CN204381485U - Central wing front and rear beam ADU bushing plate - Google Patents
Central wing front and rear beam ADU bushing plate Download PDFInfo
- Publication number
- CN204381485U CN204381485U CN201420635959.8U CN201420635959U CN204381485U CN 204381485 U CN204381485 U CN 204381485U CN 201420635959 U CN201420635959 U CN 201420635959U CN 204381485 U CN204381485 U CN 204381485U
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- bushing plate
- hole
- central wing
- rear beam
- drill jig
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Abstract
The utility model provides a kind of central wing front and rear beam ADU bushing plate, and it comprises: the first bushing plate, and the surface hole to be drilled of its laminating central wing front and rear beam is installed, and is provided with multiple first drill jig hole; Second bushing plate, it has the setting height(from bottom) being different from described first bushing plate, and is provided with multiple second drill jig hole; Wherein, described first bushing plate and described second bushing plate share identical locating hole and are positioned on described central wing front and rear beam, and described first drill jig hole is different with the position in described second drill jig hole.The utility model has the advantage of and position, hole originally intensive on central wing front and rear beam processing is split, by two pieces of bushing plate Combination application, the demand that ADU equipment is holed at small space can be solved, improve the drilling efficiency of existing production scene simultaneously.
Description
Technical field
The utility model relates generally to frock field, particularly relates to the central wing front and rear beam bushing plate being applied to ADU (auto-feed brill) equipment.
Background technology
When aircraft wing body docks, central wing is connected front and rear beam place and needs to get out a large amount of connecting holes with outer wing, and has higher requirements to Working position and machining accuracy.But existing bore process usually adopts the mode of Drilling operation one by one in boring procedure, and labour intensity is large.In order to improve bore process, some technical scheme is considered to adopt ADU equipment to hole, but, due to the small space at front and rear beam place, be difficult to the reasonable Arrangement and the process operation that realize ADU equipment.
Utility model content
The purpose of this utility model is to solve above-mentioned defect of the prior art, proposes a kind of bushing plate for the boring of front and rear beam place, to overcome the shortcoming cannot arranging ADU equipment in limited small space.
For this reason, the utility model provides a kind of central wing front and rear beam ADU bushing plate, and it comprises: the first bushing plate, and the surface hole to be drilled of its laminating central wing front and rear beam is installed, and is provided with multiple first drill jig hole; Second bushing plate, it has the setting height(from bottom) being different from described first bushing plate, and is provided with multiple second drill jig hole; Wherein, described first bushing plate and described second bushing plate share identical locating hole and are positioned on described central wing front and rear beam, and described first drill jig hole is different with the position in described second drill jig hole.
In scheme of the present utility model, by adopting same group of locating hole to position respectively two pieces of bushing plates, guarantee to produce minor face distance, and accurate positioning, be conducive to the machining accuracy ensureing boring.
According to a kind of embodiment, described second bushing plate structural segmented, has different setting height(from bottom)s respectively.By this way that bushing plate is structural segmented and increase, rationally can avoid complicated reinforcing rib structure, achieve and use ADU equipment to hole in small space.
Advantageously, the locating hole of described first bushing plate or the second bushing plate comprises main locating hole and time locating hole.According to a kind of embodiment, described main locating hole is located by circular alignment pin, and described time locating hole is located by diamond positioning pin.Thus, after bushing plate is roughly located by the circular alignment pin of use, while the further auxiliary positioning of diamond positioning pin, can avoid bushing plate locked.
According to a kind of embodiment, described first bushing plate or the second bushing plate also comprise location-plate, and described location-plate is provided with the handle hole inserted for positioning element or secure component.Location when location-plate can contribute to operating personnel's installing drill template and identifying operation, but be understandable that, this location-plate is not necessary.
The utility model has the advantage of and position, hole originally intensive on central wing front and rear beam processing is split, by two pieces of bushing plate Combination application, the demand that ADU equipment is holed at small space can be solved, improve the drilling efficiency of existing production scene simultaneously.
Accompanying drawing explanation
More multiple features of the present utility model and advantage are by by understanding better below in conjunction with the further description of accompanying drawing to detailed description of the invention.In accompanying drawing:
Fig. 1 is the schematic diagram of the first bushing plate of central wing front-axle beam according to the utility model one embodiment;
Fig. 2 is the schematic diagram of the second bushing plate of central wing front-axle beam according to the utility model one embodiment;
Fig. 3 is the schematical top view of the second bushing plate shown in Fig. 2;
Fig. 4 is the schematic diagram be installed on by the first bushing plate on central wing front-axle beam;
Fig. 5 is the schematic diagram be installed on by the second bushing plate on central wing front-axle beam;
Fig. 6 is the schematic diagram of the first bushing plate of the central wing back rest according to the utility model one embodiment;
Fig. 7 is the schematic diagram of the second bushing plate of the central wing back rest according to the utility model one embodiment;
Fig. 8 is the schematical top view of the second bushing plate shown in Fig. 7;
Fig. 9 is the schematic diagram be installed on by the first bushing plate on the central wing back rest;
Figure 10 is the schematic diagram be installed on by the second bushing plate on the central wing back rest.
Detailed description of the invention
Below the structure of central wing front and rear beam ADU bushing plate of the present utility model and mode of operation are described in further detail.
First see Fig. 1 to Fig. 5, the bushing plate 10,20 central wing front-axle beam being carried out to Drilling operation is shown.First bushing plate 10 is location and installation on front-axle beam 50 (Fig. 4) first, for completing the drilling operation of Part I.The shape of the body 1 of the first bushing plate 10 and the surface hole to be drilled of front-axle beam 50 adapt, and are provided with multiple first drill jig hole 8.When mounted, as shown in Figure 1, bushing plate 10 is positioned on front-axle beam 50 by circular alignment pin 2 and diamond positioning pin 5 respectively, then uses Fixed latches 3,4 and lock screw 6 to lock.The insertion location of Fixed latches 3,4 and lock screw 6 can utilize the auxiliary one or more location-plates 7 added to realize, as shown in Figure 1.After first bushing plate 10 installation, ADU rig can carry out boring work.After completing boring, the first bushing plate 10 is dismantled and the second bushing plate 20 is installed.The body 21 of the second bushing plate 20 has the setting height(from bottom) being different from the first bushing plate 10, and be provided with multiple the second drill jig hole 26 being different from the first drill jig hole 8, and, for the complicated reinforcing rib structure of front-axle beam 50, also the structural segmented of the second bushing plate 20 can be increased respectively, as shown in Figures 2 and 3.Now, insert circular alignment pin 22 and diamond positioning pin 24 respectively in same position location, install lock-screw 23 afterwards and the second bushing plate 20 is fixed on front-axle beam 50 by clamping screw 25, ADU equipment continues to bore remaining hole.Thus, achieve and use ADU equipment to carry out the process operation of a large amount of boring in small space.
To the drilling operation of the central wing back rest 60 and front-axle beam 50 similar.See Fig. 6 to Figure 10, for the first bushing plate 30 of the back rest 60 and the second bushing plate 40, there is different setting height(from bottom)s and different drill jig holes, but adopt identical locating hole equally.Specifically, the body 31 of the first bushing plate 30 adopts circular alignment pin 32 to locate at main locating hole place, secondary locating hole place adopts diamond positioning pin 34 to locate, and lock-screw or bolt 33 can adopt location-plate 35 auxiliary positioning.After using the first bushing plate 30 to machine Part I hole, remove the first bushing plate 30, the second bushing plate 40 is installed on the back rest 60.The body 41 of the second bushing plate 40 uses circular alignment pin 42 and diamond positioning pin 44 to locate at identical position location place, and adopts lock-screw or bolt 43 to lock, auxiliary positioning plate 45 now also can be adopted to carry out the location of locking member.
Technology contents of the present utility model and technical characterstic have disclosed as above, in the above-described embodiment, by the processing using two pieces of bushing plates to carry out different boring respectively, solve the demand that ADU equipment is holed at small space, effectively improve drilling efficiency.Be understandable that, under creative ideas of the present utility model, those skilled in the art can make various changes said structure and improve, but all belongs to protection domain of the present utility model.Such as, the shape of bushing plate and the position in drill jig hole are not limited to shown in figure, and those skilled in the art can design various different bushing plate structure and different drill jig pore size distributions based on above-mentioned design according to actual needs.The description of above-described embodiment is exemplary instead of restrictive, and protection domain of the present utility model determined by claim.
Claims (5)
1. central wing front and rear beam ADU bushing plate, is characterized in that, comprising:
First bushing plate, the surface hole to be drilled of its laminating central wing front and rear beam is installed, and is provided with multiple first drill jig hole;
Second bushing plate, it has the setting height(from bottom) being different from described first bushing plate, and is provided with multiple second drill jig hole;
Wherein, described first bushing plate and described second bushing plate share identical locating hole and are positioned on described central wing front and rear beam, and described first drill jig hole is different with the position in described second drill jig hole.
2. bushing plate according to claim 1, is characterized in that, described second bushing plate structural segmented, has different setting height(from bottom)s respectively.
3. bushing plate according to claim 2, is characterized in that, the locating hole of described first bushing plate or the second bushing plate comprises main locating hole and time locating hole.
4. bushing plate according to claim 3, is characterized in that, described main locating hole is located by circular alignment pin, and described time locating hole is located by diamond positioning pin.
5. bushing plate according to claim 1, is characterized in that, described first bushing plate or the second bushing plate also comprise location-plate, and described location-plate is provided with the handle hole inserted for positioning element or secure component.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420635959.8U CN204381485U (en) | 2014-10-29 | 2014-10-29 | Central wing front and rear beam ADU bushing plate |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420635959.8U CN204381485U (en) | 2014-10-29 | 2014-10-29 | Central wing front and rear beam ADU bushing plate |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204381485U true CN204381485U (en) | 2015-06-10 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420635959.8U Active CN204381485U (en) | 2014-10-29 | 2014-10-29 | Central wing front and rear beam ADU bushing plate |
Country Status (1)
| Country | Link |
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| CN (1) | CN204381485U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108527511A (en) * | 2018-04-20 | 2018-09-14 | 株洲时代新材料科技股份有限公司 | A kind of rubber product aperture processing method and punching tool |
| CN113118493A (en) * | 2020-01-15 | 2021-07-16 | 中国商用飞机有限责任公司 | Skin opening device and process method |
-
2014
- 2014-10-29 CN CN201420635959.8U patent/CN204381485U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108527511A (en) * | 2018-04-20 | 2018-09-14 | 株洲时代新材料科技股份有限公司 | A kind of rubber product aperture processing method and punching tool |
| CN113118493A (en) * | 2020-01-15 | 2021-07-16 | 中国商用飞机有限责任公司 | Skin opening device and process method |
| CN113118493B (en) * | 2020-01-15 | 2022-07-12 | 中国商用飞机有限责任公司 | Skin opening device and process method |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |