JPS6390495A - Cylindrical sonobuoy of telescope type - Google Patents

Cylindrical sonobuoy of telescope type

Info

Publication number
JPS6390495A
JPS6390495A JP23626386A JP23626386A JPS6390495A JP S6390495 A JPS6390495 A JP S6390495A JP 23626386 A JP23626386 A JP 23626386A JP 23626386 A JP23626386 A JP 23626386A JP S6390495 A JPS6390495 A JP S6390495A
Authority
JP
Japan
Prior art keywords
cylinder
sonobuoy
barrel
receiver
lid
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
JP23626386A
Other languages
Japanese (ja)
Inventor
Taizo Kiyota
清田 泰三
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to JP23626386A priority Critical patent/JPS6390495A/en
Publication of JPS6390495A publication Critical patent/JPS6390495A/en
Pending legal-status Critical Current

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  • Measurement Of Velocity Or Position Using Acoustic Or Ultrasonic Waves (AREA)

Abstract

PURPOSE:To promote the reduction of space in an aircraft for storing a sonobuoy to be housed, by forming the miniaturized sonobuoy of telescope type building its receiver, transmitter, amplifier, etc. to be formed in small size and light weight. CONSTITUTION:A sonobuoy, if it reaches the surface of the sea, lifts a pressure receiving plate 12 and a supporting pawl 50, which are built in a cylinder mouth metal 10, to the upper by a colliding pressure against water, dislocating the supporting pawl 50 from a supporting pawl groove 53 by acting force of a supporting pawl spring 51, and the pressure receiving plate 12 is released being thrown out into the seawater together with a series of parts of a dying tube 29, wave receiver retaining plate 13, wave receiver 25 and a wave receiver receiving plate 26. The drying tube 29 floats on the surface of the sea while dissolves, and the wave receiver sinks into the sea while extending a lead wire 55. An antenna 42 is opened being vertically positioned, and the sonobuoy, in which a battery starts to be discharged, turns on a beacon light 44 actuating the wave receiver, radio receiver, amplifier and a transmitter.

Description

【発明の詳細な説明】 (イ)産業上の利用分野 この発明は、収納保管する時は体容積を縮小の状態で行
い、使用する時は中筒、外筒を段階的に伸延し、体容積
を増加し、海面水中における浮力を増大して使用するソ
ノブイに関する。
Detailed Description of the Invention (a) Industrial Application Field This invention reduces the body volume when stored, and when used, the inner cylinder and outer cylinder are stretched in stages. This invention relates to a sonobuoy that is used by increasing its volume and increasing its buoyancy in sea water.

(ロ)従来の技術 従来、単一筒に受波器、受信器、増幅器、送信器、電源
、電池等を内臓して組立てているソノブイは、外径12
4粍、長さ915粍(以下「A型」という。)の円筒の
ものが最も多く使用され、他に、外径124粍、長さ6
10粍(以下「P型」という。)、外径76耗、長さ5
33耗(以下「B型」という6)等のものも使用されて
いる。A型は内臓組付は部品の体容積に比較して筒容積
が甚大であり、不用の体容積をもち、収納保管する場所
の体容積は効率性に欠ける。特に、航空機にとう戟する
場合は、とう載容積に限度があシ、体容積の大きいソノ
ブイはとう載数量が少な(、F型、B型のものは、内臓
部品の体容積に比例して、筒容積も小さく、航空機から
投下使用する際、浮力不足によシ、着水の瞬間に海面下
に深く潜り、再浮上までの過穆で水圧や水抵抗により、
アンテナの展開、沈下する受波器リード線の展張に不具
合を発生しやすく、浮遊時波浪に影響を受けやすく、ツ
ノブイ機能を低下する欠点がある。
(b) Conventional technology Conventionally, sonobuoys, which are assembled into a single cylinder with a receiver, receiver, amplifier, transmitter, power supply, battery, etc., have an outer diameter of 12 mm.
The cylindrical type with an outer diameter of 124 mm and a length of 6 mm is most commonly used.
10 mm (hereinafter referred to as "P type"), outer diameter 76 wear, length 5
Type 33 (hereinafter referred to as ``Type B'') is also used. Type A has an extremely large cylindrical volume compared to the body volume of the parts when it is internally assembled, has unnecessary body volume, and lacks efficiency in the volume of the storage area. In particular, when flying an aircraft, there is a limit to the cargo capacity, and sonobuoys with a large body volume have a small cargo capacity. The cylinder volume is also small, and when dropped from an aircraft, due to lack of buoyancy, it dives deep under the sea surface at the moment of landing, and due to water pressure and water resistance until it resurfaces.
Problems tend to occur in the deployment of the antenna and the extension of the submerged receiver lead wires, and they are easily affected by waves when floating, which reduces the horn buoy function.

(ハ)発明が解決しようとする問題点 この発明は、小型軽量化した部品を使用して小形となっ
た受信器、送信器、増幅器等を内臓組付け、不要の体容
積を減じて総体容積を小さくすることにより、保管収納
特に航空機においての空間場所の効率化を計ることがで
き、使用する時に体容積を増大し、海面上で十分な浮力
をもち安定j−て浮標し、電子および音響機能を有効に
発揮できるソノブイを得ることを目的としている。
(c) Problems to be solved by the invention This invention uses smaller and lighter parts to internally assemble a smaller receiver, transmitter, amplifier, etc., thereby reducing unnecessary body volume. By making it smaller, it is possible to improve the efficiency of space for storage, especially on aircraft, and increase the body volume when in use, allowing it to be stably buoyed with sufficient buoyancy on the sea surface, and for electronic and acoustic equipment. The aim is to obtain a sonobuoy that can effectively demonstrate its functions.

に)問題点を解決しようとする手段 この発明を実施例の図面にもとづいて説明すると、次の
とおりである。
B) Means for solving the problems The present invention will be explained as follows based on the drawings of the embodiments.

第1図から第8図において、上方筒口に外リムを形成す
る基筒胴6と、その上方筒口にねじ妖め組付け、溶解栓
59を組込む基部蓋11と、下方筒口にねじ嵌めし、外
周に筒ロブリム52、爪掛は溝54を、内周に受圧板1
2の支持爪50を引掛ける支持爪溝53を形成する筒口
金10とで構成する基筒1と、その外側に、下方筒口に
内リムを、上方筒口に外リムを形成する中筒胴7と、そ
の上方筒口に、連通孔28を穿孔した中筒蓋21をねじ
嵌め組付けて構成する中筒2を嵌被し、更に、その外側
に、下方筒口に中筒2と同様な内リムを形成し、上方筒
口に、周縁を等分割矩形波状で、周面にコ字型溝を形成
する花弁縁60をもち、底板に溶解栓59を組込む、皿
状の外筒蓋32を組付けて構成する外[3を嵌被した多
段筒の構造とし、基fmlK注入管9を貫通して、筒口
金10側に差込み口31を、基部蓋11側に封止弁30
を取付け、筒内に電池室隔壁15、シール58を円周に
嵌め溶解栓59を組付けた水密隔壁14を固定して、電
子機器室24、電池室23、受波器室22を区画して設
け、電子機器室24に電源、受信器、増幅器、送信器を
、電池室23に電池を内臓し組付け、受波器室22には
、電池室隔壁15の下面にカートリッジ・スイッチ17
、受波器スプリング27を固定し、その下方に受波器受
皿26、長尺の受波器リード線55を周囲に巻きたたん
でいる受波器25、染色筒29を保持する受波器押板1
3を組み重ね、その下部を、支持爪スプリング51、対
で作用する支持爪50を組付けた受圧板12で覆い、こ
の支持爪50の端部の爪を筒口金lOの内周面に形成す
る支持爪溝53に嵌め込んで、受波器室22内の部品全
体を固定支持する。
In FIGS. 1 to 8, the base barrel 6 forms an outer rim at the upper barrel opening, the base lid 11 is screwed onto the upper barrel opening and the dissolving plug 59 is assembled, and the base lid 11 is screwed into the lower opening and forms the outer rim. There is a cylindrical lob rim 52, a groove 54 for the hook, and a pressure receiving plate 1 on the inner periphery.
A base cylinder 1 is composed of a base cylinder 1 and a cylinder cap 10 forming a support claw groove 53 for hooking a support claw 50 of No. 2, and a middle cylinder body 7 having an inner rim formed at a lower cylinder mouth and an outer rim formed at an upper cylinder mouth on the outside of the base cylinder 1. A middle cylinder 2, which is constructed by screwing and assembling a middle cylinder lid 21 with a communication hole 28, is fitted onto the upper cylinder opening, and an inner rim similar to the middle cylinder 2 is fitted on the outside of the lower cylinder opening. A dish-shaped outer cylinder lid 32 is attached to the upper cylinder opening, which has a petal edge 60 with an equally divided rectangular wave shape and a U-shaped groove on the peripheral surface, and a dissolving plug 59 incorporated in the bottom plate. It has a multi-stage structure in which an outer tube (3) is fitted over the base fmlK injection tube 9, and an insertion port 31 is provided on the tube cap 10 side, and a sealing valve 30 is provided on the base lid 11 side.
is attached, and the battery chamber partition 15, the watertight partition 14 with the seal 58 fitted around the circumference and the melting plug 59 assembled are fixed in the cylinder to partition the electronic equipment chamber 24, the battery chamber 23, and the receiver chamber 22. A power supply, a receiver, an amplifier, and a transmitter are installed in the electronic equipment room 24, a battery is installed in the battery room 23, and a cartridge switch 17 is installed on the lower surface of the battery room partition wall 15 in the receiver room 22.
, a receiver spring 27 is fixed, a receiver tray 26 is placed below the receiver spring 27, a receiver 25 has a long receiver lead wire 55 wound around it, and a receiver holds a dye tube 29. Push plate 1
3 are assembled one on top of the other, and the lower part thereof is covered with a pressure receiving plate 12 on which a support claw spring 51 and a support claw 50 acting in pairs are assembled, and the claw at the end of the support claw 50 is formed on the inner circumferential surface of the cylindrical cap lO. It is fitted into the supporting claw groove 53 to fixedly support the entire component inside the receiver chamber 22.

外筒M32の皿部にアンテナ42、標識灯44・カート
リッジ・ビン40を有するピン・カートリッジ16を固
定し、外筒蓋32の上部には、空中での落下速度を回転
翼により緩速する場合、第1図、第2図、第3図、第4
図、第9図において、ホーク49を組付けたそれぞれの
翼4をヒンジ・ビン46、ヒンジ・スプリング63で組
付けたヨーク18を、ヨーク・ボルト19、ワッシャ4
7、ナツト48で頭頂部中央の回転軸受20に組込み、
内側中間部に、外筒蓋スプリング45を下面に取付けた
スプリング押板43を固定し、外筒蓋32に設けたコ字
型溝の花弁縁60と全対称的に嵌め込みができる形状の
花弁R61を下方周縁に形成した支持蓋5を乗架し、空
中での落下速度を落下傘により緩速する場合、第9図に
おいて、補助傘68と組みする落下傘65を折りたたみ
収納し、開傘錘66を取付け、内側中間部に、支持蓋5
と同様な外筒蓋スプリング45を下面に組付けたスプリ
ング押え板43を固定し、外周に筒蓋プリム80を固着
して、下方周縁に花弁縁67を形成する収納筒蓋64を
乗架する。
A pin cartridge 16 having an antenna 42, a marker light 44, and a cartridge bin 40 is fixed to the dish part of the outer cylinder M32, and a pin cartridge 16 having an antenna 42, a marker light 44, and a cartridge bin 40 is fixed to the top of the outer cylinder lid 32. , Figure 1, Figure 2, Figure 3, Figure 4
9, each wing 4 with a hawk 49 attached thereto is assembled with a yoke 18 with a hinge pin 46 and a hinge spring 63, with a yoke bolt 19 and a washer 4.
7. Insert into the rotating bearing 20 at the center of the top of the head with the nut 48,
A spring press plate 43 with an outer cylinder lid spring 45 attached to the lower surface is fixed to the inner middle part, and a petal R61 is shaped so that it can be fitted symmetrically to the petal edge 60 of the U-shaped groove provided on the outer cylinder lid 32. In the case where the support lid 5 with the auxiliary umbrella 68 formed on the lower periphery is mounted on the support lid 5 to slow down the falling speed in the air with a parachute, the parachute 65 assembled with the auxiliary umbrella 68 is folded and stored, and the opening weight 66 is Install, support lid 5 on the inner middle part
A spring holding plate 43 with an outer cylinder lid spring 45 similar to that assembled on the lower surface is fixed, a cylinder lid prim 80 is fixed to the outer periphery, and a storage cylinder lid 64 forming a petal edge 67 on the lower periphery is mounted. .

支持M5または収納筒蓋64の花弁a61.67と外筒
蓋32の花弁縁60を噛合せ、コ字型溝にスプリング・
リング41を嵌込み緊締し、その両端のスプリング・リ
ング端孔62にカートリッジ・ビン40を挿入して、外
筒3の頭部に落下緩速機構を確実に結合する。中筒2、
外[3の筒内には、ピン・カートリッジ16、カートリ
ッジ・スイッチ17、電源のそれぞれの間を電気接続す
るカートリッジ・リード線57と、アンテナ42、標識
灯44と受信器、送信器のそれぞれの間を電気接続する
アンテナ・標識灯り一ド1IJ56とを長くたぐり重ね
た状態で配線定置する。
Engage the support M5 or the petal a61.67 of the storage tube lid 64 with the petal edge 60 of the outer tube lid 32, and insert the spring into the U-shaped groove.
The ring 41 is fitted and tightened, and the cartridge bin 40 is inserted into the spring ring end holes 62 at both ends of the ring 41 to securely connect the fall slowing mechanism to the head of the outer cylinder 3. Middle tube 2,
Inside the cylinder of the outside [3] are cartridge lead wires 57 for electrically connecting the pin cartridge 16, cartridge switch 17, and power source, as well as the antenna 42, indicator light 44, receiver, and transmitter. Place the wiring in a long, overlapping state with the antenna, marker light, and 1IJ56 electrically connected between them.

基筒1を基準として中筒2、外筒3を伸長状態に固定す
るため、第1図、第6図、第7図、第8図において、基
筒胴6、中筒胴7の上方リムの外周面が、それぞれ、中
筒胴7、外筒胴8の内胴面に、中筒胴7、外筒胴8の下
方リムの内周面が、それぞれ、基筒胴6、中m胴7の外
胴面に溝嵌合し、中筒胴7、外筒胴8の下方にある内リ
ムの内周面に、それぞれ複数個の2ブチ・スプリング溝
33.35を掘設し、その各溝底にラッチ・スプリング
34を固定し、中[2、外筒3が伸長した界隈位置に、
ラッチ・スプリング34の頂辺が嵌合するラッチ・スプ
リング受1!11136.38を基筒胴6、中筒胴7の
外側面上方周面にそれぞれ掘設し、基筒胴6、中筒胴7
の上方外リムの角周囲に°O”リング37.39を嵌め
、中筒胴7、外筒胴8の筒口内リムの周囲上面に°0“
す/グ受面を形成している。
In order to fix the middle cylinder 2 and the outer cylinder 3 in an extended state with the base cylinder 1 as a reference, the upper rims of the base cylinder body 6 and the middle cylinder body 7 are shown in FIGS. 1, 6, 7, and 8. The outer peripheral surfaces of the lower rims of the middle barrel 7 and the outer barrel 8 are the inner barrel surfaces of the middle barrel 7 and the outer barrel 8, respectively, and the inner circumferential surfaces of the lower rims of the middle barrel 7 and outer barrel 8 are the base barrel 6 and the middle barrel 8, respectively. A plurality of two-pronged spring grooves 33 and 35 are dug into the inner peripheral surfaces of the inner rims located below the middle cylinder body 7 and the outer cylinder body 8, respectively. A latch spring 34 is fixed to the bottom of each groove, and a latch spring 34 is fixed to the bottom of each groove.
A latch spring receiver 1!11136.38 into which the top side of the latch spring 34 fits is dug into the upper circumferential surface of the outer surface of the base barrel 6 and the middle barrel 7, respectively. 7
Fit °O" rings 37 and 39 around the corners of the upper outer rim, and attach °O" rings 37 and 39 to the upper surfaces around the inner rims of the cylinder mouths of the middle cylinder body 7 and the outer cylinder body 8.
Forms a receiving surface.

に)作用 このソノブイの音響・無線機能を除く、構造に関する操
作動について説明すると、第1図から第11図において
、通常、倉庫または機内等に保管するときは、外筒3の
中に中筒2を、中筒2の中に基fi11を収納し、翼4
または落下傘65を折りたたんだ状態の落下緩速機構を
外筒3の上部に結合した状態(以下「短縮状態ソノブイ
」という。)で行う。地上で機体に装備する発射装置に
装填するときは、短縮状態ソノブイの姿で発射筒69の
筒内に、射出口より挿入して押込む。筒口金10の下面
が発射筒690筒底に組付ける受皿70JC当て嵌まり
、発射スプリング71を圧縮しながら筒口全把手機構の
複数のリンク爪72が、それぞれ、爪スプリング730
反発力に抗しながら筒口金10の外郭形状に沿って爪掛
は溝54に嵌まる。
2) Function To explain the operation of this sonobuoy regarding its structure, excluding the acoustic and wireless functions, as shown in Figures 1 to 11, when it is stored in a warehouse or on board an aircraft, the inner cylinder is normally placed inside the outer cylinder 3. 2, the base fi11 is stored in the middle cylinder 2, and the wing 4 is
Alternatively, the parachute 65 may be folded with a fall slowing mechanism connected to the upper part of the outer cylinder 3 (hereinafter referred to as a "shortened state sonobuoy"). When loading the launcher installed on the aircraft on the ground, the sonobuoy is inserted into the launch tube 69 from the ejection port in the form of a shortened sonobuoy. The lower surface of the barrel cap 10 fits into the saucer 70JC to be assembled to the bottom of the firing barrel 690, and while compressing the firing spring 71, the plurality of link claws 72 of the barrel mouth full grip mechanism each engage the claw springs 730.
The hook fits into the groove 54 along the outer shape of the tube cap 10 while resisting the repulsive force.

同時に、ガス供給ロア9が差込み口31に挿入される。At the same time, the gas supply lower 9 is inserted into the insertion port 31.

筒口全把手機構のアクチェータ74をロックすることに
より、短縮状態ソノブイはリンク爪72で筒口金10が
堅固に保持され、横断面方向の動きは、筒ロブリム52
、折りたたんだ翼4または筒蓋プリム80の外径面で発
射筒69内に安定して保持する。
By locking the actuator 74 of the barrel full handle mechanism, the link claw 72 of the sonobuoy in the shortened state holds the barrel cap 10 firmly, and movement in the cross-sectional direction is controlled by the barrel rim 52.
, it is stably held within the firing tube 69 by the outer diameter surface of the folded wings 4 or the tube cover prim 80.

ソノブイは射出直前に、短縮状態から伸長するため、ガ
ス供給ロア9から注入tf!9に圧搾ガスまたは空気を
送入すると、封止弁30が開弁じ、圧搾ガス等は中筒2
の筒内、中筒蓋21の連通孔28を通過して、中筒2、
外筒3の筒内に充満し、その内圧力で外筒胴8の内胴面
と下方内リム内周面は、それぞれ、中筒胴7の上方外リ
ム外周面と外胴面を摺動し、また、中筒胴7の内胴面と
下方内リム内周面は、それぞれ、基筒胴6の上方外リム
外周面と外胴面を摺動し、外筒3、中筒2が伸延し、基
筒胴6.中筒胴7の上方外リム角に取付ける°0°リン
グ37.39に、中筒胴7、外筒胴8の下方内リムのそ
れぞれの°O°リング受面が回着圧縮し、同時に、中筒
胴7、外筒胴8の下方内リムのラッチ、スプリング溝3
3.35に固定するラッチ・スプリング34が、それぞ
れ、基筒胴6、中筒胴7の外胴面の上方周面に掘設した
ラッチ・スプリング受溝36.38に嵌合し、中筒側7
下方は基筒111i16の上方に、外筒胴8下方は中筒
胴7の上方に堅実に固定し、伸長形態で基筒1、中筒2
、外筒3は強固な一体筒となる。筒内ガス等の気密は°
0”1ノング37.39と封止弁30により保持し、そ
のガス等圧力は封止弁30により大気圧より高めに保圧
する。
Immediately before injection, the sonobuoy extends from the shortened state, so inject tf! from the gas supply lower 9! When compressed gas or air is fed into the cylinder 9, the sealing valve 30 opens, and the compressed gas etc.
inside the cylinder, passing through the communication hole 28 of the middle cylinder lid 21, the middle cylinder 2,
The inside of the outer cylinder 3 is filled, and the internal pressure causes the inner surface of the outer cylinder body 8 and the inner peripheral surface of the lower inner rim to slide on the outer peripheral surface of the upper outer rim and the outer cylinder surface of the middle cylinder body 7, respectively. In addition, the inner barrel surface and the lower inner rim inner circumferential surface of the middle barrel 7 slide on the upper outer rim outer circumferential surface and the outer barrel surface of the base barrel 6, respectively, so that the outer barrel 3 and the middle barrel 2 Distraction, base barrel 6. The respective °O° ring receiving surfaces of the lower inner rims of the middle cylinder body 7 and the outer cylinder body 8 are rotated and compressed by the °0° ring 37.39 attached to the upper outer rim corner of the middle cylinder body 7, and at the same time, Latch on lower inner rim of middle barrel 7, outer barrel 8, spring groove 3
The latch springs 34 fixed at 3.35 fit into the latch spring receiving grooves 36.38 dug in the upper circumferential surfaces of the outer surfaces of the base barrel 6 and middle barrel 7, respectively, and side 7
The lower part is firmly fixed above the base cylinder 111i16, and the lower part of the outer cylinder body 8 is firmly fixed above the middle cylinder body 7, and the base cylinder 1 and the middle cylinder 2 are fixed in the extended form.
, the outer cylinder 3 becomes a strong integral cylinder. Airtightness of cylinder gas etc.
The pressure of the gas is kept higher than atmospheric pressure by the sealing valve 30.

伸長したソノブイの射出は、機内の射出スイッチをON
にすると、電圧によりアクチェータ74が作動し、ロン
ドア5が下がるとリンク76.77.78が連動し、リ
ンク爪72が爪ス2プリング73の反発力に抗して筒口
金10の爪掛は溝54から外れると、ソノブイは発射ス
プリング71の反発力によって、発射筒69から強く空
中に射出される。
To eject the extended sonobuoy, turn on the ejection switch inside the aircraft.
When the actuator 74 is activated by the voltage, the links 76, 77, and 78 are interlocked when the Ron door 5 is lowered, and the link pawl 72 resists the repulsive force of the pawl spring 73, and the pawl hook of the tube cap 10 moves into the groove. 54, the sonobuoy is strongly ejected into the air from the launch tube 69 by the repulsive force of the launch spring 71.

落下緩速機構が回転翼のソノブイは、翼4が発射筒69
がら空中に出ると、ヒンジ・スプリング63の力で半開
傘し、重い基筒1が下方に々り翼4は空気抵抗で全開傘
し、回転軸受2oとヨーク・ポルト19の接触面を回転
滑面とする回転翼となって、落下速度を緩めて降下する
。落下緩速機構が落下傘のソノブイは、収納筒蓋64部
が発射筒69から空中に出ると、開傘錘66が飛び出し
補助傘68が開傘し、空中落下時は基筒1が下方になる
とともに、落下傘65が全開傘して落下速度を緩めて降
下する。ソノブイは、海面に到達すると、水との衝突圧
力により、筒口金10に組込まれている受圧板12と支
持爪50が上方にもち上げられ、支持爪50が支持爪ス
プリング510作用力で、支持爪溝53から外れて受圧
板12の中心方向に引きつけられると、受圧板12は染
色筒29、受波器押板13、受波器25、受波器受皿2
6の一連の部品とともに、受波器スプリング27の反発
力と一連部品に作用する重力によシ、筒口金lOの外の
海水中に放てきされ、染色筒29は海面に浮上するとと
もに溶解して、ソノブイの位置を鮮明に視認できる標識
色を漂流し、受波器25は受波器リード線55を展張し
ながら海中に沈下する。同時に、受波器スプリング27
の伸長に連動してカートリッジ・スイッチ17が作動し
、電気回路を形成し、ピン・カートリッジ16が着火爆
発し、カートリッジ・ピン4oを押し上げ、スプリング
・リング端孔62から抜は出し、外筒蓋32の花弁縁6
0のコ字m溝からスプリング・リング41が外れて離脱
機構が作動し、支持蓋5または収納筒蓋64をもつ落下
緩速機構は外筒蓋32から外れ、ソノブイから離脱する
。外筒蓋32に固定され折りたたまれたアンテナ42は
開放直立し、電池室23の電池に海水が侵入しながら、
ソノブイ全体のメタヒンジを定めながら、十分な浮力を
もって安定した姿勢で水面に浮き、電池が起電を開始し
、電源が安定すると標識灯44は点灯し、受波器、受信
器、増幅器、送信器が正常な機能で作動する。所定時間
作動させ使用した後は、水密隔壁14、基部蓋11、外
筒蓋32に組付けている溶解栓59が、海水の化学作用
によって溶解し、海水の浸水とともにソノブイは海底に
沈下する。
In a sonobuoy whose fall slowing mechanism is a rotary wing, the wing 4 is the launch tube 69.
Once in the air, the umbrella half-opens due to the force of the hinge spring 63, the heavy base tube 1 swings downward, and the wings 4 open fully due to air resistance, rotating and sliding on the contact surface between the rotary bearing 2o and the yoke port 19. It turns into a rotating wing and descends at a slower rate. In a sonobuoy whose fall slowing mechanism is a parachute, when the storage tube lid 64 comes out of the launch tube 69 into the air, the opening weight 66 pops out and the auxiliary umbrella 68 opens, and when the sonobuoy falls in the air, the base tube 1 moves downward. At the same time, the parachute 65 fully opens and descends at a slower falling speed. When the sonobuoy reaches the sea surface, the pressure receiving plate 12 and the support claw 50 incorporated in the tube cap 10 are lifted upward by the collision pressure with the water, and the support claw 50 is supported by the action force of the support claw spring 510. When the pressure receiving plate 12 is removed from the claw groove 53 and pulled toward the center of the pressure receiving plate 12, the pressure receiving plate 12 is moved to the dyeing tube 29, the receiver press plate 13, the receiver 25, and the receiver tray 2.
Due to the repulsive force of the receiver spring 27 and the gravity acting on the series of parts 6, the dyeing tube 29 is thrown into the seawater outside the tube cap lO, and the dyeing tube 29 rises to the sea surface and dissolves. The sonobuoy's position is clearly visible and the marker color drifts, and the receiver 25 sinks into the sea while extending the receiver lead wire 55. At the same time, the receiver spring 27
The cartridge switch 17 operates in conjunction with the extension of the spring ring, forming an electric circuit, causing the pin cartridge 16 to ignite and explode, pushing up the cartridge pin 4o, pulling it out from the spring ring end hole 62, and opening the outer cylinder lid. 32 petal edges 6
The spring ring 41 comes off from the U-shaped M groove of 0 and the release mechanism is activated, and the fall slowing mechanism with the support lid 5 or the storage cylinder lid 64 comes off from the outer cylinder lid 32 and separates from the sonobuoy. The folded antenna 42 fixed to the outer cylinder lid 32 stands open and erect, and seawater enters the battery in the battery compartment 23.
While determining the metahinge of the entire sonobuoy, it floats on the water surface in a stable posture with sufficient buoyancy, the battery starts generating electricity, and when the power becomes stable, the beacon light 44 lights up, and the receiver, receiver, amplifier, and transmitter is functioning normally. After being operated and used for a predetermined period of time, the dissolving plug 59 assembled to the watertight bulkhead 14, base lid 11, and outer tube lid 32 is dissolved by the chemical action of seawater, and the sonobuoy sinks to the seabed as the seawater floods.

(へ)発明の効果 この発明は以上説明したように、小型軽量化された部品
で構成する電子・音響機器を内臓組込むツノブイの長所
を生かし、海面での浮力不足と耐波性に欠ける短所を補
い、保管、収納は小体容積で行い、海面で使用するとき
は体容積を大きくして、浮力と耐波性を十分持たすこと
にょシ、ソノブイ機能を有効に発揮することができ、航
空機とう載については、従来の人世ソノブイ“と比較し
、積載空間場所の体容積を著しく減じ、積載数量では著
しく増加することができる効果がある。
(f) Effects of the Invention As explained above, this invention takes advantage of the advantages of the horn buoy, which incorporates electronic and audio equipment made of smaller and lighter parts, and compensates for the disadvantages of lack of buoyancy on the sea surface and lack of wave resistance. The sonobuoy function can be effectively demonstrated by using a small body volume for storage and storage, and by increasing the body volume when used at sea surface to ensure sufficient buoyancy and wave resistance. This has the effect of significantly reducing the volume of the loading space and significantly increasing the number of loads compared to the conventional sonobuoy.

なお、ソノブイの総重量と浮力等との相関関係およびそ
の他の条件から、よシー層この発明の効果がある場合は
2段または4段筒でもよい。
In addition, from the correlation between the total weight of the sonobuoy and buoyancy, etc., and other conditions, a two-stage or four-stage cylinder may be used if the present invention is effective in terms of the shear layer.

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

第1図は、回転翼による落下緩速機構を上部に組付けた
短縮状態の本発明ソノブイの縦断面図、第2図は、同正
面図、第3図は、同平面図、第4図は、同アーア断面平
面図、第5図は、同下面図、第6図は、基筒1を基準と
し、中筒2、外筒3を伸延し、翼4が開いた本発明ソノ
ブイの1部縦縦断面と発射筒69の概略位置図、第7図
は、第6図のP部、Q部の拡大縦断面図、第8図は、第
7図のイーイ断面図、vg9図は、落下緩速機構の支持
蓋5を外筒蓋32に固定する状態を示す斜面図、第10
図は、収納筒蓋64による落下緩速機構の縦断面図、第
11図は1本発明ソノブイの発射装置機構を説明する断
面図である。
Fig. 1 is a longitudinal sectional view of the sonobuoy of the present invention in a shortened state with a fall slowing mechanism using rotary blades attached to the upper part, Fig. 2 is a front view of the same, Fig. 3 is a plan view of the same, and Fig. 4 5 is a bottom view of the same, and FIG. 6 is a sectional view of the sonobuoy of the present invention with the base tube 1 as a reference, the inner tube 2 and the outer tube 3 extended, and the wings 4 opened. Fig. 7 is an enlarged longitudinal cross-sectional view of the P part and Q part of Fig. 6, Fig. 8 is a cross-sectional view of Ei of Fig. 7, and Fig. 9 is a schematic position diagram of the firing tube 69. 10th perspective view showing a state in which the support lid 5 of the fall slowing mechanism is fixed to the outer cylinder lid 32;
The figure is a longitudinal sectional view of a fall slowing mechanism using the storage cylinder lid 64, and FIG. 11 is a sectional view illustrating the sonobuoy launcher mechanism of the present invention.

Claims (1)

【特許請求の範囲】[Claims] 基筒胴(6)、基部蓋(11)、筒口金(10)で構造
し、封止弁(30)、差込み口(31)をもつ注入管(
9)を貫通して、受波器、電池、電源、受信器、送信器
のソノブイ主幹機器を組立て内臓する基筒(1)の外側
に、中筒胴(7)、連通孔(28)を有する中筒蓋(2
1)で構造する中筒(2)を、滑合で嵌被し、更に、そ
の外側に、外筒胴(8)とアンテナ(42)、標識灯(
44)、ピン・カートリッジ(16)を組付けた外筒蓋
(32)で構造し、その頭部に、離脱機構を有する回転
する翼(4)または落下傘(65)を組付けた落下緩速
機構を乗架結合する外筒(3)を、滑合で嵌被し、基部
胴(6)と中筒胴(7)のそれぞれの上方外リム角周囲
に、“0”リング(37)、(39)を組付け、中筒胴
(7)と外筒胴(8)のそれぞれの筒口内リムの円周上
面に、“0”リング(37)、(39)の受面を形成し
、伸延時、中筒(2)と基部(1)を、また、外筒(3
)と中筒(2)を固定するラッチ・スプリング(34)
を、中筒胴(7)、外筒胴(8)のそれぞれ下方内リム
内周面のラッチ・スプリング溝(33)、(35)の底
面に固定し、基部胴(6)、中筒胴(7)のそれぞれの
筒外面上方周面に、ラッチ・スプリング(34)のラッ
チ・スプリング受溝(36)、(38)を掘設した構造
とし、空気またはガス圧力で中筒(2)、外筒(3)を
伸長し、体容積を増大できる特徴のテレスコープ型ソノ
ブイ。
An injection tube (structured with a base barrel (6), a base lid (11), and a tube cap (10), and having a sealing valve (30) and an insertion port (31)
9), and on the outside of the base cylinder (1) in which the sonobuoy main equipment of the receiver, battery, power supply, receiver, and transmitter is assembled and built, the middle cylinder body (7) and the communication hole (28) are installed. The inner cylinder lid (2
The inner cylinder (2) constructed in 1) is fitted by a sliding fit, and the outer cylinder body (8), antenna (42), and marker light (
44), a slow-falling mechanism consisting of an outer cylinder lid (32) fitted with a pin cartridge (16), and a rotating wing (4) or parachute (65) with a detachment mechanism attached to the head of the outer cylinder lid (32). The outer cylinder (3) that connects the mechanism is fitted by a sliding fit, and a "0" ring (37), (39) is assembled, and the receiving surfaces of the "0" rings (37) and (39) are formed on the circumferential upper surface of the inner rim of the cylinder mouth of each of the middle barrel (7) and the outer barrel (8), During distraction, the middle tube (2) and base (1) are
) and the latch spring (34) that secures the middle cylinder (2).
are fixed to the bottom surfaces of the latch spring grooves (33) and (35) on the inner peripheral surface of the lower inner rim of the middle barrel (7) and outer barrel (8), respectively, and The latch spring receiving grooves (36) and (38) for the latch spring (34) are dug in the upper peripheral surface of the outer surface of each cylinder (7), and the middle cylinder (2), A telescope type sonobuoy that is characterized by the ability to extend the outer cylinder (3) and increase the body volume.
JP23626386A 1986-10-06 1986-10-06 Cylindrical sonobuoy of telescope type Pending JPS6390495A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP23626386A JPS6390495A (en) 1986-10-06 1986-10-06 Cylindrical sonobuoy of telescope type

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP23626386A JPS6390495A (en) 1986-10-06 1986-10-06 Cylindrical sonobuoy of telescope type

Publications (1)

Publication Number Publication Date
JPS6390495A true JPS6390495A (en) 1988-04-21

Family

ID=16998189

Family Applications (1)

Application Number Title Priority Date Filing Date
JP23626386A Pending JPS6390495A (en) 1986-10-06 1986-10-06 Cylindrical sonobuoy of telescope type

Country Status (1)

Country Link
JP (1) JPS6390495A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008118617A2 (en) * 2007-03-26 2008-10-02 Raytheon Company Methods and apparatus for surveillance sonar systems

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008118617A2 (en) * 2007-03-26 2008-10-02 Raytheon Company Methods and apparatus for surveillance sonar systems
WO2008118617A3 (en) * 2007-03-26 2008-12-11 Raytheon Co Methods and apparatus for surveillance sonar systems

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