CN206084443U - General several millers of aircraft small -scale structure spare dress - Google Patents
General several millers of aircraft small -scale structure spare dress Download PDFInfo
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- CN206084443U CN206084443U CN201620821634.8U CN201620821634U CN206084443U CN 206084443 U CN206084443 U CN 206084443U CN 201620821634 U CN201620821634 U CN 201620821634U CN 206084443 U CN206084443 U CN 206084443U
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Abstract
The utility model discloses a general several millers of aircraft small -scale structure spare dress, including installing universal tool base (1) on machine tool table (6), install and be used for pressing from both sides tight quick pressure plate assembly (2) with part (5) on universal tool base (1), be provided with equidistance locating hole (10) on universal tool base (1), equidistance constant head tank (11) and be used for installing the T type groove (9) of quick pressure plate assembly (2), still include part locating pin (3), T type groove (9), equidistance locating hole (10), equidistance constant head tank (11) one -to -one setting and constitute a set of location compact structure, above -mentioned location compact structure's quantity is three groups. Through the structure of the utility model, the utility model is suitable for a not unidimensional spare part of processing to the save time cost, and improve lathe main shaft utilization ratio, and then improve production efficiency, reduce enterprise's processing cost, promote enterprise profit.
Description
Technical field
This utility model is related to mechanical frock field of fixtures, specifically, is a kind of general several millings of aircraft small-scale structure part
Frock.
Background technology
There are a large amount of small scale structures parts in aircraft structure part, such as little angle box, gusset plate, hinge etc. primarily serve connection
The effect of the large-scale main load-bearing part of aircraft, this kind of design of part type is more, and unit quantity is big.Such part processing characteristic is many product
Kind, need frequently to change the outfit, and the digital control processing time is shorter, so if process program disunity, or part changes the outfit time mistake
If length, machine tool chief axis utilization rate can be very low（General only 25% ~ 30%）, production efficiency is by considerable influence, these phenomenon meetings
Enterprise's processing cost is caused to increase, enterprise profit is difficult to be lifted.
Utility model content
The purpose of this utility model is to provide a kind of aircraft small-scale structure part general several milling tools, is added in a frock
The parts of work different size size, solve the problems, such as high processing costs.
This utility model is achieved through the following technical solutions：A kind of general several milling tools of aircraft small-scale structure part, including peace
It is mounted on platen and is adapted to the universal fixture base of the part of different size size, uses on universal fixture base
In the quick Anchor plate kit for clamping part.
Further, in order to more preferably realize this utility model, be provided with the universal fixture base equidistant location hole,
The equidistant locating slot being correspondingly arranged with equidistant location hole and the T-slot for installing quick Anchor plate kit, also including being plugged on
The part alignment pin positioned for part in equidistant location hole and equidistant locating slot.
Further, in order to more preferably realize this utility model, the T-slot, equidistant location hole, one a pair of equidistant locating slot
Should arrange and constitute one group of positioning compression structure；The quantity of the positioning compression structure is three groups, is in vertical direction etc. respectively
Away from the A group positioning compression structures, B group positioning compression structures, C group positioning compression structures that are arranged side by side；The T-slot includes length
The AT type grooves successively decreased successively, BT type grooves, CT type grooves；The equidistant location hole includes the equidistant location holes of A, the equidistant location holes of B, C etc.
Away from location hole；Equidistant locating slot includes that the equidistant locating slots of the A being placed equidistant in the horizontal direction, the equidistant locating slots of B, C are equidistantly positioned
Groove；The equidistant locating slot of the AT type grooves, the equidistant location holes of A, A is corresponded to arrange and constitutes A group positioning compression structures；The BT types
The equidistant locating slot of the equidistant location hole of groove, B, B is corresponded to arrange and constitutes B group positioning compression structures；The CT type grooves, C are equidistantly fixed
Position hole, the equidistant locating slots of C are corresponded to arrange and constitute C group positioning compression structures.
Further, in order to more preferably realize this utility model, in the T-slot, be slidably fitted with T-nut, also include with
T-nut is with the use of with the screw of the quick Anchor plate kit of compression.
Further, in order to more preferably realize this utility model, arrange between the nut of the screw and quick Anchor plate kit
There is the pad for increasing quick Anchor plate kit lifting surface area.
Further, in order to more preferably realize this utility model, chute on the platen, has equidistantly been arranged side by side,
On the platen, relevant position is connected with Universal pressing plate component；Slidably connect in chute for universal fixture base
The tool locating step pin of positioning；On universal fixture base, relevant position is provided with Universal pressing plate component collective effect to incite somebody to action
Universal fixture base is pressed on the frock pressing groove on platen.
This utility model compared with prior art, with advantages below and beneficial effect：
（1）Several milling tools in this utility model be applied to different size size parts machining, during use, be not required to because
Frock is frequently changed for the different of accessory size size, so as to save time cost, and machine tool chief axis utilization rate is improved, and then
Improve production efficiency, reduces enterprise's processing cost, enterprise profit.
（2）In this utility model, universal fixture base, quick Anchor plate kit and parts to be processed are positioned using pin,
It is easy to operate, accurate positioning；This utility model realizes the compression between each part by the way of screw in compression, simple operation,
And then improve practicality of the present utility model.
（3）In each group of positioning compression mechanism of the present utility model, the equidistant locating slot for part positioning has necessarily
Length, and quick Anchor plate kit can as needed, shift position, using aforesaid way, realizes in each group of positioning compression
The processing of the parts in mechanism to size within the specific limits；Above-mentioned positioning compression mechanism total quantity is three groups, and logical
It is distributed in equidistant arrangement with tooling base, and per group of equidistant locating slot and equidistant location hole in three groups of positioning compression mechanisms
The distance between differ, in equidistant arrangement, using said structure, be capable of achieving the positioning to different size part and process, and then
Improve practicality of the present utility model.
Description of the drawings
Fig. 1 is structural representation of the present utility model；
Fig. 2 is left view structural representation of the present utility model；
Fig. 3 is backsight structural representation of the present utility model；
Structural representations of the Fig. 4 for embodiment 1；
Structural representations of the Fig. 5 for embodiment 2；
Fig. 6 is the structural representation of universal fixture base in embodiment 2；
Structural representations of the Fig. 7 for embodiment 3；
Fig. 8 is the structural representation of universal fixture base in embodiment 3；
Fig. 9 is the structural representation of universal fixture base in embodiment 4.
Wherein：1-universal fixture base, 2-quick Anchor plate kit, 3-part alignment pin, 4-tool locating step pin,
5-part, 6-platen, 7-Universal pressing plate component, 8-frock pressing groove, 9-T-slot, 91-AT type grooves, 92-
BT type grooves, 93-CT type grooves, 10-equidistant location hole, the equidistant location holes of 101-A, the equidistant location holes of 102-B, 103-C are equidistant
Location hole, 11-equidistant locating slot, the equidistant locating slots of 111-A, the equidistant locating slots of 112-B, the equidistant locating slots of 113-C, 12-
T-nut, 13-screw, 14-pad.
Specific embodiment
This utility model is described in further detail with reference to embodiment, but embodiment of the present utility model is not
It is limited to this.
Embodiment 1：
As shown in figure 4, in the present embodiment, the general several milling tools of a kind of aircraft small-scale structure part, including installed in lathe worker
Make on platform 6 and be adapted to the universal fixture base 1 of the part 5 of different size size, on universal fixture base 1 for by zero
The quick Anchor plate kit 2 that part 5 is clamped.
Using said structure, the frock in this utility model is applied to the parts machining of different size size, during use,
Be not required to frock frequently be changed because of the different of 5 size of part, so as to save time cost, and improve machine tool chief axis utilization
Rate, and then improve production efficiency, reduce enterprise's processing cost, enterprise profit.
Embodiment 2：
The present embodiment is further qualified to embodiment 1, as shown in Fig. 2, Fig. 5, Fig. 6, in the present embodiment, above-mentioned general
Equidistant location hole 10, equidistant locating slot 11 and the T-slot 9 for installing quick Anchor plate kit 2 are provided with tooling base 1,
The part alignment pin 3 positioned for part 5 in also including being plugged on equidistant location hole 10 and equidistant locating slot 11.
As the specific embodiment of the present embodiment, during frock in using the present embodiment, on part 5 to be processed
Two are bored with 3 corresponding location hole of part alignment pin, part alignment pin 3 is inserted in above-mentioned location hole, it is subsequently that two parts are fixed
Position pin 3 is inserted in equidistant location hole 10 and equidistant locating slot 11 respectively, as equidistant locating slot 11 is the groove with certain length
Body, position of the part alignment pin 3 in equidistant locating slot 11 can left and right change, therefore this frock is applied to the different part 5 of size.
Part 5 is compressed by the quick Anchor plate kit 2 referred in a upper embodiment, so as to ensure zero during processing
Part 5 will not produce displacement；Connected mode of the present embodiment to quick Anchor plate kit 2 on universal fixture base 1 is further limited
Fixed, i.e., quick Anchor plate kit 2 is arranged on universal fixture base 1 by the T-slot 9 on universal fixture base 1.
Part 5 to be processed and universal fixture bottom are realized by equidistant location hole 10 and equidistant locating slot 11 in the present embodiment
The quick positioning of seat 1；Different length, the part 5 of height are realized in adjustment back and forth by quick Anchor plate kit 2 in T-slot 9
Fast-holding.
Embodiment 3：
The present embodiment is further qualified to embodiment 2, as shown in Figure 7, Figure 8, in the present embodiment, the T-slot 9, etc.
Correspond away from location hole 10, equidistant locating slot 11 and arrange and constitute one group of positioning compression structure；The positioning compression structure
Quantity is three groups, be respectively be equidistantly arranged side by side in vertical direction A group positioning compression structures, B group positioning compression structures, C groups
Positioning compression structure；The T-slot 9 includes the AT type grooves 91 that length successively decreases successively, BT type grooves 92, CT type grooves 93；It is described equidistant
Location hole 10 includes the equidistant location hole of the equidistant location hole 102, C of the equidistant location holes 101, B of A 103；Equidistant locating slot 11 is included in water
Square to the equidistant locating slot of the equidistant locating slot 112, C of the equidistant locating slots 111, B of A that is placed equidistant 113；Described AT type grooves 91, A etc.
Correspond to arrange away from the equidistant locating slot 111 of location hole 101, A and constitute A group positioning compression structures；The BT type grooves 92, B are equidistant
The equidistant locating slot 112 of location hole 102, B is corresponded to arrange and constitutes B group positioning compression structures；The CT type grooves 93, C are equidistantly fixed
The equidistant locating slot 113 in position hole 103, C is corresponded to arrange and constitutes C group positioning compression structures.
In frock mentioned in the present embodiment, one has 3 positioning compression structures, and user can increase according to practical situation
Pressurization locking structure bar number；Between three positioning compression structures, spacing is traditionally arranged to be 60mm, and user can be special according to 5 structure of part
Levy change spacing；Three positioning compression structures, equidistant location hole 10 are different with the distance between equidistant locating slot 11, in etc.
Away from arrangement, 45mm is traditionally arranged to be, to realize the processing of different size part 5；Wherein the distance of A groups positioning compression structure is most
Greatly, the adaptable full-size processing of the frock can be realized, the distance of B group positioning compression structures is medium, can realize medium size
Part 5 is processed, and the distance of C group positioning compression structures is minimum, can realize that the part 5 of minimum dimension is processed；Right side 9 length of T-slot
Also it is different, realize the quick positioning and clamping of different size specification part 5 to be processed.
Using said structure, the scope of parts that this utility model is suitable for is expanded, improve its practicality.
Embodiment 4：
The present embodiment is further improved on the basis of embodiment 2, as shown in Fig. 1, Fig. 3, Fig. 9, in the present embodiment, on
T-nut 12 is slidably fitted with stating T-slot 9, is also included with T-nut 12 with the use of to compress quick Anchor plate kit 2
Screw 13, and be provided between the nut and quick Anchor plate kit 2 of screw 13 for increasing 2 stress surface of quick Anchor plate kit
Long-pending pad 14.
The present embodiment is further qualified to the fastening means of quick Anchor plate kit 2, and the middle part of quick Anchor plate kit 2 opens up
For the groove through screw 13, during assembling, by screw 13 through after pad 14, groove, the top of subsequent screw 13 are then passed through
Stretch in the screwed hole of T-nut 12, and realize threaded connection；Subsequently T-nut 12 is snapped in above-mentioned T-slot 9；Use
When, after part 5 is positioned by user, one end of quick Anchor plate kit 2 can be pressed in 5 upper surface of part, the other end is pressed in general
On tooling base 1；Subsequently user recycles screw 13 to be matched for clamping tightly part 5 with T-nut 12, realizes the work(of fastenings 5
Energy.
Using aforesaid way, the frock mentioned by the present embodiment, its pretightning force for passing through screw thread realize the compression to part 5
Effect, so that this utility model is more convenient to operate, and causes to compress more firmly, and then improves this utility model
Practicality and stability.
Fixed form of the present embodiment to universal fixture base 1 on platen 6 is further defined, this enforcement
In example, chute on platen 6, is equidistantly arranged side by side, relevant position is connected with general pressure on the platen 6
Board component 7；The tool locating step pin 4 for the positioning of universal fixture base 1 is slidably connected in chute；At universal fixture bottom
On seat 1, relevant position is provided with 7 collective effect of Universal pressing plate component so that universal fixture base 1 is pressed on platen 6
On frock pressing groove 8.
During use, user is inserted into tool locating step pin 4 in the location hole of 1 lower surface of universal fixture base, with
Again tool locating step pin 4 is snapped in chute afterwards, move the pressure of the position of universal fixture base 1 down to Universal pressing plate component 7
Tight portion can be pressed in frock pressing groove 8, immediately user operation Universal pressing plate component 7, so as to realize universal fixture base 1 in machine
Substrate hold-down function on bed workbench 6.
Using above-mentioned design, fastening means of the universal fixture base 1 in the present embodiment on platen 6 are flexible,
It is easy to operation, so as to improve motility of the present utility model and practicality.
The above, is only preferred embodiment of the present utility model, and any pro forma limit is not done to this utility model
System, every any simple modification made to above example according to technical spirit of the present utility model, equivalent variations, each falls within
Within protection domain of the present utility model.
Claims (1)
1. a kind of aircraft small-scale structure part universal numerical control milling machine frock, it is characterised in that：Including universal fixture base（1）And setting
In the universal fixture base（1）Upper surface part positioning compression structure；The part positioning compression structure includes T-slot
（2）, location hole（3）And locating slot（4）Three kinds；The T-slot（2）It is arranged on the universal fixture base（1）Upper surface
At two minor faces, the location hole（3）And locating slot（4）The T-slot being arranged at two minor faces（2）Between；The T-slot
（2）With the locating slot（4）Long side and the universal fixture base（1）Long side it is parallel；The universal fixture base（1）'s
Two long edge positions of upper surface are provided with frock pressing groove（5）；The universal fixture base（1）Lower surface be provided with it is removable
Tool locating step pin（6）；The T-slot（2）On be provided with removable quick Anchor plate kit（7）；The universal fixture bottom
Seat（1）Upper surface be provided with 3 groups of part positioning compression structures being equally spaced in a lateral direction；Each group is all included from one
1 T-slot that individual minor face is arranged to another minor face（2）, 1 location hole（3）, 1 locating slot（4）With 1 T-slot（2）；
At one of minor face, 3 T-slots（2）Equal length, at another minor face, 3 T-slots（2）Length, and in
Between T-slot（2）Length is most short；The location hole（3）It is arranged on 3 T-slots of equal length（2）Side, 3 location holes（3）
With the T-slot with group equal length（2）Distance it is equal；The locating slot（4）It is arranged on unequal 3 T-slots of length（2）
Side, 3 locating slots（4）Equal length, and the unequal T-slot of length is organized with same（2）Distance it is equal；Every group of location hole（3）
And locating slot（4）The distance between it is unequal, and middle one group of distance is most short.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620821634.8U CN206084443U (en) | 2016-08-02 | 2016-08-02 | General several millers of aircraft small -scale structure spare dress |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620821634.8U CN206084443U (en) | 2016-08-02 | 2016-08-02 | General several millers of aircraft small -scale structure spare dress |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206084443U true CN206084443U (en) | 2017-04-12 |
Family
ID=58467972
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620821634.8U Active CN206084443U (en) | 2016-08-02 | 2016-08-02 | General several millers of aircraft small -scale structure spare dress |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109227183A (en) * | 2018-11-26 | 2019-01-18 | 法兰泰克重工股份有限公司 | A kind of clamping apparatus |
| CN109605092A (en) * | 2018-12-12 | 2019-04-12 | 成都飞机工业（集团）有限责任公司 | A kind of General hydraulic quick clamping tool |
| CN109759975A (en) * | 2019-03-21 | 2019-05-17 | 成都飞机工业（集团）有限责任公司 | A kind of positioning fixture of augmented reality artificial target's object of aircraft freight space auxiliary operation |
| CN110834207A (en) * | 2019-10-17 | 2020-02-25 | 成都飞机工业（集团）有限责任公司 | Lapping plate replacing tool for multi-surface machining of parts and using method thereof |
| CN113263311A (en) * | 2021-07-16 | 2021-08-17 | 成都飞机工业（集团）有限责任公司 | Modularized positioning system for airplane rapid assembly and assembling and adjusting method thereof |
-
2016
- 2016-08-02 CN CN201620821634.8U patent/CN206084443U/en active Active
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109227183A (en) * | 2018-11-26 | 2019-01-18 | 法兰泰克重工股份有限公司 | A kind of clamping apparatus |
| CN109605092A (en) * | 2018-12-12 | 2019-04-12 | 成都飞机工业（集团）有限责任公司 | A kind of General hydraulic quick clamping tool |
| CN109759975A (en) * | 2019-03-21 | 2019-05-17 | 成都飞机工业（集团）有限责任公司 | A kind of positioning fixture of augmented reality artificial target's object of aircraft freight space auxiliary operation |
| CN110834207A (en) * | 2019-10-17 | 2020-02-25 | 成都飞机工业（集团）有限责任公司 | Lapping plate replacing tool for multi-surface machining of parts and using method thereof |
| CN110834207B (en) * | 2019-10-17 | 2021-07-02 | 成都飞机工业（集团）有限责任公司 | Lapping plate replacing tool for multi-surface machining of parts and using method thereof |
| CN113263311A (en) * | 2021-07-16 | 2021-08-17 | 成都飞机工业（集团）有限责任公司 | Modularized positioning system for airplane rapid assembly and assembling and adjusting method thereof |
| CN113263311B (en) * | 2021-07-16 | 2021-09-28 | 成都飞机工业（集团）有限责任公司 | Modularized positioning system for airplane rapid assembly and assembling and adjusting method thereof |
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