配置該等組件,被安裝在鼻錐13之一引信(未圖示)是一安全裝置,以確保該拋射體10在被推進到離開拋射裝置一段距離後引爆,其作動方式係於拋射體10離開該拋射裝置後,因該拋射體10離開拋射裝置後,該拋射體10因拋射管設置,使該拋射體10呈現旋轉方式飛行,該旋轉動作使該拋射體10內之失衡轉子旋轉,致使該引信進行解鎖動作,而該失衡轉子旋轉速率被一小齒輪總成,及一邊界總成作用,而於該失衡轉子轉動一段時間,才啟動該引信1產生引爆之動作,盡一步達到延時目的。其中,該引爆方式,係透過設置於該失衡轉子一端之針刺雷管,對準該設置於拋射體內之彈尖引爆針,而一但該失衡轉子對準該彈尖引爆針時,即達到備炸位置,當該拋射物體撞擊到目標物時,即對該 目標物進行爆炸動作。 Please refer to FIG. 1 , which is a schematic diagram of US Pat. No. 6,237,495. As shown, the structure of the projectile 10 includes a casing 11 , an elastic body 12 and a nose cone 13 along a longitudinal axis A. The components are arranged in sequence, and a fuse (not shown) mounted on the nose cone 13 is a safety device to ensure that the projectile 10 is detonated after being advanced to a distance from the projectile, the actuation of which is based on ejection. After the body 10 leaves the projecting device, after the projectile 10 leaves the projecting device, the projectile 10 is arranged by the projectile tube to cause the projectile body 10 to fly in a rotating manner, which rotates the unbalanced rotor in the projectile body 10 Causing the fuze to perform an unlocking action, and the unbalanced rotor rotation rate is acted upon by a pinion assembly and a boundary assembly, and when the unbalanced rotor rotates for a period of time, the fuze 1 is activated to generate a detonation action, which is achieved one step at a time. Delay purpose. Wherein, the detonation method is performed by aligning the needle tip detonator disposed at one end of the unbalanced rotor with the bullet tip detonating needle disposed in the projectile body, and when the unbalanced rotor is aligned with the bullet tip detonating needle, the preparation is completed. The position of the bombing, when the projectile hits the target, The target is exploding.
如上所述,該衝擊引爆機構需配合可精確移動之機械零件,且於該投射物體,非正面撞擊到目標物時,該引信結構會因無正面撞擊,致使該引信結構產生破壞,發生無法引爆的狀況,或因為在搬運過程中,誤擊產生引爆之狀況。 As described above, the impact igniting mechanism needs to cooperate with a mechanical part that can be accurately moved, and when the projection object is non-frontal impact on the target object, the fuze structure may be damaged due to no frontal impact, and the fuze structure may be detonated. The condition of the explosion, or because of the accidental attack during the handling process.
鑒於上述習知技術之缺點,本發明主要之目的在於提供一種延時引信控制方法,以風力發電機作為提供啟動引信模組所需電力,達到驅動及控制延時引信之目的。 In view of the above disadvantages of the prior art, the main object of the present invention is to provide a delay fuze control method, which uses the wind turbine as the power required to provide the start fuse module to achieve the purpose of driving and controlling the delay fuze.
本發明又一目的,係提供一種延時引信結構改良,於該本體內設置一發電單元,利用該發電單元提供驅動引信模組所需之電力,進一步達到結構簡單化之目的。 Another object of the present invention is to provide a delay fuze structure structure, in which a power generating unit is disposed in the body, and the power required by the power generating unit to drive the fuze module is further provided, thereby further simplifying the structure.
為達上述目的,本發明係提供一種延時引信結構改良,其係為一種運用於風力驅動之延時引信結構改良,透過拋射時所產生之風力,驅動引信模組作動之延時引信結構改良,該結構係包括一具有容置空間及進氣通道之本體、一容設於該本體內之發電單元、一容設於該本體內之引信模組,及一設置於該本體週缘之控制單元,其中,該發電單元係以對應該進氣通道位置方式設置於該本體內,且與該引信模組及該控制單元電性連接,當該本體受到拋射作動時,利用控制單元設定啟動引信模組所需之條件,拋射作動所產生之氣體沿該進氣通道進入該本體內,並驅動該發電單元作動,並產生驅動引 信模組所需之電力,藉以達到控制及驅動延時引信之目的。 In order to achieve the above object, the present invention provides a delay fuze structure improvement, which is a structural improvement of a delay fuze applied to a wind drive, and improves the delay fuze structure of the driving fuze module by the wind generated by the ejecting, the structure The utility model comprises a main body having an accommodating space and an air inlet passage, a power generating unit housed in the body, a fusible module housed in the body, and a control unit disposed on the periphery of the body, wherein The power generating unit is disposed in the body in a manner corresponding to the position of the intake passage, and is electrically connected to the fuse module and the control unit. When the body is subjected to the projectile action, the control unit is used to set the start fuse module. The required condition, the gas generated by the projectile moves into the body along the intake passage, and drives the power generating unit to actuate, and generates driving guide The power required by the letter module is used to control and drive the delay fuze.
10‧‧‧拋射體 10‧‧‧ projectile
11‧‧‧彈殼 11‧‧‧Capsule
12‧‧‧彈體 12‧‧‧
13‧‧‧鼻錐 13‧‧‧ nose cone
21‧‧‧本體 21‧‧‧ body
22‧‧‧發電單元 22‧‧‧Power unit
23‧‧‧引信模組 23‧‧‧ Fuze Module
24‧‧‧控制單元 24‧‧‧Control unit
231‧‧‧電容 231‧‧‧ Capacitance
232‧‧‧引信電路 232‧‧‧ Fuze circuit
233‧‧‧電雷管 233‧‧‧Electric detonator
211‧‧‧出氣口 211‧‧‧ gas outlet
B‧‧‧進氣通道 B‧‧‧Intake passage
S1~S3‧‧‧方法步驟流程 S1~S3‧‧‧ method step flow
第1圖係為美國專利第6237495號示意圖。 Figure 1 is a schematic representation of U.S. Patent No. 6,237,495.
第2圖係為本發明延時引信結構改良結構示意圖。 Figure 2 is a schematic diagram showing the improved structure of the delay fuze structure of the present invention.
第3圖係為本發明延時引信控制方法步驟流程示意圖。 Figure 3 is a schematic flow chart of the steps of the delay fuze control method of the present invention.
以下係藉由特定的具體實例說明本發明之實施方式,熟悉此技藝之人士可由本說明書所揭示之內容瞭解本發明之其他優點與功效。 The embodiments of the present invention are described below by way of specific examples, and those skilled in the art can understand the other advantages and advantages of the present invention from the disclosure.
請參閱第2圖,係為本發明延時引信結構改良結構示意圖,如圖所示,其係為一種運用於風力驅動之延時引信結構改良,透過拋射時所產生之風力,驅動引信作動之延時引信結構改良,該結構係包括本體21、發電單元22、引信模組23及控制單元24,該本體21係為一具有容置空間之柱體,於該柱體一端設置有一進氣通道B,該發電單元22係為一風力發電機,以對應該進氣通道B位置容設於該本體21內,該引信模組23係容設於該本體21內,且該引信模組23與該發電單元22電性連接,且於該本體21一側,設置有一用以調整該啟動該引信模組23控制條件之控制單元24,其中,該本體21複包括一出氣口 211,該引信模組23係包括一電容231、一引信電路232及一電雷管233,當該本體21受到拋射作動時,利用控制單元24設定啟動引信模組23所需之條件,其中,該控制單元24係為電子輸入面板、轉盤、按鍵面板其中一種,當拋射作動所產生之氣體沿該進氣通道進入該本體21內,並驅動該發電單元22作動產生驅動引信模組23所需之電力,藉以達到驅動及控制延時引信之目的。 Please refer to FIG. 2 , which is a schematic structural diagram of the improved structure of the delay fuze according to the present invention. As shown in the figure, it is a structural improvement of the delay fuze applied to the wind drive, and the delay fuze driven by the fuze is driven by the wind generated during the ejection. The structure is improved, and the structure includes a body 21, a power generating unit 22, a fuze module 23, and a control unit 24. The body 21 is a cylinder having a receiving space, and an intake passage B is disposed at one end of the cylinder. The power generating unit 22 is a wind power generator, and is disposed in the body 21 corresponding to the position of the air inlet channel B. The fuse module 23 is received in the body 21, and the fuze module 23 and the power generating unit are 22 is electrically connected, and on the side of the body 21, a control unit 24 is provided for adjusting the control condition for starting the fuze module 23, wherein the body 21 includes an air outlet 211, the fuze module 23 includes a capacitor 231, a fuze circuit 232, and an electric detonator 233. When the main body 21 is subjected to ejection, the control unit 24 is used to set a condition required to start the fuze module 23, wherein The control unit 24 is one of an electronic input panel, a turntable, and a button panel. When the gas generated by the projectile action enters the body 21 along the intake passage, the control unit 22 is driven to generate the drive fuze module 23. Electricity, in order to drive and control the delay fuze.
請參閱第3圖,係為本發明延時引信控制方法步驟流程示意圖,如圖所示,其係為一種運用於風力驅動之延時引信控制,透過拋射時所產生之風力,驅動引信作動之延時引信控制方法,該方法步驟係包括:步驟1(S1):提供一具有容置空間之本體,於該本體一端形成有一進氣通道,且於該本體週缘設置有一控制單元;步驟2(S2):提供一發電單元,該發電單元係以對應該進氣通道位置,設置於該本體內,且於該發電單元一側電性連接一引信模組及控制單元;步驟3(S3):利用控制單元設定啟動該引信模組所需之條件,當該本體受到拋射作動時,拋射動作所產生之氣體沿該進氣通道進入該本體內,並驅動該發電單元作動,並產生驅動引信模組所需之電力,藉以達到驅動及控制延時引信之目的。 Please refer to FIG. 3 , which is a schematic flow chart of the step of the delay fuze control method of the present invention. As shown in the figure, it is a delay fuze control applied to the wind drive, and the fuze generated by the propeller is driven by the wind generated by the ejecting. The control method includes the following steps: Step 1 (S1): providing a body having an accommodating space, forming an intake passage at one end of the body, and providing a control unit at a periphery of the body; Step 2 (S2) Providing a power generation unit, the power generation unit is disposed in the body corresponding to the position of the intake passage, and is electrically connected to a fuse module and a control unit on the side of the power generation unit; Step 3 (S3): utilizing control The unit sets the conditions required to activate the fuze module. When the body is subjected to the projectile action, the gas generated by the ejecting action enters the body along the intake passage, and drives the power generating unit to actuate, and generates a driving fuze module. The power required to drive and control the delay fuze.
上述之實施例僅為例示性說明本發明之特點及 其功效,而非用於限制本發明之實質技術內容的範圍。任何熟習此技藝之人士均可在不違背本發明之精神及範疇下,對上述實施例進行修飾與變化。因此,本發明之權利保護範圍,應如後述之申請專利範圍所列。 The above embodiments are merely illustrative of the features of the present invention and The efficiencies are not intended to limit the scope of the technical content of the invention. Modifications and variations of the above-described embodiments can be made by those skilled in the art without departing from the spirit and scope of the invention. Therefore, the scope of protection of the present invention should be as set forth in the scope of the claims described below.
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| TW107130788A TWI646301B (en) | 2018-08-30 | 2018-08-30 | Delay fuze structure and control method thereof |
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| TW107130788A TWI646301B (en) | 2018-08-30 | 2018-08-30 | Delay fuze structure and control method thereof |
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| TWI646301B true TWI646301B (en) | 2019-01-01 |
| TW202009442A TW202009442A (en) | 2020-03-01 |
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Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2100090A2 (en) * | 2006-12-14 | 2009-09-16 | Simmonds Precision Products, Inc. | Spin stabilizer projectile trajectory control |
| CN101749985A (en) * | 2008-12-02 | 2010-06-23 | 刘清成 | Electronic device for training grenade |
| US20120291613A1 (en) * | 2010-02-10 | 2012-11-22 | Omnitek Partners Llc | Miniature Safe and Arm Mechanisms For Fuzing of Gravity Dropped Small Weapons |
| US9945649B2 (en) * | 2010-08-25 | 2018-04-17 | Bae Systems Rokar International Ltd. | System and method for guiding a cannon shell in flight |
| CN207331689U (en) * | 2017-08-22 | 2018-05-08 | 华北水利水电大学 | Rocket bores earth anchor |
-
2018
- 2018-08-30 TW TW107130788A patent/TWI646301B/en active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2100090A2 (en) * | 2006-12-14 | 2009-09-16 | Simmonds Precision Products, Inc. | Spin stabilizer projectile trajectory control |
| US7963442B2 (en) * | 2006-12-14 | 2011-06-21 | Simmonds Precision Products, Inc. | Spin stabilized projectile trajectory control |
| CN101749985A (en) * | 2008-12-02 | 2010-06-23 | 刘清成 | Electronic device for training grenade |
| CN101749985B (en) | 2008-12-02 | 2013-10-30 | 刘清成 | Electronic device for training grenade |
| US20120291613A1 (en) * | 2010-02-10 | 2012-11-22 | Omnitek Partners Llc | Miniature Safe and Arm Mechanisms For Fuzing of Gravity Dropped Small Weapons |
| US9945649B2 (en) * | 2010-08-25 | 2018-04-17 | Bae Systems Rokar International Ltd. | System and method for guiding a cannon shell in flight |
| CN207331689U (en) * | 2017-08-22 | 2018-05-08 | 华北水利水电大学 | Rocket bores earth anchor |
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