[go: up one dir, main page]

JPH09105600A - Power source for fuse - Google Patents

Power source for fuse

Info

Publication number
JPH09105600A
JPH09105600A JP25902295A JP25902295A JPH09105600A JP H09105600 A JPH09105600 A JP H09105600A JP 25902295 A JP25902295 A JP 25902295A JP 25902295 A JP25902295 A JP 25902295A JP H09105600 A JPH09105600 A JP H09105600A
Authority
JP
Japan
Prior art keywords
fuse
coils
fuze
magnet
power source
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.)
Pending
Application number
JP25902295A
Other languages
Japanese (ja)
Inventor
Takashi Shironita
孝 白仁田
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.)
Yokogawa Denshikiki Co Ltd
Original Assignee
Yokogawa Denshikiki Co Ltd
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 Yokogawa Denshikiki Co Ltd filed Critical Yokogawa Denshikiki Co Ltd
Priority to JP25902295A priority Critical patent/JPH09105600A/en
Publication of JPH09105600A publication Critical patent/JPH09105600A/en
Pending legal-status Critical Current

Links

Landscapes

  • Permanent Magnet Type Synchronous Machine (AREA)

Abstract

PROBLEM TO BE SOLVED: To simplify the mechanism of a power source for a fuse, lower a cost and facilitate storage and management by providing a plurality of coils arranged in the periphery of a magnet in a case provided in a spinning and flying fuse. SOLUTION: A revolving bullet 1 comprises a tube part 2 filled with an explosive and a fuse 3. When the revolving bullet 1 is shot, the revolving bullet 1 spins at an angular velocity and flies toward a direction shown by an arrow A. This angular velocity ω is accelerated up to 10000rpm during about 10msec immediately after shooting. During this acceleration, a main body case 5 and coils 141 and 145 rotates about a central axis G at the angular velocity ω. On the other hand, a magnet 11 is rotatably supported by bearings 6 and 7, it maintains its stationary state depending on law of inertia. That is, the coils 141 and 145 rotate about the magnet 11. As a result, the coils 141 and 145 induce an induced electromotive force. Thus, a power source 4 for a fuse built in the fuse 3 generates electric power.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は、信管の電源として
用いられる信管用電源に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a fuze power source used as a power source for a fuze.

【0002】[0002]

【従来の技術】近接信管等の信管には、導爆薬を点火す
るための電気雷管を有する発火部並びに電波を発信又は
検知して近接信号を得るための電子回路を作動させるた
めの電源が必要であり、その電源としては、次のような
要件を満足するものが好ましい。 (1)長期の保存においても充電等の保守作業が不要で
あること。 (2)発射前にはエネルギーを発生せず、発射されたこ
とを自動的に検出して、短時間の間にエネルギーを発生
できること。 (3)小型、軽量であること。 上記要件を略満足する電源としては、風車発電機、注液
式電池、熱電池等が用いられている。
2. Description of the Related Art A fuze such as a proximity fuze requires a firing unit having an electric detonator for igniting an explosive charge and a power supply for operating an electronic circuit for transmitting or detecting radio waves to obtain a proximity signal. As the power source, a power source that satisfies the following requirements is preferable. (1) Maintenance work such as charging is unnecessary even for long-term storage. (2) Energy must not be generated before it is fired, but it can be automatically detected that it has been fired and energy can be generated in a short time. (3) Small size and light weight. As a power source that substantially satisfies the above requirements, a wind turbine generator, a liquid injection battery, a thermal battery, or the like is used.

【0003】[0003]

【発明が解決しようとする課題】ところで、上述した風
車発電機においては、信頼性を確保するために複雑な機
構とされているため、製造コストが高いという欠点があ
った。また、上述した注液電池、熱電池等においては、
上記欠点に加えて、化学物質が用いられていることから
保管・管理が非常に面倒であるという欠点があった。
The wind turbine generator described above, however, has a drawback that the manufacturing cost is high because it has a complicated mechanism for ensuring reliability. Further, in the above-mentioned liquid injection battery, thermal battery, etc.,
In addition to the above-mentioned drawbacks, there is a drawback that storage and management are very troublesome because chemical substances are used.

【0004】本発明は、上記事情に鑑み、機構が単純で
コストが安く、かつ保管・管理が容易である信管用電源
を提供することを目的としている。
In view of the above circumstances, it is an object of the present invention to provide a fuze power source having a simple mechanism, low cost, and easy storage / management.

【0005】[0005]

【課題を解決するための手段】請求項1に記載の発明
は、スピンしながら飛行する信管内部に設けられたケー
スと、自身の中心軸と前記信管の中心軸とが一致するよ
うに前記ケースに軸受手段を介して回転自在に軸支され
た軸部材と、前記軸部材に取り付けられた磁石と、前記
ケースに設けられ、前記磁石の周囲に配設された複数の
コイルととを具備することを特徴とする。
According to a first aspect of the present invention, there is provided a case provided inside a fuze that spins while flying, and the case is such that the center axis of the case and the center axis of the fuze coincide with each other. A shaft member rotatably supported via bearing means, a magnet attached to the shaft member, and a plurality of coils provided in the case and arranged around the magnet. It is characterized by

【0006】請求項2に記載の発明は、請求項1に記載
の信管用電源において、前記複数のコイルに誘起される
電力を蓄積する電力蓄積手段を具備することを特徴とす
る。
According to a second aspect of the present invention, in the fuze power source according to the first aspect, there is provided power storage means for storing power induced in the plurality of coils.

【0007】請求項3に記載の発明は、請求項1または
2に記載の信管用電源において、前記軸部材に取り付け
られた重量付加手段を具備することを特徴とする。
According to a third aspect of the present invention, in the fuze power source according to the first or second aspect, a weight adding means attached to the shaft member is provided.

【0008】[0008]

【発明の実施の形態】以下、図面を参照して本発明の実
施形態について説明する。図1は本発明の一実施形態に
よる信管用電源が内蔵された信管が装着された旋転弾の
構成を示す側面図である。この図において、旋転弾1
は、火薬が充填された筒部2と信管3とから構成されて
いる。この旋転弾1は、発射時にスピンが掛けられ、中
心軸Gを軸として角速度ωでスピンしながら飛行する。
4は、信管3に内蔵された信管用電源であり、旋転弾1
の発射後の角速度ωを利用して発電をする。
BEST MODE FOR CARRYING OUT THE INVENTION Embodiments of the present invention will be described below with reference to the drawings. FIG. 1 is a side view showing the configuration of a rotary ammunition equipped with a fuze having a built-in fuze power source according to an embodiment of the present invention. In this figure,
Is composed of a tube portion 2 filled with explosive and a fuze 3. The turning bullet 1 is spun at the time of launch and flies while spinning at an angular velocity ω with the central axis G as an axis.
Reference numeral 4 denotes a fuze power source built in the fuze 3, and a turning bullet 1
Generates power using the angular velocity ω after the launch of.

【0009】図2は、図1に示す信管用電源4の構成を
示す拡大断面図である。この図において、5は、本体ケ
ースであり、円筒部材5aと、該円筒部材5aの上面を
塞ぐ円板部材5bと、円板部材5aの下面を塞ぎ略中央
に開口部5dが形成された部材5cとが一体に形成され
てなるものである。6は、本体ケース5の円板部材5b
の下面に取り付けられたベアリングである。7は、本体
ケース5の部材5cの開口部5dに取り付けられたベア
リングである。20は、軸部材であり、その両端部がベ
アリング6、7により回転自在に軸支されている。この
軸部材20の中心軸は、旋転弾1(図1参照)の中心軸
Gと一致している。
FIG. 2 is an enlarged sectional view showing the structure of the fuze power source 4 shown in FIG. In this figure, reference numeral 5 denotes a main body case, which is a cylindrical member 5a, a disk member 5b that closes the upper surface of the cylindrical member 5a, and a member that closes the lower surface of the disk member 5a and has an opening 5d formed substantially in the center. 5c is integrally formed. 6 is a disc member 5b of the body case 5
Is a bearing attached to the lower surface of the. Reference numeral 7 denotes a bearing attached to the opening 5d of the member 5c of the main body case 5. Reference numeral 20 denotes a shaft member, both ends of which are rotatably supported by bearings 6 and 7. The central axis of the shaft member 20 coincides with the central axis G of the rotary bullet 1 (see FIG. 1).

【0010】上記軸部材20には、下からスペーサ8、
慣性円盤9、スペーサ10、磁石11、スペーサ12が
各々取り付け固定されている。上記慣性円盤9は、一定
の重量を有しており、慣性モーメントを大きくする役目
をしている。磁石11は、略円柱形状をなし図3に示す
ように、一方の半部がS極、他方の半部がN極に着磁さ
れている。この磁石11の周囲には、8個のヨーク13
1〜138が配設されており、該ヨーク131〜138に
は、各々コイル141〜148が巻回されている。
On the shaft member 20, the spacers 8 and
The inertial disk 9, the spacer 10, the magnet 11, and the spacer 12 are attached and fixed. The inertial disk 9 has a constant weight and serves to increase the moment of inertia. The magnet 11 has a substantially columnar shape, and as shown in FIG. 3, one half of the magnet 11 is magnetized as an S pole and the other half is magnetized as an N pole. Eight yokes 13 are provided around the magnet 11.
1 to 13 are provided, and coils 141 to 148 are wound around the yokes 131 to 138, respectively.

【0011】ここで、上述した一実施形態による信管用
電源の電気的構成を図4に示す。この図において、コイ
ル141〜148は、各々の一端が接地され、各々の他端
が整流用のダイオード151〜158を介してコンデンサ
16の一方の電極に接続されている。
Here, FIG. 4 shows an electrical configuration of the fuze power source according to the above-described embodiment. In the figure, each of the coils 141 to 148 has one end grounded and the other end connected to one electrode of the capacitor 16 via rectifying diodes 151 to 158.

【0012】次に、上述した一実施形態による信管用電
源の動作について説明する。図1において、旋転弾1が
発射されると、旋転弾1は、角速度ωでスピンしつつ同
図に矢印Aで示す方向へ飛行する。この角速度ωは、発
射直後から約10msecの間に0rpmから1000
0rpmまで加速する。
Next, the operation of the fuze power source according to the above-described embodiment will be described. In FIG. 1, when the whirling bullet 1 is fired, the whirling bullet 1 spins at an angular velocity ω and flies in a direction indicated by an arrow A in the figure. This angular velocity ω ranges from 0 rpm to 1000 within 10 msec immediately after launch.
Accelerate to 0 rpm.

【0013】上記加速時において、図3に示すように本
体ケース5およびヨーク131〜138(コイル141〜
148)は、中心軸Gを軸として角速度ωで回転する。
一方、軸部材20、慣性円盤9および磁石11は、ベア
リング6、7により回転自在に支持されているため慣性
の法則により、静止状態が維持される。すなわち、磁石
11の周囲をコイル141〜148が回転する。この結
果、コイル141〜148と鎖交する磁石11の磁束密度
が正弦的に変化するため、図4に示すようにコイル14
1〜148には、誘導起電力v1〜v8が各々誘起される。
この誘導起電力v1〜v8による電流i1〜i2は、ダイオ
ード151〜158により各々半波整流され、コンデンサ
16に流れ、該コンデンサ16には、電荷が蓄積され起
電力Vが発生する。
At the time of acceleration, as shown in FIG. 3, the main body case 5 and the yokes 131 to 138 (coils 141 to
148) rotates about the central axis G at an angular velocity ω.
On the other hand, since the shaft member 20, the inertial disk 9 and the magnet 11 are rotatably supported by the bearings 6 and 7, the stationary state is maintained according to the law of inertia. That is, the coils 141 to 148 rotate around the magnet 11. As a result, since the magnetic flux density of the magnet 11 that links the coils 141 to 148 changes sinusoidally, as shown in FIG.
Induced electromotive forces v1 to v8 are induced in 1 to 148, respectively.
The currents i1 to i2 generated by the induced electromotive forces v1 to v8 are half-wave rectified by the diodes 151 to 158 and flow into the capacitor 16, where electric charges are accumulated in the capacitor 16 to generate an electromotive force V.

【0014】そして、上記磁石11等は、ベアリング
6、7の摩擦力により除々に回転し、発射から10〜2
0sec経過すると、本体ケース5等と同一の角速度ω
で回転する。すなわち、磁石11等と本体ケース5との
回転差がなくなることから、上記コイル141〜148に
は誘導起電力v1〜v8が誘起されず発電が終了する。
The magnet 11 and the like gradually rotate due to the frictional force of the bearings 6 and 7, and 10 to 2 from the firing.
After 0 seconds, the same angular velocity ω as that of the main body case 5 etc.
Rotate with. That is, since there is no difference in rotation between the magnet 11 and the like and the main body case 5, induced electromotive forces v1 to v8 are not induced in the coils 141 to 148, and power generation ends.

【0015】そして、上記コンデンサ16に充電された
電荷は、図示しないトリガスイッチ等により放電され、
前述した電子回路等へ供給される。
The electric charge charged in the capacitor 16 is discharged by a trigger switch (not shown) or the like,
It is supplied to the electronic circuit and the like described above.

【0016】[0016]

【発明の効果】本発明によれば、機構が単純でコストが
安く、かつ保管・管理が容易な信管用電源を得ることが
できる。
According to the present invention, it is possible to obtain a fuze power source having a simple mechanism, low cost, and easy storage and management.

【図面の簡単な説明】[Brief description of the drawings]

【図1】本発明の一実施形態による信管用電源が内蔵さ
れた信管が装着された旋転弾1の構成を示す側面図であ
る。
FIG. 1 is a side view showing a configuration of a turning bullet 1 equipped with a fuze including a fuze power source according to an embodiment of the present invention.

【図2】図1に示す信管用電源4の構成を示す拡大断面
図である。
FIG. 2 is an enlarged cross-sectional view showing the configuration of the fuze power supply 4 shown in FIG.

【図3】図2に示すA−A’線視断面図である。3 is a cross-sectional view taken along the line A-A ′ shown in FIG.

【図4】本発明の一実施形態による信管用電源の電気的
構成を示す回路図である。
FIG. 4 is a circuit diagram showing an electrical configuration of a fuze power supply according to an embodiment of the present invention.

【符号の説明】[Explanation of symbols]

1 旋転弾 3 信管 4 信管用電源 5 本体ケース 6、7 ベアリング 9 慣性円盤 11 磁石 141〜148 コイル 16 コンデンサ 20 軸部材 1 Rotating bullet 3 Fuze 4 Fuze power supply 5 Main body case 6, 7 Bearing 9 Inertial disk 11 Magnet 141 to 148 Coil 16 Capacitor 20 Shaft member

Claims (3)

【特許請求の範囲】[Claims] 【請求項1】 スピンしながら飛行する信管内部に設け
られたケースと、 自身の中心軸と前記信管の中心軸とが一致するように前
記ケースに軸受手段を介して回転自在に軸支された軸部
材と、 前記軸部材に取り付けられた磁石と、 前記ケースに設けられ、前記磁石の周囲に配設された複
数のコイルと、 とを具備することを特徴とする信管用電源。
1. A case provided inside a fuze that flies while spinning, and rotatably supported by a case via bearing means so that the center axis of the case coincides with the center axis of the fuze. A fuze power supply, comprising: a shaft member; a magnet attached to the shaft member; and a plurality of coils provided in the case and arranged around the magnet.
【請求項2】 前記複数のコイルに誘起される電力を蓄
積する電力蓄積手段、 を具備することを特徴とする請求項1に記載の信管用電
源。
2. The fuze power supply according to claim 1, further comprising: a power storage unit that stores power induced in the plurality of coils.
【請求項3】 前記軸部材に取り付けられた重量付加手
段、 を具備することを特徴とする請求項1または2に記載の
信管用電源。
3. The fuze power source according to claim 1, further comprising a weight adding unit attached to the shaft member.
JP25902295A 1995-10-05 1995-10-05 Power source for fuse Pending JPH09105600A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP25902295A JPH09105600A (en) 1995-10-05 1995-10-05 Power source for fuse

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP25902295A JPH09105600A (en) 1995-10-05 1995-10-05 Power source for fuse

Publications (1)

Publication Number Publication Date
JPH09105600A true JPH09105600A (en) 1997-04-22

Family

ID=17328268

Family Applications (1)

Application Number Title Priority Date Filing Date
JP25902295A Pending JPH09105600A (en) 1995-10-05 1995-10-05 Power source for fuse

Country Status (1)

Country Link
JP (1) JPH09105600A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100988849B1 (en) * 2006-09-14 2010-10-20 닛타 고지 generator
KR101249803B1 (en) * 2011-07-25 2013-04-02 국방과학연구소 Apparatus of ammunition fuze

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100988849B1 (en) * 2006-09-14 2010-10-20 닛타 고지 generator
US7939983B2 (en) 2006-09-14 2011-05-10 Norimasa Okamoto Generator having first and second windings with same-direction electromotive forces
KR101249803B1 (en) * 2011-07-25 2013-04-02 국방과학연구소 Apparatus of ammunition fuze

Similar Documents

Publication Publication Date Title
US5831358A (en) Rotor end cap
US4665332A (en) Electric generator assembly for a projectile
CN107425647B (en) On-board flywheel battery with five-degree-of-freedom hybrid magnetic bearing
US5271328A (en) Pendulum based power supply for projectiles
CN105896819B (en) Device and method for driving rotor to generate electric energy
US4591746A (en) Ignition signal generator for internal combustion engines
KR101546822B1 (en) Wind Power Generator
US10804819B2 (en) Pulsed start-up system for electrostatic generators
US8443726B2 (en) Miniature safe and arm (S and A) mechanisms for fuzing of gravity dropped small weapons
JPS6287666A (en) Chain saw or similar portable type working machine operated by internal combustion engine
US4004519A (en) Projectile power generator
NO130801B (en)
US5101728A (en) Precision guided munitions alternator
JPS58127659A (en) Power source for heart fine movement remover
CA1062959A (en) Spinning projectile equipped with an electromagnetic ignition current generator
CA1037777A (en) Projectile fuse for a spinning projectile containing a detonator cap and an electromagnetic firing or ignition current generator
JPH09105600A (en) Power source for fuse
US3973500A (en) Electromagnetic generator for projectiles
JPH09113199A (en) Trigger source for fuse
US2990776A (en) Wind driven generator
JP2002130278A (en) Flywheel type power-storing device and magnetic bearing device
PL347826A1 (en) Mortar fuze with a rotatable fan
US2681008A (en) Fuse
CN108365698A (en) A kind of flying wheel battery of round trip flight wheel construction
US2692957A (en) Permanent magnet type generator

Legal Events

Date Code Title Description
A02 Decision of refusal

Free format text: JAPANESE INTERMEDIATE CODE: A02

Effective date: 20011016