CN107745825A - It is a kind of to draw aperture apparatus and its application method using Magnetic oriented - Google Patents
It is a kind of to draw aperture apparatus and its application method using Magnetic oriented Download PDFInfo
- Publication number
- CN107745825A CN107745825A CN201710898344.2A CN201710898344A CN107745825A CN 107745825 A CN107745825 A CN 107745825A CN 201710898344 A CN201710898344 A CN 201710898344A CN 107745825 A CN107745825 A CN 107745825A
- Authority
- CN
- China
- Prior art keywords
- bar magnet
- magnetic
- cavity
- aperture apparatus
- magnetic ball
- 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.)
- Granted
Links
- 238000000034 method Methods 0.000 title claims abstract description 15
- 229920005479 Lucite® Polymers 0.000 claims abstract description 15
- 239000004926 polymethyl methacrylate Substances 0.000 claims abstract description 15
- 239000011521 glass Substances 0.000 claims abstract description 5
- QJVKUMXDEUEQLH-UHFFFAOYSA-N [B].[Fe].[Nd] Chemical compound [B].[Fe].[Nd] QJVKUMXDEUEQLH-UHFFFAOYSA-N 0.000 claims description 3
- 239000003822 epoxy resin Substances 0.000 claims description 3
- 229910052602 gypsum Inorganic materials 0.000 claims description 3
- 239000010440 gypsum Substances 0.000 claims description 3
- 238000009434 installation Methods 0.000 claims description 3
- 229910001172 neodymium magnet Inorganic materials 0.000 claims description 3
- 238000005498 polishing Methods 0.000 claims description 3
- 229920000647 polyepoxide Polymers 0.000 claims description 3
- 229920002430 Fibre-reinforced plastic Polymers 0.000 claims description 2
- 239000011151 fibre-reinforced plastic Substances 0.000 claims description 2
- 230000008569 process Effects 0.000 abstract description 3
- 230000007812 deficiency Effects 0.000 abstract description 2
- 238000004519 manufacturing process Methods 0.000 abstract description 2
- 239000000446 fuel Substances 0.000 description 4
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 239000011152 fibreglass Substances 0.000 description 3
- 238000005728 strengthening Methods 0.000 description 3
- 239000010936 titanium Substances 0.000 description 3
- 229910052719 titanium Inorganic materials 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 230000002787 reinforcement Effects 0.000 description 2
- 230000008439 repair process Effects 0.000 description 2
- 239000004593 Epoxy Substances 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 230000015271 coagulation Effects 0.000 description 1
- 238000005345 coagulation Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/40—Maintaining or repairing aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
Draw aperture apparatus and its application method using Magnetic oriented the present invention relates to a kind of, including organic glass base, cavity version, bar magnet, bolt, magnetic ball, the lucite base and cavity version are bolted, the lucite base is provided with bar magnet mounting hole according to casing position of opening, the bar magnet is filled in mounting hole, the present invention is installed at the die cavity of nonmagnetic closed box, magnetic ball is placed by outside the enclosure portion, magnetic ball automatic absorbing is on the axis of bar magnet position, position of opening can be accurately positioned, perforate is aided in the device, accurate positioning, simplify operating process, operation difficulty is greatly lowered, improve production efficiency and repairing quality simultaneously, eliminate the quality problems of the perforate deviation caused by artificial technical ability deficiency.
Description
Technical field
It is specifically a kind of to draw aperture apparatus and its user using Magnetic oriented the present invention relates to drawing hole positioning field
Method.
Background technology
In aircaft configuration reinforcement repairing, it is often necessary to multiple bolts hole are newly opened, it is determined that the tradition of newly-increased bolt hole position
Method is the requirement according to pitch-row and back gauge, is rule using ruler and combines the position that crossing method determines hole, the method ratio
Relatively it is applied to the more open repair area in the visual field.When the not-go-end of newly-increased perforate is located at relative closure region, and closed area knot
When structure is relative complex, easily blocked by the structural member of box house, cause perforate difficulty or damaged structure, it is difficult to be applicable.
The content of the invention
The technical problems to be solved by the invention are to propose a kind of to draw aperture apparatus and its user using Magnetic oriented
Method, realize the lossless accurate perforate positioning to aircraft closing space structural strengthening.
The technical problems to be solved by the invention are realized using following technical scheme：
A kind of aperture apparatus that draws using Magnetic oriented, including organic glass base, cavity version, bar magnet, bolt, casing,
Magnetic ball, the lucite base and the cavity version are by the bolt connection, and the lucite base is according to drawing hole
Position sets some positioning holes, and the bar magnet is arranged in corresponding positioning hole.The magnetic ball the outer surface of casing with it is corresponding
Bar magnet attracting be accompanied by for locating holes position
The cavity version uses epoxy resin by making fiber reinforced plastic mold according to the cavity shape of casing opening area
Or extraordinary gypsum injection polishing forms.
Bar magnet and the magnetic ball uses neodymium iron boron strong magnet.
A kind of application method for drawing aperture apparatus using Magnetic oriented, including step：
S1 cavity version) is made according to die cavity；
S2 cavity version and lucite base) are connected, in lucite base correspondence position perforate and fills in bar magnet；
S3) aperture apparatus is drawn corresponding to installation in box house die cavity；
S4) magnetic ball is placed in outside the enclosure portion, is adsorbed mutually with the bar magnet of box house, is determined position of opening.
The beneficial effects of the invention are as follows：Perforate is aided in using apparatus of the present invention, accurate positioning, simplifies operating process, is grasped
It is greatly lowered as difficulty, while improves production efficiency and repairing quality, entirely drew the process in hole from past 30 minutes per capita
It is promoted to 1 minute, eliminates the quality problems of the perforate deviation caused by artificial technical ability deficiency.
Brief description of the drawings
The present invention is further described with reference to the accompanying drawings and examples.
Fig. 1 is that the present invention removes the structural representation after magnetic ball；
Fig. 2 is the schematic internal view when present invention is connected with casing；
Fig. 3 is the outside schematic diagram when present invention is connected with casing.
Embodiment
In order that the technical means, the inventive features, the objects and the advantages of the present invention are easy to understand, below it is right
The present invention is expanded on further.
Aircaft configuration reinforcement is the important content of aircraft maintenance maintenance, it is often necessary to bolt hole is opened structural member again, but
For closed structure part, machine leakproof fuel cell like flying, traditional perforate mode location difficulty is careless slightly to damage internal structure
Part causes perforate to fail.Illustrated below with the repair procedures of aircraft leakproof fuel cell proposed by the present invention a kind of using Magnetic oriented
Draw aperture apparatus.
Schematic device as shown in Figure 1：
A kind of aperture apparatus that draws using Magnetic oriented, including organic glass base 1, cavity version 2, bar magnet 3, bolt 4, will
Lucite base 1 and cavity version 2 open screwed hole, wherein the screwed hole of cavity version 2 not breakthrough model, use bolt 4 will
Lucite base 1 and cavity version 2 are connected, and are provided with some positioning holes 11 on lucite 2 according to position of opening, will
Bar magnet 3 is filled in corresponding positioning hole 11.
Box house schematic diagram as shown in Figure 2：
The casing 5 is fuel tanker casing, and casing 5 is made of titanium plate, nonmagnetic, is had inside casing 5 for strengthening
The step 51 of structure, can form the relatively thin die cavity 52 of relative thickness between step, typically can be in the area of die cavity 52 during structural strengthening
Domain carry out perforate, using manual laying mode opening area die cavity 52 in make fiberglass, treat epoxy resin solidification with
Model is taken out afterwards, step 51 clearly shows on fiberglass after shaping, take out fiberglass after, toward groove in injection ring
Oxygen tree fat or extraordinary gypsum, and the glass epoxy made by hand is added, again after coagulation forming, repaired, formed by polishing
The cavity version 2 to be fitted like a glove with leakproof fuel cell titanium plate die cavity.It will be fixed on after each component combination shown in Fig. 1 inside die cavity 52
For locating holes position.
Casing outside schematic diagram as shown in Figure 3：
The surface of casing 5 is placed on using magnetic ball 6, because the bar magnet 3 and magnetic ball 6 use the strong magnetic of neodymium iron boron, axial charging
Bar magnet 3 and magnetic ball 6 only there is magnetic in the axial direction, so when the fixation of bar magnet 3 on non magnetic sheet material, magnetic field can be worn
More nonmagnetic substance, the strong magnetic ball that another surface of sheet material is placed are always automatic to stagnate under the disturbed condition of no extraneous strong magnetic
On the axis of strong bar magnet, that is, magnetic field most strength, and the casing 5 is made using titanium plate, and it is nonmagnetic, will not be to magnetic ball 6
Suction-operated is produced, therefore the position of opening of casing can be accurately determined by the position of magnetic ball 6.
A kind of application method for drawing aperture apparatus using Magnetic oriented, including step：
S1 cavity version) is made according to die cavity；
S2 cavity version and lucite base) are connected, in lucite base correspondence position perforate and fills in bar magnet；
S3) aperture apparatus is drawn corresponding to installation in box house die cavity；
S4) magnetic ball is placed in outside the enclosure portion, is adsorbed mutually with the bar magnet of box house, is determined position of opening.
General principle, principal character and the advantages of the present invention of the present invention has been shown and described above.The technology of the industry
For personnel it should be appreciated that the present invention is not limited to the above embodiments, that described in above-described embodiment and specification is the present invention
Principle, without departing from the spirit and scope of the present invention, various changes and modifications of the present invention are possible, these change and
Improvement all fall within the protetion scope of the claimed invention.The claimed scope of the invention is by appended claims and its equivalent
Thing defines.
Claims (4)
1. a kind of draw aperture apparatus using Magnetic oriented, it is characterised in that：Including organic glass base (1), cavity version (2),
Bar magnet (3), bolt (4), magnetic ball (6), the lucite base (1) are connected with the cavity version (2) by the bolt (4)
Connect, the lucite base (1) sets some positioning holes (11) according to drawing hole site, and the bar magnet (3) is arranged on corresponding
In positioning hole (11), the magnetic ball (6) the outer surface of casing (5) with corresponding bar magnet (3) is attracting is accompanied by for locating holes
Position.
A kind of draw aperture apparatus using Magnetic oriented 2. according to claim 1, it is characterised in that：The cavity version
(2) by making fiber reinforced plastic mold according to the cavity shape of casing (5) opening area, it is molded using epoxy resin or extraordinary gypsum
Polishing forms.
A kind of draw aperture apparatus using Magnetic oriented 3. according to claim 1, it is characterised in that：The bar magnet (3) and
Magnetic ball (6) uses neodymium iron boron strong magnet.
A kind of 4. application method for drawing aperture apparatus using Magnetic oriented, it is characterised in that：Including step：
S1 cavity version) is made according to die cavity；
S2 cavity version and lucite base) are connected, in lucite base correspondence position perforate and fills in bar magnet；
S3) aperture apparatus is drawn corresponding to installation in box house die cavity；
S4) magnetic ball is placed in outside the enclosure portion, is adsorbed mutually with the bar magnet of box house, is determined position of opening.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710898344.2A CN107745825B (en) | 2017-09-28 | 2017-09-28 | Hole guiding device positioned by magnetic field and using method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710898344.2A CN107745825B (en) | 2017-09-28 | 2017-09-28 | Hole guiding device positioned by magnetic field and using method thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107745825A true CN107745825A (en) | 2018-03-02 |
| CN107745825B CN107745825B (en) | 2021-02-12 |
Family
ID=61255967
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710898344.2A Active CN107745825B (en) | 2017-09-28 | 2017-09-28 | Hole guiding device positioned by magnetic field and using method thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107745825B (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110327734A (en) * | 2019-08-01 | 2019-10-15 | 大唐东营发电有限公司 | A kind of power generation station-service flue gas desulfurization and denitrification device |
| CN114719727A (en) * | 2022-03-25 | 2022-07-08 | 四川腾盾科技有限公司 | Method for assembling, positioning and detecting aircraft finished product based on magnet heteropolar attraction |
| CN115615302A (en) * | 2022-09-19 | 2023-01-17 | 成都飞机工业（集团）有限责任公司 | Aircraft skin hole guiding device suitable for narrow space and using method thereof |
| CN115815650A (en) * | 2022-10-26 | 2023-03-21 | 陕西飞机工业有限责任公司 | Device and method for leading holes in composite material parts with closed structure |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20030170082A1 (en) * | 2002-03-08 | 2003-09-11 | The Boeing Company | Multiple-port drill plate and method for debris containment |
| CN202015918U (en) * | 2011-03-29 | 2011-10-26 | 三星高新电机（天津）有限公司 | Printed circuit board product arraying pallet |
| CN104338955A (en) * | 2013-08-05 | 2015-02-11 | 哈尔滨飞机工业集团有限责任公司 | Tool drilling method for parts in closed space |
| CN104668631A (en) * | 2015-01-26 | 2015-06-03 | 哈尔滨飞机工业集团有限责任公司 | Positioning structure and method of blind holes |
| CN206270343U (en) * | 2016-10-27 | 2017-06-20 | 杭州凯珥医疗科技有限公司 | A kind of guider and fixture |
-
2017
- 2017-09-28 CN CN201710898344.2A patent/CN107745825B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20030170082A1 (en) * | 2002-03-08 | 2003-09-11 | The Boeing Company | Multiple-port drill plate and method for debris containment |
| CN202015918U (en) * | 2011-03-29 | 2011-10-26 | 三星高新电机（天津）有限公司 | Printed circuit board product arraying pallet |
| CN104338955A (en) * | 2013-08-05 | 2015-02-11 | 哈尔滨飞机工业集团有限责任公司 | Tool drilling method for parts in closed space |
| CN104668631A (en) * | 2015-01-26 | 2015-06-03 | 哈尔滨飞机工业集团有限责任公司 | Positioning structure and method of blind holes |
| CN206270343U (en) * | 2016-10-27 | 2017-06-20 | 杭州凯珥医疗科技有限公司 | A kind of guider and fixture |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110327734A (en) * | 2019-08-01 | 2019-10-15 | 大唐东营发电有限公司 | A kind of power generation station-service flue gas desulfurization and denitrification device |
| CN110327734B (en) * | 2019-08-01 | 2024-12-27 | 大唐东营发电有限公司 | A flue gas desulfurization and denitrification device for power plants |
| CN114719727A (en) * | 2022-03-25 | 2022-07-08 | 四川腾盾科技有限公司 | Method for assembling, positioning and detecting aircraft finished product based on magnet heteropolar attraction |
| CN114719727B (en) * | 2022-03-25 | 2024-06-11 | 四川腾盾科技有限公司 | Aircraft finished product assembling, positioning and detecting method based on magnetic heteropolar attraction |
| CN115615302A (en) * | 2022-09-19 | 2023-01-17 | 成都飞机工业（集团）有限责任公司 | Aircraft skin hole guiding device suitable for narrow space and using method thereof |
| CN115815650A (en) * | 2022-10-26 | 2023-03-21 | 陕西飞机工业有限责任公司 | Device and method for leading holes in composite material parts with closed structure |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107745825B (en) | 2021-02-12 |
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