CN207139314U - Guided missile rudder piece hole-drilling system - Google Patents
Guided missile rudder piece hole-drilling system Download PDFInfo
- Publication number
- CN207139314U CN207139314U CN201720838169.3U CN201720838169U CN207139314U CN 207139314 U CN207139314 U CN 207139314U CN 201720838169 U CN201720838169 U CN 201720838169U CN 207139314 U CN207139314 U CN 207139314U
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- China
- Prior art keywords
- turntable
- plate
- rudder piece
- hole
- groove
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Abstract
The utility model discloses guided missile rudder piece hole-drilling system, including feeding device, clamping device and drilling equipment, feeding device and drilling equipment are separately positioned on the left and right sides of clamping device；Described feeding device includes turntable and manipulator, and turntable is arranged on the top of fixed platform, and turntable is provided with multigroup position-limit mechanism perpendicular to turntable, through hole A is provided with the turntable immediately below position-limit mechanism, cylinder A is provided with below through hole A；Described clamping device includes plate and cylinder B, in plate, push pedal is placed in groove, push pedal is connected with cylinder B；The drill bit of described drilling equipment is horizontally set on the horizontal direction of clamping device further groove；Described feeding device, clamping device and drilling equipment is connected with control panel, and control panel is arranged on the front side of clamping element device.The beneficial effects of the utility model are：Automaticity is higher, production efficiency is high, reduces labor intensity.
Description
Technical field
It the utility model is related to the technical field of missile weapon system centered rudder piece processing, particularly guided missile rudder piece drilling system
System.
Background technology
At present, as raising of the war to weapon performance requirement, precision strike are increasingly favored by countries in the world, its
It is middle than it is more prominent be guided cartridge（That is guided missile）, guided missile is because lethality is strong, collateral damage is small, reflecting time is short, effect of fighting
Can be high, strike is accurate the features such as, controlling the flight attitude of guided missile was as the preferred ammunition that precision strike is realized in modern war
Performed by operating station, and rudder piece is one of vital part of operating station, by controlling control vane piece to rotate so as to produce
Raw enough aerodynamic moments, ensure that guided missile awing meets the flight attitude of target spot ballistic design.New Generation Missile typically makes
With inertial navigation, GPS navigation or both dual-purpose, in the starting stage of transmitting, track operation of the guided missile along initial transmissions, by bullet
After road peak, GPS obtains navigation signal, and operating station has flown remaining distance by control flaps piece, and according to
Need to be adjusted direction, so as to reach the purpose of precision strike.
Rudder piece, it is necessary to after being clamped to its frock, then is drilled when being drilled, and the clamping of transmission is that rudder piece is artificial
Lift and be placed in clamping tool, then fixed drilling, due to rudder piece, weight itself is big, causes the intensity of hand labor big, and
Clamping spends time length, causes the operating efficiency of the drilling of rudder piece low.
Utility model content
The shortcomings that the purpose of this utility model is to overcome prior art, there is provided automaticity is higher, production efficiency is high,
Reduce the guided missile rudder piece hole-drilling system of labor intensity.
The purpose of this utility model is achieved through the following technical solutions：Guided missile rudder piece hole-drilling system, including feeding device,
Clamping device and drilling equipment, feeding device and drilling equipment are separately positioned on the left and right sides of clamping device；
Described feeding device includes turntable and manipulator, and turntable is arranged on the top of fixed platform, and turntable, which is provided with, to hang down
Directly in multigroup position-limit mechanism of turntable, position-limit mechanism includes more gag lever posts, rudder piece is placed between gag lever post, positioned at position restrainer
Through hole A is provided with turntable immediately below structure, jacking block is provided with through hole A, jacking block is connected by push rod with cylinder A, gag lever post
Top is additionally provided with inductor, and manipulator is set close to turntable, and clamping jaw is provided with manipulator；
Described clamping device includes plate and cylinder B, and the upper surface of plate forward part is provided with boss, plate boss
Upper surface is provided with groove, is placed with rudder piece in groove, is provided with cylinder B on the upper surface of part after plate, cylinder B passes through push rod
Penetrate groove with push pedal to be connected, push pedal is located in groove and push pedal is located at the rear side of rudder piece, close to groove position on plate boss
Pressing plate has been installed, rotating shaft is fixed with rear side of plate, rotating shaft is fixed on lathe by scroll chuck；
The drill bit of described drilling equipment is horizontally set on the horizontal direction of clamping device further groove；
Described feeding device, clamping device and drilling equipment is connected with control panel, and control panel is arranged on clamping
The front side of part device；
Described pressing plate is fixed by screws on plate；
Described groove is adapted with rudder piece, and gear is provided between the plate boss upper cylinder B and groove close to cylinder B
Wall, retaining wall are provided with through hole B, and push rod is connected after passing through through hole B with push pedal.
The quantity of described position-limit mechanism is four groups, and the quantity of gag lever post is four in each group of position-limit mechanism, gag lever post
Lower end be fixed on sliding block, the elongated slot being adapted with sliding block is provided with turntable, sliding block is placed in elongated slot and sliding block passes through spiral shell
Nail is fixed on turntable, and elongated slot is radially arranged along through hole A's.
Described control panel is provided with the button corresponding with feeding device, clamping device and drilling equipment.
The utility model has advantages below：Automaticity is higher, production efficiency is high, reduces labor intensity.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model；
Fig. 2 is turntable and the top view of position-limit mechanism entirety；
Fig. 3 is the structural representation of position-limit mechanism；
Fig. 4 is the left view of clamp system；
Fig. 5 is the front view of clamp system；
In figure, 1-turntable, 2-manipulator, 3-fixed platform, 4-position-limit mechanism, 5-gag lever post, 6-rudder piece, 7-
Jacking block, 8-cylinder A, 9-inductor, 10-clamping jaw, 11-plate, 12-cylinder B, 13-groove, 14-push pedal, 15-pressure
Plate, 16-rotating shaft, 17-control panel, 18-sliding block, 19-elongated slot.
Embodiment
The utility model is further described below in conjunction with the accompanying drawings, the scope of protection of the utility model be not limited to
It is lower described：
As shown in Fig. 1~Fig. 5, guided missile rudder piece hole-drilling system, including feeding device, clamping device and drilling equipment, feeding
Device is located at the left side of clamping device, and drilling equipment is located at the right side of clamping device；
Described feeding device includes turntable 1 and manipulator 2, and manipulator 2 is arranged on the left side of clamping device, and turntable 1 is set
Put and four groups of position-limit mechanisms 4 perpendicular to turntable 1 are provided with the left side of manipulator 2, turntable 1, position-limit mechanism 4 includes four limits
Position bar 5, is placed with rudder piece 6 in gag lever post 5, and gag lever post 5 plays a part of fixed rudder piece 6, below the region that gag lever post 5 surrounds
Through hole A is provided with turntable 1, is provided with jacking block 7 below through hole A, jacking block 7 is connected by push rod with cylinder A8, passes through cylinder A8
Drive push pedal 14 to move up, so as to drive rudder piece 6 to move up, the upper end of gag lever post 5 is provided with inductor 9, inductor 9 with
Cylinder A8 is arranged on the front side of clamping device with control panel 17, control panel 17, when inductor 9 measures the upper of gag lever post 5
When portion does not have rudder piece 6, cylinder A8 starts, and the rudder piece 6 of the bottom of gag lever post 5 is up pushed up, and plays the purpose of supplement rudder piece 6, machinery
Hand 2 is by setting clamping jaw 10 to pick up rudder piece 6；
Described clamping device includes plate 11 and cylinder B12, and boss, plate are provided with the upper surface of the forward part of plate 11
The upper surface of the boss of part 11 is provided with groove 13, and rudder piece 6 is placed with groove 13, and groove 13 is adapted with rudder piece 6, plate rear portion
Cylinder 12 is provided with the upper surface divided, gear is provided between the boss upper cylinder B12 of plate 11 and groove 13 close to cylinder B12
Wall, retaining wall are provided with through hole B, and push rod is connected after passing through through hole B with push pedal 14, and push pedal 14 is located in groove 13 and push pedal 14 is located at
The rear side of rudder piece 6, the position of groove 13 is provided with pressing plate 15 on the boss of plate 11, pressing plate 15 pushes down rudder piece 6, then passes through
Pressing plate 15 is fixed on plate 11 by screw, it is achieved thereby that the fixation to rudder piece 6, the rear side of plate 11 is fixed with rotating shaft 16,
Rotating shaft 16 is fixed on lathe by scroll chuck, and lathe drives plate 11 to rotate by rotating shaft 16, and plate 11 drives 6 turns of rudder piece
It is dynamic；
The drill bit of described drilling equipment is horizontally set on the horizontal direction of clamping device further groove 13, when rudder piece turns over 90
When spending, rudder piece 6 can be implemented to drill；
Described feeding device, clamping device and drilling equipment is connected with control panel 17, and control panel 17 is arranged on
The front side of clamping element device, control panel 17 are provided with the button corresponding with feeding device, clamping device and drilling equipment, lead to
Cross clamping and drilling that control panel realizes guided missile rudder piece.
During work, the top of position-limit mechanism 4 is moved to by control panel control machinery hand 2, by clamping jaw 10 by rudder piece 6
Pick up and put into groove 13, it is artificial to promote rudder piece 6 to be in contact with push pedal 14 after clamping jaw 10 unclamps, then pressed rudder piece 6 with pressing plate 15
Firmly, pressing plate 15 is fixed on plate 11 with screw, by lathe drive plate 11 rotate so that the bore position of rudder piece 6 with
Drilling equipment is relative, then rudder piece 6 is drilled；After rudder piece 6 drills, unscrew screw, push pedal 14 is driven by cylinder B
By a certain position in rudder piece 6 to groove 13, the position is easy to manipulator 2 to add the rudder piece 6 after drilling, and manipulator 2 will add
The rudder piece risen is placed in finished product area；Manipulator 2 turns again to the top of position-limit mechanism 4, and cylinder A8 is by jacking block 7 by other rudders
Piece 6 is jacked up, and manipulator 2 is gripped by claw 10 again, after one group of centered rudder piece 6 of position-limit mechanism 4 is by gripping, is rotated and is turned
Platform 1 so that next group of position-limit mechanism 4 is in upper one group of position-limit mechanism 4 position, and upper one group by the position restrainer after gripping
Structure 4 is then added rudder piece 6.
In the present embodiment, the lower end of described gag lever post 8 is fixed on sliding block 18, is provided with turntable 1 and is fitted with the phase of sliding block 18
The elongated slot 19 matched somebody with somebody, sliding block 18 is placed in elongated slot 19 and sliding block 18 is fixed by screws on turntable 1, and elongated slot 19 is along through hole A's
It is radially arranged, the movement of gag lever post 8 is realized by slip of the sliding block 18 in elongated slot 19, so as to realizes to different size rudder pieces 6
Clamping.
Described above is only preferred embodiment of the present utility model, it should be understood that the utility model is not limited to herein
Disclosed form, the exclusion to other embodiment is not to be taken as, and can be used for various other combinations, modification and environment, and
It can be modified in contemplated scope described herein by the technology or knowledge of above-mentioned teaching or association area.And this area
The change and change that personnel are carried out do not depart from spirit and scope of the present utility model, then all should be in right appended by the utility model
It is required that protection domain in.
Claims (3)
1. guided missile rudder piece hole-drilling system, it is characterised in that：Including feeding device, clamping device and drilling equipment, feeding device and
Drilling equipment is separately positioned on the left and right sides of clamping device；
Described feeding device includes turntable（1）And manipulator（2）, turntable（1）It is arranged on fixed platform（3）Top, turntable
（1）It is provided with perpendicular to turntable（1）Multigroup position-limit mechanism（4）, position-limit mechanism（4）Including more gag lever posts（5）, gag lever post
（5）Between be placed with rudder piece（6）, positioned at position-limit mechanism（4）The turntable of underface（1）On be provided with through hole A, be provided with through hole A
Jacking block（7）, jacking block（7）Pass through push rod and cylinder A（8）It is connected, gag lever post（5）Top be additionally provided with inductor（9）, manipulator
（2）Close to turntable（1）Set, manipulator（2）On clamping jaw is installed（10）；
Described clamping device includes plate（11）With cylinder B（12）, plate（11）The upper surface of forward part is provided with boss, plate
Part（11）The upper surface of boss is provided with groove（13）, groove（13）In be placed with rudder piece（6）, plate（11）The upper surface of part afterwards
On be provided with cylinder B（12）, cylinder B（12）Groove is penetrated by push rod（13）With push pedal（14）It is connected, push pedal（14）Positioned at recessed
Groove（13）Interior and push pedal（14）Positioned at rudder piece（6）Rear side, in plate（11）Close to groove on boss（13）Position is provided with pressing plate
（15）, plate（11）Rear side be fixed with rotating shaft（16）, rotating shaft（16）It is fixed on by scroll chuck on lathe；
The drill bit of described drilling equipment is horizontally set on clamping device further groove（13）Horizontal direction；
Described feeding device, clamping device and drilling equipment is and control panel（17）It is connected, control panel（17）It is arranged on
The front side of clamping element device；
Described pressing plate（15）It is fixed by screws in plate（11）On；
Described groove（13）With rudder piece（6）It is adapted, close to cylinder B（12）Plate（11）Boss upper cylinder B（12）With
Groove（13）Between be provided with retaining wall, retaining wall is provided with through hole B, push rod pass through after through hole B with push pedal（14）It is connected.
2. guided missile rudder piece hole-drilling system according to claim 1, it is characterised in that：Described position-limit mechanism（4）Quantity
For four groups, each group of position-limit mechanism（4）Middle gag lever post（5）Quantity be four, gag lever post（5）Lower end be fixed on sliding block（18）
On, turntable（1）On be provided with and sliding block（18）The elongated slot being adapted（19）, sliding block（18）It is placed on elongated slot（19）In and sliding block（18）
It is fixed by screws in turntable（1）On, elongated slot（19）Along being radially arranged for through hole A.
3. guided missile rudder piece hole-drilling system according to claim 1, it is characterised in that：Described control panel（17）It is provided with
The button corresponding with feeding device, clamping device and drilling equipment.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2016211409755 | 2016-10-20 | ||
| CN201621140975 | 2016-10-20 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207139314U true CN207139314U (en) | 2018-03-27 |
Family
ID=61675114
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720838169.3U Expired - Fee Related CN207139314U (en) | 2016-10-20 | 2017-07-12 | Guided missile rudder piece hole-drilling system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207139314U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108723152A (en) * | 2018-05-03 | 2018-11-02 | 傅飞 | A kind of wheel hub cover process equipment |
-
2017
- 2017-07-12 CN CN201720838169.3U patent/CN207139314U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108723152A (en) * | 2018-05-03 | 2018-11-02 | 傅飞 | A kind of wheel hub cover process equipment |
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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 |
Granted publication date: 20180327 Termination date: 20190712 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |