JP4083363B2 - Injection battery - Google Patents

Injection battery Download PDF

Info

Publication number
JP4083363B2
JP4083363B2 JP2000045590A JP2000045590A JP4083363B2 JP 4083363 B2 JP4083363 B2 JP 4083363B2 JP 2000045590 A JP2000045590 A JP 2000045590A JP 2000045590 A JP2000045590 A JP 2000045590A JP 4083363 B2 JP4083363 B2 JP 4083363B2
Authority
JP
Japan
Prior art keywords
ampoule
head
inner case
case
type battery
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 - Lifetime
Application number
JP2000045590A
Other languages
Japanese (ja)
Other versions
JP2001236944A (en
Inventor
光弘 中西
朋也 渡邉
保廣 西村
哲次 林
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.)
Panasonic Corp
Panasonic Holdings Corp
Original Assignee
Panasonic Corp
Matsushita Electric Industrial 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 Panasonic Corp, Matsushita Electric Industrial Co Ltd filed Critical Panasonic Corp
Priority to JP2000045590A priority Critical patent/JP4083363B2/en
Publication of JP2001236944A publication Critical patent/JP2001236944A/en
Application granted granted Critical
Publication of JP4083363B2 publication Critical patent/JP4083363B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • Y02E60/12

Landscapes

  • Filling, Topping-Up Batteries (AREA)
  • Primary Cells (AREA)

Description

【0001】
【発明の属する技術分野】
本発明は、電解液を封入したガラスアンプルを外部衝撃により破壊して発電させる注液式電池に関するもので、特にアンプルを保持する部分の改良に関するものである。
【0002】
【従来の技術】
電解液を封入したガラスアンプルを外部衝撃により破壊して発電させる注液式電池は、保存特性が良好であるとともにアンプルを破壊すれば直ちに発電して所望とする性能を発揮するので、砲弾などの飛翔体に搭載された制御装置の電源として用いられている。
飛翔体に搭載された注液式電池は、飛翔体の発射時の衝撃力、すなわち発射方向と反対方向に加わる衝撃力によりガラスアンプルが破壊するように作られている。ところが近年は、飛翔体の自動装填方式が導入され、飛翔体を発射台に装填する際、発射衝撃とは逆方向の衝撃力が電池に印加されるようになった。従来は飛翔体の発射台への装填は手動により行われていたので、発射衝撃とは逆方向の衝撃力が印加されることは想定されていない。このため、従来の電池では、自動装填時に印加される発射衝撃とは逆方向の衝撃力によってアンプルが破壊してしまう。
そこで、アンプルの強度を強化することが考えられるが、アンプルの強度を上げると、通常作動時にアンプルが破壊されないという不都合が生じる。
【0003】
【発明が解決しようとする課題】
本発明は、以上に鑑み、従来の構成を大幅に変更せずに、飛翔体の自動装填時における逆方向の衝撃力を緩衝してアンプルが破壊せず、しかも通常作動時には正常に動作する注液式電池を提供することを目的とする。
【0004】
【課題を解決するための手段】
本発明の注液式電池は、発電要素を被覆するとともに中央空洞部に連通した電解液注入口を有する筒状の樹脂成形体からなる内ケース、前記中央空洞部内において前記内ケースの頂部閉塞部に頭部を当接し、底部がリング状座金に支持された電解液を封入したガラスアンプル、前記アンプルの底部と対向する内底部にアンプル破壊用突起を設けたアンプル受具、および前記内ケースを収容した金属製外装ケースを具備し、前記アンプルの頭部方向への推進力により生じる衝撃力によって前記アンプルを破壊して発電させる注液式電池であって、前記ガラスアンプルの頭部が、前記ガラスアンプルの本体から突出しており、前記突出した頭部を受ける内ケースの頂部閉塞部に、外装ケースとの間に空隙部を有する肉薄部で構成した衝撃吸収部を設けたことを特徴とする。
前記肉薄部の厚みは、1.0〜2.5mmであることが好ましい。
【0005】
【発明の実施の形態】
本発明は、発電要素を被覆するとともに中央空洞部に連通した電解液注入口を有する筒状の樹脂成形体からなる内ケース、前記中央空洞部内において前記内ケースの頂部閉塞部に頭部を当接し、底部がリング状座金に支持された電解液を封入したガラスアンプル、前記アンプルの底部と対向する内底部にアンプル破壊用突起を設けたアンプル受具、および前記内ケースを収容した金属製外装ケースを具備し、前記アンプルの頭部方向への推進力により生じる衝撃力によって前記アンプルを破壊して発電させる注液式電池において、前記アンプルを保護するためのものであった内ケースを改良し、アンプルの突出した頭部を受ける内ケースの頂部閉塞部に、外装ケースとの間に空隙部を有する肉薄部で構成した衝撃吸収部を設けるものである。
本発明によれば、従来の樹脂成形体からなる内ケースの一部分を変更するのみで、逆方向の衝撃力を上記の衝撃吸収部で緩衝し、アンプルの破壊を防止し、しかも通常の衝撃力を受けた際には従来と全く同様に作動する注液式電池を得ることができる。
【0006】
以下、本発明の実施の形態を図面を参照して説明する。
1は筒部1aと上蓋1bとを一体プレス加工により接合した金属製の外装ケースであり、その内部には樹脂製の内ケース3が収容されている。外装ケース1の底部は樹脂製の下蓋2により閉塞されている。
ケース1の上部に設けたソケット4には、正、負極端子をはじめ、電池使用機器の制御装置に接続される端子部が設けられている。
内ケース3は、リング状の発電要素5を内外から被覆して中央に空洞部7を有するようにモールド成形したものである。発電要素5は、例えば鉛粉を活物質とする負極板、セルロース製セパレータ、および二酸化鉛粉を活物質とする正極板からなる単セルを直列接続となるように積層したものである。発電要素5を収容した内ケース3の内部には、空洞部7と連通するスリット(図示しない)から電解液が注入される。そして、電池を搭載した飛翔体の回転により生じる遠心力によって瞬時に電解液が発電要素の隅々にまで供給されるようになっている。内ケース3内には、過剰に供給される電解液を吸収して液絡を防止するダミーセルからなる余剰液収容部6を有する。
【0007】
内ケース3の中央空洞部7には、過塩素酸水溶液からなる電解液8を収容したガラスアンプル9がセットされる。すなわち、アンプル9は、その本体から突出した頭部を有し、その頭部が空洞部7の頂部閉塞部12に当接され、底部がリング状の座金10で支持される。座金10は、空洞部7へ押し込んで固定したコップ状のアンプル受具11の上部にセットされている。アンプル受具11はその内底部に突起11aを有している。
この電池は、その頭部が飛翔体の進行方向となるように装着され、飛翔体発射時には、その進行方向に加速度が加えられる結果、アンプル9は座金10をたわませて受具11内へ落下し、突起11aに衝突して破壊する。アンプルから開放された電解液は、飛翔体の回転により生じる遠心力により、空洞部7と連通するスリットから内ケース3内へ入り、電池を発電可能とする。
【0008】
上記の構成においては、電池に対して上記とは反対方向の衝撃力が加えられたとき、アンプルは内ケース3の頂部閉塞部12に衝突することとなる。従来においては、頂部閉塞部12は肉厚であり、かつ上蓋1bに接していたので、前記のような衝撃力が加えられると、アンプル9は容易に破壊してしまう。
【0009】
本実施の形態においては、以下のようにして頂部閉塞部12に衝撃吸収部として作用するように構成した。
内ケース3における空洞部7の頂部閉塞部12は、そのケース1の上蓋1bとの間に空隙部13を形成することにより肉薄部とし、これによってアンプル9に対する衝撃吸収部を構成している。
この肉薄部は、これに接するアンプルの頭部より一回り大きい面積を有するものとし、厚みは1.0〜2.5mmとすると、適度の弾性を有するものとなり、アンプルに対する衝撃吸収部として有効に働く。肉薄部と上蓋1bとの隙間は、アンプルに対する衝撃により肉薄部が上方にたわんだ際上蓋1bに衝突しないように、2.0〜4.0mmとするのが適当である。従来の内ケースでは、頂部閉塞部12は、直に上蓋1bに接し、厚み5mm程度であった。本発明によれば、内ケース3の頂部閉塞部12を部分的に改良するのみで、逆方向の衝撃力が印加されたときのアンプルの破壊を防止することができる。
頂部閉塞部12によりアンプルを保護する衝撃吸収部とする代わりに、アンプルの頭部へ衝撃吸収材などを取り付ける方法も考えられる。しかし、そのような別部材を加えると、電池活性化のためにアンプルを破壊させたとき、それらの部材が電解液の発電部への供給を阻害することとなる。従って、別部材を加えるのは採用できない。
【0010】
【実施例】
次に具体的な実施例を示す。
図示のような構成において、アンプル9として、頭部の直径約5mmで重量約2.4gのものを用いた。内ケース3は、ポリ塩化ビニル製で、頂部閉塞部12の肉薄部は、直径約8mmの円形で、厚み2.0mmとした。また、肉薄部と上蓋1bとの空隙は2.5mmとした。この内ケースを用いた本発明による電池をaとし、空隙部13を設けない内ケースを用いた比較例の電池をbとする。
これらの電池について、飛翔体に装填したときの発射衝撃とは逆方向の衝撃力を印加してアンプルが破壊するかどうかを調べた。その結果を表1に示す。なお、試料数は各50個とした。
【0011】
【表1】

Figure 0004083363
【0012】
表から明らかなように、比較例の電池bは、逆方向の衝撃力58,800m/S2(6000G)を印加したとき破壊率は30%に達し、78,400m/S2(8000G)を印加したとき破壊率は90%である。これに対して、本発明による電池aは、逆方向の衝撃力58,800m/S2(6000G)を印加したとき破壊率は0であり、78,400m/S2(8000G)を印加しても破壊率は30%である。因みに飛翔体発射時の衝撃力は11,760〜58,800m/S2(1,200〜6,000G)である。
【0013】
【発明の効果】
以上のように本発明によれば、本来の性能を損なうことなく、逆方向の衝撃力でアンプルが破壊しない注液式電池を提供することができる。
【図面の簡単な説明】
【図1】本発明の一実施例における注液式電池の縦断面図である。
【符号の説明】
1 外装ケース
1a 筒部
1b 上蓋
2 下蓋
3 内ケース
4 ソケット
5 発電要素
6 余剰液収容部
7 空洞部
8 電解液
9 アンプル
10 座金
11 アンプル受具
11a 突起
12 頂部閉塞部
13 空隙部[0001]
BACKGROUND OF THE INVENTION
The present invention relates to a liquid injection type battery that generates power by breaking a glass ampoule in which an electrolytic solution is encapsulated by an external impact, and particularly relates to improvement of a portion that holds the ampoule.
[0002]
[Prior art]
The injection type battery that generates electricity by breaking the glass ampoule encapsulating the electrolyte with external impact has good storage characteristics, and if the ampoule is destroyed, it immediately generates power and exhibits the desired performance. It is used as a power source for control devices mounted on flying objects.
The liquid injection type battery mounted on the flying object is made so that the glass ampoule is destroyed by the impact force when the flying object is launched, that is, the impact force applied in the direction opposite to the launching direction. However, in recent years, an automatic loading method for flying objects has been introduced, and when a flying object is loaded on a launch pad, an impact force in the direction opposite to the firing impact is applied to the battery. Conventionally, since the flying object is manually loaded on the launch pad, it is not assumed that an impact force in the direction opposite to the launch impact is applied. For this reason, in the conventional battery, the ampoule is destroyed by the impact force in the direction opposite to the firing impact applied during automatic loading.
Therefore, it is conceivable to increase the strength of the ampule. However, when the strength of the ampule is increased, there is a disadvantage that the ampule is not broken during normal operation.
[0003]
[Problems to be solved by the invention]
In view of the above, the present invention does not significantly change the conventional configuration, buffers the impact force in the reverse direction when the flying object is automatically loaded, does not break the ampule, and operates normally during normal operation. An object is to provide a liquid battery.
[0004]
[Means for Solving the Problems]
An injection type battery according to the present invention includes an inner case made of a cylindrical resin molded body that covers an electric power generation element and has an electrolyte injection port communicating with a central cavity, and a top closing portion of the inner case in the central cavity A glass ampule in which an electrolyte solution whose bottom is supported by a ring washer is sealed, an ampule holder having an ampule breaking projection on the inner bottom portion facing the bottom portion of the ampule, and the inner case A liquid-filled battery comprising a metal outer case accommodated and generating power by destroying the ampoule by an impact force generated by a propulsive force toward the head of the ampoule, wherein the head of the glass ampoule is protrudes from the body of the glass ampoule, on top closed portion of the case for receiving the head and the projecting, the impact absorbing portion configured in thin portion having a gap portion between the outer case And wherein the digit.
The thickness of the thin part is preferably 1.0 to 2.5 mm.
[0005]
DETAILED DESCRIPTION OF THE INVENTION
The present invention includes an inner case made of a cylindrical resin molded body that covers an electric power generation element and has an electrolyte inlet that communicates with a central cavity, and a head is applied to the top closed portion of the inner case in the central cavity. A glass ampule in contact with and enclosing an electrolyte solution supported by a ring washer, an ampule holder provided with an ampule breaking projection on an inner bottom portion facing the bottom portion of the ampule, and a metal exterior housing the inner case In a liquid injection type battery having a case and generating power by destroying the ampoule by an impact force generated by a propulsive force toward the head of the ampoule, the inner case which was intended to protect the ampoule was improved. An impact absorbing portion constituted by a thin portion having a gap between the outer case and the outer case is provided at the top closed portion of the inner case that receives the head from which the ampule protrudes .
According to the present invention, the impact force in the reverse direction is buffered by the above-mentioned impact absorbing portion only by changing a part of the inner case made of the conventional resin molded body, and the ampoule is prevented from being broken, and the normal impact force is also provided. When this is received, a liquid injection type battery that operates in the same manner as before can be obtained.
[0006]
Hereinafter, embodiments of the present invention will be described with reference to the drawings.
Reference numeral 1 denotes a metal outer case in which a cylindrical portion 1a and an upper lid 1b are joined by integral pressing, and a resin inner case 3 is accommodated therein. The bottom of the outer case 1 is closed by a resin lower lid 2.
The socket 4 provided in the upper part of the case 1 is provided with terminal portions that are connected to a control device for battery-powered equipment, including positive and negative terminals.
The inner case 3 is formed by covering a ring-shaped power generation element 5 from the inside and outside and molding it so as to have a hollow portion 7 in the center. The power generation element 5 is formed by stacking, for example, single cells composed of a negative electrode plate using lead powder as an active material, a separator made of cellulose, and a positive electrode plate using lead dioxide powder as an active material so as to be connected in series. An electrolyte is injected into the inside of the inner case 3 containing the power generation element 5 from a slit (not shown) communicating with the cavity 7. Then, the electrolytic solution is instantaneously supplied to every corner of the power generation element by the centrifugal force generated by the rotation of the flying body on which the battery is mounted. The inner case 3 has a surplus liquid container 6 made of a dummy cell that absorbs an excessively supplied electrolyte and prevents a liquid junction.
[0007]
A glass ampoule 9 containing an electrolytic solution 8 made of a perchloric acid aqueous solution is set in the central cavity 7 of the inner case 3. That is, the ampoule 9 has a head protruding from the main body, the head is in contact with the top closing part 12 of the cavity 7, and the bottom is supported by the ring-shaped washer 10. The washer 10 is set on the upper part of a cup-shaped ampoule receiver 11 which is pushed into the cavity 7 and fixed. The ampoule receiver 11 has a protrusion 11a on its inner bottom.
This battery is mounted so that its head is in the traveling direction of the flying object, and when the flying object is launched, acceleration is applied in the traveling direction. As a result, the ampoule 9 deflects the washer 10 into the receiver 11. It falls and collides with the protrusion 11a to destroy it. The electrolytic solution released from the ampoule enters the inner case 3 through the slit communicating with the cavity 7 by the centrifugal force generated by the rotation of the flying body, and enables the battery to generate power.
[0008]
In the above configuration, when an impact force in the opposite direction to the above is applied to the battery, the ampoule collides with the top closing portion 12 of the inner case 3. Conventionally, the top closing portion 12 is thick and is in contact with the upper lid 1b. Therefore, when the impact force as described above is applied, the ampoule 9 is easily broken.
[0009]
In the present embodiment, the top closing portion 12 is configured to act as an impact absorbing portion as follows.
The top closing portion 12 of the hollow portion 7 in the inner case 3 is formed into a thin portion by forming a gap portion 13 between the upper lid 1 b of the case 1, thereby constituting an impact absorbing portion for the ampoule 9.
This thin part has an area that is slightly larger than the head of the ampoule in contact with this, and if the thickness is 1.0 to 2.5 mm, it has moderate elasticity and is effective as an impact absorbing part for the ampoule. work. The gap between the thin portion and the upper lid 1b is suitably 2.0 to 4.0 mm so that the thin portion does not collide with the upper lid 1b when the thin portion is bent upward due to an impact on the ampoule. In the conventional inner case, the top closing portion 12 is in direct contact with the upper lid 1b and has a thickness of about 5 mm. According to the present invention, the ampoule can be prevented from being broken when a reverse impact force is applied by only partially improving the top closing portion 12 of the inner case 3.
A method of attaching a shock absorbing material or the like to the head of the ampoule instead of the shock absorbing part for protecting the ampoule by the top closing part 12 can be considered. However, when such another member is added, when the ampoule is broken for battery activation, these members impede the supply of the electrolytic solution to the power generation unit. Therefore, it is not possible to employ another member.
[0010]
【Example】
Next, specific examples will be described.
In the configuration shown in the figure, the ampule 9 having a head diameter of about 5 mm and a weight of about 2.4 g was used. The inner case 3 was made of polyvinyl chloride, and the thin portion of the top closing portion 12 was a circle having a diameter of about 8 mm and had a thickness of 2.0 mm. The gap between the thin part and the upper lid 1b was 2.5 mm. The battery according to the present invention using the inner case is denoted by a, and the battery of the comparative example using the inner case without the gap 13 is denoted by b.
For these batteries, it was investigated whether or not the ampoule was destroyed by applying an impact force in the direction opposite to the launch impact when loaded on the flying object. The results are shown in Table 1. The number of samples was 50 each.
[0011]
[Table 1]
Figure 0004083363
[0012]
As is clear from the table, the battery b of the comparative example had a fracture rate of 30% when a reverse impact force of 58,800 m / S 2 (6000 G) was applied, and 78,400 m / S 2 (8000 G) was applied. Sometimes the destruction rate is 90%. On the other hand, the battery a according to the present invention has a fracture rate of 0 when a reverse impact force of 58,800 m / S 2 (6000 G) is applied, and breaks even when 78,400 m / S 2 (8000 G) is applied. The rate is 30%. Incidentally, the impact force when launching a flying object is 11,760 to 58,800 m / S 2 (1,200 to 6,000 G).
[0013]
【The invention's effect】
As described above, according to the present invention, it is possible to provide a liquid injection type battery in which an ampoule is not broken by an impact force in a reverse direction without impairing the original performance.
[Brief description of the drawings]
FIG. 1 is a longitudinal sectional view of an injection type battery in one embodiment of the present invention.
[Explanation of symbols]
DESCRIPTION OF SYMBOLS 1 Exterior case 1a Cylinder part 1b Upper cover 2 Lower cover 3 Inner case 4 Socket 5 Power generation element 6 Excess liquid storage part 7 Cavity part 8 Electrolytic solution 9 Washer 11 Ampoule receiver 11a Protrusion 12 Top part obstruction | occlusion part 13 Cavity part

Claims (2)

発電要素を被覆するとともに中央空洞部に連通した電解液注入口を有する筒状の樹脂成形体からなる内ケース、前記中央空洞部内において前記内ケースの頂部閉塞部に頭部を当接し、底部がリング状座金に支持された電解液を封入したガラスアンプル、前記アンプルの底部と対向する内底部にアンプル破壊用突起を設けたアンプル受具、および前記内ケースを収容した金属製外装ケースを具備し、前記アンプルの頭部方向への推進力により生じる衝撃力によって前記アンプルを破壊して発電させる注液式電池であって、前記ガラスアンプルの頭部が、前記ガラスアンプルの本体から突出しており、前記突出した頭部を受ける内ケースの頂部閉塞部に、外装ケースとの間に空隙部を有する肉薄部で構成した衝撃吸収部を設けたことを特徴とする注液式電池。An inner case made of a cylindrical resin molded body that covers the power generation element and has an electrolyte inlet that communicates with the central cavity, the head abutting on the top closed portion of the inner case in the central cavity, and the bottom A glass ampoule enclosing an electrolyte supported by a ring washer, an ampoule holder provided with an ampoule breaking projection on the inner bottom part facing the bottom part of the ampoule, and a metal outer case housing the inner case A liquid injection type battery that generates power by destroying the ampoule by an impact force generated by a propulsive force in the head direction of the ampoule, wherein the head of the glass ampoule protrudes from the main body of the glass ampoule, on top closed portion of the case inner receiving the head and the protruding, characterized in that a shock absorbing portion constituted by the thin portion having a gap portion between the outer case Liquid type battery. 前記肉薄部の厚みが1.0〜2.5mmである請求項1記載の注液式電池。  The injection type battery according to claim 1, wherein the thin portion has a thickness of 1.0 to 2.5 mm.
JP2000045590A 2000-02-23 2000-02-23 Injection battery Expired - Lifetime JP4083363B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2000045590A JP4083363B2 (en) 2000-02-23 2000-02-23 Injection battery

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2000045590A JP4083363B2 (en) 2000-02-23 2000-02-23 Injection battery

Publications (2)

Publication Number Publication Date
JP2001236944A JP2001236944A (en) 2001-08-31
JP4083363B2 true JP4083363B2 (en) 2008-04-30

Family

ID=18568146

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2000045590A Expired - Lifetime JP4083363B2 (en) 2000-02-23 2000-02-23 Injection battery

Country Status (1)

Country Link
JP (1) JP4083363B2 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL1022034C2 (en) * 2002-11-29 2004-06-11 Thales Nederland Bv Spare battery and its application options.
JP2008071745A (en) * 2006-08-17 2008-03-27 Matsushita Electric Ind Co Ltd Liquid filling battery
JP2008071741A (en) * 2006-08-18 2008-03-27 Matsushita Electric Ind Co Ltd Liquid injection battery
KR101125519B1 (en) * 2009-07-08 2012-03-23 주식회사 비츠로셀 reserved battery
KR101293523B1 (en) 2012-01-25 2013-08-06 주식회사 비츠로셀 Reserve battary type of ampoule
CN110556505B (en) * 2019-08-26 2024-02-09 龙能科技(宁夏)有限责任公司 Machine adjusting device and method for liquid injection pump of liquid injection machine

Also Published As

Publication number Publication date
JP2001236944A (en) 2001-08-31

Similar Documents

Publication Publication Date Title
CN100382358C (en) Battery and battery pack
JP4083363B2 (en) Injection battery
US6844108B1 (en) Ultraminiaturized reserve battery cell
US6080506A (en) Pressure activated current interrupter for electrochemical cells
US3592693A (en) Consumable metal anode with dry electrolytic enclosed in envelope
JPH06215746A (en) Explosion-proof safety device and battery having it
JPH10302811A (en) Liquid injection type battery
JP2007323878A (en) Immersion cell
JP2007265762A (en) Immersion cell
US20090202891A1 (en) Inertially activated battery
US2990442A (en) Spin activated battery
US3343993A (en) Deferred action battery comprising independently completely closed containers
US3556858A (en) Control apparatus
JPH11111244A (en) Sealed storage battery
JPS6118613Y2 (en)
GB1160193A (en) Improvements in or relating to Electric Current-Producing Cells
JP6071336B2 (en) Non-aqueous electrolyte secondary battery and battery module using the same
JP4352116B2 (en) Injection battery
JP4130647B2 (en) Injection battery
KR20190095176A (en) Activation of the electrolyte injection system stockpile battery
JPS63236255A (en) Cylindrical alkaline battery
JP4423143B2 (en) Injection battery
JP2000084105A (en) Car battery and device for stopping function of car battery
CN216301493U (en) High unmanned aerial vehicle data storage device of security
JP2004319176A (en) Liquid filling battery

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20040311

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20071017

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20071025

A521 Written amendment

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20071218

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20080117

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20080213

R150 Certificate of patent or registration of utility model

Free format text: JAPANESE INTERMEDIATE CODE: R150

Ref document number: 4083363

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20110222

Year of fee payment: 3

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20120222

Year of fee payment: 4

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20130222

Year of fee payment: 5

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20130222

Year of fee payment: 5

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20140222

Year of fee payment: 6

EXPY Cancellation because of completion of term