CN104401868A - Missile lifting appliance with quick state regulation function and automatic locking function - Google Patents
Missile lifting appliance with quick state regulation function and automatic locking function Download PDFInfo
- Publication number
- CN104401868A CN104401868A CN201410687848.6A CN201410687848A CN104401868A CN 104401868 A CN104401868 A CN 104401868A CN 201410687848 A CN201410687848 A CN 201410687848A CN 104401868 A CN104401868 A CN 104401868A
- Authority
- CN
- China
- Prior art keywords
- guided missile
- suspender
- lifting
- hoist block
- main girder
- 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.)
- Granted
Links
Classifications
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Lining And Supports For Tunnels (AREA)
- Load-Engaging Elements For Cranes (AREA)
Abstract
The invention discloses a missile lifting appliance with a quick state regulation function and an automatic locking function. The missile lifting appliance comprises a lifting appliance girder, a positioning device, a lifting ring, a front lifting block and a rear safety device, wherein the positioning device is arranged below the lifting ring, and is used for fixing the lifting ring at a specific position of the lifting appliance girder; a plurality of positioning holes are formed in one side of the lifting appliance girder and respectively correspond to the centre-of-gravity positions of missiles of different types; the front lifting block and the rear safety device are respectively arranged at two ends of the lifting appliance girder. The missile lifting appliance is easy to operate and high in lifting safety, and has the advantage that quick regulation is realized.
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 quick adjustment state and coupler lock.
Background technology
The lifting method of guided missile is varied, but guided missile suspender in the past or poor stability simple to operate, or the high still complicated operation of safety.And guided missile suspender regulating power is in the past poor, during the lifting of different conditions guided missile, the status adjustment of suspender takes time and effort.Therefore, need to provide a kind of new technical scheme to solve 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 quick adjustment state and coupler lock.
For solving technical matters of the present invention, the technical solution used in the present invention is:
A kind of can the guided missile suspender of quick adjustment state and coupler lock, this guided missile suspender comprises hanger main girder, registration device, hoisting ring, front hoist block and rear safety device, described registration device is arranged on below hoisting ring, hoisting ring is fixed on hanger main girder ad-hoc location by described registration device, described hanger main girder side is provided with multiple knock hole, the center-of-gravity position of the corresponding different model guided missile of multiple knock hole difference, described front hoist block and rear safety device are arranged on the two ends of hanger main girder respectively.
Described registration device comprises clip, housing and fix shaft, and described clip side has an opening, and this opening is for inserting fix shaft, and described fix shaft outer end is fixed in opening by housing.
Described fix shaft has spring along its circumference surface cover, and this spring is contained in housing.
Described rear safety device comprises 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 effect of the present invention: rear safety device can when suspender docks with guided missile coupler lock, without the need to manual operation, guarantee guided missile lifting safety; Registration device pin diameter is very little, girder can be opened more closeer knock hole, can meet the lifting of Multiple Type guided missile; During the lifting of different conditions guided missile, suspender can realize status adjustment fast.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention.
Fig. 2 is the structural representation of registration device in Fig. 1.
Fig. 3 is the side sectional view of Fig. 2 registration device.
Fig. 4 is the structural representation of rear safety device in Fig. 1.
Fig. 5 is the side sectional view of safety device after Fig. 4.
Wherein, 1, front hoist block, 2, hanger main girder, 3, registration device, 31, clip, 32, opening, 33, housing, 34, spring, 35, fix shaft, 4, hoisting ring, 5, rear safety device, 51, rear hoist block, 52, torsion spring, 53, separate lock handle, 54, backstop claw, 6, knock hole.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, the invention will be further described.Following examples, only for illustration of the present invention, are not used for limiting the scope of the invention.
With reference to figure 1, of the present invention a kind of can the guided missile suspender of quick adjustment state and coupler lock, this guided missile suspender comprises hanger main girder 2, registration device 3, hoisting ring 4, front hoist block 1 and rear safety device 5, registration device 3 is arranged on below hoisting ring 4, hoisting ring 4 is fixed on hanger main girder 2 ad-hoc location by registration device 3, hanger main girder 2 side is provided with multiple knock hole 6, the center-of-gravity position of the corresponding different model guided missile of multiple knock hole 6 difference, front hoist block 1 and rear safety device 5 are arranged on the two ends of hanger main girder 2 respectively.
Referring to figs. 2 and 3, registration device 3 comprises clip 31, housing 33 and fix shaft 35, clip 31 side has an opening 32, this opening 32 is for inserting fix shaft 35, fix shaft 35 has spring 34 along its circumference surface cover, this spring 34 is contained in housing 33, and fix shaft 35 outer end is fixed in opening 32 by housing 33.
With reference to figure 4 and Fig. 5, rear safety device 5 comprises 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 near torsion spring 52 one end separates lock handle 53.
Guided missile suspender of the present invention is made up of five parts, and registration device 3 is arranged in the middle part of hanger main girder 2, and can move with the center-of-gravity position of different guided missile, hoisting ring 4 is arranged on registration device 3.Front hoist block 1 and rear safety device 5 are installed on hanger main girder 2 two ends, for lifting by crane guided missile.
Principle of work of the present invention: front hoist block 1 is for lifting by crane guided missile front-slider, and front hoist block 1 designs manual bolt backstop slide block; Rear safety device 5 is for lifting by crane guided missile rear slider, and rear safety device 5 adopts torsion spring 52 to drive backstop claw 54 backstop slide block; Front hoist block 1 coordinates with rear safety device 5 lifting carrying out guided missile, not only easy to operate, the more important thing is safe and reliable, even if operating personal is forgotten insert artificial latch, also can guarantee guided missile lifting safety.In addition, front hoist block 1 and rear safety device 5 all arrange guide rail, can coordinate lift by crane, without the need to designing lifting eye on body with missile block.
Guided missile hanger main girder 2 side is provided with multiple knock hole 6, respectively the center-of-gravity position of corresponding different model guided missile, and guided missile positioning device of hoist 3 is easy and simple to handle, the i.e. slidably clip 1 of twisting fix shaft 35, clip 1 is moved to guided missile center-of-gravity position, oppositely twisting fix shaft 35, can fixing hoop 1.
Overall, rear safety device 5 of the present invention can when suspender docks with guided missile coupler lock, without the need to manual operation, guarantee guided missile lifting safety; Registration device 3 pin diameter is very little, girder can be opened more closeer knock hole 6, can meet the lifting of Multiple Type guided missile; During the lifting of different conditions guided missile, suspender can realize status adjustment fast.
Claims (4)
1. one kind can the guided missile suspender of quick adjustment state and coupler lock, it is characterized in that: this guided missile suspender comprises hanger main girder, registration device, hoisting ring, front hoist block and rear safety device, described registration device is arranged on below hoisting ring, hoisting ring is fixed on hanger main girder ad-hoc location by described registration device, described hanger main girder side is provided with multiple knock hole, the center-of-gravity position of the corresponding different model guided missile of multiple knock hole difference, described front hoist block and rear safety device are arranged on the two ends of hanger main girder respectively.
2. according to claim 1 a kind of can the guided missile suspender of quick adjustment state and coupler lock, it is characterized in that: described registration device comprises clip, housing and fix shaft, described clip side has an opening, this opening is for inserting fix shaft, and described fix shaft outer end is fixed in opening by housing.
3. according to claim 2 a kind of can the guided missile suspender of quick adjustment state and coupler lock, it is characterized in that: described fix shaft has spring along its circumference surface cover, and this spring is contained in housing.
4. according to claim 1 a kind of can the guided missile suspender of quick adjustment state and coupler lock, it is characterized in that: described rear safety device comprises rear hoist block, torsion spring and backstop claw, described torsion spring is installed on rear hoist block bottom, 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.
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 true CN104401868A (en) | 2015-03-11 |
| CN104401868B 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) |
Cited By (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 |
Citations (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
Patent Citations (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 |
Cited By (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 |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104401868B (en) | 2016-08-24 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US1852629A (en) | Mooring device | |
| LT2014008A (en) | Suspension device | |
| CN205790793U (en) | A kind of charging connector device of multi-storied garage | |
| CN204281046U (en) | A kind of can the guided missile suspender of quick adjustment state and coupler lock | |
| CN104401868A (en) | Missile lifting appliance with quick state regulation function and automatic locking function | |
| CN204200789U (en) | Self-locking movable bolt device | |
| CN103224190A (en) | Wire barrel lifting auxiliary mechanism | |
| EP3187739A1 (en) | Hook structure with self-locking function | |
| CN104313809A (en) | Needle not easy for falling off of thread | |
| CN105329769A (en) | Variable pitch gearbox hoisting tool for wind generating set | |
| CN203581351U (en) | Lifting lock mechanism for recycling autonomous underwater vehicle | |
| CN204920536U (en) | Abrasionproof decreases bolt | |
| CN204835064U (en) | Novel pull ring formula plug | |
| CN204114591U (en) | Be convenient to the flashlight held | |
| CN206782018U (en) | A kind of band latch limit telescopic springboard | |
| CN203959653U (en) | A kind of for changing the hanger structure of furnace roller | |
| MX2018003394A (en) | Cartridge-type vane pump. | |
| CN204619219U (en) | Slider | |
| CN204162268U (en) | A kind of auxiliary hoisting device of turbine high-pressure valve assembling | |
| CN204235505U (en) | The dual-purpose Circlip tongs of plug-in hole axle | |
| CN205686852U (en) | A kind of stretch cord of belt lock catch hook | |
| CN204565821U (en) | Grinding head motor | |
| CN204529108U (en) | Chain shrinks and regulates hoisting rig | |
| CN203239253U (en) | Mechanism capable of achieving restoring, locking and closing of baffle block of anti-disengaging lift sub | |
| CN209457612U (en) | A kind of pulley door lock rod |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |