CN206554646U - For the linking of carrier aircraft weapon suspension, spacing locking mechanism - Google Patents
For the linking of carrier aircraft weapon suspension, spacing locking mechanism Download PDFInfo
- Publication number
- CN206554646U CN206554646U CN201621213377.6U CN201621213377U CN206554646U CN 206554646 U CN206554646 U CN 206554646U CN 201621213377 U CN201621213377 U CN 201621213377U CN 206554646 U CN206554646 U CN 206554646U
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- locking key
- spacing
- locking
- locking mechanism
- hanger
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Abstract
The utility model is related to spacing, the interlock locking mechanism of a kind of suspension arrangement.The utility model, which is used for the linking of carrier aircraft weapon suspension, spacing locking mechanism, includes locking key component, bridle, spring, joining beam, spacing rocking arm, and the suspension that can be achieved multi-joint suspension arrangement hanger is spacing, be rapidly assembled and disassembled.When mounting hanger, manually handle makes spacing, interlock locking mechanism be in " loaded " position, and pull bar is released to the spacing of locking key component.When bomb shackle+hanger motion compresses locking key component upward along hanger, its locking key drives pusher dog to rotate together, and pusher dog is stirred bridle and rotated makes its retraction lath, and bomb shackle+hanger can be upwardly through.When bomb shackle+hanger, which is moved upward to, leaves suspension station axis δ mm, locking key component returns to operating position.After bomb shackle+hanger is dropped downwardly on locking key component, bridle returned in the presence of itself spring it is in situ pin bomb shackle, successively by the installation of many pieces of hangers can be completed from top to bottom.
Description
Technical field
The utility model belongs to aerial armament suspension arrangement, is related to a kind of linkage for carrier aircraft weapon suspension, limit
Position locking mechanism.
Background technology
The supporting bomb rack of existing carrier aircraft weapon suspension, bomb shackle connected mode have the fixation sides such as bolt, Quick-release pin
Formula is connected, it is necessary to use specific purpose tool, and needs more than 2 people to operate, and the cumbersome, time is long, bomb shackle of the present utility model with
Bomb rack is the automatic blocking link gear that can often mount, dismantle, simple to operate, is easy to tight working spaces in weapon-bay；
Many bullets, density suspension are used, it is easy to maintenance, using the linking of the automatic blocking, spacing locking mechanism with can reducing ordnance
Diligent operation element amount, shortens aircraft departure time again.
Utility model content
The technical problems to be solved in the utility model be to provide it is a kind of for the linking of carrier aircraft weapon suspension, it is spacing
Locking mechanism, it is easy to operate, to a greater extent utilize carrier aircraft weapon-bay, reduce aviation ground service operation element amount.
The technical solution of the utility model is, including link gear, rocking arm, joining beam, lock bridle etc. realize automatic blocking
Mount, fast quick-detach.
It is a kind of for the linking of carrier aircraft weapon suspension, spacing locking mechanism, it includes spacing locking mechanism and linkage
Mechanism, the left and right inner side for being symmetrically mounted on the left and right type beam of framework of spacing locking mechanism and link gear, wherein, spacing locking machine
Structure includes locking key, pusher dog, spring, locking key axle, bridle, and pusher dog is clipped in the centre of locking key, and locking key, pusher dog, spring pass through locking key
Axle is arranged on the middle part of left and right type beam, and bridle, spring are arranged on the middle part of left and right type beam, the work of its bridle by restraint axle
Make the hanging position of the supporting surface formation bomb shackle installation axle journal of face and locking key, spacing locking mechanism hangs bullet in suspension status
Hook installs axle journal by the firm spacing locking of locking key and bridle, and multiple bomb shackles and hanger are hung when there is multigroup locking mechanism
When, it can be realized by link gear, link gear includes control operating rod, rocking arm, spring, regulating bolt, connector, installed in limit
The bottom of position locking mechanism, link gear links together multigroup locking mechanism, when downward control operating rod, and pull bar drives many
Group pusher dog is rotated around locking key axle, and bridle is stirred around restraint axle in the head of pusher dog when rotating, and locking key is in bomb shackle installation axle
The locked position of neck, it is impossible to rotate, when bomb shackle and hanger move a segment distance upwards along framework leaves locking key, by pusher dog
The spring tightened makes locking key be rotated around locking key axle, now, and locking key and pusher dog, bridle are all in unloading lockset position of coupler, bomb shackle
The constraint of the unrestricted position locking of axle journal is installed, hanging position can be left, in unloaded state along the medial motion to mo(u)ld bottom half beam.
The beneficial effects of the utility model are to overcome complicated, cumbersome hanger locking process, from without considering lock
The use of instrument is closed, shortens many pieces of the quick of hanger and mounts, dismantles ground service time, operating space is saved, with operation
It is convenient, utilize carrier aircraft weapon-bay to a greater extent, reduce aviation ground service operation element amount, shorten aircraft departure time again, carry
High workload efficiency.The technology and like product of the country can be covered, is the new high density suspension arrangement of research and utilization, is carried out related
Technical research provides the foundation, and its technology can be used directly, with very high reference value.
Brief description of the drawings
The installment state schematic diagram of Fig. 1 a hangers；
The disassembly status schematic diagram of Fig. 1 b hangers；
Fig. 2 is linkage, spacing locking mechanical work principle figure；
Fig. 3 be linkage, spacing locking mechanism frame suspension arrangement application schematic diagram；
The regulating bolt of 1 rocking arm, 2 pusher dog, 3 locking key, 4 spring, 5 spring, 6 bridle, 7 joining beam component, 8 spring 9.
Embodiment
Below by accompanying drawing, by taking three-group linkage, spacing locking mechanism as an example, the utility model is described further.
It is a kind of for the linking of carrier aircraft weapon suspension, spacing locking mechanism, spacing locking mechanism includes locking key, dialled
Pawl, spring, locking key axle, bridle, linkage, the left and right inner side for being symmetrically mounted on the left and right type beam of framework of spacing locking mechanism are dialled
Pawl is clipped in the centre of locking key, and locking key, pusher dog, spring are by locking key axle installed in the middle part of left and right type beam, and bridle, spring are leaned on
Restraint axle is arranged on the middle part of left and right type beam, and the working face of its bridle and the supporting surface formation bomb shackle of locking key install axle journal
Hanging position, spacing locking mechanism in suspension status, bomb shackle install axle journal by the firm limiting lock of locking key and bridle
Close, when there is multigroup locking mechanism to hang multiple bomb shackles with hanger, can be realized by locking link gear, link gear bag
Control operating rod, rocking arm, spring, regulating bolt, connector are included, installed in the bottom of spacing locking mechanism, link gear will be multigroup
Locking mechanism links together, when downward control operating rod, and pull bar drives multigroup pusher dog to be rotated around locking key axle, and the head of pusher dog exists
During rotation, bridle is stirred around restraint axle, and the locked position of axle journal is installed in locking key in bomb shackle, it is impossible to rotate, work as bomb shackle
When moving a segment distance upwards along framework with hanger and leaving locking key, the spring tightened by pusher dog makes locking key be rotated around locking key axle,
Now, locking key and pusher dog, bridle are all in unloading lockset position of coupler, and bomb shackle installs the constraint of the unrestricted position locking of axle journal, can
Along the medial motion to mo(u)ld bottom half beam, hanging position is left, in unloaded state.
Because the connector of link gear makes multigroup locking mechanism connect in groups in the horizontal direction, a control operating rod, just
Make the rotation of multigroup spacing locking mechanism synchronous coordination unanimously, complete loading and the unloading of bomb shackle and hanger.
In loading condition, when bomb shackle is moved from bottom to top with hanger, bomb shackle, which installs axle journal, makes spacing locking machine
The locking key of structure, pusher dog are rotated around locking key axle, and pusher dog is stirred bridle and rotated around restraint axle, make bomb shackle installation axle neck grease smoothly from
Under move upward to the hanging position that need to be installed to, when installing multigroup spacing locking mechanism in order, each group of limiting lock
Close the locking key in mechanism to install under the pressure effect of axle journal in bomb shackle, in locking states.
Now, when downward control operating rod makes spacing locking mechanism be in unloaded state, locking key is still in locking states, only
When a certain hanging position bomb shackle installs axle journal one segment distance of motion leaves locking key upwards when, the locking key of the hanging position could be from
Hanging position is opened, in unloaded state.And the bomb shackle of other hanging positions installs axle journal by the firm limit of locking key and bridle
Position locking.
In unloaded state, pusher dog is stirred bridle and rotated around restraint axle, and the working face of bridle goes to bottom, not to hanging bullet
Hook install axle journal it is spacing, but bridle another restraint face turn to limitation bomb shackle install axle journal run up, make bomb shackle
Installing axle journal can only move in the limited position of hanging position, so, the bomb shackle of hanging position and hanger need to be unloaded also not
Understand unrestricted movement upwards and influence the bomb shackle and hanger of upper hanging position, so as to safety in order from most lower past
On unload by turn.
Linkage, the link gear of spacing locking mechanism link together multigroup spacing locking mechanism by joining beam component,
When operation handle makes locking mechanism be in loading condition or unloaded state, multigroup spacing locking mechanism synchronization start, reset are realized
Linkage, the synchronous interaction of spacing locking mechanism, interlocking.
For locking, hanger is installed, without any instrument, makes bomb shackle and the reliable locking of hanger on ground first,
Then, manually handle pull bar handle is in " loaded " position, and pull bar does not work to locking key.When bomb shackle+hanger along hanger to
During upper motion compresses locking key, its locking key drives pusher dog to rotate together, and pusher dog is stirred bridle and rotated makes its retraction lath, hangs bullet
Hook and hanger can be upwardly through, when bomb shackle and hanger, which are moved upward to, leaves δ millimeters of suspension station axis, now,
Locking key returns to operating position, and after slip hook is dropped downwardly in locking key with hanger, bridle is returned in the presence of itself spring
Pin bomb shackle and hanger in original position.Complete installation, the locking of bomb shackle and hanger (see Fig. 1 a).
When unloading bullet, handle is in the next (unloading position).Now pull bar, which moves down and rotates pusher dog, tightens locking key bullet
Spring, pusher dog is stirred bridle and rotated simultaneously makes its retraction lath, so that bomb shackle can be moved up with hanger.Bomb shackle with
When hanger moves upwardly off locking key, the spring tightened by pusher dog makes locking key retraction lath, now, dynamic with handing down, and makes
Bomb shackle+hanger realizes the fast quick-detach of bomb shackle and hanger downward away from hitch point position (see Fig. 1 b).
Claims (1)
1. it is a kind of for the linking of carrier aircraft weapon suspension, spacing locking mechanism, it is characterised in that including spacing locking mechanism
And link gear, the left and right inner side for being symmetrically mounted on the left and right type beam of framework of spacing locking mechanism and link gear, wherein,
Spacing locking mechanism includes locking key, pusher dog, spring, locking key axle, bridle, and pusher dog is clipped in the centre of locking key, locking key, dials
Pawl, spring are arranged on the middle part of left and right type beam by locking key axle, and bridle, spring are arranged in left and right type beam by restraint axle
Portion, the working face of its bridle and the supporting surface formation bomb shackle of locking key install the hanging position of axle journal, and spacing locking mechanism exists
During suspension status, bomb shackle installs axle journal by the firm spacing locking of locking key and bridle, and when having, multigroup locking mechanism suspension is more
When individual bomb shackle is with hanger, it can be realized by link gear,
Link gear includes control operating rod, rocking arm, spring, regulating bolt, connector, installed in the bottom of spacing locking mechanism,
Link gear links together multigroup locking mechanism, when downward control operating rod, and pull bar drives multigroup pusher dog to turn around locking key axle
Dynamic, bridle is stirred around restraint axle in the head of pusher dog when rotating, and the locked position of axle journal is installed in locking key in bomb shackle, no
It can rotate, when bomb shackle and hanger move a segment distance upwards along framework leaves locking key, the spring tightened by pusher dog makes lock
Key is rotated around locking key axle, now, and locking key and pusher dog, bridle are all in unloading lockset position of coupler, and it is unrestricted that bomb shackle installs axle journal
The constraint of position locking, can leave hanging position, in unloaded state along the medial motion to mo(u)ld bottom half beam.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621213377.6U CN206554646U (en) | 2016-11-09 | 2016-11-09 | For the linking of carrier aircraft weapon suspension, spacing locking mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621213377.6U CN206554646U (en) | 2016-11-09 | 2016-11-09 | For the linking of carrier aircraft weapon suspension, spacing locking mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206554646U true CN206554646U (en) | 2017-10-13 |
Family
ID=60368355
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621213377.6U Active CN206554646U (en) | 2016-11-09 | 2016-11-09 | For the linking of carrier aircraft weapon suspension, spacing locking mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206554646U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110304253A (en) * | 2019-06-04 | 2019-10-08 | 成都飞机工业集团电子科技有限公司 | It is a kind of for the linkage of airborne external hanging device, limit, automatically controlled throwing mechanism |
| CN114687548A (en) * | 2022-04-15 | 2022-07-01 | 重庆渝能建筑安装工程有限公司 | Attached lifting scaffold |
-
2016
- 2016-11-09 CN CN201621213377.6U patent/CN206554646U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110304253A (en) * | 2019-06-04 | 2019-10-08 | 成都飞机工业集团电子科技有限公司 | It is a kind of for the linkage of airborne external hanging device, limit, automatically controlled throwing mechanism |
| CN114687548A (en) * | 2022-04-15 | 2022-07-01 | 重庆渝能建筑安装工程有限公司 | Attached lifting scaffold |
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