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CN109514200A - The manufacturing method of non-linear arc T tail - Google Patents

The manufacturing method of non-linear arc T tail
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Publication number
CN109514200A
CN109514200ACN201811489240.7ACN201811489240ACN109514200ACN 109514200 ACN109514200 ACN 109514200ACN 201811489240 ACN201811489240 ACN 201811489240ACN 109514200 ACN109514200 ACN 109514200A
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China
Prior art keywords
arc
empennage
shape
tooling
tail
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CN201811489240.7A
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Chinese (zh)
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CN109514200B (en
Inventor
何辰佳
吴杰
梁石
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Shanghai Radio Equipment Research Institute
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Shanghai Radio Equipment Research Institute
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Abstract

The present invention relates to a kind of manufacturing methods of non-linear arc T tail, include: S1, the blank shape that cuboid is formed to blank material grinding;S2, blank shape is assembled in matched tooling;S3, roughing is carried out using first side and second side of the five-axis NC machine center to blank shape, preliminarily forms arc empennage;S4, the first side of arc empennage is finished;S5, the first side of arc empennage is fixed in tooling, the second side of arc empennage is finished;S6, using wire electric discharge machine method, slotted to arc empennage, aperture and cut off processing;S7, arc empennage is positioned using drill jig, and bores side through-hole to it, obtain the arc empennage completed the process.The present invention may be implemented to carry out five-axle linkage processing to the labyrinth of thin-walled, non-linear cambered surface, it is ensured that processing quality improves processing efficiency, has high efficiency and reliability.

Description

The manufacturing method of non-linear arc T tail
Technical field
The present invention relates to a kind of manufacturing methods of non-linear arc T tail, belong to the technology of thin-walled, non-linear curved face processingField.
Background technique
Critical component one of of the arc empennage as aircraft, is the complexity with thin-walled and non-linear cambered surfaceConstitutional detail.The blank material of the arc empennage is TC4 forging, currently, the difficulty of puzzlement this part of arc empennage processing and manufacturingTopic has two o'clock: 1, the part two sides are the thin-walled of wide-angle, non-linear cambered surface, and difficulty of processing is very big;2, since part is thinWall pieces, the thickness of part thinnest part only have 0.0028mm, and processing stability and vibration resistance are difficult to ensure.
Currently, being for the means of production of the arc empennage: using the ball head knife of Milling Motion in Three-axes NC to the two of TC4 forgingSide carries out curved face processing.Since the two sides cambered surface of arc empennage is extremely complex non-linear globoidal structure, after processingThe cambered surface cambered surface that fails and be pre-designed reach completely the same, and since arc empennage is thin-wall part, can also have rigidity notThe problem of foot, the surface quality that the vibration generated in process will lead to cambered surface is overproof, so that processing quality is difficult to ensure.
Based on above-mentioned, the present invention proposes a kind of manufacturing method of novel non-linear arc T tail, to solve the prior artPresent in disadvantage and limitation.
Summary of the invention
The object of the present invention is to provide a kind of manufacturing method of non-linear arc T tail, may be implemented to thin-walled, non-linearThe labyrinth of cambered surface carries out five-axle linkage processing, it is ensured that processing quality improves processing efficiency, has high efficiency and reliability.
To achieve the above object, the present invention provides a kind of manufacturing method of non-linear arc T tail comprising the steps of:
S1, grinding is carried out to blank material, forms the blank shape of rectangular shape;
The tooling that S2, production are matched with the blank shape in S1, and by blank shape assembly in the tooling;
S3, roughing is carried out using first side and second side of the five-axis NC machine center to blank shape, justStep forms arc empennage;
S4, the first side of arc empennage is finished;
S5, the first side of arc empennage is fixed in tooling, the second side of arc empennage is finished;
S6, using wire electric discharge machine method, slotted to arc empennage, aperture and cut off processing;
S7, arc empennage is positioned using drill jig, and bores side through-hole to it, obtain the arc empennage completed the process.
The groove matched with blank shape is offered in the S2, in tooling, and the end insertion of blank shape is setIt sets in the groove of the tooling, and be fixed by pressing plate.
In the S2, the positioning of X, Y-direction of the recess sidewall control blank shape of tooling in clamping;Tooling it is recessedBottom surface controls the positioning of Z-direction of the blank shape in clamping.
In the S5, the first side of arc empennage is fixed on the groove of tooling using solid gum.
In the S6, comprising the following steps:
S61, the first passage: the root notches of processing arc empennage form root shape;
S62, the second passage: the inner hole and second side shape of processing arc empennage;
S63, third passage: the remaining shape of the first side of arc empennage is cut off.
In the S7, the root shape of drill jig and arc empennage is exactly matched, and using the tip of arc empennage and brillMould is fixed, and lateral through aperture processing is carried out.
In conclusion the manufacturing method of non-linear arc T tail provided by the present invention, may be implemented to thin-walled, non-linearThe labyrinth of cambered surface carries out five-axle linkage processing and effectively avoids by using clamped one time positioning process because of multiple clamping instituteThe positioning cumulative errors of generation, it is ensured that processing quality improves processing efficiency, has high efficiency and reliability.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the non-linear arc T tail after processing is completed in the present invention;
Fig. 2 is the top view of the blank shape and tooling assembly in the present invention;
Fig. 3 is the side view of the blank shape and tooling assembly in the present invention
Fig. 4 is that the first side of arc empennage is fixed on the signal of the assembly in tooling using solid gum in the present inventionFigure;
Fig. 5 is the assembling schematic diagram of the arc empennage and drill jig in the present invention.
Specific embodiment
Below in conjunction with FIG. 1 to FIG. 5, by preferred embodiment to technology contents of the invention, construction feature, reached purposeAnd effect is described in detail.
The manufacturing method of non-linear arc T tail provided by the present invention comprising the steps of:
S1, grinding is carried out to blank material, to form the blank shape of rectangular shape, as adding for subsequent handlingWork positioning datum;
The tooling that S2, production are matched with the blank shape in S1, position reference and pressing device as subsequent handling;And by blank shape assembly in the tooling, which plays the role of Set and Positioning;
It is S3, equal using up and down two sides (first side and second side) of the five-axis NC machine center to blank shapeRoughing is carried out, arc empennage is preliminarily formed;
S4, the first side of arc empennage is finished;
S5, the first side of arc empennage is fixed in tooling, the second side of arc empennage is finished;
S6, using wire electric discharge machine method, slotted to arc empennage, aperture and cut off processing;
S7, arc empennage is positioned using drill jig, and bores side through-hole to it, obtain the arc empennage completed the process.
As shown in Figures 2 and 3, in the S2, the groove matched with blank shape 2 is offered in tooling 1, by blankThe end insertion of shape 2 is arranged in the groove of the tooling 1, and is fixed by pressing plate 3.
In the S2, blank shape 2 is on the basis of upper and lower side, two sides side and non-processing end face and tooling1 groove matches, and fit tolerance is within 5.
In the S2, the side wall and bottom surface of the groove of tooling 1 have positioning function, it is ensured that blank shape 2 is addingWork becomes the positioning accuracy during arc empennage;Wherein, the recess sidewall control blank shape 2 of tooling 1 is in clampingX, the positioning of Y-direction;The positioning of Z-direction of the bottom portion of groove granule surface contral blank shape 2 of tooling 1 in clamping.
In the S3, after first side and second side to blank shape 2 complete roughing, single side surplus need to be retained0.1, to guarantee rigid requirements.
In the S4 and S5, after first side and second side to arc empennage complete finishing, it need to ensure to reachThe precision of design requirement.
As shown in figure 4, the first side of arc empennage 4 to be fixed on to the groove of tooling 1 using solid gum in the S5On, the arc empennage of thin-walled can be prevented in process due to vibrating caused by rigidity deficiency.
In the S6, comprising the following steps:
S61, the first passage: the root notches of processing arc empennage form root shape, by live on arc empennageIt drills wire hole and slots at intermediate position and realize;
S62, the second passage: the inner hole and second side shape of processing arc empennage pass through the centre drill in arc empennageIf through-hole, and cut off the realization of the half shape in second side;
S63, third passage: cutting off the remaining shape of the first side of arc empennage, outside the circular arc by arcuately empennageShape connect it is flat after cut off the remaining shape of the other half side wall and realize.
It is described connect it is flat specifically refer to complete to dock with the cambered surface of machined completion, form the surface of same radian, it is ensured thatCutter trade is not seen.
As shown in figure 5, the root shape 6 of drill jig 5 and arc empennage 4 exactly matches, and uses arc tail in the S7The tip 7 of the wing 4 and drill jig 5 are fixed, carry out lateral through aperture processing, to finally obtain after processing is completed non-as shown in Figure 1Linear arc T tail.
In conclusion the manufacturing method of non-linear arc T tail provided by the present invention, is pressed from both sides by the tooling of design specializedTool is positioned, and realizes that blank part facilitates the Set and Positioning of accurate stable in numerical control processing;And select reasonable biteTool and machined parameters, it is ensured that the realization of efficient high-accuracy process;In conjunction with Electric Discharge Wire-cutting Technology, the manufacture of part is realizedProcess.
The present invention is a kind of side that may be implemented to carry out the labyrinth of thin-walled, non-linear cambered surface five-axle linkage processingBlank material assembly in tooling and is finally mounted on numerical control table, NC table by method, with numerical control integrated technique substitution common machineBed is processed, to realize the high-precision processing and manufacturing of thin-walled parts.Since the present invention uses clamped one time positioning process, haveEffect is avoided because positioning cumulative errors caused by multiple clamping, not only the consistency of guarantee converted products, the stability of quality, andAnd make to process simpler easy to operate, effectively improve processing quality and processing efficiency.The present invention is with processing high efficiency and reliablyProperty and continuous production, can promote become can be commonly used to thin-walled, non-linear cambered surface labyrinth highly-efficient processing handSection.
It is discussed in detail although the contents of the present invention have passed through above preferred embodiment, but it should be appreciated that above-mentionedDescription is not considered as limitation of the present invention.After those skilled in the art have read above content, for of the inventionA variety of modifications and substitutions all will be apparent.Therefore, protection scope of the present invention should be limited to the appended claims.

Claims (6)

CN201811489240.7A2018-12-062018-12-06Method for manufacturing nonlinear arc-shaped empennageActiveCN109514200B (en)

Priority Applications (1)

Application NumberPriority DateFiling DateTitle
CN201811489240.7ACN109514200B (en)2018-12-062018-12-06Method for manufacturing nonlinear arc-shaped empennage

Applications Claiming Priority (1)

Application NumberPriority DateFiling DateTitle
CN201811489240.7ACN109514200B (en)2018-12-062018-12-06Method for manufacturing nonlinear arc-shaped empennage

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CN109514200Atrue CN109514200A (en)2019-03-26
CN109514200B CN109514200B (en)2020-07-31

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
CN112173160A (en)*2019-07-022021-01-05宁波海曙昱图航空科技有限公司Forming process and clamping tool for wings and empennage of unmanned aerial vehicle
CN113001125A (en)*2021-03-192021-06-22沈阳万事达机械有限公司Process flow of empennage framework

Citations (8)

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Publication numberPriority datePublication dateAssigneeTitle
EP2368651A1 (en)*2008-12-242011-09-28Open Joint Stock Company "Aviadvigatel"Method for producing a hollow fan blade
CN103506813A (en)*2013-09-122014-01-15哈尔滨汽轮机厂有限责任公司 A kind of processing method of tapered sleeve gauge measuring tool
CN106002088A (en)*2016-05-242016-10-12湖北三江航天红阳机电有限公司Manufacturing method for integral wing-body-fused cabin
CN106181228A (en)*2015-05-072016-12-07哈尔滨飞机工业集团有限责任公司A kind of mechanical process technique of one side complex-shaped surface mould large-scale part
CN106271416A (en)*2016-08-242017-01-04成都飞机工业(集团)有限责任公司A kind of joint parts processing method
CN106271459A (en)*2016-09-202017-01-04哈尔滨东安发动机(集团)有限公司The processing method of complex-curved integral wheel
CN107052715A (en)*2017-03-302017-08-18陕西飞机工业(集团)有限公司A kind of large-scale Integral Wing Panel numerical-control processing method
CN108655669A (en)*2018-05-182018-10-16陕西测易机电设备有限公司A kind of processing method of space flight and aviation thin-walled parts

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
EP2368651A1 (en)*2008-12-242011-09-28Open Joint Stock Company "Aviadvigatel"Method for producing a hollow fan blade
CN103506813A (en)*2013-09-122014-01-15哈尔滨汽轮机厂有限责任公司 A kind of processing method of tapered sleeve gauge measuring tool
CN106181228A (en)*2015-05-072016-12-07哈尔滨飞机工业集团有限责任公司A kind of mechanical process technique of one side complex-shaped surface mould large-scale part
CN106002088A (en)*2016-05-242016-10-12湖北三江航天红阳机电有限公司Manufacturing method for integral wing-body-fused cabin
CN106271416A (en)*2016-08-242017-01-04成都飞机工业(集团)有限责任公司A kind of joint parts processing method
CN106271459A (en)*2016-09-202017-01-04哈尔滨东安发动机(集团)有限公司The processing method of complex-curved integral wheel
CN107052715A (en)*2017-03-302017-08-18陕西飞机工业(集团)有限公司A kind of large-scale Integral Wing Panel numerical-control processing method
CN108655669A (en)*2018-05-182018-10-16陕西测易机电设备有限公司A kind of processing method of space flight and aviation thin-walled parts

Cited By (2)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
CN112173160A (en)*2019-07-022021-01-05宁波海曙昱图航空科技有限公司Forming process and clamping tool for wings and empennage of unmanned aerial vehicle
CN113001125A (en)*2021-03-192021-06-22沈阳万事达机械有限公司Process flow of empennage framework

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