CN108083103A - One kind can lift by crane slide block type and lifting lug formula guided missile Universal hanger - Google Patents
One kind can lift by crane slide block type and lifting lug formula guided missile Universal hanger Download PDFInfo
- Publication number
- CN108083103A CN108083103A CN201611048024.XA CN201611048024A CN108083103A CN 108083103 A CN108083103 A CN 108083103A CN 201611048024 A CN201611048024 A CN 201611048024A CN 108083103 A CN108083103 A CN 108083103A
- Authority
- CN
- China
- Prior art keywords
- rail
- hook
- girder
- guided missile
- claw
- 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
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
- B66C1/68—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 mounted on, or guided by, jibs
-
- 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
- B66C1/34—Crane hooks
- B66C1/36—Crane hooks with means, e.g. spring-biased detents, for preventing inadvertent disengagement of loads
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B66—HOISTING; LIFTING; HAULING
- B66C—CRANES; LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS, WINCHES, OR TACKLES
- B66C13/00—Other constructional features or details
- B66C13/04—Auxiliary devices for controlling movements of suspended loads, or preventing cable slack
- B66C13/06—Auxiliary devices for controlling movements of suspended loads, or preventing cable slack for minimising or preventing longitudinal or transverse swinging of loads
Abstract
The present invention provides one kind can lift by crane slide block type and lifting lug formula guided missile Universal hanger, it is characterized in that, including girder (3), fromer rail (1), rear rail (7), preceding hook (2), the rear hook (6) being removably sleeved on by quick-release latch (10) on girder (3), the hanging ring guide rail (7) being fixed by screws on girder (3), installation position adjustment hole on girder (3)；Fromer rail (1) and rear rail (7) are arranged in pairs, and fromer rail (1) or rear rail (7) are moved by position adjustment hole on girder (3), can lift by crane the guided missile of different hanging spacing；Preceding hook (2), rear hook (6) are arranged in pairs, preceding hook, rear hook are arranged between fromer rail, rear rail, and preceding hook, rear hook limit the relative motion between guided missile lifting lug and hook by two quick-release latch (9).
Description
Technical field
The present invention relates to a kind of guided missile Universal hangers, can lift by crane slide block type more particularly to one kind and lifting lug formula guided missile is general
Suspender.
Background technology
Guided missile suspender is essential lifting device during guided missile transhipment lifting, and the generalization suspender being integrally mostly used
It is future developing trend.Previous suspender used is mostly the guided missile for lifting by crane single form, such as the suspender in Fig. 1：1) phase can only be lifted by crane
The guided missile of form should be lifted by crane, lifting lug formula guided missile cannot be lifted by crane with slide block type guided missile with same suspender；2) different model guided missile needs
Otherwise with suspender, each model all must someone specially design, design repeated workload it is big, manufacture cost it is higher.Therefore, need
The guided missile that generalization suspender is designed to be applicable in the form of different liftings.
The content of the invention
The present invention provides one kind can lift by crane slide block type and lifting lug formula guided missile Universal hanger, which is characterized in that including girder
(3), fromer rail (1), rear rail (7), the preceding hook being removably sleeved on by quick-release latch (10) on girder (3)
(2), rear hook (6), the hanging ring guide rail (7) being fixed by screws on girder (3), installation position adjustment hole on girder (3)；
Fromer rail (1) and rear rail (7) are arranged in pairs, and fromer rail (1) or rear rail (7) are by position adjustment hole in girder
(3) moved on, the guided missile of different hanging spacing can be lifted by crane；
Preceding hook (2), rear hook (6) are arranged in pairs, and preceding hook, rear hook are arranged at fromer rail, rear rail
Between, preceding hook, rear hook limit the opposite fortune between guided missile lifting lug and hook by two quick-release latch (9)
It is dynamic；
Hanging ring guide rail (7) is arranged between preceding hook, rear hook, and hanging ring (5) is arranged on above hanging ring guide rail (7) simultaneously
Mobile along hanging ring guide rail (7), hanging ring is equipped with positioner (8), and positioner (8) insertion position adjustment hole realizes hanging ring in master
Location determination on beam (3).
Further, fromer rail (1) includes fromer rail main body (11), wrench shaft (12), torsional spring (13), shaft sleeve
(14), fluting thin nut (15) and claw (18) are combined into forced locking device,
Wrench shaft (12) is installed on by flat key in shaft sleeve (14), and torsional spring (13) is sleeved on shaft sleeve (14),
Claw (18) is mounted on the both ends of shaft sleeve (14), and fluting thin nut (15) is threaded in wrench shaft (12) one end, will pull
Hand axis (12) is fixed in fromer rail main body (11)；
On fromer rail main body (11) suit girder (3), guide groove is set, sliding block (17) squeezes upwards in fromer rail main body (11)
Claw (18) is pressed into guide groove, claw (18) automatically resets locking sliding block (17) under torsional spring (13) effect；Sliding block exits
When, sliding block is smoothly exited guide rail by rotating spanner axis (12) other end, claw (18) around wrench shaft (12) Unscrew.Pass through
The effect of claw (18) and torsional spring (13) can make missile block (17) be clamped on guide groove.
Further, stop block (16) is set on the stroke of claw (18), when claw (18) rotates up opening, by backstop
Block (16) backstop, at this point, claw (18) end lower surface is flushed with the top surface edge of guide groove.By setting stop block
(16), to avoid the upward excessively rotation of claw (18) missile block can be caused to collide with guide groove upper limb, and claw
(18) end lower surface is flushed with the top surface edge of guide groove can help sliding block to slip into guide groove along claw (18).
1) guide rail and hook are integrated, can lift by crane the guided missile of different suspension connection modes；
2) guide rail can overturn on girder from hook, be mobile with dismantling, it can be achieved that the guided missile of different hanging spacing lifts by crane；
3) multiple position adjustment holes on girder are set, hanging ring position is positioned by positioner, guided missile difference can be met
The hanging demand of center of gravity condition；
4) limit the relative rotation of guided missile lifting lug and hook with two quick-release latch, can guarantee guided missile and suspender without
Acutely rock.
Description of the drawings：
The guided missile suspender schematic diagram of Fig. 1 prior arts；A) slide block type guided missile suspender,
B) lifting lug formula guided missile suspender；
Fig. 2 is a kind of use state diagram of the present invention；
Fig. 3 is a kind of use state diagram of the present invention；
Fig. 4 is the structure diagram of fromer rail.
Specific embodiment：
The present invention is described in further detail below in conjunction with the accompanying drawings.
Refering to Fig. 2, one kind can lift by crane slide block type and lifting lug formula guided missile Universal hanger, which is characterized in that including girder 3, lead to
Fromer rail 1, rear rail 7, preceding hook 2, rear hook 6 that quick-release latch 10 is removably sleeved on girder 3 are crossed, is passed through
Screw is fixed on the hanging ring guide rail 7 on girder 3, installation position adjustment hole on girder 3；
Fromer rail 1 and rear rail 7 are arranged in pairs, and fromer rail 1 or rear rail 7 are moved by position adjustment hole on girder 3,
The guided missile of different hanging spacing can be lifted by crane；
Preceding hook 2, rear hook 6 are arranged in pairs, and preceding hook, rear hook are arranged between fromer rail, rear rail,
Preceding hook, rear hook limit the relative motion between guided missile lifting lug and hook by two quick-release latch 9；
Hanging ring guide rail 7 is arranged between preceding hook, rear hook, and hanging ring 5 is arranged on the top of hanging ring guide rail 7 and along hanging ring
Guide rail 7 moves, and hanging ring is equipped with positioner 8, and 8 insertion position adjustment hole of positioner realizes position of the hanging ring on girder 3
It determines.
Refering to Fig. 4, fromer rail 1 includes fromer rail main body 11, wrench shaft 12, torsional spring 13, shaft sleeve 14, fluting thin nut
15 and claw 18 be combined into forced locking device,
Wrench shaft 12 is installed on by flat key in shaft sleeve 14, and torsional spring 13 is sleeved on shaft sleeve 14, and claw 18 is pacified
Mounted in the both ends of shaft sleeve 14, fluting thin nut 15 is threaded in 12 one end of wrench shaft, wrench shaft 12 is fixed on leading
In rail main body 11；
Fromer rail main body 11 is set on girder 3, and guide groove, 17 upward claw 18 of sliding block are set in fromer rail main body 11
Into in guide groove, claw 18 automatically resets locking sliding block 17 under the effect of torsional spring 13；When sliding block exits, rotating spanner axis 12 is another
Sliding block is smoothly exited guide rail by one end, claw 18 around 12 Unscrew of wrench shaft.It can be with by the effect of claw 18 and torsional spring 13
Missile block 17 is made to be clamped on guide groove.
Further, stop block 16 on the stroke of claw 18 is set, when claw 18 rotates up opening, is stopped by stop block 16
Gear, at this point, 18 end lower surface of claw is flushed with the top surface edge of guide groove.It, can be to avoid card by setting stop block 16
Pawl 18 excessively rotates and missile block is caused to collide with guide groove upper limb upwards, and 18 end lower surface of claw and guide rail
The top surface edge of slot, which flushes, can help sliding block to slip into guide groove along claw 18.
Use process：
Operation principle：Suspender when Fig. 2 is lifting lifting lug formula guided missile lifts by crane state, and hook 2 before setting on girder rear rises
Suspension hook 6, preceding hook 2, rear hook 6 can be docked with guided missile lifting lug and lifted by crane, and suspension hook has locking catch, can ensure to lead
It bounces and hangs safety, two quick-release latch limit the relative rotation of guided missile lifting lug and preceding hook 2 and rear hook 6, can prevent
Only guided missile is in the swing in course direction.
Suspender when Fig. 3 is lifting slide block type guided missile lifts by crane state, during lifting, preceding hook 2, rear hook 6 is upward
180 ° of overturning until the top of girder 3, according to hanging spacing, determines the position of fromer rail 1 and rear rail 7, then by missile block into
Enter guide groove, then 18 energy auto lock sliding block of claw slowly steadily lifts by crane guided missile.After lifting, rotating spanner axis 17,
Sliding block is exited out of guide rail.
Claims (3)
1. one kind can lift by crane slide block type and lifting lug formula guided missile Universal hanger, which is characterized in that including girder (3), be stopped by quick-release
Dynamic pin (10) is removably sleeved on fromer rail (1), rear rail (7), preceding hook (2), rear hook (6) on girder (3),
The hanging ring guide rail (7) being fixed by screws on girder (3), installation position adjustment hole on girder (3)；
Fromer rail (1) and rear rail (7) are arranged in pairs, and fromer rail (1) or rear rail (7) are by position adjustment hole in girder (3)
Upper movement can lift by crane the guided missile of different hanging spacing；
Preceding hook (2), rear hook (6) are arranged in pairs, and preceding hook, rear hook are arranged between fromer rail, rear rail,
Preceding hook, rear hook limit the relative motion between guided missile lifting lug and hook by two quick-release latch (9)；
Hanging ring guide rail (7) is arranged between preceding hook, rear hook, and hanging ring (5) is arranged on above hanging ring guide rail (7) and edge is hung
Ring guide rail (7) is mobile, and hanging ring is equipped with positioner (8), and positioner (8) insertion position adjustment hole realizes hanging ring in girder
(3) location determination on.
2. according to claim 1 lift by crane slide block type and lifting lug formula guided missile Universal hanger, which is characterized in that fromer rail
(1) fromer rail main body (11), wrench shaft (12), torsional spring (13), shaft sleeve (14), fluting thin nut (15) and claw are included
(18) forced locking device is combined into,
Wrench shaft (12) is installed on by flat key in shaft sleeve (14), and torsional spring (13) is sleeved on shaft sleeve (14), claw
(18) both ends of shaft sleeve (14) are mounted on, fluting thin nut (15) is threaded in wrench shaft (12) one end, by wrench shaft
(12) it is fixed in fromer rail main body (11)；
On fromer rail main body (11) suit girder (3), guide groove, sliding block (17) upward card are set in fromer rail main body (11)
Into in guide groove, claw (18) automatically resets locking sliding block (17) pawl (18) under torsional spring (13) effect；When sliding block exits, turn
Sliding block is smoothly exited guide rail by wrench axis (12) other end, claw (18) around wrench shaft (12) Unscrew.
3. according to claim 2 lift by crane slide block type and lifting lug formula guided missile Universal hanger, which is characterized in that claw (18)
Stroke on stop block (16) is set, when claw (18) rotates up opening, by stop block (16) backstop, at this point, claw (18)
End lower surface is flushed with the top surface edge of guide groove.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611048024.XA CN108083103A (en) | 2016-11-22 | 2016-11-22 | One kind can lift by crane slide block type and lifting lug formula guided missile Universal hanger |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611048024.XA CN108083103A (en) | 2016-11-22 | 2016-11-22 | One kind can lift by crane slide block type and lifting lug formula guided missile Universal hanger |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108083103A true CN108083103A (en) | 2018-05-29 |
Family
ID=62170247
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611048024.XA Pending CN108083103A (en) | 2016-11-22 | 2016-11-22 | One kind can lift by crane slide block type and lifting lug formula guided missile Universal hanger |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108083103A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109100216A (en) * | 2018-09-17 | 2018-12-28 | 江西洪都航空工业集团有限责任公司 | A kind of missile block hanging load tool structure |
| CN109775552A (en) * | 2019-01-29 | 2019-05-21 | 杨胜 | Simple and easy hoisting device is used in a kind of installation of steel structure bridge |
| CN109969926A (en) * | 2019-04-16 | 2019-07-05 | 中建四局第六建筑工程有限公司 | A kind of movable pulley hoisting sling |
| CN110217690A (en) * | 2019-06-21 | 2019-09-10 | 河北巨力应急装备科技有限公司 | A kind of adjustable multipurpose way guided missile suspender |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0616380A (en) * | 1992-07-03 | 1994-01-25 | Toshiba Eng & Constr Co Ltd | Plug suspending jig |
| JP2003301217A (en) * | 2002-04-11 | 2003-10-24 | Nippon Steel Corp | Roll exchanging device |
| CN1765727A (en) * | 2005-11-18 | 2006-05-03 | 沈阳重型机械集团有限责任公司 | Half body gear dedicated sling |
| CN202594616U (en) * | 2012-05-04 | 2012-12-12 | 国营武汉长虹机械厂 | Multifunctional combined hanger |
| CN203411228U (en) * | 2013-07-22 | 2014-01-29 | 北京航天发射技术研究所 | Lifting appliance for lifting projectile body of weapon system |
| CN104071689A (en) * | 2014-07-02 | 2014-10-01 | 北京机械设备研究所 | Changeable centroid module vertical lifting appliance |
| CN104401868A (en) * | 2014-11-26 | 2015-03-11 | 江西洪都航空工业集团有限责任公司 | Missile lifting appliance with quick state regulation function and automatic locking function |
| CN204727441U (en) * | 2015-06-19 | 2015-10-28 | 河南宝起华东起重机有限公司 | A kind of hoisting crane self-locking sling |
| CN204778326U (en) * | 2015-07-15 | 2015-11-18 | 江西洪都航空工业集团有限责任公司 | Marine two some guided missile hoists of hanging |
-
2016
- 2016-11-22 CN CN201611048024.XA patent/CN108083103A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0616380A (en) * | 1992-07-03 | 1994-01-25 | Toshiba Eng & Constr Co Ltd | Plug suspending jig |
| JP2003301217A (en) * | 2002-04-11 | 2003-10-24 | Nippon Steel Corp | Roll exchanging device |
| CN1765727A (en) * | 2005-11-18 | 2006-05-03 | 沈阳重型机械集团有限责任公司 | Half body gear dedicated sling |
| CN202594616U (en) * | 2012-05-04 | 2012-12-12 | 国营武汉长虹机械厂 | Multifunctional combined hanger |
| CN203411228U (en) * | 2013-07-22 | 2014-01-29 | 北京航天发射技术研究所 | Lifting appliance for lifting projectile body of weapon system |
| CN104071689A (en) * | 2014-07-02 | 2014-10-01 | 北京机械设备研究所 | Changeable centroid module vertical lifting appliance |
| CN104401868A (en) * | 2014-11-26 | 2015-03-11 | 江西洪都航空工业集团有限责任公司 | Missile lifting appliance with quick state regulation function and automatic locking function |
| CN204727441U (en) * | 2015-06-19 | 2015-10-28 | 河南宝起华东起重机有限公司 | A kind of hoisting crane self-locking sling |
| CN204778326U (en) * | 2015-07-15 | 2015-11-18 | 江西洪都航空工业集团有限责任公司 | Marine two some guided missile hoists of hanging |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109100216A (en) * | 2018-09-17 | 2018-12-28 | 江西洪都航空工业集团有限责任公司 | A kind of missile block hanging load tool structure |
| CN109100216B (en) * | 2018-09-17 | 2021-05-18 | 江西洪都航空工业集团有限责任公司 | Guided missile slider hanging and loading tool structure |
| CN109775552A (en) * | 2019-01-29 | 2019-05-21 | 杨胜 | Simple and easy hoisting device is used in a kind of installation of steel structure bridge |
| CN109969926A (en) * | 2019-04-16 | 2019-07-05 | 中建四局第六建筑工程有限公司 | A kind of movable pulley hoisting sling |
| CN109969926B (en) * | 2019-04-16 | 2023-11-03 | 中建四局第六建筑工程有限公司 | Movable pulley lifting sling |
| CN110217690A (en) * | 2019-06-21 | 2019-09-10 | 河北巨力应急装备科技有限公司 | A kind of adjustable multipurpose way guided missile suspender |
| CN110217690B (en) * | 2019-06-21 | 2024-03-12 | 河北巨力应急装备科技有限公司 | Adjustable multipurpose missile hoist |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180529 |
|
| RJ01 | Rejection of invention patent application after publication |