CN104874835A - Longitudinal adjustable drill plate of composite material component - Google Patents
Longitudinal adjustable drill plate of composite material component Download PDFInfo
- Publication number
- CN104874835A CN104874835A CN201510249256.0A CN201510249256A CN104874835A CN 104874835 A CN104874835 A CN 104874835A CN 201510249256 A CN201510249256 A CN 201510249256A CN 104874835 A CN104874835 A CN 104874835A
- Authority
- CN
- China
- Prior art keywords
- composite element
- longitudinal direction
- bushing plate
- composite material
- material component
- 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.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B47/00—Constructional features of components specially designed for boring or drilling machines; Accessories therefor
- B23B47/28—Drill jigs for workpieces
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B49/00—Measuring or gauging equipment on boring machines for positioning or guiding the drill; Devices for indicating failure of drills during boring; Centering devices for holes to be bored
- B23B49/02—Boring templates or bushings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B2226/00—Materials of tools or workpieces not comprising a metal
- B23B2226/27—Composites
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Drilling And Boring (AREA)
Abstract
The invention discloses a longitudinal adjustable drill plate of a composite material component. The longitudinal adjustable drill plate of the composite material component comprises a drill plate body (1), an inserting pin (2), a locating pin (3), a drilling sleeve (4), the composite material component (5), a drilling bushing (6) and two pin bushings (7). With the adoption of the longitudinal adjustable drill plate of the composite material component, the purpose of drilling a hole can be reached; the interchangeability of the drill plate of the composite material component can be achieved; a die can be quickly and conveniently repaired; the demands of a composite material production workshop on each model can be met; the labor intensity of workers can be reduced; the production efficiency can be increased.
Description
Technical field
The invention belongs to composite processing field, be specifically related to the composite element bushing plate that a kind of longitudinal direction is adjustable.
Background technology
In the process of composite element, often have the situation needing boring to occur, in prior art, great majority first rule to hole again, or on shaping mould, mark position, hole cross hairs, is printed on multiple material part time shaping; Hole again.Adopt above method drilling, have some limitations.For product part existing porous, then need to mark the position line corresponding to each hole, be difficult to the relative position ensureing each hole.
Summary of the invention
Instant invention overcomes the deficiencies in the prior art, the composite element bushing plate that a kind of longitudinal direction is adjustable is provided, when part exists the product boring of porous, ensure that the relative position in each hole; Composite element bushing plate is utilized to enhance productivity.Not only convenient, fast but also be conducive to the operation of workman, reach the object shortening the production cycle, increase economic efficiency.
Consider the problems referred to above of prior art, according to an aspect disclosed by the invention, the present invention by the following technical solutions:
The composite element bushing plate that a kind of longitudinal direction of the present invention is adjustable, by bushing plate (1), latch (2), alignment pin (3), drill bushing (4), composite element (5), drilling liners (6), two dowel bushings (7) compositions, it is characterized in that, composite element (5) side arranges drilling liners (6), opposite side longitudinal direction is arranged respectively two dowel bushings (7), composite element (5), drilling liners (6) and dowel bushings (7) are solidified into entirety, then with bushing plate (1) latch (2), alignment pin (3) connects, wherein latch (2) inserts in a dowel bushings (7) on composite element (5) opposite side longitudinal direction, alignment pin (3) inserts in another dowel bushings (7) on composite element (5) opposite side longitudinal direction, drill bushing (4) is arranged on the position of bushing plate (1) corresponding to drilling liners (6), because drilling liners (6) and dowel bushings (7) position dimension are fixing, in solidification process, between two dowel bushings (7), longitudinal size will change, so the upper pin hole corresponding to alignment pin (3) of bushing plate (1) makes slotted hole at longitudinal direction, longitudinal direction is adjustable,
On the composite element bushing plate that same set of longitudinal direction is adjustable, ensure that the size of boring is identical, position location is identical, and under the condition that location dimension is identical, bushing plate (1) is removable.
By the composite element bushing plate that longitudinal direction of the present invention is adjustable, reach the object drilling hole, and achieve composite element bushing plate interchangeability, cause mould to be reprocessed quick and easy.Meet multiple each model type demand of material workshop, reduce labor strength, improve production efficiency.
Accompanying drawing explanation
Fig. 1 shows longitudinally adjustable composite element bushing plate overall work section of structure.
Fig. 2 shows longitudinally adjustable composite element bushing plate overall work structure left view.
Fig. 3 shows bushing plate top view.
Fig. 4 shows bushing plate profile.
Fig. 5 shows latch.
Detailed description of the invention
Below in conjunction with embodiment, the present invention is described in further detail, but embodiments of the present invention are not limited thereto.
As Fig. 1-5 of the present invention, the composite element bushing plate that a kind of longitudinal direction of the present invention is adjustable, by bushing plate (1), latch (2), alignment pin (3), drill bushing (4), composite element (5), drilling liners (6), two dowel bushings (7) compositions, it is characterized in that, composite element (5) side arranges drilling liners (6), opposite side longitudinal direction is arranged respectively two dowel bushings (7), composite element (5), drilling liners (6) and dowel bushings (7) are solidified into entirety, then with bushing plate (1) latch (2), alignment pin (3) connects, wherein latch (2) inserts in a dowel bushings (7) on composite element (5) opposite side longitudinal direction, alignment pin (3) inserts in another dowel bushings (7) on composite element (5) opposite side longitudinal direction, drill bushing (4) is arranged on the position of bushing plate (1) corresponding to drilling liners (6), because drilling liners (6) and dowel bushings (7) position dimension are fixing, in solidification process, between two dowel bushings (7), longitudinal size will change, so the upper pin hole corresponding to alignment pin (3) of bushing plate (1) makes slotted hole at longitudinal direction, longitudinal direction is adjustable,
On the composite element bushing plate that same set of longitudinal direction is adjustable, ensure that the size of boring is identical, position location is identical, and under the condition that location dimension is identical, bushing plate (1) is removable.
The all die shapes of the present invention are very simple and direct.During the dismounting of this bushing plate, do not need professional tool, reprocess conveniently.Assembly structure Fig. 1 is the preferably mode of composite element bushing plate work structuring schematic diagram longitudinally adjustable in the present invention.Solidified by composite element 5, drilling liners 6, dowel bushings 7, make it to become entirety to be then connected with bushing plate 1 latch 2, alignment pin 3, air drill is utilized to drill hole on multiple material after assembling, bushing plate is convenient disassembly on drill jig, maintenance is quick, shorten the production cycle, enhance productivity.
Claims (1)
1. the composite element bushing plate that a longitudinal direction is adjustable, by bushing plate (1), latch (2), alignment pin (3), drill bushing (4), composite element (5), drilling liners (6), two dowel bushings (7) compositions, it is characterized in that, composite element (5) side arranges drilling liners (6), opposite side longitudinal direction is arranged respectively two dowel bushings (7), composite element (5), drilling liners (6) and dowel bushings (7) are solidified into entirety, then with bushing plate (1) latch (2), alignment pin (3) connects, wherein latch (2) inserts in a dowel bushings (7) on composite element (5) opposite side longitudinal direction, alignment pin (3) inserts in another dowel bushings (7) on composite element (5) opposite side longitudinal direction, drill bushing (4) is arranged on the position of bushing plate (1) corresponding to drilling liners (6), because drilling liners (6) and dowel bushings (7) position dimension are fixing, in solidification process, between two dowel bushings (7), longitudinal size will change, so the upper pin hole corresponding to alignment pin (3) of bushing plate (1) makes slotted hole at longitudinal direction, longitudinal direction is adjustable,
On the composite element bushing plate that same set of longitudinal direction is adjustable, ensure that the size of boring is identical, position location is identical, and under the condition that location dimension is identical, bushing plate (1) is removable.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510249256.0A CN104874835A (en) | 2015-05-15 | 2015-05-15 | Longitudinal adjustable drill plate of composite material component |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510249256.0A CN104874835A (en) | 2015-05-15 | 2015-05-15 | Longitudinal adjustable drill plate of composite material component |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104874835A true CN104874835A (en) | 2015-09-02 |
Family
ID=53942656
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510249256.0A Pending CN104874835A (en) | 2015-05-15 | 2015-05-15 | Longitudinal adjustable drill plate of composite material component |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104874835A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108127148A (en) * | 2017-12-22 | 2018-06-08 | 中航沈飞民用飞机有限责任公司 | Detachable drill jig and its method for drilling composite material location hole |
| CN111644664A (en) * | 2020-06-24 | 2020-09-11 | 中国商用飞机有限责任公司 | Eccentrically reamed eccentric orientation assembly, eccentric dosing assembly, eccentric reaming assembly, kit and method |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4294567A (en) * | 1979-01-11 | 1981-10-13 | Garfield Wiggins | Doweling jig template |
| CN2865988Y (en) * | 2005-12-16 | 2007-02-07 | 中国重型汽车集团有限公司 | Drill clamping device |
| CN201361730Y (en) * | 2009-02-05 | 2009-12-16 | 沈阳飞机工业（集团）有限公司 | Bushing plate |
| CN102310212A (en) * | 2011-08-31 | 2012-01-11 | 西安陕鼓动力股份有限公司 | Universal drill jig used for drilling among existing distribution holes on barrel |
| CN102528127A (en) * | 2010-12-10 | 2012-07-04 | 张勇毅 | Adjustable coordinate drill jig |
| CN202517087U (en) * | 2012-04-13 | 2012-11-07 | 哈尔滨飞机工业集团有限责任公司 | Drilling jig of slotted hole lining installation hole in drilling tooling |
| CN102896507A (en) * | 2012-09-07 | 2013-01-30 | 苏州市职业大学 | Novel adjustable efficient drilling disk type fixture |
| CN203044979U (en) * | 2013-01-10 | 2013-07-10 | 哈尔滨飞机工业集团有限责任公司 | Tooling clamping plate positioning hole drill jig |
| CN103203581A (en) * | 2013-04-24 | 2013-07-17 | 哈尔滨飞机工业集团有限责任公司 | Bias correction method of drill bushing mounting hole of drill plate |
-
2015
- 2015-05-15 CN CN201510249256.0A patent/CN104874835A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4294567A (en) * | 1979-01-11 | 1981-10-13 | Garfield Wiggins | Doweling jig template |
| CN2865988Y (en) * | 2005-12-16 | 2007-02-07 | 中国重型汽车集团有限公司 | Drill clamping device |
| CN201361730Y (en) * | 2009-02-05 | 2009-12-16 | 沈阳飞机工业（集团）有限公司 | Bushing plate |
| CN102528127A (en) * | 2010-12-10 | 2012-07-04 | 张勇毅 | Adjustable coordinate drill jig |
| CN102310212A (en) * | 2011-08-31 | 2012-01-11 | 西安陕鼓动力股份有限公司 | Universal drill jig used for drilling among existing distribution holes on barrel |
| CN202517087U (en) * | 2012-04-13 | 2012-11-07 | 哈尔滨飞机工业集团有限责任公司 | Drilling jig of slotted hole lining installation hole in drilling tooling |
| CN102896507A (en) * | 2012-09-07 | 2013-01-30 | 苏州市职业大学 | Novel adjustable efficient drilling disk type fixture |
| CN203044979U (en) * | 2013-01-10 | 2013-07-10 | 哈尔滨飞机工业集团有限责任公司 | Tooling clamping plate positioning hole drill jig |
| CN103203581A (en) * | 2013-04-24 | 2013-07-17 | 哈尔滨飞机工业集团有限责任公司 | Bias correction method of drill bushing mounting hole of drill plate |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108127148A (en) * | 2017-12-22 | 2018-06-08 | 中航沈飞民用飞机有限责任公司 | Detachable drill jig and its method for drilling composite material location hole |
| CN108127148B (en) * | 2017-12-22 | 2019-07-02 | 中航沈飞民用飞机有限责任公司 | Detachable drill jig and its method for drilling composite material location hole |
| CN111644664A (en) * | 2020-06-24 | 2020-09-11 | 中国商用飞机有限责任公司 | Eccentrically reamed eccentric orientation assembly, eccentric dosing assembly, eccentric reaming assembly, kit and method |
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| C06 | Publication | ||
| PB01 | Publication | ||
| EXSB | Decision made by sipo to initiate substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20150902 |
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| WD01 | Invention patent application deemed withdrawn after publication |