CN104401868B - A kind of can the guided missile suspender of quickly adjustment state and automatic blocking - Google Patents
A kind of can the guided missile suspender of quickly adjustment state and automatic blocking Download PDFInfo
- Publication number
- CN104401868B CN104401868B CN201410687848.6A CN201410687848A CN104401868B CN 104401868 B CN104401868 B CN 104401868B CN 201410687848 A CN201410687848 A CN 201410687848A CN 104401868 B CN104401868 B CN 104401868B
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- CN
- China
- Prior art keywords
- guided missile
- suspender
- main girder
- positioner
- hanger main
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B66—HOISTING; LIFTING; HAULING
- B66C—CRANES; LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS, WINCHES, OR TACKLES
- B66C1/00—Load-engaging elements or devices attached to lifting or lowering gear of cranes or adapted for connection therewith for transmitting lifting forces to articles or groups of articles
- B66C1/10—Load-engaging elements or devices attached to lifting or lowering gear of cranes or adapted for connection therewith for transmitting lifting forces to articles or groups of articles by mechanical means
- B66C1/22—Rigid members, e.g. L-shaped members, with parts engaging the under surface of the loads; Crane hooks
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Lining And Supports For Tunnels (AREA)
- Load-Engaging Elements For Cranes (AREA)
Abstract
The invention discloses a kind of can the guided missile suspender of quickly adjustment state and automatic blocking, this guided missile suspender includes hanger main girder, positioner, hoisting ring, front hoist block and rear safety, positioner is arranged on below hoisting ring, hoisting ring is fixed on hanger main girder ad-hoc location by positioner, hanger main girder side is provided with hole, multiple location, the position of centre of gravity of the most corresponding different model guided missile in hole, multiple location, front hoist block and rear safety are separately mounted to the two ends of hanger main girder.The guided missile suspender of the present invention, simple to operate, lifting safety is high, it is achieved that the quick regulatory function of guided missile suspender.
Description
Technical field
The present invention relates to a kind of guided missile suspender, particularly relate to a kind of can the guided missile suspender of quickly adjustment state and automatic blocking.
Background technology
The lifting method of guided missile is varied, but conventional guided missile suspender or poor stability simple to operate, otherwise but safety is high operates complexity.And conventional guided missile suspender regulating power is poor, during the lifting of different conditions guided missile, the status adjustment of suspender takes time and effort.Accordingly, it is desirable to provide a kind of new technical scheme solves the problems referred to above.
Summary of the invention
The technical issues that need to address of the present invention be to provide a kind of can the guided missile suspender of quickly adjustment state and automatic blocking.
For solving the technical problem of the present invention, the technical solution used in the present invention is:
A kind of can the guided missile suspender of quickly adjustment state and automatic blocking, this guided missile suspender includes hanger main girder, positioner, hoisting ring, front hoist block and rear safety, described positioner is arranged on below hoisting ring, hoisting ring is fixed on hanger main girder ad-hoc location by described positioner, described hanger main girder side is provided with hole, multiple location, the position of centre of gravity of the most corresponding different model guided missile in hole, multiple location, described front hoist block and rear safety are separately mounted to the two ends of hanger main girder.
Described positioner includes that clip, housing and locating shaft, described clip side have an opening, and this opening is used for inserting locating shaft, and described locating shaft outer end is fixed in opening by housing.
Described locating shaft is cased with spring along its periphery, and this spring is contained in housing.
Described rear safety include rear hoist block, torsion spring and backstop claw, and described torsion spring is installed on rear hoist block bottom, and backstop claw is installed at described torsion spring two ends, and described rear hoist block bottom is provided with solution lock handle near one end.
Beneficial effects of the present invention: rear safety can when suspender docks with guided missile automatic blocking, it is not necessary to manual operation, it is ensured that guided missile lifting safety；Positioner pin diameter is the least, girder can be opened more closeer hole, location, it is possible to meet the lifting of Multiple Type guided missile；During the lifting of different conditions guided missile, suspender can quickly realize status adjustment.
Accompanying drawing explanation
Fig. 1 is the structural representation of the present invention.
Fig. 2 is the structural representation of positioner in Fig. 1.
Fig. 3 is the side sectional view of Fig. 2 positioner.
Fig. 4 is the structural representation of rear safety in Fig. 1.
Fig. 5 is the side sectional view of safety after Fig. 4.
Wherein, 1, front hoist block, 2, hanger main girder, 3, positioner, 31, clip,
32, opening, 33, housing, 34, spring, 35, locating shaft, 4, hoisting ring, 5, rear safety, 51, rear hoist block, 52, torsion spring, 53, solve lock handle, 54, backstop claw, 6, hole, location.
Detailed description of the invention
The invention will be further described with specific embodiment below in conjunction with the accompanying drawings.Following example are merely to illustrate the present invention, are not limited to protection scope of the present invention.
With reference to Fig. 1, the a kind of of the present invention can the guided missile suspender of quickly adjustment state and automatic blocking, this guided missile suspender includes hanger main girder 2, positioner 3, hoisting ring 4, front hoist block 1 and rear safety 5, positioner 3 is arranged on below hoisting ring 4, hoisting ring 4 is fixed on hanger main girder 2 ad-hoc location by positioner 3, hanger main girder 2 side is provided with hole, multiple location 6, the position of centre of gravity of the most corresponding different model guided missile in hole 6, multiple location, front hoist block 1 and rear safety 5 are separately mounted to the two ends of hanger main girder 2.
Referring to figs. 2 and 3, positioner 3 includes clip 31, housing 33 and locating shaft 35, clip 31 side has an opening 32, this opening 32 is used for inserting locating shaft 35, locating shaft 35 is cased with spring 34 along its periphery, this spring 34 is contained in housing 33, and locating shaft 35 outer end is fixed in opening 32 by housing 33.
With reference to Fig. 4 and Fig. 5, rear safety 5 include rear hoist block 51, torsion spring 52 and backstop claw 54, and torsion spring 52 is installed on rear hoist block 51 bottom, and backstop claw 54 is installed at torsion spring 52 two ends, and rear hoist block 51 bottom is provided with solution lock handle 53 near torsion spring 52 one end.
The guided missile suspender of the present invention is made up of five parts, and positioner 3 is arranged in the middle part of hanger main girder 2, can move with the position of centre of gravity of different guided missiles, and hoisting ring 4 is arranged on positioner 3.Front hoist block 1 and rear safety 5 are installed on hanger main girder 2 two ends, are used for lifting by crane guided missile.
The operation principle of the present invention: front hoist block 1 is used for lifting by crane guided missile front-slider, front hoist block 1 designs manual bolt backstop slide block；Rear safety 5 are used for lifting by crane guided missile rear slider, and rear safety 5 use torsion spring 52 to drive backstop claw 54 backstop slide block；Front hoist block 1 coordinates the lifting carrying out guided missile with rear safety 5, the most easy to operate, it is often more important that safe and reliable, even if operator forget to insert artificial latch, also ensures that guided missile lifts by crane safety.It addition, front hoist block 1 and rear safety 5 are respectively provided with guide rail, can coordinate with missile block and lift by crane, it is not necessary on body, design lifting eye.
Guided missile hanger main girder 2 side is provided with hole, multiple location 6, the position of centre of gravity of the most corresponding different model guided missile, and guided missile positioning device of hoist 3 is easy and simple to handle, twisting locating shaft 35 the most slidably clip 1, clip 1 is moved to guided missile position of centre of gravity, reversely twisting locating shaft 35, can fixing hoop 1.
Overall, the rear safety 5 of the present invention can when suspender docks with guided missile automatic blocking, it is not necessary to manual operation, it is ensured that guided missile lifting safety；Positioner 3 pin diameter is the least, girder can be opened more closeer hole, location 6, it is possible to meet the lifting of Multiple Type guided missile；During the lifting of different conditions guided missile, suspender can quickly realize status adjustment.
Claims (2)
1. one kind can the guided missile suspender of quickly adjustment state and automatic blocking, it is characterized in that: this guided missile suspender includes hanger main girder, positioner, hoisting ring, front hoist block and rear safety, described positioner is arranged on below hoisting ring, hoisting ring is fixed on hanger main girder ad-hoc location by described positioner, described hanger main girder side is provided with hole, multiple location, the position of centre of gravity of the most corresponding different model guided missile in hole, multiple location, described front hoist block and rear safety are separately mounted to the two ends of hanger main girder；Described positioner includes that clip, housing and locating shaft, described clip side have an opening, and this opening is used for inserting locating shaft, and described locating shaft outer end is fixed in opening by housing；Described rear safety include rear hoist block, torsion spring and backstop claw, and described torsion spring is installed on rear hoist block bottom, and backstop claw is installed at described torsion spring two ends, and described rear hoist block bottom is provided with solution lock handle near one end.
The most according to claim 1 a kind of can the guided missile suspender of quickly adjustment state and automatic blocking, it is characterised in that: described locating shaft is cased with spring along its periphery, and this spring is contained in housing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410687848.6A CN104401868B (en) | 2014-11-26 | 2014-11-26 | A kind of can the guided missile suspender of quickly adjustment state and automatic blocking |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410687848.6A CN104401868B (en) | 2014-11-26 | 2014-11-26 | A kind of can the guided missile suspender of quickly adjustment state and automatic blocking |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104401868A CN104401868A (en) | 2015-03-11 |
| CN104401868B true CN104401868B (en) | 2016-08-24 |
Family
ID=52639557
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410687848.6A Active CN104401868B (en) | 2014-11-26 | 2014-11-26 | A kind of can the guided missile suspender of quickly adjustment state and automatic blocking |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104401868B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105347176A (en) * | 2015-11-11 | 2016-02-24 | 平高集团有限公司 | Lifting appliance |
| CN108083103A (en) * | 2016-11-22 | 2018-05-29 | 江西洪都航空工业集团有限责任公司 | One kind can lift by crane slide block type and lifting lug formula guided missile Universal hanger |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201990370U (en) * | 2011-02-22 | 2011-09-28 | 北车风电有限公司 | Complete machine hanger with adjustable center of gravity |
| CN202030435U (en) * | 2011-04-18 | 2011-11-09 | 北京航天发射技术研究所 | Multi-point self-balancing hoisting sling |
| CN202465027U (en) * | 2012-03-05 | 2012-10-03 | 湘潭电机股份有限公司 | Balance adjusting sling |
| CN202594616U (en) * | 2012-05-04 | 2012-12-12 | 国营武汉长虹机械厂 | Multifunctional combined hanger |
| CN204281046U (en) * | 2014-11-26 | 2015-04-22 | 江西洪都航空工业集团有限责任公司 | A kind of can the guided missile suspender of quick adjustment state and coupler lock |
-
2014
- 2014-11-26 CN CN201410687848.6A patent/CN104401868B/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN104401868A (en) | 2015-03-11 |
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