JPS62440B2 - - Google Patents

Info

Publication number
JPS62440B2
JPS62440B2 JP53128647A JP12864778A JPS62440B2 JP S62440 B2 JPS62440 B2 JP S62440B2 JP 53128647 A JP53128647 A JP 53128647A JP 12864778 A JP12864778 A JP 12864778A JP S62440 B2 JPS62440 B2 JP S62440B2
Authority
JP
Japan
Prior art keywords
fuze
firing pin
blocking body
detonator
bullet
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
JP53128647A
Other languages
Japanese (ja)
Other versions
JPS5477500A (en
Inventor
Ahoterotsutsu Rooberuto
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rheinmetall Air Defence AG
Original Assignee
Werkzeugmaschinenfabrik Oerlikon Buhrle AG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Werkzeugmaschinenfabrik Oerlikon Buhrle AG filed Critical Werkzeugmaschinenfabrik Oerlikon Buhrle AG
Publication of JPS5477500A publication Critical patent/JPS5477500A/en
Publication of JPS62440B2 publication Critical patent/JPS62440B2/ja
Granted legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C1/00—Impact fuzes, i.e. fuzes actuated only by ammunition impact
    • F42C1/02—Impact fuzes, i.e. fuzes actuated only by ammunition impact with firing-pin structurally combined with fuze
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C1/00—Impact fuzes, i.e. fuzes actuated only by ammunition impact
    • F42C1/02—Impact fuzes, i.e. fuzes actuated only by ammunition impact with firing-pin structurally combined with fuze
    • F42C1/04—Impact fuzes, i.e. fuzes actuated only by ammunition impact with firing-pin structurally combined with fuze operating by inertia of members on impact

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Air Bags (AREA)
  • Vibration Dampers (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Spark Plugs (AREA)

Description

【発明の詳細な説明】 本発明は雷管と、機械的遅延装置と、2つの慣
性スリーブとを有する弾底着発信管にして、雷管
はばね力で作動する撃針によつて信管裏側から刺
突可能であり、機械的遅延装置は阻止体と、撃針
の横孔と、信管部分の環溝とから成り、その阻止
位置において、阻止体は撃針の横孔及び信管部分
の環溝に係合しており、2つの慣性スリーブは信
管部分に対して同軸に相前後して配設されてお
り、慣性スリーブは弾着減速度の消失後に阻止体
を釈放する弾底着発信管に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention provides a bottom landing transmitter tube having a detonator, a mechanical delay device, and two inertia sleeves, the detonator being pierced from the back side of the fuze by a firing pin actuated by a spring force. The mechanical retardation device may consist of a blocking body, a lateral bore in the firing pin, and an annulus in the fuze section, in which the blocking body engages the lateral bore in the firing pin and the annulus in the fuze section. The two inertia sleeves are arranged coaxially and one after the other with respect to the fuze part, the inertia sleeves relating to the bottom landing tube which releases the blocking body after the impact deceleration has disappeared.

この種の公知の信管(スイス国特許明細書第
360927号)は、目標物への弾着に際し、弾丸の小
さい減速度で初めて弾丸炸薬の点火が行われるよ
うに形成されている。時間的応答遅延を伴うかか
る信管は、大きな破壊効果を得るために点火前に
できるだけ深く目標物中に侵入すべき弾丸に適し
ている。即ち目標物が弾丸の侵入に際して大きな
抵抗を有さない場合、従つて大きな減速度は生じ
ない場合に適する。
Known fuzes of this type (Swiss patent specification no.
No. 360927) is designed so that the explosive charge is ignited only at a small deceleration of the bullet when it hits the target. Such fuzes with a temporal response delay are suitable for bullets that should penetrate as deep as possible into the target before ignition in order to obtain a large destructive effect. That is, it is suitable when the target does not have a large resistance to the penetration of the bullet, and therefore when a large deceleration does not occur.

しかるにかかる信管を備えた弾丸が非常に硬い
目標物、たとえばコンクリート板又は硬い岩石に
命中し侵入できない場合には大きな減速度が生
じ、この減速度は時間的に遅延された点火を行う
前に信管を破壊する。従つてかかる信管はこの場
合には応答せずかつ弾丸は不発に終わる。
However, if a bullet equipped with such a fuze hits a very hard target, such as a concrete plate or a hard rock, and cannot penetrate it, a large deceleration occurs, which decelerates the fuse before the time-delayed ignition occurs. destroy. Such a fuse would therefore not respond in this case and the bullet would fail to explode.

(本発明の課題) 弾着減速度が極めて大きい場合でも機能を発揮
し、かつ弾体及び信管が点火を可能にしない程強
く変形される前に適時に応答するような弾丸の弾
底着発信管を創造する課題が本発明により解決さ
れるべきである。
(Problem of the present invention) A bullet bottom impact signal that functions even when the impact deceleration is extremely large and responds in a timely manner before the bullet and fuse are deformed so strongly that they cannot be ignited. The problem of creating a tube is to be solved by the present invention.

(課題の解決のための手段) 本発明の課題は雷管と、機械的遅延装置と、2
つの慣性スリーブとを有する弾底着発信管にし
て、雷管はばね力で作動する撃針によつて信管裏
側から刺突可能であり、機械的遅延装置は阻止体
と、撃針の横孔と、信管部分の環溝とから成り、
かつその阻止位置において、阻止体は撃針の横孔
と信管部分の環溝とに係合しており、2つの慣性
スリーブは信管部分に対して同軸に相前後して配
設されており、慣性スリーブは弾着減速度の消失
後に阻止体を釈放する弾底着発信管において、位
置固定の信管部分はシアピンによつて信管ケーシ
ング内に固定されており、それによつて非常に大
きな弾着減速度の際、撃針が阻止位置にある阻止
体によつて信管部分と結合したまま遅延なしに雷
管を刺突くようにしたことによつて解決される。
(Means for Solving the Problems) The problems of the present invention are to provide a detonator, a mechanical delay device, and two
The detonator can be pierced from the back side of the fuze by a spring-loaded firing pin, and the mechanical delay device is connected to the blocking body, the side hole of the firing pin, and the fuze. It consists of a ring groove in the part,
And in its blocking position, the blocking body engages with the transverse hole of the firing pin and the annular groove of the fuze part, and the two inertia sleeves are arranged coaxially one after the other with respect to the fuze part, and the inertia The sleeve releases the blocking body after the impact deceleration disappears.In the bottom landing transmitter tube, the fuze part, which is fixed in position, is fixed in the fuze casing by a shear pin, which allows for a very large impact deceleration. This problem is solved by allowing the firing pin to pierce the detonator without delay while remaining connected to the fuze part by the blocking body in the blocking position.

以下本発明による弾底着発信管の実施例を図面
に基づいて説明する。
DESCRIPTION OF THE PREFERRED EMBODIMENTS Embodiments of the bullet bottom landing transmitter tube according to the present invention will be described below with reference to the drawings.

(実施例) 第1図によると弾丸は炸薬11を含んでいる中
空の弾体10を有する。炸薬の後方にはアルミニ
ウム筒12があり、このアルミニウム筒は炸薬1
1と信管13とを区切つている。このアルミニウ
ム筒の後方にはリング状の鋼板14があり、この
鋼板は弾体10中に遊隙をもつて挿入されてい
る。アルミニウム筒12中及び鋼板を貫通して補
強薬15が侵入し、補強薬は信管13の前端に固
定されている。
Embodiment According to FIG. 1, the bullet has a hollow shell 10 containing an explosive charge 11. There is an aluminum cylinder 12 behind the explosive charge, and this aluminum cylinder holds the explosive charge 1.
1 and fuse 13. There is a ring-shaped steel plate 14 behind this aluminum cylinder, and this steel plate is inserted into the bullet 10 with a gap. A reinforcing agent 15 penetrates through the aluminum cylinder 12 and the steel plate, and is fixed to the front end of the fuse 13.

信管13は保持機構16によつて弾体10の空
洞中に固定されている。この保持機構16は信管
13の前端を支持している第1のリング17と、
弾体10に固定されている第2のリング18とを
有する。この第2のリング18はおねじを有しか
つ、弾体10のめねじ中にねじ込まれている。両
リング17と18はシリンダ状のウエブ19によ
つて相互に一体的に結合されている。更に保持機
構16は信管13の後端を支持している第3のリ
ング20と、弾体10に固定されている第4のリ
ング21とを有する。第4のリング21は同じく
おねじを有しかつ弾体10のめねじ中にねじ込ま
れている。これらの両リング20と21もシリン
ダ状のウエブ22によつて相互に一体的に結合さ
れている。
The fuse 13 is fixed in the cavity of the bullet 10 by a holding mechanism 16. This holding mechanism 16 includes a first ring 17 supporting the front end of the fuze 13;
and a second ring 18 fixed to the elastic body 10. This second ring 18 has an external thread and is screwed into the internal thread of the elastic body 10. The two rings 17 and 18 are integrally connected to each other by a cylindrical web 19. Furthermore, the holding mechanism 16 includes a third ring 20 supporting the rear end of the fuse 13 and a fourth ring 21 fixed to the bullet 10. The fourth ring 21 also has an external thread and is screwed into the internal thread of the elastic body 10. The two rings 20 and 21 are also integrally connected to each other by a cylindrical web 22.

中空の弾体10の内壁と両ウエブ19と22と
の間、及び両ウエブ19、と22と信管13との
間との間には各々1つの変形空域23と24が存
在する。
Between the inner wall of the hollow shell 10 and the two webs 19 and 22 and between the two webs 19 and 22 and the fuse 13, there is a deformation space 23 and 24, respectively.

第2〜4図によると信管13は孔25中に遅延
された点火のための装置を有する。信管13に固
定された信管部分(シリンダ部分とも称する)2
6がその固定されている孔の末端からこの孔25
中に侵入している。信管部分の前端は全周に1つ
の環溝27を備えており、環溝は前方へは斜めの
面28により区切られている。孔25中において
運動可能なスリーブ29は信管部分26上方に引
き上げられ、休止位置においてデスク42上に座
着している。スリーブ29の孔段部30と撃針3
1の後端との間にばね32が挿入されている。
According to FIGS. 2-4, fuse 13 has a device for delayed ignition in bore 25. Fuze part (also referred to as cylinder part) 2 fixed to fuze 13
6 is fixed from the end of the hole to this hole 25
It's getting inside. The front end of the fuze part is provided with an annular groove 27 around the entire circumference, which is bounded forward by an oblique surface 28. The sleeve 29, movable in the bore 25, is pulled up over the fuze part 26 and sits on the desk 42 in the rest position. Hole step 30 of sleeve 29 and firing pin 3
A spring 32 is inserted between the rear end of 1 and the rear end of 1.

信管部分26の前端は撃針31の孔33中に侵
入している。撃針31はその運動を阻止している
阻止体(球)34により、すなわち撃針31の横
孔35中に配設され、かつばね32の押圧力によ
つて、信管体と連結された信管部分26の斜め面
28に圧着されている阻止体34によりシリンダ
状部分26と連結されかつ確保されている。それ
によつて機械的遅延装置が形成されている。同時
に阻止体34は同じく孔25中に通されているス
リーブ36の内壁に対しても押圧されていて摩擦
力によつて保持される。スリーブ36はスリーブ
29の前方部分の孔と同じ直径の孔を有し、かつ
スリーブ29の端面の斜めの端面37と接合して
いる。先細りの部分38はスライダ39の案内路
の後方まで突き出ている。スライダ39は弾丸の
回転により弾丸軸線に対して横に移動可能であ
り、かつ雷管40を有し(第3図)、雷管はスラ
イダ39と共に第2図に示す阻止位置から第3図
に示す撃発位置へと移動される。信管部分26の
後端にはシヤピン41によつて1つのデスク42
が固定されており、デスクは孔25に同心の、信
管体の空所45中にあり、かつ前方へは肩部46
に支持されている。
The forward end of the fuze portion 26 extends into the bore 33 of the firing pin 31. The firing pin 31 is moved by a blocking body (ball) 34 that prevents its movement, that is, by a fuze portion 26 that is arranged in a transverse hole 35 of the firing pin 31 and connected to the fuze body by the pressing force of a spring 32. It is connected and secured to the cylindrical part 26 by a blocking body 34 which is pressed onto the oblique surface 28 of the cylindrical part 26. A mechanical delay device is thereby formed. At the same time, the blocking body 34 is also pressed against the inner wall of the sleeve 36, which is also passed through the hole 25, and is held by frictional force. The sleeve 36 has a hole of the same diameter as the hole in the front part of the sleeve 29 and joins an oblique end surface 37 of the end face of the sleeve 29. The tapered portion 38 projects to the rear of the guide path of the slider 39. The slider 39 is movable transversely with respect to the bullet axis due to the rotation of the bullet, and has a detonator 40 (FIG. 3), which together with the slider 39 moves from the blocking position shown in FIG. 2 to the firing position shown in FIG. moved to position. A desk 42 is attached to the rear end of the fuze portion 26 by a shear pin 41.
is fixed, the desk is located in the cavity 45 of the fuze body, concentric with the hole 25, and forwardly extends from the shoulder 46.
is supported by

(本発明の作用) 上記の弾底着発信管の作用方は次の通りであ
る。
(Operation of the present invention) The operation of the above bullet bottom landing transmitter tube is as follows.

弾丸の発射前に弾底着発信管の記載の部分は第
2図による位置を占めている。弾丸が発射される
や否やスライダ39は雷管40と共に弾丸の回転
によつて第2図による位置から第3図及び第4図
の位置に移動する。
Before firing the bullet, the indicated part of the bullet landing tube assumes the position according to FIG. As soon as the bullet is fired, the slider 39, together with the detonator 40, is moved by the rotation of the bullet from the position according to FIG. 2 to the position according to FIGS. 3 and 4.

次に弾着の際撃針による雷管の刺突が行われる
が、これには2つの場合がある。
Next, upon impact, the detonator is pierced by the firing pin, which can occur in two ways.

第1の場合;弾着の際の減速度が大きい場合、
第3図によればシアピン41は直ちに剪断され、
そしてスリーブ29および36並びに信管部分2
6は阻止体34及び撃針31と共に第3図に示す
ように前方へ動かされ、即ち撃針31が阻止位置
にある阻止体34によつて信管部分26と結合し
たまま雷管40を時間的遅延なしに直ちに刺突
く。
First case: If the deceleration at the time of impact is large,
According to FIG. 3, the shear pin 41 is immediately sheared,
and sleeves 29 and 36 and fuze portion 2
6 is moved forward with blocking body 34 and firing pin 31 as shown in FIG. Immediate stabbing.

第2の場合:目標におけにる弾丸の着地が小さ
い減速度で行われると、シアピン41は剪断され
ない。両スリーブ36及び29は弾着によつてば
ね32の力に坑して前方へ動かされる。前部スリ
ーブ36は第4図によるその最前位置に達する。
弾着の後ばね32はスリーブ29を再び第4図に
よる最前位置に押し戻す位置にある。それによつ
て阻止されずに、撃針31はばね32の力によつ
て雷管40を刺突く方向に急速に移動することが
できる。その際阻止体34はスリーブ36の斜面
37によつて撃針31の孔33内へ向けられ、そ
の結果、撃針31は阻止されずにスリーブ36に
衝突するまで雷管40を刺突く。
Second case: If the landing of the bullet on the target takes place with a small deceleration, the shear pin 41 is not sheared. Both sleeves 36 and 29 are moved forward against the force of spring 32 by the impact. The front sleeve 36 reaches its forwardmost position according to FIG.
After impact, the spring 32 is in a position to push the sleeve 29 back into its forward position according to FIG. Unhindered thereby, the firing pin 31 can rapidly move in the direction of piercing the detonator 40 by the force of the spring 32. The blocking body 34 is then directed by the bevel 37 of the sleeve 36 into the bore 33 of the firing pin 31, so that the firing pin 31 pierces the detonator 40 without being blocked until it impinges on the sleeve 36.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は信管付弾丸の縦断面図、第2図〜4図
は第1図の−線に沿う信管の拡大断面図を
種々の位置について示し、即ち第2図は輸送位置
における信管、第3図は大きな減速度をもつて弾
着した場合の信管、第4図は小さい減速度で弾着
した後の信管を示す。 図中符号、26……信管部分、31……撃針、
34……阻止体、40……雷管、41……シアピ
ン。
FIG. 1 is a longitudinal cross-sectional view of a bullet with a fuze, and FIGS. 2 to 4 are enlarged cross-sectional views of the fuse along the line - in FIG. 1 at various positions, i.e., FIG. Figure 3 shows the fuse when the bullet hits with a large deceleration, and Figure 4 shows the fuse after the bullet hits with a small deceleration. Symbols in the figure: 26...fuze part, 31...firing pin,
34...blocker, 40...detonator, 41...shear pin.

Claims (1)

【特許請求の範囲】 1 雷管と、機械的遅延装置と、2つの慣性スリ
ーブとを有する弾底着発信管にして、雷管はばね
力で作動する撃針によつて信管裏側から刺突可能
であり、機械的遅延装置は阻止体と、撃針の横孔
と、信管部分の環溝とから成り、かつその阻止位
置において、阻止体は撃針の横孔と信管部分の環
溝とに係合しており、2つの慣性スリーブは信管
部分に対して同軸に相前後して配設されており、
慣性スリーブは弾着減速度の消失後に阻止体を釈
放する弾底着発信管において、 位置固定の信管部分26はシアピン41によつ
て信管ケーシング内に固定されており、それによ
つて非常に大きな弾着減速度の際、撃針31が阻
止位置にある阻止体34によつて信管部分26と
結合したまま遅延なしに雷管40を刺突くことを
特徴とする弾底着発信管。
[Scope of Claims] 1. A bottom-landing transmitter tube having a detonator, a mechanical delay device, and two inertia sleeves, the detonator being capable of being pierced from the back side of the fuze by a firing pin actuated by a spring force. , the mechanical delay device comprises a blocking body, a firing pin transverse hole, and an annular groove in the fuze section, and in the blocking position, the blocking body engages the firing pin transverse hole and the fuze section annular groove. The two inertia sleeves are arranged coaxially and one after the other with respect to the fuse part,
The inertial sleeve releases the blocking body after the impact deceleration has dissipated.In the bottom landing transmitter tube, the fixed position fuze section 26 is fixed in the fuze casing by a shear pin 41, thereby making it possible to release the blocking body after the impact deceleration has disappeared. The bottom landing transmitter tube is characterized in that during landing deceleration, the firing pin 31 pierces the detonator 40 without delay while being connected to the fuze portion 26 by the blocking body 34 in the blocking position.
JP12864778A 1977-10-20 1978-10-20 Bullet arrival and departure fuse Granted JPS5477500A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH1277977A CH623408A5 (en) 1977-10-20 1977-10-20

Publications (2)

Publication Number Publication Date
JPS5477500A JPS5477500A (en) 1979-06-20
JPS62440B2 true JPS62440B2 (en) 1987-01-07

Family

ID=4386314

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12864778A Granted JPS5477500A (en) 1977-10-20 1978-10-20 Bullet arrival and departure fuse

Country Status (7)

Country Link
JP (1) JPS5477500A (en)
CH (1) CH623408A5 (en)
DE (1) DE2842882C3 (en)
FR (1) FR2406802A1 (en)
GB (1) GB2006401B (en)
IT (1) IT1099957B (en)
SE (1) SE437884B (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3535854A1 (en) * 1985-10-08 1987-04-09 Diehl Gmbh & Co HIT WITH A IGNITION CAPSULE
DE3933436A1 (en) * 1989-10-06 1991-04-18 Diehl Gmbh & Co FLOOR IGNITION FOR PISTON GUN BULLETS WITH OPTIONAL FUNCTION
US11415399B1 (en) * 2020-12-15 2022-08-16 The United States Of America As Represented By The Secretary Of The Navy Ignition apparatus for projectile
CN112863143A (en) * 2021-02-25 2021-05-28 上海克故消防设备有限公司 Oxygen test and early warning device in car

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB190709160A (en) 1907-04-23 1908-04-23 Frederick Marten Hale Improvement connected with Explosive Shells.
GB572571A (en) * 1940-07-13 1945-10-15 George Temple Improved delay action device for fuzes
US2750888A (en) * 1946-11-13 1956-06-19 Robert O Wynn Long delay bomb tail fuze
US2748705A (en) * 1952-10-28 1956-06-05 Frank B Hale Inertia and point detonation impact fuze
NL236971A (en) * 1958-03-28
GB916007A (en) * 1961-07-20 1963-01-16 Mititaka Yamamoto Proximity switch system
DE1210362B (en) * 1964-07-14 1966-02-03 Diehl Fa Impact fuse for projectiles
CH430505A (en) * 1965-12-06 1967-02-15 Oerlikon Buehrle Holding Ag Impact fuse
CH459002A (en) * 1966-06-21 1968-06-30 Oerlikon Buehrle Holding Ag Impact fuse for projectiles

Also Published As

Publication number Publication date
DE2842882C3 (en) 1981-03-19
FR2406802A1 (en) 1979-05-18
GB2006401B (en) 1982-03-24
SE437884B (en) 1985-03-18
SE7810081L (en) 1979-04-21
DE2842882A1 (en) 1979-04-26
DE2842882B2 (en) 1980-07-03
IT1099957B (en) 1985-09-28
IT7828851A0 (en) 1978-10-18
JPS5477500A (en) 1979-06-20
GB2006401A (en) 1979-05-02
CH623408A5 (en) 1981-05-29
FR2406802B1 (en) 1980-09-19

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