CN208952793U - Launching tube Quick Connect Kit - Google Patents
Launching tube Quick Connect Kit Download PDFInfo
- Publication number
- CN208952793U CN208952793U CN201821355413.1U CN201821355413U CN208952793U CN 208952793 U CN208952793 U CN 208952793U CN 201821355413 U CN201821355413 U CN 201821355413U CN 208952793 U CN208952793 U CN 208952793U
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- CN
- China
- Prior art keywords
- launching tube
- lock tongue
- supporting leg
- guide
- locking 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.)
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Abstract
The utility model discloses a kind of launching tube Quick Connect Kit, which includes supporting leg, locking device, guide-rail plate and unlocking mechanism；The upper end of the supporting leg is fixedly connected with launching tube, and the dovetail groove on the lower end and guide-rail plate of supporting leg is slidably matched；Locking device and tripper are fixedly mounted on the lower section of guide-rail plate, and the tripper is connected with locking device simultaneously；The supporting leg generates elastic displacement by locking device after guide rail sliding in place and realizes rigid locking；When launching tube needs to unlock, make locking device generation linkage that elastic force be overcome to realize elasticity unlock by rotating tripper.The utility model can be realized the accurate docking of launching tube and vehicle transmitting platform or the portable hair control device of individual soldier, while also meet fast operating demand.
Description
Technical field
The utility model relates to aerial vehicle launcher technical fields, and in particular to send out used in the operation of wound packages aircraft
Shooting cylinder and flat pad fast joint structure.
Background technique
The attachment device of conventional launching tube is two-level configuration, and fast-assembling guide rail is connected by anchor ear with launching tube, is changed the outfit spare
It needs first to remove the launching tube emitted together with anchor ear when bullet, then unclamps anchor ear, remove original launching tube, then change the outfit spare
Bullet (contains new launching tube), is connected finally by guide rail with launcher.The operation of the mechanisms such as locking in launching tube side, space by
Limit, it is inconvenient, and be double-stage operation, it cannot really realize quick connection.Anchor ear is two semi-circular structures, and unstable, is held
Launching tube deformation is easily led to, aircraft is influenced and goes out cylinder.
Utility model content
In view of this, the present invention provides a kind of launching tube Quick Connect Kit, launching tube and vehicle-mounted can be realized
The accurate docking of flat pad or the portable hair control device of individual soldier, while also meeting fast operating demand.
A kind of launching tube Quick Connect Kit, the attachment device include supporting leg, retaining mechanism, guide-rail plate and unlocking mechanism；
The upper end of the supporting leg is fixedly connected with launching tube, and the dovetail groove on the lower end and guide-rail plate of supporting leg is slidably matched；The locking
Mechanism and unlocking mechanism are fixedly mounted on the lower section of guide-rail plate, and the unlocking mechanism is connected with retaining mechanism simultaneously；The branch
Leg generates elastic displacement by retaining mechanism after guide rail sliding in place and realizes rigid locking；When launching tube needs to unlock, by turning
Dynamic unlocking mechanism makes retaining mechanism generation linkage that elastic force be overcome to realize elasticity unlock.
Further, the retaining mechanism includes lock box, lock tongue and locking spring；There is a limiting stand on the lock tongue
Rank, lock box are fixedly connected on the lower section of guide rail, and locking spring is sleeved on lock tongue and is packed into lock box, and the both ends of locking spring are distinguished
It is contacted with the inner bottom surface of limited step and lock box, the head of locking spring lock tongue in free state is located at the upper of dovetail groove plane
Side.
Further, the unlocking mechanism includes side plate, driving lever, lock tongue shift fork and lock tongue pin；The side plate is fixedly connected
On the bottom surface of guide-rail plate, the both ends of driving lever and side plate are rotatably assorted for hole axle, and the side plate of the every one end of driving lever is set as two pieces, and two
Driving lever between block side plate is processed into plat shaft, and one end of lock tongue shift fork is sleeved on the plat shaft of driving lever, lock tongue shift fork it is another
One end is connected by the tail portion of lock tongue pin and lock tongue.
Further, the head of the lock tongue is inclined-plane, and the insertion direction of motion to supporting leg is met on inclined-plane.
Further, by supporting leg compressed spring after the bottom of the dovetail groove is installed in place equipped with spring jackscrew, launching tube
Jackscrew, spring jackscrew provide augmented thrust when dismantling for launching tube.
The utility model has the advantages that
1, the utility model is open by loudspeaker and the guide-localization of dovetail groove inserts launching tube and flat pad realization
Bit manipulation simplicity is set, personnel can fully achieve blindmate by simple exercise, fast implement war fighting requirement.
2, the utility model is convenient for disassembly and assembly, only launching tube supporting leg need to be directed at dovetail groove guide rail when launching tube is installed and pushed away
Enter, in place after, retaining mechanism bounces automatically blocks launching tube supporting leg rear portion, realize quick locking；When disassembly, fast-assembling need to be only rotated
Driving lever is locked, backward pull launching tube, equipment can be carried and quickly withdraw battlefield by meeting Quick universal aircraft or individual soldier
It is required that.
3, the utility model can be used as a kind of universal architecture, can be not only used for vehicle-mounted, carrier-borne or launched by airplane platform, is also suitable
Device is controlled in the portable hair of individual soldier, interchangeability is good, does not need to be equipped with different launching tubes for different flat pads.
4, the utility model assembly and disassembly operations direction of motion is consistent with vehicle launch direction, general unrestricted, so to it
His space hold is small, compact-sized, convenient for layout.
5, the utility model retaining mechanism is locked using inclined-plane, and preloading spring jackscrew can not only provide auxiliary when disassembly
Thrust, can also effective compensation launching tube supporting leg mismachining tolerance, make device have better versatility.
Detailed description of the invention
Fig. 1 is the shaft side figure of the utility model
Fig. 2 is the main view of the utility model
Fig. 3 is locking mechanism structure schematic diagram
Fig. 4 is the left view of the utility model
Wherein: 1- launching tube, 2- supporting leg, 3- retaining mechanism, 4- guide-rail plate, 5- spring jackscrew, 6- lock tongue, 7- lock bullet
Spring, 8- driving lever, 9- lock tongue shift fork, 10- lock box, 11- lock tongue pin, 12- side plate.
Specific embodiment
With reference to the accompanying drawings and examples, the utility model is described in detail.
As shown in figure 1 and 2, the utility model provides a kind of launching tube Quick Connect Kit, which includes
Supporting leg 2, retaining mechanism 3, guide-rail plate 4 and unlocking mechanism；
The upper end of supporting leg 2 is fixedly connected with launching tube 1, and lower end and the dovetail groove on guide-rail plate 4 of supporting leg 2 are slidably matched；
Retaining mechanism 3 and unlocking mechanism are fixedly mounted on the lower section of guide-rail plate 4.
As shown in Fig. 3, retaining mechanism 3 includes lock box 10, lock tongue 6 and locking spring 7；There is a limiting stand on lock tongue
The head of rank, lock tongue 6 is inclined-plane, and the insertion direction of motion to supporting leg 2 is met on inclined-plane.
Lock box 10 is fixedly connected on the lower section of guide-rail plate 4, and locking spring 7 is sleeved on lock tongue 6 and is packed into lock box, locking
The both ends of spring 7 are contacted with the inner bottom surface of limited step and lock box 10 respectively, the head of the lock tongue 6 in free state of locking spring 7
Portion is located at the top of dovetail groove plane, and the tail portion of lock tongue 6 passes through the bottom of lock box 10 and is located at the outside of lock box 10.
Unlocking mechanism includes side plate 12, driving lever 8, lock tongue shift fork 9 and lock tongue pin 11；Side plate 12 is fixedly connected on guide-rail plate 4
Bottom surface on, both ends and the side plate 12 of driving lever 8 are rotatably assorted for hole axle, and the side plate 12 of the every one end of driving lever 8 is set as two pieces, two pieces
Driving lever 8 between side plate 12 is processed into plat shaft, and one end of lock tongue shift fork 9 is sleeved on the plat shaft of driving lever 8, lock tongue shift fork 9
The other end be flexibly connected with the tail portion of lock tongue 6 by lock tongue pin 11.
The bottom of dovetail groove be equipped with spring jackscrew 5, launching tube 1 be installed in place after by front end 2 compressed spring jackscrew of supporting leg
5, spring jackscrew provides augmented thrust when dismantling for launching tube 1.
In filling, the supporting leg 2 on launching tube 1 is directed at dovetail groove horn mouth and is pushed forward launching tube 1 backward, and supporting leg can be depressed
Lock tongue 6 moves forward, supporting leg 2 in place after, front is blocked by the closed end of guide-rail plate 4, lock tongue 6 locking spring 7 act on
It bounces automatically down, blocks rear support leg, entire launching tube is firmly locked in dovetail groove.
When disassembly, rotating lever 8, driving lever 8 drives lock tongue shift fork 9 to depress lock tongue 6, and launching tube 1 realizes unlock, operator
Pull launching tube 1 backward again, can quickly withdraw from launching tube 1.
As shown in Fig. 4, also there is a rectangular convex block, by the convex block convenient for operation and rotating lever on driving lever 8
8。
In conclusion the above is only the preferred embodiments of the present utility model only, it is not intended to limit the utility model
Protection scope.Within the spirit and principle of the utility model, any modification, equivalent replacement, improvement and so on should all wrap
Containing being within the protection scope of the utility model.
Claims (5)
1. a kind of launching tube Quick Connect Kit, which is characterized in that the attachment device includes supporting leg, locking device, guide-rail plate and
Unlocking mechanism；The upper end of the supporting leg is fixedly connected with launching tube, and the dovetail groove on the lower end and guide rail of supporting leg is slidably matched；Institute
The lower section that locking device and tripper are fixedly mounted on guide-rail plate is stated, the tripper is connected with locking device simultaneously；
The supporting leg generates elastic displacement by locking device after guide rail sliding in place and realizes rigid locking；When launching tube needs to unlock,
Make locking device generation linkage that elastic force be overcome to realize elasticity unlock by rotating tripper.
2. launching tube Quick Connect Kit according to claim 1, which is characterized in that the locking device include lock box,
Lock tongue and locking spring；There is a limited step, lock box is fixedly connected on the lower section of guide-rail plate, locking spring on the lock tongue
It is sleeved on lock tongue and is packed into lock box, the both ends of locking spring are contacted with the inner bottom surface of limited step and lock box respectively, lock bullet
The head of spring lock tongue in free state is located at the top of dovetail groove plane.
3. launching tube Quick Connect Kit according to claim 2, which is characterized in that the unlocking mechanism include side plate,
Driving lever, lock tongue shift fork and lock tongue pin；The side plate is fixedly connected on the bottom surface of guide-rail plate, and the both ends of driving lever and side plate are hole axle
It is rotatably assorted, the side plate of the every one end of driving lever is set as two pieces, and the driving lever between two blocks of side plates is processed into plat shaft, lock tongue shift fork
One end is sleeved on the plat shaft of driving lever, and the other end of lock tongue shift fork is connected by the tail portion of lock tongue pin and lock tongue.
4. launching tube Quick Connect Kit according to claim 2, which is characterized in that the head of the lock tongue is inclined-plane,
Meet the insertion direction of motion to supporting leg in inclined-plane.
5. launching tube Quick Connect Kit according to claim 1, which is characterized in that the bottom of the dovetail groove is equipped with bullet
Spring jackscrew, launching tube be installed in place after by supporting leg compressed spring jackscrew, spring jackscrew is provides augmented thrust when launching tube disassembly.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821355413.1U CN208952793U (en) | 2018-08-16 | 2018-08-16 | Launching tube Quick Connect Kit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821355413.1U CN208952793U (en) | 2018-08-16 | 2018-08-16 | Launching tube Quick Connect Kit |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208952793U true CN208952793U (en) | 2019-06-07 |
Family
ID=66735397
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821355413.1U Active CN208952793U (en) | 2018-08-16 | 2018-08-16 | Launching tube Quick Connect Kit |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208952793U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113044233A (en) * | 2021-04-30 | 2021-06-29 | 河南华讯方舟航空科技有限公司 | Unmanned aerial vehicle emitter |
-
2018
- 2018-08-16 CN CN201821355413.1U patent/CN208952793U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113044233A (en) * | 2021-04-30 | 2021-06-29 | 河南华讯方舟航空科技有限公司 | Unmanned aerial vehicle emitter |
| CN113044233B (en) * | 2021-04-30 | 2022-12-09 | 河南创仕航空科技有限公司 | Unmanned aerial vehicle emitter |
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| GR01 | Patent grant |