CN206450141U - A kind of fixing device of imitating shell missile wing - Google Patents
A kind of fixing device of imitating shell missile wing Download PDFInfo
- Publication number
- CN206450141U CN206450141U CN201720051668.8U CN201720051668U CN206450141U CN 206450141 U CN206450141 U CN 206450141U CN 201720051668 U CN201720051668 U CN 201720051668U CN 206450141 U CN206450141 U CN 206450141U
- Authority
- CN
- China
- Prior art keywords
- grab
- cross bar
- pad
- hole
- fixing device
- 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.)
- Expired - Fee Related
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Abstract
The utility model discloses a kind of fixing device of imitating shell missile wing, motion grab is locked whippletree by spring effect, so as to reach the effect of two parts above and below fixed, simple to operate, locking effect is notable；This novel fixing device is served only for training and mounted, it is strict not as good as live shell to intensity requirement, therefore aluminum alloy materials are used, and be not required to adjust the direction of the launch, i.e., it is internal without cable machinery, it is simple in construction, processing cost is low, and reliability is higher, and training operation is time saving and energy saving, there is very much training practicality, training goal can be reached well.
Description
Technical field
The utility model is related to imitating shell technical field, more particularly to a kind of fixing device of imitating shell missile wing.
Background technology
Because the on-hook of the rudder wing is flown in live shell, and it is related to the effect of the regulation direction of the launch, so strong to fixing device
Degree and internal mechanism requirement are strict.Fixing device employs titanium alloy material in live shell, and internal mechanism is related to cable and accurate dress
Put, design is fine, production and processing difficulty is big, and cost is high, and needs specific purpose tool to be operated, be unfavorable for carry training.
Utility model content
In view of this, the utility model provides a kind of fixing device of imitating shell missile wing, simple to operate, and locking effect shows
Write.
A kind of fixing device of imitating shell missile wing, including grab motion and cross bar fixed mechanism；The grab motion
Mechanism includes fixed seat (3), pad (1), spring (2), grab (4) and sprue (7)；Fixed seat (3) upper end is connected to
On the missile wing of imitating shell, lower end is docked with cross bar fixed mechanism；The cross bar fixed mechanism includes fixes sleeve (8) and cross bar
(9), the fixes sleeve (8) is arranged in the mounting hole of imitating shell body setting, and cross bar (9) is diametrically mounted to fixes sleeve
(8) in；
The fixed seat (3) is provided with through hole, and the pad (1) is arranged in the through hole, and the through hole bottom is provided with band
The sprue (7) in hole, the upper end of pad (1) is circumferentially provided with projection, and its raised upper end is stuck on the step of through hole, raised lower end
Spring (2) is set, and the lower end of pad (1) is passed from the hole of sprue (7)；Under nature, the spring (2) is compression shape
State；One end that pad (1) stretches out fixed seat (3) is flexibly connected by pad steady pin (6) with one end of the grab (4)；Card
The other end of hook (4) is folded upward at, and is connected at the flex point of the bending by grab steady pin (5) with the fixed seat (3)；Institute
State fixed seat (3) lower end and breach is set, be connected on the cross bar (9), the crooked place and cross bar (9) of the grab (4) are right
Standard, after pad (1) is pushed and is discharged, the cross bar (9) is blocked in the bending of grab (4) from below.
The fixed transposition uses aluminum alloy materials.
The utility model has the advantages that：
Fixing device of the present utility model, motion grab is locked whippletree by spring effect, so as to reach on fixed
The effect of lower two parts, simple to operate, locking effect is notable.
This novel fixing device is served only for training and mounted, strict not as good as live shell to intensity requirement, therefore uses aluminum alloy materials,
And be not required to adjust the direction of the launch, i.e., internal without cable machinery, simple in construction, processing cost is low, and reliability is higher, training operation
It is time saving and energy saving, there is very much training practicality, training goal can be reached well.
Brief description of the drawings
Fig. 1 (a) is the sectional view of fixing device of the present utility model.
Fig. 1 (b) is the side view of fixing device of the present utility model.
Fig. 2 is cross bar fixed mechanism installation diagram of the present utility model.
Fig. 3 is the schematic cross-sectional view of fixed seat of the present utility model.
Fig. 4 pad schematic diagrames of the present utility model.
Fig. 5 is hook structure schematic diagram of the present utility model.
Fig. 6 (a) is the schematic diagram under fixing device nature of the present utility model, and Fig. 6 (b) is of the present utility model solid
Determine the schematic diagram under device pressed status.
Wherein, 1- pads；2- springs；3- fixed seats；4- grabs；5- grab steady pins；6- pad steady pins；7- sprues；
8- fixes sleeves；9- cross bars.
Embodiment
With reference to the accompanying drawings and examples, the utility model is described in detail.
A kind of fixing device of imitating shell missile wing, including grab motion and cross bar fixed mechanism；The grab motion
Mechanism includes fixed seat 3, pad 1, spring 2, grab 4 and sprue 7；The upper end of fixed seat 3 is connected to the missile wing of imitating shell
On, lower end is docked with cross bar fixed mechanism；The cross bar fixed mechanism includes fixes sleeve 8 and cross bar 9, the fixes sleeve 8
In the mounting hole for being arranged on the setting of imitating shell body, cross bar 9 is diametrically mounted in fixes sleeve 8；
The fixed seat 3 is provided with through hole, and the pad 1 is arranged in the through hole, and the through hole bottom is provided with holes
Sprue 7, the upper end of pad 1 is circumferentially provided with projection, and its raised upper end is stuck on the step of through hole, and raised lower end sets spring
2, the lower end of pad 1 is passed from the hole of sprue 7；Under nature, the spring 2 is compressive state；Pad 1 stretches out fixed seat
3 one end is flexibly connected by pad steady pin 6 with one end of the grab 4；The other end of grab 4 is folded upward at, described curved
It is connected at the flex point of folding by grab steady pin 5 with the fixed seat 3；The lower end of fixed seat 3 sets breach, is connected to described
On cross bar 9, the crooked place of the grab 4 is aligned with cross bar 9, after pad 1 is pushed and is discharged, and the bending of grab 4 is from below
Block the cross bar 9.
The key of this mechanism be spring 2 install when be in compressive state, so be shown in Fig. 1 in the raw, when
When being in downward pressure to pad 1, spring 2 continues to shrink, while pad 1 drives grab 4 inwardly to rotate by pad steady pin 6
(see Fig. 5), it is right when grab 4 is rotated to whippletree 9 (whippletree 9 is fixed on simulation bomb body tail position) smoothly turnover groove position
The release pressure of pad 1, the resilience of spring 2, lead agency back to nature state (see Fig. 6 (a)), now grab 4 and whippletree 9 are in lock
Tight state.Similarly, when needing grab 4 to be unlocked with whippletree 9, downward pressure (see Fig. 6 (b)) also is in pad 1, when grab 4 revolves
Go to whippletree 9 smoothly turnover groove position when, extract out motion clip hook device, and to pad 1 discharge pressure.
In summary, preferred embodiment of the present utility model is these are only, is not intended to limit of the present utility model
Protection domain.It is all it is of the present utility model spirit and principle within, any modification, equivalent substitution and improvements made etc. all should be wrapped
It is contained within protection domain of the present utility model.
Claims (2)
1. a kind of fixing device of imitating shell missile wing, it is characterised in that including grab motion and cross bar fixed mechanism；It is described
Grab motion includes fixed seat (3), pad (1), spring (2), grab (4) and sprue (7)；On the fixed seat (3)
End is connected on the missile wing of imitating shell, and lower end is docked with cross bar fixed mechanism；The cross bar fixed mechanism includes fixes sleeve (8)
With cross bar (9), the fixes sleeve (8) is arranged in the mounting hole of imitating shell body setting, and cross bar (9) is diametrically mounted to solid
Determine in sleeve (8)；
The fixed seat (3) is provided with through hole, and the pad (1) is arranged in the through hole, and the through hole bottom is provided with holes
Sprue (7), the upper end of pad (1) is circumferentially provided with projection, and its raised upper end is stuck on the step of through hole, and raised lower end is set
Spring (2), the lower end of pad (1) is passed from the hole of sprue (7)；Under nature, the spring (2) is compressive state；Pressure
One end that pin (1) stretches out fixed seat (3) is flexibly connected by pad steady pin (6) with one end of the grab (4)；Grab (4)
The other end be folded upward at, be connected at the flex point of the bending by grab steady pin (5) with the fixed seat (3)；It is described solid
Reservation (3) lower end sets breach, is connected on the cross bar (9), the crooked place of the grab (4) is aligned with cross bar (9),
After pad (1) is pushed and discharged, the cross bar (9) is blocked in the bending of grab (4) from below.
2. a kind of fixing device of imitating shell missile wing as claimed in claim 1, it is characterised in that the fixed transposition uses aluminium
Alloy material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720051668.8U CN206450141U (en) | 2017-01-17 | 2017-01-17 | A kind of fixing device of imitating shell missile wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720051668.8U CN206450141U (en) | 2017-01-17 | 2017-01-17 | A kind of fixing device of imitating shell missile wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206450141U true CN206450141U (en) | 2017-08-29 |
Family
ID=59671613
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720051668.8U Expired - Fee Related CN206450141U (en) | 2017-01-17 | 2017-01-17 | A kind of fixing device of imitating shell missile wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206450141U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108760998A (en) * | 2018-08-27 | 2018-11-06 | 普雷沃流体控制科技（芜湖）有限公司 | A kind of air quality detector |
| CN108871097A (en) * | 2018-08-02 | 2018-11-23 | 西安星恒通通信技术有限公司 | The mortar simulated training ammunition of ejection system built in a kind of band |
| CN115060124A (en) * | 2022-07-08 | 2022-09-16 | 江西洪都航空工业集团有限责任公司 | Portable missile wing locking device of commonality |
-
2017
- 2017-01-17 CN CN201720051668.8U patent/CN206450141U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108871097A (en) * | 2018-08-02 | 2018-11-23 | 西安星恒通通信技术有限公司 | The mortar simulated training ammunition of ejection system built in a kind of band |
| CN108871097B (en) * | 2018-08-02 | 2024-02-13 | 西安星恒通智能装备有限公司 | Mortar training simulation bomb with built-in ejection system |
| CN108760998A (en) * | 2018-08-27 | 2018-11-06 | 普雷沃流体控制科技（芜湖）有限公司 | A kind of air quality detector |
| CN115060124A (en) * | 2022-07-08 | 2022-09-16 | 江西洪都航空工业集团有限责任公司 | Portable missile wing locking device of commonality |
| CN115060124B (en) * | 2022-07-08 | 2023-11-03 | 江西洪都航空工业集团有限责任公司 | Portable missile wing locking device of commonality |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20180129 Address after: 264001 two road, Yantai, Shandong, No. 188, No. two Co-patentee after: Zhengzhou Zheng Aircraft Electric Technology Co., Ltd. Patentee after: Naval Aeronautical Engineering Institute PLA Address before: 264001 Yantai City, Zhifu Province, No. two road, No. 188, Department of research, Patentee before: Naval Aeronautical Engineering Institute PLA |
|
| 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: 20170829 Termination date: 20210117 |