JPH06257991A - Supporting structure for gun barrel - Google Patents

Supporting structure for gun barrel

Info

Publication number
JPH06257991A
JPH06257991A JP6596493A JP6596493A JPH06257991A JP H06257991 A JPH06257991 A JP H06257991A JP 6596493 A JP6596493 A JP 6596493A JP 6596493 A JP6596493 A JP 6596493A JP H06257991 A JPH06257991 A JP H06257991A
Authority
JP
Japan
Prior art keywords
barrel
support
breech
gun
taper
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.)
Granted
Application number
JP6596493A
Other languages
Japanese (ja)
Other versions
JP3241853B2 (en
Inventor
Moriyoshi Yoshimatsu
盛喜 吉松
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.)
Japan Steel Works Ltd
Original Assignee
Japan Steel Works 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 Japan Steel Works Ltd filed Critical Japan Steel Works Ltd
Priority to JP06596493A priority Critical patent/JP3241853B2/en
Publication of JPH06257991A publication Critical patent/JPH06257991A/en
Application granted granted Critical
Publication of JP3241853B2 publication Critical patent/JP3241853B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Abstract

PURPOSE:To absorb thermal expansion, processing error of a gun barrel by interposing an elastic element between a supporting part of a support and an outer periphery of the barrel in a supporting structure for supporting an intermediate part of the barrel by the part of the cylindrical support integral with a sliding breech of a gun. CONSTITUTION:A sliding breech 2 of a machine gun is supported to a cradle 4 supported to a carriage through a height unit 8, and a base end of a gun barrel 1 is mounted at an end of the breech 2 through a stepped spring 10. A cylindrical support 9 concentric with the barrel 1 is fixed to an end face of the breech 2. In this case, an annular cutout 9b is formed at a supporting part 9a of a part opposed to a longitudinal intermediate part of the barrel 1 of the support 9, and an annular supporting unit 11 is provided at the cutout 9b. The unit 11 is formed in a structure in which a pair of taper rings are provided between an inner ring and an outer ring made of elastic materials such as rubber, elastomer, etc., to absorb thermal expansion, processing error of the barrel 1 by elastic deformations of the materials.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は、砲身の支持構造に関す
るものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a barrel supporting structure.

【0002】[0002]

【従来の技術】機関砲等の砲において砲尾部に取付ける
砲身は、従来、取付け、取外し作業性を考慮した取付け
構造となつており、一般的には図8に示すように砲身1
の基端部を砲尾部2に段隔ねじ10にて結合させてい
る。そして、砲身1の自重によるたわみ(垂下量)を減
少させ、かつ、砲身1の砲尾部2に対する振れ量を軽減
させるため、砲尾部2の前端に筒状のサポート50を固
着し、このサポート50の先端部の内向きフランジ状を
なす支持部50aによつて砲身1の中間部外周面を支え
ることが行われている。
2. Description of the Related Art A gun barrel attached to the breech of a machine gun or the like has conventionally been constructed so as to be easily attached and detached. Generally, as shown in FIG.
The base end portion of is connected to the breech portion 2 with a step screw 10. Then, in order to reduce the deflection (hanging amount) of the barrel 1 due to its own weight and reduce the amount of deflection of the barrel 1 with respect to the breech part 2, a tubular support 50 is fixed to the front end of the breech part 2, and this support 50 The outer peripheral surface of the intermediate portion of the barrel 1 is supported by the inward flange-shaped support portion 50a at the tip of the.

【発明が解決しようとする課題】[Problems to be Solved by the Invention]

【0003】しかしながら、このような従来の砲身の支
持構造にあつては、砲尾部2と砲身1との間の段隔ねじ
10部分及び砲身1とサポート50の支持部50aとの
間に、図9に示す弾丸18の発射に伴う砲身1の熱膨
張、加工精度等を考慮してある程度の隙間2c,2d,
bを設けているため、砲の射撃に際して弾着点のばらつ
き、いわゆる射弾散布が大きくなり、命中率が低下する
という技術的課題が存在している。
However, in such a conventional supporting structure for a barrel, a stepping screw 10 portion between the breech portion 2 and the barrel 1 and a portion between the barrel 1 and the supporting portion 50a of the support 50 are illustrated. Considering the thermal expansion of the barrel 1 associated with the firing of the bullet 18 shown in FIG.
Since b is provided, there is a technical problem that the dispersion of the impact points when shooting the gun, that is, the so-called shot dispersion becomes large and the hit rate decreases.

【0004】射弾散布に与える要因としては、一般には
下記のものが考えられる。 ア.弾丸18の重量、重心等のばらつき イ.発射薬の量、性状のばらつき ウ.弾丸18の初速のばらつき エ.照準誤差 オ.風等の外的要因 カ.砲架又は砲身1の振れによる砲口1aの向きの変化 キ.砲身1の振れによる弾丸18への横方向速度の付加
The following factors are generally conceivable as factors affecting the spray dispersion. A. Variation in weight and center of gravity of bullet 18 a. Variation in amount and properties of propellant c. Initial velocity variation of bullet 18 d. Aiming error e. External factors such as wind power. Changes in the orientation of the muzzle 1a due to the swing of the gun rack or barrel 1. Addition of lateral velocity to bullet 18 due to deflection of barrel 1

【0005】ここで、砲身1に関係する上記のカ.キ.
項の現象が生ずる理由については、次のようである。弾
丸18の発射に際しては、砲身1内に高圧のガスが急激
に発生し、また、この高圧ガスが弾丸18を砲口1aに
向けて強く押し出す。その際、砲身1が振動する。この
振動に起因して、段隔ねじ10部分又はサポート50の
支持部50aに隙間2c,2d,bを有する状態におい
て、先ず、砲身1が主として段隔ねじ10の隙間2c分
だけ一次振れ角度αにて振れ、砲口1aの向きに変化を
生じる。次に、振動する砲身1は、支持部50aの内面
に激突して一旦停止し、続いて反対方向に跳ね返つて一
旦復帰した後更に二次振れ角度α’にて振れ、砲口1a
の向きに変化を生じ、弾丸18の飛び出す方向にばらつ
きを生ずることとなる。なお、隙間bは支持部50aの
内面と砲身1との隙間、隙間2cは段隔ねじ10の中心
軸線方向の隙間、隙間2dは段隔ねじ10付近の砲身1
と砲尾部2との間の隙間である。
Here, the above-mentioned power supply related to the barrel 1. G.
The reason for the phenomenon of the term is as follows. When the bullet 18 is fired, high-pressure gas is rapidly generated in the barrel 1, and the high-pressure gas strongly pushes the bullet 18 toward the muzzle 1a. At that time, the barrel 1 vibrates. Due to this vibration, in the state where the gaps 2c, 2d, and b are provided in the step screw 10 portion or the support portion 50a of the support 50, first, the barrel 1 is mainly moved by the gap 2c of the step screw 10 and the primary deflection angle α. Shakes and changes the direction of the muzzle 1a. Next, the vibrating barrel 1 crashes into the inner surface of the support portion 50a, temporarily stops, then bounces in the opposite direction and once returns, and then further swings at the secondary deflection angle α ', and the muzzle 1a
Changes in the direction of the bullets 18 and causes variations in the direction in which the bullets 18 project. The gap b is the gap between the inner surface of the support portion 50a and the barrel 1, the gap 2c is the gap in the central axis direction of the step screw 10, and the gap 2d is the barrel 1 near the step screw 10.
And the breech section 2.

【0006】そして、跳ね返りの前・後では砲口1aの
振れる方向は反対で、かつ、跳ね返り前の振れ速度の方
が大きくなる。弾丸18は、通常この一次,二次振れの
間に砲口1aから発射される。そのため、砲口1aを出
るときの弾丸18は正規の進行方向に対して横方向の速
度を受ける。
Before and after the bounce, the muzzle 1a swings in the opposite direction, and the swing speed before the bounce is higher. The bullet 18 is normally fired from the muzzle 1a during the primary and secondary runouts. Therefore, when the bullet 18 exits the muzzle 1a, the bullet 18 receives a lateral velocity with respect to the normal traveling direction.

【0007】図9に示すように弾丸18が砲口1aを出
る際に砲口1aがVtの速度で一次振れを生じている場
合には、弾丸18は砲口1aの向きの速度Voと砲口1
aの速度Vtとの合成された方向に速度Vにて飛び出
し、砲口1aの向きからもそれる。このそれる角度は、
tan-1Vt/Vo=βとなる。例えば、砲口1aの速
度Vtが1m/sであり、弾丸18の速度がVo=10
00m/sの場合、β=1/1000となり、命中率の
低下をもたらす上で無視できない値となる。なお、弾丸
18が砲口1aを出る際に砲口1aがVt’の速度で二
次振れを生じている場合には、それる角度はβ’とな
る。
As shown in FIG. 9, when the muzzle 1a makes a primary runout at a speed of Vt when the muzzle 18 exits the muzzle 1a, the muzzle 18 moves toward the muzzle 1a at a speed Vo and Mouth 1
It jumps out at a velocity V in a direction combined with the velocity Vt of a and deviates from the direction of the muzzle 1a. This deviating angle is
tan −1 Vt / Vo = β. For example, the velocity Vt of the muzzle 1a is 1 m / s, and the velocity of the bullet 18 is Vo = 10.
In the case of 00 m / s, β = 1/1000, which is a value that cannot be ignored because the hit rate is reduced. In addition, when the muzzle 1a makes a secondary shake at a velocity of Vt ′ when the bullet 18 exits the muzzle 1a, the angle of deviation is β ′.

【0008】[0008]

【課題を解決するための手段】本発明は、このような従
来の技術的課題に鑑みてなされたものであり、その構成
は、砲の砲尾部2の先端部に砲身1の基端部を結合し、
該砲尾部2と一体をなす筒状のサポート9の支持部9a
により、該砲身1の中心軸線方向の中間部を支持する砲
身の支持構造であつて、該サポート9の支持部9aと砲
身1の外周面との間に、弾性体(12若しくは15又は
13,14)を介在させることを特徴とする砲身の支持
構造である。そして、弾性体(12若しくは15又は1
3,14)に初圧縮量を与えることができる。
SUMMARY OF THE INVENTION The present invention has been made in view of the above-mentioned conventional technical problems, and has a structure in which a base end portion of a barrel 1 is provided at a tip end portion of a breech portion 2 of a gun. Combine,
Support part 9a of a cylindrical support 9 that is integral with the breech part 2
With the structure for supporting the middle portion of the barrel 1 in the direction of the central axis, an elastic body (12 or 15 or 13, between the supporting portion 9a of the support 9 and the outer peripheral surface of the barrel 1 is provided. 14) is a barrel supporting structure characterized by interposing 14). And an elastic body (12 or 15 or 1
3, 14) can be given an initial compression amount.

【0009】[0009]

【作用】基端部を砲尾部に結合した砲身の中心軸線方向
の中間部を、砲尾部と一体をなす筒状のサポートの支持
部に設けた弾性体を介して支持した状態で、砲身内に弾
丸を供給して射撃すれば、砲身が振れる傾向を呈する。
しかして、砲身は、その中心軸線方向の中間部が、弾性
体によつて支持されているので、射撃に伴う振れが緩衝
されて良好に抑制される。
Function: Inside the barrel, with the intermediate part in the central axis direction of the barrel connecting the base end part to the turret part supported by the elastic body provided on the support part of the tubular support integrated with the turret part. If a bullet is supplied and shot at, the barrel will tend to swing.
Since the middle part of the barrel in the direction of the central axis is supported by the elastic body, the shake due to the shooting is buffered and suppressed well.

【0010】射撃に伴う砲身の一次振れは、弾性体が弾
性的に変形することによつて緩衝され、再び砲身を反対
方向へ振り戻すので二次振れを生ずる。この間に、弾性
体によつてエネルギが吸収される。
The primary deflection of the barrel caused by the shooting is buffered by the elastic deformation of the elastic body, and the barrel is swung back in the opposite direction, resulting in a secondary deflection. During this time, energy is absorbed by the elastic body.

【0011】しかして、射撃に際する砲身の一次,二次
振れ角度は著しく減少し、砲口の向きの正規な方向から
のずれ角は著しく減少する。更に、砲口の向きと直角方
向の砲口の速度も小さくなるので、弾丸が砲口の向きか
らそれる角度は著しく減少する。その結果、射弾散布が
小さくなる。すなわち、砲尾部と砲身との間の結合部
に、弾丸の発射に伴う砲身の熱膨張、加工精度等を考慮
してある程度の隙間を設けているが、この隙間を確保し
ながら、砲身とサポートの支持部との間の隙間を弾性体
によつて実質的に0として、射弾散布を小さくすること
ができる。なお、弾丸の発射に伴う砲身の熱膨張、加工
精度等は、弾性体が弾性変形することによつても吸収さ
れる。
However, the primary and secondary deflection angles of the barrel during firing are significantly reduced, and the deviation angle of the muzzle orientation from the normal direction is significantly reduced. Further, the velocity of the muzzle in the direction perpendicular to the muzzle direction is also reduced, so that the angle at which the bullet deviates from the muzzle direction is significantly reduced. As a result, the dispersion of shots is reduced. In other words, there is a certain amount of clearance at the joint between the breech and the barrel considering the thermal expansion of the barrel due to the firing of the bullet, the processing accuracy, etc. The gap between the support and the support can be made substantially zero by the elastic body, and the spraying can be made small. Note that the thermal expansion of the barrel, the processing accuracy, and the like that accompany the firing of the bullet are also absorbed by the elastic deformation of the elastic body.

【0012】そして、弾性体に初圧縮量を与えれば、弾
性体を適正な状態として、砲身とサポートの支持部との
間に緊密に介在させることができる。
If the elastic body is given an initial compression amount, the elastic body can be brought into a proper state and can be tightly interposed between the barrel and the support portion of the support.

【0013】[0013]

【実施例】以下、本発明の実施例について図面を参照し
て説明する。図1〜図7は、本発明に係る砲身の支持構
造を機関砲に適用した1実施例を示す。先ず、図1,図
2を参照して機関砲の要部について説明する。砲架5に
は、一対の耳軸6によつて揺架4の前端部が揺動自在に
支持され、砲架5と揺架4の前端部との間には高低装置
8が介在している。この揺架4には、その前後端部にそ
れぞれ両側のスライド7を介して砲尾部2が支持され、
砲尾部2の先端部には、砲身1の基端部が段隔ねじ10
によつて結合されている。また、砲尾部2内には、遊底
3が配設され、遊底3によつて砲身1内に弾丸18を供
給できるようになつている。なお、段隔ねじ10に代え
て、砲尾部2と砲身1の基端部との間を通常の嵌合い結
合とする場合もある。
Embodiments of the present invention will be described below with reference to the drawings. 1 to 7 show an embodiment in which a support structure for a barrel according to the present invention is applied to a machine gun. First, the essential parts of the machine gun will be described with reference to FIGS. A front end portion of the swing 4 is swingably supported on the gun rack 5 by a pair of ear shafts 6, and a height device 8 is interposed between the gun rack 5 and the front end portion of the rock rack 4. There is. The turret portion 2 is supported on the cradle 4 via slides 7 on both sides at the front and rear ends thereof,
At the tip of the breech section 2, the base end of the barrel 1 is a step screw 10
Are combined by. Further, a breech hole 3 is arranged in the turret portion 2 so that a bullet 18 can be supplied into the barrel 1 by the breech hole 3. It should be noted that the stepped screw 10 may be replaced by a normal fitting connection between the breech portion 2 and the base end portion of the barrel 1.

【0014】そして、砲尾部2の先端面には、砲身1と
同心状に筒状のサポート9が固着され、その先端部は内
向きフランジ状をなす支持部9aを形成し、この支持部
9aが砲身1の中心軸線方向の中間部に臨んでいる。こ
のサポート9の支持部9aの前端内周部に形成した環状
切欠き部9bには環状の支持装置11を設け、砲身1を
弾性的に支持させる。支持装置11は、図3に詳示する
ように内リング12、一対のテーパリング13,14、
外リング15及び複数個のボルト16を有し、内リング
12、外リング15及び一対のテーパリング13,14
がゴム又はエラストマからなる弾性体にて形成されてい
る。
A tubular support 9 concentric with the barrel 1 is fixed to the tip surface of the breech section 2, and the tip section forms a support section 9a having an inward flange shape. Faces the middle portion of the barrel 1 in the direction of the central axis. An annular support device 11 is provided in an annular notch 9b formed in the inner peripheral portion of the front end of the support 9a of the support 9 to elastically support the barrel 1. As shown in detail in FIG. 3, the support device 11 includes an inner ring 12, a pair of taper rings 13 and 14,
It has an outer ring 15 and a plurality of bolts 16, and has an inner ring 12, an outer ring 15 and a pair of taper rings 13, 14.
Is formed of an elastic body made of rubber or elastomer.

【0015】内リング12は、図4に示すようにスリッ
ト12aを有して欠環状をなし、拡径又は縮径変形が弾
性的に可能であると共に、外周面が、中心軸線方向の両
側に次第に縮径するテーパ面12b,12cを対称に形
成し、内周面が、砲身1の外周面に密着する円筒面12
dを形成している。外リング15は、図4に示すように
スリット15aを有して欠環状をなし、拡径又は縮径変
形が弾性的に可能であると共に、内周面が、中心軸線方
向の両側に次第に拡径するテーパ面15b,15cを対
称に形成し、外周面が、環状切欠き部9bに密着する円
筒面15dを形成している。
As shown in FIG. 4, the inner ring 12 has a slit 12a and is formed in an annular shape so that it can be elastically expanded or reduced in diameter, and its outer peripheral surfaces are located on both sides in the central axis direction. Cylindrical surface 12 in which tapered surfaces 12b and 12c that gradually decrease in diameter are formed symmetrically, and the inner peripheral surface is in close contact with the outer peripheral surface of barrel 1.
forming d. As shown in FIG. 4, the outer ring 15 has a slit 15a and has an annular shape, and can be elastically expanded or reduced in diameter, and the inner peripheral surface gradually expands to both sides in the central axis direction. The diametrically tapered surfaces 15b and 15c are formed symmetrically, and the outer peripheral surface forms a cylindrical surface 15d that is in close contact with the annular notch 9b.

【0016】一方のテーパリング13は、図3,図5に
示すように台形断面を有して環状をなし、内周面がテー
パ面13aを形成し、外周面がテーパ面13bを形成し
ている。他方のテーパリング14は、図3,図6に示す
ように台形断面を有して環状をなし、内周面がテーパ面
14aを形成し、外周面がテーパ面14bを形成してい
る。
As shown in FIGS. 3 and 5, one taper ring 13 has an annular shape with a trapezoidal cross section, and an inner peripheral surface forms a tapered surface 13a and an outer peripheral surface forms a tapered surface 13b. There is. As shown in FIGS. 3 and 6, the other taper ring 14 has an annular shape with a trapezoidal cross section, and an inner peripheral surface forms a tapered surface 14a and an outer peripheral surface forms a tapered surface 14b.

【0017】一方のテーパリング13の内周面のテーパ
面13aは、内リング12の一方のテーパ面12bと係
合し、外周面のテーパ面13bは、外リング15の一方
のテーパ面15bと係合する。また、他方のテーパリン
グ14の内周面のテーパ面14aは、内リング12の他
方のテーパ面12cと係合し、外周面のテーパ面14b
は、外リング15の他方のテーパ面15cと係合する。
そして、一方のテーパリング13には、周方向の所定間
隔にて複数個(実施例では4個)の貫通孔13cが形成
され、他方のテーパリング14には、周方向の所定間隔
にて複数個のねじ孔14cが各貫通孔13cと対応させ
て形成されている。
The taper surface 13a on the inner peripheral surface of one taper ring 13 engages with one taper surface 12b of the inner ring 12, and the taper surface 13b on the outer peripheral surface of the one taper surface 13b with one taper surface 15b of the outer ring 15. Engage. Further, the taper surface 14a on the inner peripheral surface of the other taper ring 14 engages with the other taper surface 12c of the inner ring 12, and the taper surface 14b on the outer peripheral surface.
Engages with the other tapered surface 15c of the outer ring 15.
A plurality of (four in the embodiment) through holes 13c are formed in one taper ring 13 at predetermined circumferential intervals, and a plurality of through holes 13c are formed in the other taper ring 14 at predetermined circumferential intervals. Individual screw holes 14c are formed so as to correspond to the respective through holes 13c.

【0018】支持装置11は、外リング15と内リング
12との間に両テーパリング13,14を組み合わせた
状態で、サポート9の支持部9aの前端内周部に形成し
た環状切欠き部9bと砲身1の外周面との間に介在させ
る。この状態で、外リング15の外周面である円筒面1
5dが環状切欠き部9bの円筒面に対向し、内リング1
2の内周面である円筒面12dが砲身1の外周面に対向
している。この支持装置11の組付け作業は、内リング
12ではスリット12aが弾性的に拡大し、外リング1
5ではスリット15aが弾性的に縮小するので、容易に
なされる。
The support device 11 is an annular notch 9b formed in the inner peripheral portion of the front end of the support portion 9a of the support 9 in a state where both taper rings 13 and 14 are combined between the outer ring 15 and the inner ring 12. And the outer peripheral surface of the barrel 1. In this state, the cylindrical surface 1 which is the outer peripheral surface of the outer ring 15
5d faces the cylindrical surface of the annular notch 9b, and the inner ring 1
The cylindrical surface 12d, which is the inner peripheral surface of the barrel 2, faces the outer peripheral surface of the barrel 1. In the assembling work of the support device 11, the slit 12a in the inner ring 12 elastically expands and the outer ring 1
5, the slit 15a is elastically contracted, so that the slit 15a can be easily formed.

【0019】この状態から、ボルト16を一方のテーパ
リング13の貫通孔13cから挿入して、他方のテーパ
リング14のねじ孔14cにねじ込むことにより、両テ
ーパリング13,14が締め付けられる。これにより、
両テーパリング13,14の外周のテーパ面13b,1
4bとテーパ面15b,15cが係合する外リング15
が弾性的に拡径変形すると共に圧縮変形し、両テーパリ
ング13,14の内周のテーパ面13a,14aとテー
パ面12b,12cが係合する内リング12が弾性的に
縮径変形すると共に圧縮変形して、両テーパリング1
3,14の弾性的な圧縮変形と相まつて、砲身1がサポ
ート9の支持部9aに隙間なく緊密に支持される。
From this state, the bolts 16 are inserted through the through holes 13c of the one taper ring 13 and screwed into the screw holes 14c of the other taper ring 14, whereby the two taper rings 13, 14 are tightened. This allows
Outer taper surfaces 13b, 1 of both taper rings 13, 14
The outer ring 15 in which the 4b and the tapered surfaces 15b and 15c are engaged with each other.
Elastically expands in diameter and compressively deforms, and the inner ring 12 in which the tapered surfaces 13a, 14a and the tapered surfaces 12b, 12c of the inner circumferences of the tapered rings 13, 14 engage with each other elastically contracts in diameter. Compressed and deformed, both taper rings 1
Coupled with the elastic compression deformation of 3, 14, the barrel 1 is tightly supported by the support portion 9a of the support 9 without a gap.

【0020】かくして、弾性体である内リング12及び
外リング15に、ボルト16のねじ込み量に応じた所定
の初圧縮量が与えられる。その際、内リング12ではス
リット12aが縮小し、外リング15ではスリット15
aが拡大する。なお、加工誤差は、砲尾部2と砲身1と
の間の段隔ねじ10部分の従来例と同一箇所の隙間c,
dによつて吸収され、又は弾性体である内リング12若
しくは外リング15又は両テーパリング13,14が弾
性変形して吸収される。
Thus, the inner ring 12 and the outer ring 15 which are elastic bodies are given a predetermined initial compression amount according to the screwing amount of the bolt 16. At that time, the slit 12a is reduced in the inner ring 12 and the slit 15a is reduced in the outer ring 15.
a expands. The processing error is due to the gap c between the breech 2 and the barrel 1 at the same position as the conventional example of the step screw 10 portion,
d is absorbed, or the inner ring 12 or the outer ring 15 or both tapered rings 13 and 14 which are elastic bodies are elastically deformed and absorbed.

【0021】このようにして砲身1の基端部を砲尾部2
に段隔ねじ10によつて結合し、砲身1の中心軸線方向
の中間部をサポート9の支持部9aに設けた支持装置1
1によつて弾性的に支持した状態で、遊底3によつて砲
身1内に図外の弾丸18を供給し、射撃すれば、砲身1
が振れる傾向を呈する。しかして、砲身1は、その中心
軸線方向の中間部が、支持装置11によつて隙間なく緊
密に支持されているので、射撃に伴う振れが良好に抑制
される。
In this way, the base end of the barrel 1 is connected to the breech 2
Support device 1 in which the intermediate portion of the barrel 1 in the direction of the central axis is provided on the support portion 9a of the support 9
When the bullet 18 (not shown) is supplied into the barrel 1 by the breech bolt 3 while being elastically supported by the barrel 1, the barrel 1
Tends to swing. Since the middle portion of the barrel 1 in the direction of the central axis is tightly supported by the support device 11 without a gap, the shake due to the shooting is suppressed well.

【0022】具体的には、射撃に伴う砲身1の一次振れ
は、弾性体である内リング12、外リング15及び一対
のテーパリング13,14が弾性的に変形することによ
つて緩衝され、その後、砲身1が反対方向へ振り戻され
て二次振れを生ずる。この間に、内リング12及び外リ
ング15のテーパ面12b,12c,15b,15c
と、各テーパリング13,14のテーパ面13a,13
b,14a,14bとの摩擦及び弾性体である内リング
12、外リング15及び一対のテーパリング13,14
の内部損失によつてエネルギが吸収され、砲身1の振れ
が抑制される。内リング12、外リング15及び両テー
パリング13,14の弾発力は、ボルト16のねじ込み
量を変えてこれらの初圧縮量を変えることにより調整で
きる。
Specifically, the primary runout of the barrel 1 caused by the shooting is damped by elastic deformation of the inner ring 12, the outer ring 15, and the pair of taper rings 13 and 14, which are elastic bodies, After that, the barrel 1 is swung back in the opposite direction to cause secondary shake. In the meantime, the tapered surfaces 12b, 12c, 15b, 15c of the inner ring 12 and the outer ring 15
And the tapered surfaces 13a, 13 of the taper rings 13, 14
b, 14a, 14b and inner ring 12, outer ring 15, which is an elastic body, and a pair of taper rings 13, 14
Energy is absorbed by the internal loss of the barrel, and the swinging of the barrel 1 is suppressed. The elastic forces of the inner ring 12, the outer ring 15, and the tapered rings 13 and 14 can be adjusted by changing the screwing amount of the bolt 16 and changing the initial compression amounts thereof.

【0023】しかして、射撃時の砲口1aの向きの正規
方向からのずれ量は、砲身1の一次,二次振れ角度(図
8に示すα,α’)の減少によつて著しく減少し、ま
た、砲口1aの向きと直角方向の砲口1aの速度(図9
に示すVt,Vt’)及びその絶対値の差も小さくな
る。その結果、射弾散布が小さくなる。すなわち、図7
に示すように段隔ねじ10部分の隙間c,dを従来より
も若干小さく確保しながら、砲身1とサポート9の支持
部9aとの間の隙間(従来の隙間b)を支持装置11に
よつて実質的に0として、射弾散布を小さくすることが
できる。この砲身1とサポート9の支持部9aとの間の
隙間が支持装置11によつて実質的に0に設定され、砲
身1の向きが安定するので、段隔ねじ10部分の隙間
c,dを従来よりも若干小さく確保した状態で、弾丸1
8の発射に伴う砲身1の熱膨張、加工精度等を良好に吸
収することが可能である。
However, the deviation amount of the direction of the muzzle 1a from the normal direction at the time of shooting is remarkably reduced by the decrease of the primary and secondary deflection angles (α, α'shown in FIG. 8) of the barrel 1. , The velocity of the muzzle 1a in the direction perpendicular to the direction of the muzzle 1a (see FIG.
The difference between Vt and Vt ′) and the absolute value thereof also becomes small. As a result, the dispersion of shots is reduced. That is, FIG.
As shown in FIG. 3, while maintaining the gaps c and d in the stepped screw 10 to be slightly smaller than the conventional one, the support device 11 is used to form the gap (conventional gap b) between the barrel 1 and the support portion 9a of the support 9. Therefore, it is possible to reduce the spray dispersion to substantially zero. The gap between the barrel 1 and the support portion 9a of the support 9 is set to substantially 0 by the support device 11, and the orientation of the barrel 1 is stabilized. Bullet 1 with slightly smaller size than before
It is possible to satisfactorily absorb the thermal expansion of the barrel 1, the processing accuracy, etc. associated with the firing of 8.

【0024】ところで、上記の実施例にあつては内リン
グ12、外リング15及び一対のテーパリング13,1
4を共に弾性体にて形成したが、内リング12若しくは
外リング15又は一対のテーパリング13,14の内の
少なくも一つが弾性体にて形成されていれば、砲身1と
サポート9の支持部9aとの間の隙間を実質的に0とし
て、かつ、砲身1を弾性的に支持することが可能であ
る。
By the way, in the above embodiment, the inner ring 12, the outer ring 15 and the pair of taper rings 13, 1 are provided.
Although both 4 are formed of an elastic body, if at least one of the inner ring 12 or the outer ring 15 or the pair of taper rings 13 and 14 is formed of an elastic body, the barrel 1 and the support 9 are supported. It is possible to make the gap between the portion 9a and the portion 9a substantially zero and to elastically support the barrel 1.

【0025】[0025]

【発明の効果】以上の説明によつて理解されるように、
本発明に係る砲身の支持構造によれば、砲身の中間部を
弾性体を介して支持するので、砲身の熱膨張、加工誤差
等を弾性体の弾性変形によつて吸収することができる。
加えて、弾丸発射に際する砲身の振れ量を軽減して、砲
口の向きの正規な方向からのずれ角を小さくできると共
に、砲身の振れの速度を小さくでき、弾丸の砲口からそ
れる角度を小さくできる。その結果、弾性体を付加する
という簡素な構造によつて射弾散布を小さくして、命中
率を著しく高めることが可能になつた。
As can be understood from the above description,
According to the barrel supporting structure of the present invention, since the middle portion of the barrel is supported via the elastic body, thermal expansion of the barrel, processing error and the like can be absorbed by elastic deformation of the elastic body.
In addition, the amount of deflection of the barrel when firing a bullet can be reduced, the deviation angle of the muzzle direction from the normal direction can be reduced, and the speed of the deflection of the barrel can be reduced, and it deviates from the muzzle of the bullet. The angle can be reduced. As a result, it has become possible to reduce the shot-scattering by using a simple structure in which an elastic body is added, and to significantly increase the hit rate.

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

【図1】 本発明の1実施例に係る砲身の支持構造を断
面にて示す正面図。
FIG. 1 is a cross-sectional front view of a barrel supporting structure according to an embodiment of the present invention.

【図2】 同じく一部切開して示す背面図。FIG. 2 is a rear view showing the same with a partial incision.

【図3】 同じく要部を示す断面図。FIG. 3 is a sectional view showing a main part of the same.

【図4】 同じく内リング及び外リングを分解して示す
斜視図。
FIG. 4 is a perspective view showing the inner ring and the outer ring in an exploded manner.

【図5】 同じく一方のテーパリングの要部を示す図。FIG. 5 is a diagram showing a main part of one taper ring of the same.

【図6】 同じく他方のテーパリングの要部を示す図。FIG. 6 is a diagram showing a main part of the other taper ring.

【図7】 同じく段隔ねじ部分を示す断面図。FIG. 7 is a sectional view showing a stepped screw portion of the same.

【図8】 従来例を示す断面図。FIG. 8 is a sectional view showing a conventional example.

【図9】 同じく作用説明図。FIG. 9 is an explanatory view of the same operation.

【符号の説明】[Explanation of symbols]

1:砲身、2:砲尾部、3:遊底、4:揺架、5:砲
架、6:耳軸、7:スライド、9:サポート、9a:支
持部、9b:環状切欠き部、10:段隔ねじ、11:支
持装置、12:内リング(弾性体)、12a:スリッ
ト、12b,12c:テーパ面、12d:円筒面、1
3,14:テーパリング、13a,13b,14a,1
4b:テーパ面、13c:貫通孔、14c:ねじ孔、1
5:外リング(弾性体)、15a:スリット、15b,
15c:テーパ面、15d:円筒面、16:ボルト、1
8:弾丸。
1: barrel, 2: breech, 3: breech, 4: swing, 5: gun shaft, 6: ear shaft, 7: slide, 9: support, 9a: support, 9b: annular notch, 10: Step screw, 11: support device, 12: inner ring (elastic body), 12a: slit, 12b, 12c: tapered surface, 12d: cylindrical surface, 1
3, 14: taper ring, 13a, 13b, 14a, 1
4b: tapered surface, 13c: through hole, 14c: screw hole, 1
5: outer ring (elastic body), 15a: slit, 15b,
15c: tapered surface, 15d: cylindrical surface, 16: bolt, 1
8: bullet.

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】 砲の砲尾部の先端部に砲身の基端部を結
合し、該砲尾部と一体をなす筒状のサポートの支持部に
より、該砲身の中心軸線方向の中間部を支持する砲身の
支持構造であつて、該サポートの支持部と砲身の外周面
との間に、弾性体を介在させることを特徴とする砲身の
支持構造。
1. A base end portion of a barrel is coupled to a tip portion of a breech portion of a gun, and a support portion of a cylindrical support which is integral with the breech portion supports an intermediate portion in the central axis direction of the barrel. A support structure for a barrel, wherein an elastic body is interposed between a support portion of the support and an outer peripheral surface of the barrel.
【請求項2】 弾性体に初圧縮量が与えられていること
を特徴とする請求項1の砲身の支持構造。
2. A support structure for a barrel according to claim 1, wherein an initial compression amount is given to the elastic body.
JP06596493A 1993-03-03 1993-03-03 Barrel support structure Expired - Fee Related JP3241853B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP06596493A JP3241853B2 (en) 1993-03-03 1993-03-03 Barrel support structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP06596493A JP3241853B2 (en) 1993-03-03 1993-03-03 Barrel support structure

Publications (2)

Publication Number Publication Date
JPH06257991A true JPH06257991A (en) 1994-09-16
JP3241853B2 JP3241853B2 (en) 2001-12-25

Family

ID=13302193

Family Applications (1)

Application Number Title Priority Date Filing Date
JP06596493A Expired - Fee Related JP3241853B2 (en) 1993-03-03 1993-03-03 Barrel support structure

Country Status (1)

Country Link
JP (1) JP3241853B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6205696B1 (en) * 1996-07-16 2001-03-27 Steyr-Daimler-Puch Aktiengesellschaft Gun with detachable barrel mounting

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101374745B1 (en) * 2012-03-15 2014-03-17 국방과학연구소 Device for generating dynamic pressure and experimental system of gun having the same
DE102015008794B4 (en) 2015-07-10 2021-02-25 Rheinmetall Waffe Munition Gmbh Weapon barrel storage

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6205696B1 (en) * 1996-07-16 2001-03-27 Steyr-Daimler-Puch Aktiengesellschaft Gun with detachable barrel mounting

Also Published As

Publication number Publication date
JP3241853B2 (en) 2001-12-25

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