CN206634468U - A kind of missile transport frame of rotatable lifting - Google Patents
A kind of missile transport frame of rotatable lifting Download PDFInfo
- Publication number
- CN206634468U CN206634468U CN201720251458.3U CN201720251458U CN206634468U CN 206634468 U CN206634468 U CN 206634468U CN 201720251458 U CN201720251458 U CN 201720251458U CN 206634468 U CN206634468 U CN 206634468U
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- CN
- China
- Prior art keywords
- support frame
- guided missile
- leading screw
- frame
- missile support
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- 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.)
- Expired - Fee Related
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- Forklifts And Lifting Vehicles (AREA)
Abstract
Ammunition transport field is the utility model is related to, specifically a kind of missile transport frame of rotatable lifting, including base and guided missile support frame, is flexibly connected between the guided missile support frame and base by support shaft；The guided missile support frame is internally provided with support frame elevating mechanism, support frame as described above elevating mechanism includes leading screw, it is equipped with the internal thread sliding block on leading screw, middle strut, motor and electric operating case, leading screw one end is coaxially disposed in driving motor output shaft, the leading screw other end is arranged on guided missile support frame by bearing, the top of middle strut is be hinged to be arranged at guided missile support frame top, the bottom of middle strut is be hinged to be arranged on internal thread sliding block, the missile transport frame of rotatable lifting of the present utility model, guided missile is set to carry out rotation process directly on pallet, amendment, which is hung, plays angle, the orientation of whole transport vehicle, which need not be adjusted, can complete to the installation on aircraft, it can be positioned on any angle and carry out lifting extension bullet operation, hang and play efficiency high.
Description
Technical field
Ammunition transport field is the utility model is related to, specifically a kind of missile transport frame of rotatable lifting.
Background technology
The effect of missile transport frame puts extension pop-off suitable for aircraft airborne guided missile is transported from ammunition depot, and by guided missile lifting
To guided missile hanger height, complete to hang spring operation work to facilitate.
After guided missile fortune is put sheet point by current missile transport frame, guided missile can only be vertically moved up or down, it is impossible to which bullet is hung in rotation adjustment
Angle, it is necessary to repeatedly adjust aligned position after can just rise, to aircraft on install, therefore missile transport frame is in some ground locations
Narrow and small place adjustment is highly inconvenient, has raised the use condition of missile transport frame, and extends extension and play the time, hangs bullet effect
Rate is not high, influences army's corresponding time.
Utility model content
Goal of the invention of the present utility model a kind of is hung so as to realize in lifting in the technological deficiency in background technology is overcome
It is capable of the angle correction of freedom and flexibility before bullet, improves the missile transport frame for hanging the rotatable lifting for playing efficiency.
For achieving the above object, the technical solution of the utility model is：A kind of missile transport frame of rotatable lifting,
Including base and guided missile support frame, the guided missile support frame is fixedly installed on base, between the guided missile support frame and base
It is flexibly connected by support shaft, guided missile support frame can rotate around support shaft；The guided missile support frame is internally provided with support frame liter
Descending mechanism, support frame as described above elevating mechanism include leading screw, are equipped with the internal thread sliding block on leading screw, middle strut, driving electricity
Machine and electric operating case, the motor are fixedly installed on guided missile support frame one end, and leading screw one end is coaxially disposed in driving electricity
On machine output shaft, the leading screw other end is arranged on guided missile support frame by bearing, and the top of middle strut is be hinged to be arranged at guided missile
Support frame top, the bottom of middle strut is be hinged to be arranged on internal thread sliding block, and electric operating case is fixedly installed on guided missile support frame
One end, the control motor work of electric operating case.
As optimal technical scheme of the present utility model, the guided missile support frame sets the opposite end of motor one end to set
Hand-operated lifting handle is equipped with, hand-operated lifting handle can drive leading screw to rotate by driving member, final to drive guided missile support frame to complete
Lifting action, in the case where condition does not allow, hand-operated lifting guided missile support frame make missile transport frame have stronger adaptability and
The ability of more remarkable reply emergency case.
As optimal technical scheme of the present utility model, the be hinged bullet that is provided with described guided missile support frame one end fixes machine
Structure, bullet fixed mechanism can be spun upside down around jointed shaft, body can be reinforced during missile transport, ensure that
Guided missile is safe and reliable in transportation.
As optimal technical scheme of the present utility model, guided missile support frame sets the opposite end of bullet fixed mechanism one end to consolidate
Surely draw bar, the scalable end for being inserted into guided missile support frame of the draw bar are provided with, draw bar has scalable design, not the used time
It can be withdrawn into guided missile support frame, both save space, while do not influence the work of missile transport frame again.
The beneficial effect of the missile transport frame of rotatable lifting of the present utility model：
1. the missile transport frame of rotatable lifting of the present utility model, is lived between guided missile support frame and base by support shaft
Dynamic connection, guided missile support frame can rotate around support shaft, and such structure makes guided missile to carry out rotation process directly on pallet,
Amendment, which is hung, plays angle, it is not necessary to which adjusting the orientation of whole transport vehicle can complete, to the installation on aircraft, to can be positioned on any angle
Degree carries out lifting and hangs bullet operation.
2. the missile transport frame of rotatable lifting of the present utility model, guided missile support frame sets the relative of motor one end
End is provided with hand-operated lifting handle, be equipped with it is electronic with manual two kinds of modes of operation, can meet it is a variety of under the conditions of extension bullet demand, make
Missile transport frame has the ability of stronger adaptability and more remarkable reply emergency case.
3. the missile transport frame of rotatable lifting of the present utility model, guided missile support frame one end is be hinged to be provided with bullet and fixes
Mechanism, bullet fixed mechanism can be spun upside down around jointed shaft, body can be reinforced during missile transport, be ensured
Guided missile is safe and reliable in the transportation.
Brief description of the drawings
Fig. 1 is the structural representation of the missile transport frame of rotatable lifting of the present utility model；
Fig. 2 is Fig. 1 overlooking the structure diagram；
Fig. 3 is Fig. 1 left view structural representation.
Referring to Fig. 1-3：1- bases, 2- guided missile support frames, 3- support shafts, 4- support frame elevating mechanisms, 401- leading screws, 402-
Internal thread sliding block, 403- centres strut, 404- motors, 405- electric operating casees, 5- hand-operated lifting handles, 6- bullets fix machine
Structure, 7- draw bars.
Embodiment
Below in conjunction with the accompanying drawings and by specific embodiment to the missile transport frame of rotatable lifting of the present utility model
Do more detailed description.
Embodiment 1：
The missile transport frame of rotatable lifting of the present utility model, including base 1 and guided missile support frame 2, the guided missile branch
Support 2 is fixedly installed on base 1, is flexibly connected between the guided missile support frame 2 and base 1 by support shaft 3, guided missile support
Frame 2 can rotate around support shaft 3；The guided missile support frame 2 is internally provided with support frame elevating mechanism 4, support frame as described above lift
Structure 4 includes leading screw 401, is equipped with the internal thread sliding block 402 on leading screw, middle strut 403, motor 404 and electronic behaviour
Make case 405, the motor 404 is fixedly installed on the one end of guided missile support frame 2, and the one end of leading screw 401 is coaxially disposed in driving electricity
On defeated 404 shaft of machine, the other end of leading screw 401 is arranged on guided missile support frame 2 by bearing, and the top of middle strut 403 is hinged
The top of guided missile support frame 2 is arranged at, the bottom of middle strut 403 is be hinged to be arranged on internal thread sliding block 402, electric operating case 405
The one end of guided missile support frame 2 is fixedly installed on, electric operating case 405 controls motor 404 to work.
The guided missile support frame 2 sets the opposite end of the one end of motor 404 to be provided with hand-operated lifting handle 5, rises manually
Drop handle 5 can drive leading screw 401 to rotate by driving member, final to drive guided missile support frame 2 to complete lifting action, the guided missile branch
The one end of support 2 is be hinged to be provided with bullet fixed mechanism 6, and bullet fixed mechanism 6 can be spun upside down around jointed shaft, can be in guided missile
Body is reinforced in transportation.
Guided missile support frame 2 sets the opposite end of the one end of bullet fixed mechanism 6 to be fixedly installed draw bar 7, the draw bar 7
The scalable end for being inserted into guided missile support frame 2.
The schematical embodiment of the utility model is the foregoing is only, is not limited to model of the present utility model
Enclose, any those skilled in the art on the premise of the utility model design and principle is not departed from the equivalent variations made and
Modification, the scope of the utility model protection all should be belonged to.
Claims (4)
1. a kind of missile transport frame of rotatable lifting, including base and guided missile support frame, the guided missile support frame fixed setting
In on base, it is characterised in that：It is flexibly connected between the guided missile support frame and base by support shaft, guided missile support frame can be around
Support shaft rotates；The guided missile support frame is internally provided with support frame elevating mechanism, support frame as described above elevating mechanism include leading screw,
It is equipped with the internal thread sliding block on leading screw, middle strut, motor and electric operating case, the motor fixed setting
In guided missile support frame one end, leading screw one end is coaxially disposed in driving motor output shaft, and the leading screw other end is arranged at by bearing
On guided missile support frame, the top of middle strut is be hinged to be arranged at guided missile support frame top, and the bottom of middle strut is be hinged to be arranged at
On internal thread sliding block, electric operating case is fixedly installed on guided missile support frame one end, the control motor work of electric operating case.
2. the missile transport frame of rotatable lifting according to claim 1, it is characterised in that：The guided missile support frame is set
The opposite end of motor one end is provided with hand-operated lifting handle, and hand-operated lifting handle can drive leading screw to rotate by driving member,
It is final to drive guided missile support frame to complete lifting action.
3. the missile transport frame of rotatable lifting according to claim 1, it is characterised in that：Described guided missile support frame one end
Be hinged to be provided with bullet fixed mechanism, bullet fixed mechanism can be spun upside down around jointed shaft.
4. the missile transport frame of the rotatable lifting according to claim 1-3 any one claims, it is characterised in that：
Guided missile support frame sets the opposite end of bullet fixed mechanism one end to be fixedly installed draw bar, and the draw bar is scalable to be inserted into
The end of guided missile support frame.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720251458.3U CN206634468U (en) | 2017-03-15 | 2017-03-15 | A kind of missile transport frame of rotatable lifting |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720251458.3U CN206634468U (en) | 2017-03-15 | 2017-03-15 | A kind of missile transport frame of rotatable lifting |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206634468U true CN206634468U (en) | 2017-11-14 |
Family
ID=60249241
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720251458.3U Expired - Fee Related CN206634468U (en) | 2017-03-15 | 2017-03-15 | A kind of missile transport frame of rotatable lifting |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206634468U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108423280A (en) * | 2018-03-27 | 2018-08-21 | 朱新福 | A kind of environmental protection fixed conveyor |
| CN110027799A (en) * | 2019-04-01 | 2019-07-19 | 黑龙江兰德超声科技股份有限公司 | It is a kind of to couple the pipeline transportation fixed device of adjusting for increasing oil suitable for oil well |
-
2017
- 2017-03-15 CN CN201720251458.3U patent/CN206634468U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108423280A (en) * | 2018-03-27 | 2018-08-21 | 朱新福 | A kind of environmental protection fixed conveyor |
| CN108423280B (en) * | 2018-03-27 | 2019-11-19 | 黄涌炜 | A kind of environmental protection fixed conveyor |
| CN110027799A (en) * | 2019-04-01 | 2019-07-19 | 黑龙江兰德超声科技股份有限公司 | It is a kind of to couple the pipeline transportation fixed device of adjusting for increasing oil suitable for oil well |
| CN110027799B (en) * | 2019-04-01 | 2020-06-19 | 黑龙江兰德超声科技股份有限公司 | Adjusting and fixing device for pipeline transportation suitable for oil well coupling oil increasing |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20171114 Termination date: 20200315 |