JPH0571896A - Jet deflecting device for flying body launcher - Google Patents

Jet deflecting device for flying body launcher

Info

Publication number
JPH0571896A
JPH0571896A JP23615791A JP23615791A JPH0571896A JP H0571896 A JPH0571896 A JP H0571896A JP 23615791 A JP23615791 A JP 23615791A JP 23615791 A JP23615791 A JP 23615791A JP H0571896 A JPH0571896 A JP H0571896A
Authority
JP
Japan
Prior art keywords
launcher
main body
jet
end section
horizontal axis
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.)
Withdrawn
Application number
JP23615791A
Other languages
Japanese (ja)
Inventor
Nobuyuki Muraoka
信之 村岡
Sumiyuki Kobayashi
純之 小林
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.)
Churyo Engineering Co Ltd
Mitsubishi Heavy Industries Ltd
Original Assignee
Churyo Engineering Co Ltd
Mitsubishi Heavy Industries 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 Churyo Engineering Co Ltd, Mitsubishi Heavy Industries Ltd filed Critical Churyo Engineering Co Ltd
Priority to JP23615791A priority Critical patent/JPH0571896A/en
Publication of JPH0571896A publication Critical patent/JPH0571896A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00Rocket or torpedo launchers
    • F41F3/04Rocket or torpedo launchers for rockets
    • F41F3/042Rocket or torpedo launchers for rockets the launching apparatus being used also as a transport container for the rocket
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A23/00Gun mountings, e.g. on vehicles; Disposition of guns on vehicles
    • F41A23/34Gun mountings, e.g. on vehicles; Disposition of guns on vehicles on wheeled or endless-track vehicles
    • F41A23/42Gun mountings, e.g. on vehicles; Disposition of guns on vehicles on wheeled or endless-track vehicles for rocket throwers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00Rocket or torpedo launchers
    • F41F3/04Rocket or torpedo launchers for rockets
    • F41F3/0413Means for exhaust gas disposal, e.g. exhaust deflectors, gas evacuation systems

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)

Abstract

PURPOSE:To make it possible to clear the height limitations imposed by the Road Traffic Act by lowering the height of a jet deflecting device of a flying body launcher during running time. CONSTITUTION:The titled jet deflecting device comprises a main body 1a pivoted to a launcher 11 mounted around a horizontal shaft of a firing vehicle rotatively by way of a horizontal shaft 7a and a front end section 4 pivoted to the main body 1a by way of a horizontal shaft 5. The both ends of the device are pivoted to a deflecting board 1 of a flying body jet which rotates between a rising position and a falling position, a front end section 4 and the launcher 11. The front end section 4 is stretched on the extension of the main body 1 at the falling position while at the rising position there is installed a link 3 which folds the front end section 4.

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、走行可能な飛翔体の発
射車両に設けられた飛翔体発射機の噴流偏向装置に関す
る。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a jet deflecting device for a projectile launcher provided in a vehicle capable of traveling a projectile.

【0002】[0002]

【従来の技術】飛翔体発射機の噴流偏向板1は飛翔体の
発射車両10の後端に設けられ、図3に示すように、飛
翔体を鉛直方向上方へ発射させるときに噴流を偏向させ
るために使用されるが、発射機を移動する時は、図4に
示すように、噴流偏向板1を上にあげて移動する。この
とき、噴流偏向板1の寸法H0 が高すぎて、道路交通法
上の高さ制限を満足しない場合がある。なお、図中11
は発射車両10に搭載された飛翔体の発射機、12は発
射機11に搭載された飛翔体である。
2. Description of the Related Art A jet deflector plate 1 for a projectile launcher is provided at the rear end of a vehicle 10 for launching a projectile, and as shown in FIG. However, when moving the launcher, as shown in FIG. 4, the jet deflection plate 1 is raised and moved. At this time, the dimension H 0 of the jet flow deflector 1 may be too high to satisfy the height limit under the Road Traffic Law. In addition, 11 in the figure
Is a projectile of a projectile mounted on the launch vehicle 10, and 12 is a projectile mounted on the launcher 11.

【0003】[0003]

【発明が解決しようとする課題】図4に示すように、噴
流偏向板1を上に上げた場合に噴流偏向板が高すぎる時
には、道路交通法の高さ制限を満足せず、発射車両10
が一般公道を走行することができない。また、そのため
に、噴流偏向板1を取外して移動する時には、作業性が
悪くなることが避けられない。
As shown in FIG. 4, when the jet deflector 1 is raised and the jet deflector is too high, the height limit of the Road Traffic Law is not satisfied, and the launch vehicle 10 is not satisfied.
Can't drive on public roads. Further, for this reason, it is inevitable that the workability is deteriorated when the jet flow deflector 1 is detached and moved.

【0004】本発明は、以上の問題点を解決することが
できる飛翔体発射機の噴流偏向装置を提供しようとする
ものである。
The present invention is intended to provide a jet flow deflecting device for a projectile launcher which can solve the above problems.

【0005】[0005]

【課題を解決するための手段】本発明の飛翔体発射機の
噴流偏向装置は、発射車両に水平軸まわりに回動可能に
取付けられた発射機に水平軸を介して枢着された本体と
水平軸を介して前記本体の先端に枢着された先端部より
なり、上昇位置と下降位置の間を前記水平軸まわりに回
動する飛翔体噴流の偏向板、及び前記先端部と前記発射
機にその両端が枢着され、前記偏向板の下降位置で前記
先端部を前記本体の延長上に展伸させ、前記偏向板の上
昇位置で前記先端部を折畳むリンクを備えている。
A jet flow deflecting device for a projectile launcher according to the present invention comprises a main body pivotally attached to a launcher mounted on a launch vehicle rotatably around a horizontal axis through the horizontal axis. A deflecting plate for projectile jets, which comprises a tip portion pivotally attached to the tip of the main body via a horizontal axis and rotates around the horizontal axis between a raised position and a lowered position, and the tip portion and the launcher. Both ends thereof are pivotally attached to each other, and a link is provided that extends the tip end portion on an extension of the main body at a lower position of the deflector plate and folds the tip end portion at an ascending position of the deflector plate.

【0006】[0006]

【作用】本発明では、偏向板の本体が水平軸まわりに回
動して下降位置をとった時には、リンク装置によって偏
向板の先端部が前記本体の延長上に展伸され、前記本体
と前記先端部の両者で発射される飛翔体の噴流を受け、
これを確実に偏向させる。
According to the present invention, when the main body of the deflecting plate is rotated around the horizontal axis and takes the lowered position, the tip end portion of the deflecting plate is extended by the link device to extend the extension of the main body. Receiving jets of projectiles fired at both tips,
This is surely deflected.

【0007】一方、偏向板の本体が水平軸まわりに回動
して上昇位置をとった時には、リンク装置によって偏向
板の先端部が折畳まれて、偏向板の高さが低くなって道
路交通法上の高さ制限内におさまり、発射車両の一般公
道の走行が可能になる。
On the other hand, when the main body of the deflecting plate is rotated around the horizontal axis to reach the raised position, the tip of the deflecting plate is folded by the link device, and the height of the deflecting plate becomes low, so that the road traffic becomes low. It will be within the legal height limit, and the launch vehicle will be able to run on the public road.

【0008】[0008]

【実施例】本発明の一実施例を、図1及び図2によって
説明する。10は自走可能な発射車両で、飛翔体の発射
機11が同車両10に搭載され、発射機11は同車両1
0の後端付近の水平軸まわりに回動できるように同車両
10に取付けられている。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS An embodiment of the present invention will be described with reference to FIGS. 10 is a self-propelled launch vehicle, in which a projectile 11 is mounted on the vehicle 10.
The vehicle 10 is mounted so as to be rotatable around a horizontal axis near the rear end of 0.

【0009】飛翔体噴流の偏向板1は、本体1aと同本
体1aの先端の水平方向のピン5によって外側に折れる
ように枢着された先端部4よりなる。前記偏向板1の前
端(図1における左端)は、発射機11の架台6の後端
のブラケット7に水平方向のピン7aを介して枢支され
ている。
The deflecting plate 1 for jets of a flying object comprises a main body 1a and a tip portion 4 pivotally attached to a tip of the main body 1a so as to be bent outward by a horizontal pin 5. The front end (left end in FIG. 1) of the deflection plate 1 is pivotally supported by a bracket 7 at the rear end of the pedestal 6 of the launcher 11 via a horizontal pin 7a.

【0010】2は発射機の架台6に発射車両10の前後
方向に配置された押し上げシリンダであり、発射車両1
0の後方へ伸びる同シリンダ2のピストン2aの端部と
偏向板の本体1aの下側に取付けられたブラケット9と
に、下方に凸のほぼ弧状をなすリンク8の両端が枢着さ
れている。
Reference numeral 2 denotes a push-up cylinder which is arranged on the base 6 of the launcher in the front-rear direction of the launch vehicle 10.
The ends of the piston 2a of the cylinder 2 extending rearward of 0 and the bracket 9 attached to the lower side of the main body 1a of the deflecting plate are pivotally attached to both ends of a downwardly protruding substantially arcuate link 8. .

【0011】3はリンクで、前記の先端部4に水平方向
の軸3bを介してその一端が枢着され、前記発射機の架
台6の後端のブラケット3aに水平方向の軸3cを介し
てその他端が枢着されている。
Reference numeral 3 denotes a link, one end of which is pivotally attached to the tip end portion 4 through a horizontal shaft 3b, and a bracket 3a at the rear end of the mount 6 of the launcher through a horizontal shaft 3c. The other end is pivotally attached.

【0012】本実施例において、発射機11が回動され
て、図3に示すように、飛翔体を鉛直方向上方へ発射す
る時には、押し上げシリンダ2を作動して、リンク8を
介して偏向板1の本体1aを、ピン7aまわりに回動し
て図1の中に実線で示される下降位置へ同本体1aを移
動させる。
In this embodiment, when the launcher 11 is rotated to launch the projectile upward in the vertical direction as shown in FIG. 3, the push-up cylinder 2 is actuated and the deflecting plate is moved through the link 8. The main body 1a of No. 1 is rotated around the pin 7a to move the main body 1a to the lowered position shown by the solid line in FIG.

【0013】この偏向板1の下降位置では、偏向板1の
先端部4は、偏向板の本体1aの延長上に展伸されてお
り、本体1aと先端部4の両者によって発射される飛翔
体の噴流を受けてこれを確実に偏向させる。
In the lowered position of the deflecting plate 1, the tip portion 4 of the deflecting plate 1 is extended on the extension of the body 1a of the deflecting plate, and the projectile is launched by both the body 1a and the tip portion 4. It receives the jet stream of and deflects it reliably.

【0014】発射車両10の走行時には、図2に示すよ
うに、発射機11をほぼ水平の位置に回動させる。この
時に、押し上げシリンダ2を作動して、リンク8を介し
て偏向板1の本体1aをピン7aまわりに回動して、図
1中に鎖線で示される上昇位置へ同本体1aを移動させ
る。
When the launch vehicle 10 is running, the launcher 11 is rotated to a substantially horizontal position as shown in FIG. At this time, the push-up cylinder 2 is operated to rotate the main body 1a of the deflection plate 1 around the pin 7a via the link 8 to move the main body 1a to the raised position shown by the chain line in FIG.

【0015】この偏向板1の上昇に伴って、リンク3に
よって、偏向板1の先端部4は、図1中鎖線で示すよう
にピン5まわりに回動して折畳まれる。従って、偏向板
1の上昇位置では、偏向板1の上端の高さが低くなり発
射機11と偏向板1を搭載した発射車両10の高さH
(図2参照)は、道路交通法の制限高さ内におさまり、
発射車両10が一般公道を走行することが可能となる。
As the deflecting plate 1 rises, the tip 3 of the deflecting plate 1 is rotated around the pin 5 and folded by the link 3 as shown by the chain line in FIG. Therefore, at the raised position of the deflection plate 1, the height of the upper end of the deflection plate 1 becomes low, and the height H of the launch vehicle 11 equipped with the launcher 11 and the deflection plate 1 is increased.
(See Fig. 2) is within the height limit of the Road Traffic Law,
The launch vehicle 10 can travel on a public road.

【0016】[0016]

【発明の効果】本発明は、以上説明したように、偏向板
の下降位置では、偏向板の本体とその延長上に展伸され
た偏向板の先端部とに発射される飛翔体の噴流を受け
て、これを確実に偏向させることができ、また偏向板の
上昇位置では前記前端部を折畳んで道路交通法上の高さ
制限の問題を解消することができる。しかも、本発明
は、偏向板の先端部を展伸、折畳むリンクを設けた極め
て簡単な構成で目的とする機能を果すことができる。
As described above, according to the present invention, when the deflecting plate is in the lowered position, the jet flow of the projectile ejected to the body of the deflecting plate and the tip of the deflecting plate extended on the extension thereof is generated. This can be received and deflected reliably, and the problem of height limitation under the Road Traffic Law can be solved by folding the front end portion at the rising position of the deflection plate. Moreover, the present invention can achieve the intended function with an extremely simple structure in which a link for extending and folding the tip portion of the deflection plate is provided.

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

【図1】本発明の一実施例の立面図である。FIG. 1 is an elevational view of one embodiment of the present invention.

【図2】同実施例が搭載された飛翔体の発射車両の立面
図である。
FIG. 2 is an elevational view of a projectile-launching vehicle equipped with the embodiment.

【図3】従来の飛翔体発射車両の飛翔体発射時の説明図
である。
FIG. 3 is an explanatory diagram of a conventional projectile-launching vehicle when a projectile is launched.

【図4】同従来の発射車両の移動時の説明図である。FIG. 4 is an explanatory diagram when the conventional launch vehicle moves.

【符号の説明】[Explanation of symbols]

1 偏向板 1a 偏向板の本体 2 押上げシリンダ 3 リンク 3b,3c ピン 4 偏向板の先端部 5 ピン 6 発射機の架台 8 リンク 10 発射車両 11 発射機 1 Deflection Plate 1a Deflection Plate Main Body 2 Push-up Cylinder 3 Links 3b, 3c Pins 4 Deflection Plate Tip 5 Pins 6 Launcher Frame 8 Links 10 Launch Vehicle 11 Launcher

───────────────────────────────────────────────────── フロントページの続き (72)発明者 小林 純之 愛知県名古屋市中村区岩塚町字九反所60番 地の1 中菱エンジニアリング株式会社内 ─────────────────────────────────────────────────── ─── Continuation of the front page (72) Inventor Junyuki Kobayashi 1 at 60, Kutanesho, Iwatsuka-cho, Nakamura-ku, Nagoya-shi, Aichi Nakabishi Engineering Co., Ltd.

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 発射車両に水平軸まわりに回動可能に取
付けられた発射機に水平軸を介して枢支された本体と水
平軸を介して前記本体に枢着された先端部よりなり、上
昇位置と下降位置の間を前記水平軸まわりに回動する飛
翔体噴流の偏向板、及び前記先端部と前記発射機にその
両端が枢着され、前記偏向板の下降位置で前記先端部を
前記本体の延長上に展伸させ、前記偏向板の上昇位置で
前記先端部を折畳むリンクを備えたことを特徴とする飛
翔体発射機の噴流偏向装置。
1. A main body pivotally supported by a launcher rotatably mounted on a launch vehicle about a horizontal axis through the horizontal axis, and a tip portion pivotally attached to the main body through the horizontal axis. A deflector plate for a jet of jets that rotates between an ascending position and a descending position around the horizontal axis, and both ends of the deflector plate are pivotally attached to the tip part and the launcher, and the tip part is pivoted at the descending position of the deflector plate. A jet deflecting device for a projectile launcher, comprising a link that is extended on an extension of the main body and that folds the tip portion at a rising position of the deflecting plate.
JP23615791A 1991-09-17 1991-09-17 Jet deflecting device for flying body launcher Withdrawn JPH0571896A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP23615791A JPH0571896A (en) 1991-09-17 1991-09-17 Jet deflecting device for flying body launcher

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP23615791A JPH0571896A (en) 1991-09-17 1991-09-17 Jet deflecting device for flying body launcher

Publications (1)

Publication Number Publication Date
JPH0571896A true JPH0571896A (en) 1993-03-23

Family

ID=16996612

Family Applications (1)

Application Number Title Priority Date Filing Date
JP23615791A Withdrawn JPH0571896A (en) 1991-09-17 1991-09-17 Jet deflecting device for flying body launcher

Country Status (1)

Country Link
JP (1) JPH0571896A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101160077B1 (en) * 2010-10-28 2012-06-28 국방과학연구소 Blocking apparatus of launcher and launch system having the same
US8978945B2 (en) 2007-03-01 2015-03-17 Yumiko Komura Musical instrument strap and musical instrument connector

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8978945B2 (en) 2007-03-01 2015-03-17 Yumiko Komura Musical instrument strap and musical instrument connector
KR101160077B1 (en) * 2010-10-28 2012-06-28 국방과학연구소 Blocking apparatus of launcher and launch system having the same

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Legal Events

Date Code Title Description
A300 Withdrawal of application because of no request for examination

Free format text: JAPANESE INTERMEDIATE CODE: A300

Effective date: 19981203