CN104266545A - Underwater horizontal hot launching device - Google Patents
Underwater horizontal hot launching device Download PDFInfo
- Publication number
- CN104266545A CN104266545A CN201410490337.5A CN201410490337A CN104266545A CN 104266545 A CN104266545 A CN 104266545A CN 201410490337 A CN201410490337 A CN 201410490337A CN 104266545 A CN104266545 A CN 104266545A
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- Prior art keywords
- launched
- launching tube
- half shell
- sail body
- adapter
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Abstract
The invention discloses an underwater horizontal hot launching device. The underwater horizontal hot launching device comprises an upper half emitting tube shell (1), a lower half emitting tube shell (2), a plurality of adapter module (3), an axial position pin (4) and a hanging ring (5); the upper half emitting tube shell (1) is formed by connecting four upper shell sections (101-104) through butt joint; the lower half emitting tube shell (2) is formed by four lower shell sections (201-204); every adapter module (3) is composed of at least four adapters (30), and gaps are formed between every two neighboring adapters; every adapter is composed of an outer layer (301) in contact with the wall of an emitting tube, a middle layer and an inner layer (303) in contact with a vessel to be launched (8); the outer surface of every adapter (30) is provided with a ring groove (30) for mounting a strap. The underwater horizontal hot launching device is used of guiding and positioning during launching of underwater vessels, and meanwhile, solves the problem of loading inconvenience of the underwater vessels with a high slenderness ratio and accordingly omits complex design of loading equipment.
Description
Technical field
The present invention relates to a kind of submerged level heat emission device.
Background technology
The emitter of missile armament is mainly used in providing guided missile to go out the guiding of a process, ensures going out a speed and going out a Gesture of guided missile.In order to ensure that missile center line is consistent with launching tube axis, preventing guided missile and cylinder from colliding simultaneously, between launching tube and guided missile, arranging adapter.Existing emitter, needs special complete filling equipment (containing filling mechanism, Zhua Dan mechanism, body, stent car, power source etc.) to realize, loads more difficult.
Summary of the invention
Technical problem to be solved by this invention is: provide a kind of filling simple submerged level heat emission device, guiding when launching for underwater sailing body and location, meanwhile, solve the problem that high-fineness ratio underwater sailing body is not easy to load, avoid designing complicated filling equipment.
The present invention includes following technical scheme:
A kind of submerged level heat emission device, comprises launching tube upper half shell, launching tube lower half shell, multiple adapter assembly, axial location pin and suspension ring; Launching tube upper half shell is formed by flange docking by four upper casing sections, and launching tube lower half shell is formed by flange docking by four lower parts; Launching tube upper half shell is provided with the gathering hole identical with adapter assembly quantity; Each upper casing section installs suspension ring; Each upper casing section and lower part form multiple osculum;
Each adapter assembly surrounds whole circle by least four pieces of adapters and forms, and has gap between adjacent two pieces of adapters; Every block adapter comprises and launches skin that barrel contacts, intermediate layer and the internal layer that contacts with sail body to be launched; The outer surface of every block adapter is formed the annular groove for installing band; Be embedded with dowel bushing in the intermediate layer of every block adapter, for separating of pin be arranged in dowel bushing; For separating of pin and dowel bushing between mounting spring; For separating of one end of pin insert in the pin-and-hole on sail body surface to be launched, the other end moves thus Compress Spring on dowel bushing, the internal layer of adapter is contacted with sail body to be launched, then by band, adapter assembly tighten is arranged on sail body to be launched; Band is made up of thin steel band, joint screw and nut;
When sail body filling to be launched, launching tube lower half shell horizontal positioned, axial location pin is arranged on launching tube lower half shell from bottom to top along launching tube lower half shell radial direction; The sail body level to be launched being provided with adapter assembly is lifted in launching tube lower half shell, ensures the pin-and-hole of axial location pin through sail body afterbody to be launched, realizes the axial location of sail body to be launched; By suspension ring, launching tube upper half shell is lifted on launching tube lower half shell, with bolt, upper and lower for launching tube half shell is fixed; After sail body filling to be launched, the joint screw of band is positioned at gathering hole scope.
Skin is low-friction material, intermediate layer is polyurethane foam; Internal layer is compressible material.
The afterbody of sail body to be launched is positioned at the first lower part, and axial location pin is arranged on described first lower part.
Multiple adapter assembly is three.
Each lower part installs two bearings.
Each upper casing section installs two suspension ring.
The present invention compared with prior art tool has the following advantages:
Submerged level heat emission device of the present invention is a kind of submerged level heat emission device of tape adapter unit, and adapter is filled between sail body to be launched and launching tube, plays located lateral and guide effect.Axial location pin is fixed on launching tube lower half shell, and after sail body filling to be launched, axial location pin, through the pin-and-hole of sail body afterbody to be launched, realizes the axial location of sail body to be launched; Thus the guiding achieved when underwater sailing body is launched and location.Upper and lower half shell of launching tube is respectively formed by flange docking by 4 cylinder section distinguish, is conducive to controlling each cylinder section distinguish length.Adopt the upper and lower splitted structure pattern of sectional, structure is simple, easy to process, can simplify filling flow process, shortens test period, reduces the difficulty of filling, avoids designing complicated filling equipment.
Accompanying drawing explanation
Fig. 1 is submerged level heat emission device composition diagram.
Fig. 2 is emitter filling process principle figure; Fig. 2 a is launching tube lower half shell schematic diagram, and Fig. 2 b installs the sail body schematic diagram to be launched with adapter assembly, and Fig. 2 c is for installing upper half shell schematic diagram, and Fig. 2 d is schematic diagram after filling.
Fig. 3 is adapter assembly structural representation, and Fig. 3 a is overall schematic, and Fig. 3 b is adapter schematic three dimensional views, and Fig. 3 c, Fig. 3 d are the adapter two-dimensional representation after adapter is separated with sail body to be launched.
Fig. 4 is that cuff structures schematic diagram installed by adapter.
Fig. 5 is submerged level heat emission device filling state 1 schematic diagram.
Fig. 6 is submerged level heat emission device filling state 2 schematic diagram.
Fig. 7 is emitter gathering hole local after sail body to be launched filling;
Fig. 8 is the sectional view of submerged level heat emission device axial location.
Detailed description of the invention
Just by reference to the accompanying drawings the present invention is described further below.
As shown in Figure 1, a kind of submerged level heat emission device of the present invention, comprises launching tube upper half shell 1, launching tube lower half shell 2, three adapter assemblies 3, axial location pin 4, suspension ring 5; Launching tube upper half shell 1 is formed by flange docking by four upper casing section 101-104, and launching tube lower half shell 2 is formed by flange docking by four lower part 201-204, and each lower part installs two bearings 7; In each upper casing section, two suspension ring 5 are installed; Transmitting upper half shell 1 is provided with three gathering holes, 105, three gathering holes 105 to be positioned on upper casing section 101-103; As shown in Figure 7, each upper casing section and each lower part form multiple osculum 106;
As shown in Figure 3, each adapter assembly 3 surrounds whole circle by least four pieces of adapters 30 and forms, and has gap between adjacent two pieces of adapters; Every block adapter comprises and launches skin 301 that barrel contacts, intermediate layer 302 and the internal layer 303 that contacts with sail body 8 to be launched; The outer surface of every block adapter 30 is formed the annular groove 304 for installing band; Be embedded with dowel bushing 306 in the intermediate layer of every block adapter 30, for separating of pin 305 be arranged in dowel bushing 306; For separating of pin 305 and dowel bushing 306 between mounting spring 307; For separating of one end of pin 305 insert in the pin-and-hole on sail body 8 surface to be launched, the other end moves thus Compress Spring 307 on dowel bushing 306, the internal layer of adapter 30 is contacted with sail body 8 to be launched, then by band 6, adapter assembly 3 tighten is arranged on sail body 8 to be launched.
As shown in Figure 4, band 6 is made up of thin steel band 601, joint screw 602 and nut 603; For mounting adapter, and ensure that adapter does not misplace or drops in sail body 8 filling process to be launched.The upper and lower distinguish of band cylinder to be launched is installed fasten, extracts out from gathering hole after fastening.
As shown in Fig. 2,5-8, when sail body 8 to be launched loads, launching tube lower half shell 2 horizontal positioned, axial location pin 4 is arranged on launching tube lower half shell 2 from bottom to top along lower part 201 radial direction of launching tube lower half shell; Sail body to be launched 8 level being provided with adapter assembly 3 is lifted in launching tube lower half shell 2, ensures the pin-and-hole of axial location pin 4 through sail body 8 afterbody to be launched, realizes the axial location of sail body 8 to be launched; As shown in Figure 6, by suspension ring 5, launching tube upper half shell 1 is lifted on launching tube lower half shell 2, with bolt, upper and lower for launching tube half shell is fixed; The joint screw that sail body 8 to be launched loads rear band is positioned at gathering hole scope, conveniently extracts band.
When sail body 8 to be launched is launched, turned on the joint screw of band by gathering hole, and extract band 6 out; Back out axial location pin 4, realize the unblock of sail body 8 to be launched and emitter; Travel forward along launching tube after sail body 8 engine ignition to be launched, the water before sail body 8 to be launched is discharged rapidly by the osculum of barrel, reduces sail body 8 water resistance to be launched; Be separated with sail body 8 to be launched under spring with hydrodynamic synergy after each adapter goes out cylinder, until sail body to be launched 8 goes out cylinder completely.
By accurately controlling launching tube internal diameter and sail body to be launched 8 outside dimension, adapter thickness is made to be greater than sail body 8 to be launched and launching tube inwall gap 1mm-1.5mm, ensure the decrement that adapter fills up gap and remains certain simultaneously, compensate processing and assembling deviation, realize sail body 8 to be launched coaxial with launching tube.
Launching tube upper half shell, lower half shell all adopt metal casting structure, and integral rigidity is better, do not affect the cylindricity of launching tube after fastening.
Adapter is layering sticking structure, and skin is low-friction material, is 0.05 under water with coefficient of friction during metal relative motion; Intermediate layer is polyurethane foam, and quality is light, and rigidity is better; Internal layer is layer of compensation, and material is softer, easily compresses, and plays the effect compensating gap between sail body 8 to be launched and launching tube.The degree of depth for the annular groove 304 installing band is about 10mm, avoid filling time and cylinder inwall interfere, facilitate band to extract simultaneously.
As shown in Figure 8, axial location pin 4 is screwed into the screwed hole on lower half shell 201 from outside to inside, and stem knob stretches into the inner chamber of cylinder through barrel.After sail body 8 to be launched forces home, stem knob, through the unthreaded hole of sail body 8 afterbody to be launched, reaches the object of restriction sail body 8 axial and circumferential motion to be launched.
The design of emitter splitted structure solves a filling difficult problem for sail body 8 to be launched.Axial direction positioning device simplicity of design, reliable operation, can effectively limit sail body 8 to be launched be loaded in launching tube transport and handling process in axial and circumferential motion, guarantee safety.Before on-test, manual demolition axial location pin, realizes the unblock of sail body 8 to be launched and launching tube.
Adapter is filled between sail body 8 to be launched and launching tube, plays located lateral and guide effect.Axial location pin is fixed on launching tube lower half shell, and after sail body 8 to be launched loads, axial location pin, through the pin-and-hole of sail body 8 afterbody to be launched, realizes the axial location of sail body 8 to be launched.This submerged level heat emission device adopts the upper and lower splitted structure pattern of sectional, and structure is simple, easy to process, can simplify filling flow process, shortens test period.
Described sail body to be launched can be actual guided missile or the test model of its guided missile and the sail body of other underwater emissions.
The unspecified part of the present invention belongs to general knowledge as well known to those skilled in the art.
Claims (6)
1. a submerged level heat emission device, it is characterized in that, comprise launching tube upper half shell (1), launching tube lower half shell (2), multiple adapter assembly (3), axial location pin (4) and suspension ring (5); Launching tube upper half shell (1) is formed by flange docking by four upper casing sections (101-104), and launching tube lower half shell (2) is formed by flange docking by four lower parts (201-204); Launching tube upper half shell (1) is provided with the gathering hole (105) identical with adapter assembly quantity; Each upper casing section is installed suspension ring (5); Each upper casing section and lower part are formed multiple osculum (106);
Each adapter assembly (3) surrounds whole circle by least four pieces of adapters (30) and forms, and has gap between adjacent two pieces of adapters; Every block adapter comprises and launches skin (301) that barrel contacts, intermediate layer (302) and the internal layer (303) that contacts with sail body to be launched (8); The outer surface of every block adapter (30) is formed the annular groove (304) for installing band; Be embedded with dowel bushing (306) in the intermediate layer of every block adapter (30), for separating of pin (305) be arranged in dowel bushing (306); For separating of pin (305) and dowel bushing (306) between mounting spring (307); For separating of one end of pin (305) insert in the pin-and-hole on sail body to be launched (8) surface, the other end above moves thus Compress Spring (307) at dowel bushing (306), the internal layer of adapter (30) is contacted with sail body to be launched (8), then by band (6), adapter assembly (3) tighten is arranged on sail body to be launched (8); Band (6) is made up of thin steel band (601), joint screw (602) and nut (603);
When sail body to be launched (8) loads, launching tube lower half shell (2) horizontal positioned, axial location pin (4) is arranged on launching tube lower half shell (2) from bottom to top along launching tube lower half shell radial direction; Sail body to be launched (8) level being provided with adapter assembly (3) is lifted in launching tube lower half shell (2), ensure that axial location pin (4) is through the pin-and-hole of sail body to be launched (8) afterbody, realizes the axial location of sail body to be launched (8); By suspension ring (5), launching tube upper half shell (1) is lifted on launching tube lower half shell (2), with bolt, upper and lower for launching tube half shell is fixed; After sail body to be launched (8) filling, the joint screw of band is positioned at gathering hole scope.
2. submerged level heat emission device as claimed in claim 1, is characterized in that: outer (301) are low-friction material, intermediate layer (302) are polyurethane foam; Internal layer (303) is compressible material.
3. submerged level heat emission device as claimed in claim 1, it is characterized in that: the afterbody of sail body to be launched is positioned at the first lower part (201), axial location pin (4) is arranged on described first lower part (201).
4. submerged level heat emission device as claimed in claim 1, is characterized in that: multiple adapter assembly (3) is three.
5. submerged level heat emission device as claimed in claim 1, is characterized in that: each lower part installs two bearings (7).
6. submerged level heat emission device as claimed in claim 1, is characterized in that: in each upper casing section, install two suspension ring (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410490337.5A CN104266545B (en) | 2014-09-23 | 2014-09-23 | A kind of submerged level heat emission device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410490337.5A CN104266545B (en) | 2014-09-23 | 2014-09-23 | A kind of submerged level heat emission device |
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| CN104266545A true CN104266545A (en) | 2015-01-07 |
| CN104266545B CN104266545B (en) | 2016-02-10 |
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| CN201410490337.5A Active CN104266545B (en) | 2014-09-23 | 2014-09-23 | A kind of submerged level heat emission device |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106516146A (en) * | 2016-11-02 | 2017-03-22 | 北京特种机械研究所 | Fixed adaptor type launch canister |
| CN110749233A (en) * | 2019-10-28 | 2020-02-04 | 上海机电工程研究所 | Honeycomb adapter and method of manufacture |
| CN112665457A (en) * | 2020-12-17 | 2021-04-16 | 中国航空工业集团公司成都飞机设计研究所 | Pressurization launching device for airborne buried weapon |
| CN113619804A (en) * | 2021-08-30 | 2021-11-09 | 贵州航天天马机电科技有限公司 | Integrated adapter |
| CN113772114A (en) * | 2021-10-18 | 2021-12-10 | 贵州航天天马机电科技有限公司 | Aircraft adapter and manufacturing method thereof |
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| US5542333A (en) * | 1983-08-15 | 1996-08-06 | Hughes Missile Systems Company | Undersea vehicle ejection from capsules |
| DE102007030509B3 (en) * | 2007-06-30 | 2008-07-31 | Howaldtswerke-Deutsche Werft Gmbh | Device for supporting and starting immersion body in submarine, has out flow pipe, supporting frame for supporting and guiding immersion body in out flow pipe and units for starting immersion body from out flow pipe |
| CN101970973A (en) * | 2008-01-31 | 2011-02-09 | 帕特里亚地面与武器系统有限公司 | Support member for supporting shell into breech-loading weapon barrel, and method |
| CN202547505U (en) * | 2011-11-01 | 2012-11-21 | 北京航天发射技术研究所 | Loading alignment equipment with bidirectional adjustments |
| KR101334731B1 (en) * | 2011-10-28 | 2013-11-29 | 국방과학연구소 | Underwater ejection launching system with shock absorbing device |
| CN104033455A (en) * | 2014-05-21 | 2014-09-10 | 北京航天发射技术研究所 | Adapter strap |
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2014
- 2014-09-23 CN CN201410490337.5A patent/CN104266545B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
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| US5542333A (en) * | 1983-08-15 | 1996-08-06 | Hughes Missile Systems Company | Undersea vehicle ejection from capsules |
| DE102007030509B3 (en) * | 2007-06-30 | 2008-07-31 | Howaldtswerke-Deutsche Werft Gmbh | Device for supporting and starting immersion body in submarine, has out flow pipe, supporting frame for supporting and guiding immersion body in out flow pipe and units for starting immersion body from out flow pipe |
| CN101970973A (en) * | 2008-01-31 | 2011-02-09 | 帕特里亚地面与武器系统有限公司 | Support member for supporting shell into breech-loading weapon barrel, and method |
| KR101334731B1 (en) * | 2011-10-28 | 2013-11-29 | 국방과학연구소 | Underwater ejection launching system with shock absorbing device |
| CN202547505U (en) * | 2011-11-01 | 2012-11-21 | 北京航天发射技术研究所 | Loading alignment equipment with bidirectional adjustments |
| CN104033455A (en) * | 2014-05-21 | 2014-09-10 | 北京航天发射技术研究所 | Adapter strap |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106516146A (en) * | 2016-11-02 | 2017-03-22 | 北京特种机械研究所 | Fixed adaptor type launch canister |
| CN110749233A (en) * | 2019-10-28 | 2020-02-04 | 上海机电工程研究所 | Honeycomb adapter and method of manufacture |
| CN112665457A (en) * | 2020-12-17 | 2021-04-16 | 中国航空工业集团公司成都飞机设计研究所 | Pressurization launching device for airborne buried weapon |
| CN113619804A (en) * | 2021-08-30 | 2021-11-09 | 贵州航天天马机电科技有限公司 | Integrated adapter |
| CN113772114A (en) * | 2021-10-18 | 2021-12-10 | 贵州航天天马机电科技有限公司 | Aircraft adapter and manufacturing method thereof |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104266545B (en) | 2016-02-10 |
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