CN104634163A - Missile launcher structure for oblique launching - Google Patents
Missile launcher structure for oblique launching Download PDFInfo
- Publication number
- CN104634163A CN104634163A CN201410815762.7A CN201410815762A CN104634163A CN 104634163 A CN104634163 A CN 104634163A CN 201410815762 A CN201410815762 A CN 201410815762A CN 104634163 A CN104634163 A CN 104634163A
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- Prior art keywords
- launcher
- cylinder bullet
- bullet
- stretcher
- mounting cylinder
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- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The invention relates to a missile launcher structure for oblique launching. The structure is formed by welding and forming section steel pipes, four barrel missiles can be carried, and the barrel missiles are pairwise arranged in an upper layer and a lower layer in a trapezoid shape. After the launcher is loaded with the barrel missiles, the running and transporting requirement of a vehicle is met. One end of the launcher is arranged on an orientation rotary table supporting lug through a connecting shaft, the other end of the launcher is connected with the stretching end of a pitching lifting cylinder, and the fixed end of the pitching lifting cylinder is connected with a rotary table. An integrated mechanism is formed by the launcher, the orientation rotary table and the pitching lifting cylinder, the launcher achieves the launching angle through the pitching lifting cylinder, and 360-degree target follow-up can be achieved through the orientation rotary table.
Description
Technical field
The invention belongs to MISSILE LAUNCHING engineering field, relate to a kind of volume large, weight is large, and rigid requirements is high, and the middle short range that integrated level is high tilts to launch the design and manufacture of Z-gun.This missile launcher is vehicle-mounted roadless transport, is to require as design basis with being easy to load based on guided missile installation accuracy.
Background technology
New missile launcher, is not only the installation foundation of guided missile, is also the installation foundation of other subsystem of MISSILE LAUNCHING.Be characterized in that volume is large, weight is large, and rigid requirements is high, and level of integrated system is high.As the foundation structure that MISSILE LAUNCHING is important, missile launcher structural design is one of important content of whole missile release system structural design, the quality of its designing quality directly has influence on the quality of missile release system, and launcher structural design more and more becomes the important step affecting MISSILE LAUNCHING technology tactics index.For this reason, we have proposed a kind of new missile launcher designing technique.
Summary of the invention
The technical problem solved
In order to avoid the deficiencies in the prior art part, the present invention proposes a kind of for ramp-launched MISSILE LAUNCHING shelf structure.
Technical scheme
A kind of for ramp-launched MISSILE LAUNCHING shelf structure, it is characterized in that comprising launcher, azimuth rotating platform and pitching elects cylinder, one end of launcher is installed on azimuth rotating platform journal stirrup by coupking shaft, and the other end and pitching are elected cylinder external part and be connected, and pitching is elected cylinder stiff end and is connected with azimuth rotating platform, described launcher comprises launcher girder, the auxiliary beam of launcher, the left stretcher of mounting cylinder bullet and the right stretcher of mounting cylinder bullet, launcher girder, the auxiliary beam of launcher, the left stretcher of mounting cylinder bullet and the right stretcher of mounting cylinder bullet adopt section bar steel pipe welding to be connected into an entirety, be divided into upper and lower two-layer symmetrical, the left stretcher of mounting cylinder bullet and the right stretcher of mounting cylinder bullet lay respectively at a left side for lower floor, right side, the left stretcher of mounting cylinder bullet, the medium position of the right stretcher of mounting cylinder bullet is respectively provided with an armstrong's patent push rod, manually push-and-pull armstrong's patent push rod launches the left stretcher of mounting cylinder bullet, the right stretcher of mounting cylinder bullet, the left stretcher of mounting cylinder bullet, the surface of the right stretcher of mounting cylinder bullet is respectively provided with 2 cylinder bullet secure mounting arrangements, the upper strata of launcher is provided with 4 cylinder bullet secure mounting arrangements.
Described cylinder bullet secure mounting arrangements comprises locating groove, left-handed closely-pitched screw rod, dextrorotation closely-pitched screw rod and the clamping block that the erection support on restriction cylinder bullet falls into automatically, manually rotates left-handed closely-pitched screw rod, dextrorotation closely-pitched screw rod makes clamping block move toward one another be fixed by cylinder bullet.
Launcher girder material adopts 20CrMnSiA, launcher auxiliary beam material selection 16Mn.
Beneficial effect
The one that the present invention proposes is used for ramp-launched MISSILE LAUNCHING shelf structure, tool following points beneficial effect:
1, this launcher, azimuth rotating platform, pitching are elected cylinder and are constituted an integrated model, achieve launcher and elect emission angle by pitching election cylinder, and realize 360 degree with moving-target by azimuth rotating platform.
2, launcher adopts section bar steel-pipe welding shaping, upper and lower two-layer design, underlying design can flared left and right attached frame so that the filling of cylinder bullet.
3, launcher upper surface is designed with inertial navigation datum clamp face, TV datum clamp face and cylinder bullet and installs fixed datum.Datum level determines the depth of parallelism of cylinder bullet axis and inertial navigation, TV axis.Lower floor's cylinder bullet installed surface benchmark with upper strata cylinder bullet datum clamp face for benchmark, rely on processing ensure that doffing bullet axis and inertial navigation, TV axis parallel.
4, design and installation 4 groups independently cylinder bullet locking device, loads smoothly for cylinder bullet and locks.
Accompanying drawing explanation
Fig. 1 launcher figure of the present invention: (a) left view; (b) right view
Fig. 2 cylinder bullet locking device
Fig. 3 launcher structure chart of the present invention: (a) front view; (b) rearview; C () loads onto the front view of cylinder; D () loads onto the rearview of cylinder;
1-launcher girder; The auxiliary beam of 2-launcher; The left stretcher of 3-mounting cylinder bullet; The right stretcher of 4-mounting cylinder bullet; 5-armstrong's patent push rod; 6-inertial navigation system datum clamp face; Tool datum clamp face taken aim at by 7-TV; 8-cylinder bullet secure mounting arrangements datum level; 9-cylinder bullet secure mounting arrangements; 10-locating groove; The left-handed closely-pitched screw rod of 11-; 12-dextrorotation closely-pitched screw rod; 13-clamping block; 14-launcher; 15-azimuth rotating platform; Cylinder is elected in 16-pitching; 17-cylinder bullet; Control case sent out by 18-guided missile; 19-guided missile secondary power supply; 20-inertial navigation system; Tool taken aim at by 21-TV; 22-command reception antenna; 23-turret supports axle.
Detailed description of the invention
Now in conjunction with the embodiments, the invention will be further described for accompanying drawing:
This launcher adopts section bar steel-pipe welding shaping, and can load 4 pieces of cylinder bullets, cylinder bullet is two-layer to be up and down arranged symmetrically with in echelon.Vehicle traveling, movement requirement is met after this launcher handling tube bullet.This launcher one end is arranged on azimuth rotating platform journal stirrup by coupking shaft, and the other end and pitching are elected cylinder external part and be connected, and pitching is elected cylinder stiff end and is connected with turntable; Launcher, azimuth rotating platform, pitching are elected cylinder and are constituted an integrated model, achieve launcher and elect cylinder to emission angle by pitching, and realize 360 degree with moving-target by azimuth rotating platform.For meeting vehicle transport and filling cylinder bullet, underlying design can flared left and right attached frame, and the filling being beneficial to lower floor's cylinder bullet is changed.Launcher upper surface is designed with inertial navigation datum clamp face, TV datum clamp face and cylinder bullet and installs fixed datum.Datum level determines the depth of parallelism of cylinder bullet axis and inertial navigation, TV axis.Lower floor's left and right attached frame devises cylinder bullet benchmark installed surface, lower floor's cylinder bullet installed surface benchmark with upper strata cylinder bullet datum clamp face for benchmark, rely on processing ensure that doffing bullet axis and inertial navigation, TV axis parallel.The depth of parallelism of levels 4 cylinder bullet axis and inertial navigation, TV axis controls within 0.4mm, and being converted into angular deviation is 0.6 '.The expansion of left and right attached frame relies on the push-and-pull of armstrong's patent push rod, development distance 300mm.Launcher is installed 4 groups of independently cylinder bullet locking devices, for the safety locking of 4 cylinder bullets; The cylinder bullet self adaptation that this locking device is designed with three guiding installs locating groove, and the erection support on restriction cylinder bullet falls into automatically; This secure mounting arrangements arranges two oppositely closely-pitched screw rod, and manually to make clamping block move toward one another cylinder be played bearing automatically stuck for rotating screw bolt; Closely-pitched screw rod has good self-locking property, and when ensure that Transport Vibration, clamping block can not loosen.
See Fig. 1, launcher adopts rectangle section bar steel-pipe welding, and launcher girder 1 material adopts 20CrMnSiA, auxiliary beam 2 material selection 16Mn.Launcher divides upper and lower two-layer design.The left and right stretcher of underlying design mounting cylinder bullet, left and right stretcher is led by guide rail, and armstrong's patent push rod 5 realizes launching, and the filling being beneficial to lower floor's cylinder bullet is changed.Launcher upper surface is designed with inertial navigation system datum clamp face 6, tool datum clamp face 7 taken aim at by TV and cylinder bullet secure mounting arrangements datum level 8.Datum level determines the depth of parallelism that tool axis taken aim at by cylinder bullet axis and inertial navigation system, TV.The left and right stretcher of lower floor devises cylinder bullet benchmark installed surface, lower floor's cylinder bullet secure mounting arrangements installed surface benchmark is with upper strata cylinder bullet datum clamp face for machining benchmark, and the axis of upper and lower four cylinder bullets takes aim at the parallel of tool axis with inertial navigation system, TV to rely on processing to ensure.
See Fig. 2, launcher has been installed independently cylinder bullet secure mounting arrangements 9, the cylinder bullet self adaptation that this apparatus design has three to lead installs locating groove 10, and the erection support on restriction cylinder bullet falls into automatically; This secure mounting arrangements arranges left-handed closely-pitched screw rod 11 and dextrorotation closely-pitched screw rod 12, and manually rotating screw bolt makes clamping block 13 move toward one another that cylinder is played bearing to kill; Closely-pitched screw rod has good self-locking property, and when ensure that Transport Vibration, clamping block can not loosen.
See Fig. 3, launcher 14, azimuth rotating platform 15, pitching are elected cylinder 16 and are constituted an integrated model, achieve launcher 14 and elect cylinder 16 to emission angle by pitching, and realize 360 degree with moving-target by azimuth rotating platform 15.Cylinder bullet 17 installed by launcher 13, control case 18 sent out by guided missile, guided missile secondary power supply 19, inertial navigation system 20, TV taken aim at tool 21 and command reception antenna 22.Launcher 13 and azimuth rotating platform 14 elect cylinder 15 by hydraulic pitch and turret supports axle 23 links together.
Claims (3)
1., for a ramp-launched MISSILE LAUNCHING shelf structure, it is characterized in that comprising launcher (14), azimuth rotating platform (15) and pitching elects cylinder (16), one end of launcher (14) is installed on azimuth rotating platform (15) journal stirrup by coupking shaft, the other end and pitching are elected cylinder (16) external part and are connected, and pitching is elected cylinder (16) stiff end and is connected with azimuth rotating platform (15), described launcher (14) comprises launcher girder (1), the auxiliary beam of launcher (2), the left stretcher of mounting cylinder bullet (3) and the right stretcher of mounting cylinder bullet (4), launcher girder (1), the auxiliary beam of launcher (2), the left stretcher of mounting cylinder bullet (3) and the right stretcher of mounting cylinder bullet (4) adopt section bar steel pipe welding to be connected into an entirety, be divided into upper and lower two-layer symmetrical, the left stretcher of mounting cylinder bullet (3) and the right stretcher of mounting cylinder bullet (4) lay respectively at a left side for lower floor, right side, the left stretcher of mounting cylinder bullet (3), the medium position of the right stretcher of mounting cylinder bullet (4) is respectively provided with an armstrong's patent push rod (5), manually push-and-pull armstrong's patent push rod (5) launches the left stretcher of mounting cylinder bullet (3), the right stretcher of mounting cylinder bullet (4), the left stretcher of mounting cylinder bullet (3), the surface of the right stretcher of mounting cylinder bullet (4) is respectively provided with 2 cylinder bullet secure mounting arrangements (9), the upper strata of launcher is provided with 4 cylinder bullet secure mounting arrangements (9).
2. one according to claim 1 is used for ramp-launched MISSILE LAUNCHING shelf structure, it is characterized in that locating groove (10), left-handed closely-pitched screw rod (11), dextrorotation closely-pitched screw rod (12) and clamping block (13) that described cylinder bullet secure mounting arrangements (9) comprises the erection support on restriction cylinder bullet and automatically falls into, manually rotate left-handed closely-pitched screw rod (11), dextrorotation closely-pitched screw rod (12) makes clamping block (13) move toward one another be fixed by cylinder bullet.
3. one according to claim 1 is used for ramp-launched MISSILE LAUNCHING shelf structure, it is characterized in that launcher girder (1) material adopts 20CrMnSiA, the auxiliary beam of launcher (2) material selection 16Mn.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410815762.7A CN104634163B (en) | 2014-12-23 | 2014-12-23 | A kind of for ramp-launched MISSILE LAUNCHING shelf structure |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410815762.7A CN104634163B (en) | 2014-12-23 | 2014-12-23 | A kind of for ramp-launched MISSILE LAUNCHING shelf structure |
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| Publication Number | Publication Date |
|---|---|
| CN104634163A true CN104634163A (en) | 2015-05-20 |
| CN104634163B CN104634163B (en) | 2016-04-06 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201410815762.7A Active CN104634163B (en) | 2014-12-23 | 2014-12-23 | A kind of for ramp-launched MISSILE LAUNCHING shelf structure |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107764133A (en) * | 2017-09-29 | 2018-03-06 | 北京航天发射技术研究所 | A kind of truss-like Missile Erecting Arm |
| CN108327616A (en) * | 2017-12-18 | 2018-07-27 | 北京新立机械有限责任公司 | A kind of ground and vehicle-mounted upper dress dual-purpose type cylinder bounces perpendicular parking device and its perpendicular method is parked, transports and risen to cylinder bullet |
| CN110108161A (en) * | 2019-05-13 | 2019-08-09 | 上海机电工程研究所 | Guided missile launcher |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5682005A (en) * | 1995-05-31 | 1997-10-28 | Loral Vought Systems Corporation | Missile container support rack |
| WO2010113170A1 (en) * | 2009-03-31 | 2010-10-07 | Defence Research & Development Organisation | An object launcher |
| KR20120010909A (en) * | 2010-07-27 | 2012-02-06 | 국방과학연구소 | Latching device and launching apparatus having the same |
| CN103697758A (en) * | 2013-11-28 | 2014-04-02 | 北京机械设备研究所 | Semitrailer launching vehicle for launching target projectile |
| CN204388707U (en) * | 2014-12-23 | 2015-06-10 | 西安电子工程研究所 | A kind of for ramp-launched MISSILE LAUNCHING shelf structure |
-
2014
- 2014-12-23 CN CN201410815762.7A patent/CN104634163B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5682005A (en) * | 1995-05-31 | 1997-10-28 | Loral Vought Systems Corporation | Missile container support rack |
| WO2010113170A1 (en) * | 2009-03-31 | 2010-10-07 | Defence Research & Development Organisation | An object launcher |
| KR20120010909A (en) * | 2010-07-27 | 2012-02-06 | 국방과학연구소 | Latching device and launching apparatus having the same |
| CN103697758A (en) * | 2013-11-28 | 2014-04-02 | 北京机械设备研究所 | Semitrailer launching vehicle for launching target projectile |
| CN204388707U (en) * | 2014-12-23 | 2015-06-10 | 西安电子工程研究所 | A kind of for ramp-launched MISSILE LAUNCHING shelf structure |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107764133A (en) * | 2017-09-29 | 2018-03-06 | 北京航天发射技术研究所 | A kind of truss-like Missile Erecting Arm |
| CN108327616A (en) * | 2017-12-18 | 2018-07-27 | 北京新立机械有限责任公司 | A kind of ground and vehicle-mounted upper dress dual-purpose type cylinder bounces perpendicular parking device and its perpendicular method is parked, transports and risen to cylinder bullet |
| CN108327616B (en) * | 2017-12-18 | 2019-12-06 | 北京新立机械有限责任公司 | Ground and vehicle-mounted dual-purpose cartridge bouncing and erecting parking device and cartridge bouncing and parking, transporting and erecting method thereof |
| CN110108161A (en) * | 2019-05-13 | 2019-08-09 | 上海机电工程研究所 | Guided missile launcher |
| CN110108161B (en) * | 2019-05-13 | 2021-05-14 | 上海机电工程研究所 | Missile launching device |
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| Publication number | Publication date |
|---|---|
| CN104634163B (en) | 2016-04-06 |
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