CN106392501A - Machining method for streamline thin-wall metal support plate - Google Patents

Machining method for streamline thin-wall metal support plate Download PDF

Info

Publication number
CN106392501A
CN106392501A CN201611118350.3A CN201611118350A CN106392501A CN 106392501 A CN106392501 A CN 106392501A CN 201611118350 A CN201611118350 A CN 201611118350A CN 106392501 A CN106392501 A CN 106392501A
Authority
CN
China
Prior art keywords
support plate
face
type face
processing method
deformation
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
Application number
CN201611118350.3A
Other languages
Chinese (zh)
Other versions
CN106392501B (en
Inventor
田孟良
蒲泽勇
窦涛
窦一涛
文金龙
张玉
王瑞
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
AECC Guizhou Liyang Aviation Power Co Ltd
Original Assignee
Guizhou Liyang Aerospace Power Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Guizhou Liyang Aerospace Power Co Ltd filed Critical Guizhou Liyang Aerospace Power Co Ltd
Priority to CN201611118350.3A priority Critical patent/CN106392501B/en
Publication of CN106392501A publication Critical patent/CN106392501A/en
Application granted granted Critical
Publication of CN106392501B publication Critical patent/CN106392501B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Straightening Metal Sheet-Like Bodies (AREA)
  • Bending Of Plates, Rods, And Pipes (AREA)

Abstract

The invention discloses a machining method for a streamline thin-wall metal support plate. Firstly, a plate is shore to form a swallow-tail form workblank with positioning grooves in the upper end and the lower end; secondly, the positioning grooves in the upper end and the lower end are used for positioning, a stamping device is used for stamping the plate plane so as to enable the edges of the upper end and the lower end to be bent, deformation of the position between the upper end and the lower end meets an unfolded semi-finished product with the part profile requirement, and an included angle is formed between profile datum lines on the two sides; thirdly, the semi-finished product is bent, and the tail end is welded for connection; and finally the semi-finished product is subject to shape correction. According to the machining method, part deformation is carried out step by step, the part profile deformation is sufficient, the profile is stable, the size accuracy is high, and the turnup face edges are free of cracks; and hydraulic equipment is used for machining, so that the part machining efficiency is improved, and the quality problem caused by manual metal plate repair by tapping is solved.

Description

A kind of processing method of Streamlined thin-wall metallic implants
Technical field
The present invention relates to thick for the material high-temperature alloy sheet material less than 1.5mm to be processed into the process of streamlined support plate, belong to In metal plate punching technical field.
Background technology
Streamlined support plate commonly uses in the structure design needing air current flow passage, is used for even in axial flow channels Connect the support of subsurface it is ensured that the circulation area demand of passage, be used for supporting in circular passage between the radial direction of surfaces externally and internally Gap, the effect played splitting streams and ensure uniform flow passage, under the working environment of high velocity air, a front edge of board requires circle Sliding, type face streamlined also to be remained is to reduce the flow losses of resistance and air-flow, in some special constructions, between support plate Passage also will keep the functional requirement of the changes of section in pneumatic, so, the physical dimension of support plate, intensity and stability are to protect The key element of card component operation performance.
In the provided with internal duct and external duct annular groove in aero-engine inlet casing, turbine bearing case and afterburning diffuser casing Generally all assemble 8 to 12 months streamlined support plates, support plate is divided into the support plate with bushing with without bushing, and support plate is essentially all use Argon arc welding is directly welded or is welded on inside and outside casing by support plate bushing, also will ensure that certain space is used in an intralamellar part The pipeline of the logical oil of assembling.Support plate section is the raised streamlined type face in both sides, and the type face of such part is in sheet metal structural technique class Shallow deformation molding structure is belonged to, the processing of this sheet metal components is typically dependence type tire using manual percussion deformation, topmost in type Problem is that the face resilience of part type is big, and deflection deficiency leads to the molding surface size of part to be difficult to reach the design requirement of product.
In order to reduce the quantity of weld seam in some engines, by support plate bushing design on support plate, such support plate is not only There is shallow deformation, end face also requires the flange of certain altitude to deform, and this kind of support plate increased technology difficulty again, so, zero Finally usually main body machined surface profile deformation deficiency in part, and surface profile is overproof, and end face flange deflection is all larger, frequently results in Crackle in edge, therefore, is usually constructed with the technical conditions allowing repair welding crackle during product design.
The part of this design structure of streamlined support plate is using very early in aircraft engine parts, in view of support plate Front deformation is difficult to stable, geomery and the technological difficulties such as flange deflection is excessive, and a board machining process of existing type is also Base oneself upon and tap shaping in panel beating.Manual percussion is molded the deformation of the sheet material that can progressively extend, and makes full use of the plasticity of sheet material, can be The ductile material of limits reaches very big deformation effect, and its technique deficiency is that part working (machining) efficiency is low, and labor strength is big, And, technical requirements height is tapped to the panel beating of workman, so, the cost of part processing is also very high, particularly in large batch of feelings Under condition, its technique deficiency is particularly evident.
The manual processing method of support plate processing is had by means of the pincers worker fixture in hinge-type two sides banding pattern face, clamp central One core, has the arc-shaped face meeting support plate part side in the both ends of the surface of fixture.First, the part shape chi according to support plate Very little, shear plate, be then in 30~40 ° with a simple type block bent plate with groove, plate after bending is gone Stress is heat-treated, erosion removal surface oxide layer, polishes edge fit to be welded, and woollen is loaded in die cavity in hinge-type fixture, then will Strike and repair the position loading sheet material center with core percussion method, by sheet material to die cavity inner mold face, make sheet material produce certain deformation, Then strike the flange repairing support plate import and export end face it is ensured that being fitted with type tire in sheet material flange face, gap is not more than 0.8.
Again sheet material and core are taken out from die cavity, are placed on workbench, tap material fit with core model face it is ensured that Gap is not more than 0.8, finally loads plate in hinge-type die cavity again, taps flange part, reinstall core to plate center, Extrusion plate laminating mold cavity surface, is so repeated several times, and checks that plate and the patch gap in clamp type face are not more than 0.8, completes to prop up The shaping work of plate.
Another kind of processing of support plate processing is using a set of swaging die device, and its primary structure is a core, up and down Type block, has in the front/rear end of type block and meets the consistent shape facility of parts flanged-edge shape.The processing technology of part is to adopt one The bending of block sheet material is V-shaped, core is loaded inside sheet material, is suppressed using mo(u)ld bottom half block on this mould, because part is under bending Deformation, and deflection is less, typically can be only done the 40~70% of type face requirement, two sides resilience is very big, and end face does not have flange, remaining Lower workload fully relies on manual striking and repaiies subject type face and fit with core, by the upper and lower module of loading of the core with part, then uses Manual percussion support plate both ends of the surface material, until the two ends of the upper mo(u)ld bottom half block of sheet material two ends laminating, completes the type face processing work of support plate, The groundwork amount of this technique is still on manual panel beating.
Content of the invention
The technical problem to be solved in the present invention is:There is provided a kind of processing method of Streamlined thin-wall metallic implants, using liquid The pressure equipment processing band streamlined support plate of flange, manual panel beating is changed into punch forming processing, overcomes manual panel beating work Amount is big, and plastic deformation is not enough, and dimensional accuracy is not high and the low defect of working (machining) efficiency.
The present invention be based on sheet material plastic deformation it is contemplated that closing streamlined support plate little in type face cavity size, Profile forms are gentle, and under integrality, sheet metal is difficult to fully produce plastic deformation, leads to resilience after the processing of part Very big, type face is difficult to obtain required shape.Then, launched to have a certain degree in the type face of support plate two sides by the present invention, Adopt arc transition to connect at the switching in type face, and design the diameter dimension of connecting arc, according to part type face expansion shape Make a special-shaped support plate sheet blank, in woollen upper and lower end Design Orientation (recessed) groove, will with the shaped device with flanging Plate stretch becomes the shallow deformation support plate with flange to launch part, and the main body of part is sufficiently moulded because creating in decompressor Property deformation, thus ensure that the molding surface size of part, flange part also completes main deflection and requires, connecting arc R with The head blend radius of support plate keep certain position relationship, provide accurate position location for follow-up bending.
Then using the connecting arc R of part as positioning datum, the head using craft or bending apparatus curved carrier plate turns Connect circular arc R, in the presence of bending apparatus type face, fulcrum body closes up formation support plate around end rotation, two sides main body to part Closed state.
Finally weld the afterbody of support plate, make the overall structure that support plate is in closing, using the school pattern tool correcting zero with core The subject type face of part and the shape of flange, thus realize shaping and the flange of part.
Technical scheme is as follows:
A kind of processing method of Streamlined thin-wall metallic implants, comprises the following steps:
Step one, plate shears are cut into the swallow-tail form blank with locating slot for the upper/lower terminal;
Plate plane, with the locating slot positioning of upper/lower terminal, is pressed into upper/lower terminal using decompressor by step 2 Curved edge, deformation between upper/lower terminal meets the semi-finished product that a template face requires, and deformation between described upper/lower terminal meets Propping up template face requires part to include arranged on left and right sides type face, and arranged on left and right sides type is connected by connecting arc R between face, and left and right The datum line in both sides type face has an angle;
Step 3, is curved to left and right type face with connecting arc R for positioning datum, then by left and right type face after bending Tail end is weldingly connected;
Step 4, correction template face and curved edge flange.
In described step 2, the datum line angular range in arranged on left and right sides type face is 90 °~150 °.
In described step 2, the radius of connecting arc R is more than support plate head radius.
In described step 2, the arc length of connecting arc R is consistent with support plate head arc length (equal).
In described step 2, arranged on left and right sides type face is connected by connecting arc R and becomes tangent state (in other words, that is, to exist In one section, connecting arc R is tangent with the section line in left and right type face respectively).
In described step 2, the radius span of connecting arc R is 5~20mm.
In described step 3, support plate tail end adopts argon arc welding to weld.
Positioned with the locating slot of upper/lower terminal in step 2, using decompressor by plate plane die mould, positioned with two Centered on groove, two edges flanging before and after sheet material is bent, it is compressing that part type surface state pressed by the sheet material of the right and left, left right model The datum line in face semi-finished product at an angle, this semi-finished product is the deployed condition in part left right model face;
As a kind of selection of decompressor, punch-forming mold is made up of upper and lower two parts, and part of the upper die includes Template, upper module, part of the lower die includes lower module, die and lower template, and upper and lower mould is positioned by guide pillar guide pin bushing, by plate during work Material elongated slot is positioned on the alignment pin of die, hydraulic press push rod jack-up lower module, and till contact sheet material, part of the upper die is in liquid Move downward in the presence of press upper mounting plate, by plate compact to lower module upper surface, then part of the upper die and sheet material and under Module is moved downwardly together, and sheet edge gets into the gap of upper module and die, forms the flange of support plate, and sheet material intermediate host exists It is squeezed into fairshaped type face up and down between model face.
In step 3, as a kind of optional bending apparatus, bending mould is made up of upper and lower two parts, and part of the upper die is Snake core mould, connects bearing forms, and part of the lower die is made up of two pieces of left and right location-plate and center curvature lower module, and upper and lower mould passes through Guide pillar guide pin bushing positions.
During work, semi-finished product to be bent are placed on location-plate, part of the upper die moves down with hydraulic press upper mounting plate, half Fabricated part is pressed between the center curvature lower module in the middle of location-plate in the presence of snake core mould, until the lower mould of bending is attached to Lower template makes sheet material brake forming, and upper mould is opened, and part moves with snake core mould, departs from part of the lower die, finally by part from curved One end of bent core is released, and completes BENDING PROCESS.
In step 4, as a kind of optional flange corrector, flange Correction Die is mainly by upper and lower and left and right four Individual part composition.
Part of the upper die includes cope match-plate pattern, convex mould base, and upper module etc. forms, and part of the lower die is by lower template, load frame, lower module With locating core mould composition, left and right tiltedly carve channel profile correcting block for band.Upper and lower mould is positioned by guide pillar guide pin bushing.
Upper and lower mold open during work, separately, hydraulic press push rod jack-up lower module, to certain altitude, will weld left and right type block Central of the parts re-entrant portion after connecing is inserted on the positioning core of lower mould, and part of the upper die moves down with upper mounting plate, and mo(u)ld top half block is by zero Move down on part press-in core and with mo(u)ld top half block.Left and right type face correcting block in the presence of the oblique wedge of upper mould from both sides to Middle mobile, after upper module goes downwards to certain position, part is sticked and is expressed to outside core and remains stationary as by type face, and upper mould continues Continuous descending, the flange part of part is extruded on the upper and lower surface of left and right correcting block upper and lower module, thus realizing part correction Flange and the function of main body streamline surface;During unlatching, upper module moves upwards, and left and right correcting block moves to both sides respectively, lathe Push rod mo(u)ld bottom half block is ejected upwards, make part depart from positioning core, take out part complete correction work.
The present invention utilizes the process characteristic of sheet-metal formed, with drawing and forming mode, first launches part, in deployed condition This part is difficult to be molded most, the big subject type face of resilience is molded by the way of die mould, allows sheet material produce sufficient plasticity and become Shape, to realize the type facial disfigurement of part and to ensure dimensionally stable, solves the problems, such as part molding surface size precision, routs up two ends simultaneously The partial shape in face, the deformation behaviour of support plate head circular arc at the change design before and after using sheet metal to deform during shaping, and The linear dimension relation that when taking into full account follow-up bending, left and right type face and connecting arc R meet is arranging between expansion shape Distance, finally determines the global shape of shaping flange, and, not produce based on obvious flow harden deformation, size is big for connecting arc R In the R value of product (support plate) head, both sides are propped up template face and are connected and become tangent state by connecting arc R, the arc length of circular arc R with The head switching arc length of former support plate is consistent, and error in length is not more than 0.5mm.
Distance between left and right two lobe support plates, to be determined with the connecting arc R of setting and arc length, according to support plate actual switching R Situation determining, typically between R5 to R20, simultaneously for being conducive to being molded flange, between the support plate of both sides between 90 ° to 150 ° of angle, Finally determine the global shape of shaping flange, then, the plate benging with flange type face welds two ends, reuses including core In mould, the school type moulds of industrial equipment of askew type block, in the presence of equipment, the subject type face of correction support plate both sides, meanwhile, compacting school type The flange shape of support plate end face is so as to meet the conical surface geomery of product requirement.Said method not only can guarantee that type face is molded Stable, and flange effect also can be more satisfactory, completely on pressing equipment and frock, production efficiency is high for whole work flow, plus Work cost is significantly reduced, and is particularly suitable for situation about producing in batches.
The present invention is the feature producing plastic deformation with high alloy sheet material under pressure, in the shaping of special construction In the presence of module in device, carry out the deformation of part step by step, make part type facial disfigurement fully, type face is stable, dimensional accuracy is high, And the edge in flange face occurs without crackle, is processed using hydraulic test, improve the efficiency of part processing, solve artificial Panel beating strikes repaiies the quality problems causing.
Brief description
Fig. 1 is the generalized section of bearing case;
Fig. 2 is the top view of Fig. 1;
Fig. 3 is the blank material figure with locating slot;
Fig. 4 is through shaping the semi-finished product unfolding state figure processing;
Fig. 5 is the sectional view of Fig. 4;
Fig. 6 is blank bent state diagram;
Fig. 7 is diel schematic diagram;
Fig. 8 is bending mould schematic diagram;
Fig. 9 is the left view of Fig. 8;
Figure 10 is flange Correction Die structural representation;
Figure 11 is the plate structure schematic diagram that welding completes;
Figure 12 is Section A-A schematic diagram in Figure 11.
Specific embodiment
If Fig. 1 and Fig. 2 is the final use state figure of support plate.The processing of the Streamlined thin-wall metallic implants that the present invention adopts Method includes following step:
(1) as Fig. 3, first sheet material line is cut into the swallow-tail form blank with locating slot for the two ends.
(2) as Fig. 4, using plate blank two ends locating notch positioning, in special shaping flange decompressor module, Using the effect of upper and lower module and edge, plate plane compacting is in bending two ends, the semi-finished product deployed condition of intermediate deformation, turn Connect circular arc R and take 15mm, the type face of part produces plastic deformation under the compacting of module, and the machined surface profile on both sides reaches product two sides Requirement, dimensionally stable not resilience, between arranged on left and right sides type line of face,mounting, angle is 135 °, such as Fig. 5, Fig. 5 middle left and right type face Datum line and horizontal line angle are 22 ° 30 ', and therefore the angle between the two is 135 °.
(3) as Fig. 6, according to manual bending, then first semi-finished product blank is assembled on type tire, strikes by hand and repair bending two Side, adjusts the position to a template face afterbody in BENDING PROCESS, it is to avoid produce dislocation after the bending of two sides, knee is with type tire (corresponding with the connecting arc R) laminating in R face it is ensured that the molding surface size precision of support plate head, according to bending mould, then adopt curved Bent device needs type face and the position consistency of core and side pressing block, type face and product, and in addition bending apparatus needs to consider and pressure The consistent location hole of type type face position co-ordination, after completing bending, part can smoothly will take out from the other end of core.
After the contact of bending two sides, by the way of argon arc welding, back edge is burn-on in support plate tail end, form an envelope The box part closing.
(4), after blank bent welding, tend to vary with support plate head flange position and deform, and, the flange of two sides In molding procedure, edge is due to being the conical surface shape of segmentation, so, the type face in processing and forming is required with product exist very big Difference, is exactly to be equipped to cell type support plate integrally school type, cell type support plate using hydraulic processes using the process with flange school type Correct body shape under mandrel and the effect of both sides surface pressure, support plate two ends flange face, by the extruding of upper mo(u)ld bottom half block, coordinates school The upper and lower surface of type outer mold piece suppresses the end face edge of support plate together, and the global shape finally realizing support plate requires, and meets product Need.
7~10 illustrating punch forming in the present invention, brake forming and type face flange school shape process below in conjunction with the accompanying drawings:
As shown in fig. 7, mould is made up of upper and lower two parts, part of the upper die includes cope match-plate pattern 1, upper module 2, under Mould part includes lower module 4, die 3 and lower template 5, and upper and lower mould is positioned by guide pillar guide pin bushing, during work, sheet material upper and lower side is fixed Position groove is positioned on the alignment pin of die 3, hydraulic press push rod jack-up lower module 4, and till contact sheet material, part of the upper die is in liquid Move downward in the presence of press upper mounting plate, by plate compact to lower module 4 upper surface, then part of the upper die and sheet material and under Module 4 is moved downwardly together, and sheet edge gets into upper module 2 and the gap of die 3, is formed main in the middle of the flange of support plate, sheet material Body is squeezed into fairshaped type face between upper and lower model face.
As shown in Figure 8 and Figure 9, bending mould is made up of upper and lower two parts, and part of the upper die is snake core mould 7, connects and props up Seat 6 composition, part of the lower die is made up of left and right two pieces of location-plates 8 and 9 and center curvature lower module, and upper and lower mould passes through guide pillar guide pin bushing Positioning.During work, semi-finished product to be bent are placed on location-plate 8 and 9, part of the upper die moves down with hydraulic press upper mounting plate, half Fabricated part is pressed between the bending lower module in the middle of locating piece 8 and 9 in the presence of snake core mould 7, until the lower mould patch of bending Make sheet material brake forming to lower template, upper mould is opened, part moves with snake core mould 7, depart from part of the lower die, finally by part from One end of snake core mould 7 is released, and completes BENDING PROCESS.
As shown in Figure 10, upper and lower and left and right four parts of flange Correction Die form.Part of the upper die includes cope match-plate pattern 10, Convex mould base 11, upper module 12 grade forms, and by lower template 16, load frame, lower 14 modules form with positioning core 15 for part of the lower die, The left and right correcting block 13 and 17 tiltedly carving channel profile 19 band for band.Upper and lower mould is positioned by guide pillar guide pin bushing.During work, upper/lower die is opened Open, left and right correcting block 13 and 17 points are opened, hydraulic press push rod jack-up lower module to certain altitude, will be empty for the Central of the parts after welding Chamber position is inserted on the positioning core 15 of lower mould, and part of the upper die moves down with upper mounting plate, and part is pressed into core 15 by mo(u)ld top half block 12 Move down above and with mo(u)ld top half block 12.Left and right type face correcting block 13 and 17 in the presence of the oblique wedge of upper mould 18 from both sides to Middle mobile, after upper module 12 goes downwards to certain position, part is sticked and keeps after being expressed to positioning core 15 outside by type face Motionless, upper module 12 continues traveling downwardly, and the flange part of part is extruded into the upper and lower table of left and right correcting block 13 and 17 by upper and lower module On face, thus realizing the function that part corrects flange and main body streamline surface;During unlatching, upper module 12 moves upwards, left and right school Positive block 13 and 17 moves to both sides respectively, and lower module 14 is ejected by the push rod of lathe upwards, makes part depart from positioning core 15, takes Go out part and complete correction work.

Claims (7)

1. a kind of processing method of Streamlined thin-wall metallic implants is it is characterised in that comprise the following steps:
Step one, plate shears are cut into the swallow-tail form blank with locating slot for the upper/lower terminal;
Plate plane, with the locating slot positioning of upper/lower terminal, is pressed into upper/lower terminal edge using decompressor by step 2 Bending, deformation between upper/lower terminal meets the semi-finished product that a template face requires, and deformation between described upper/lower terminal meets support plate Type face requires part to include arranged on left and right sides type face, and arranged on left and right sides type is connected by connecting arc R between face, and arranged on left and right sides The datum line in type face has an angle;
Step 3, is curved to left and right type face with connecting arc R for positioning datum, then by left and right type face after bending tail end It is weldingly connected;
Step 4, correction template face and curved edge flange.
2. a kind of Streamlined thin-wall metallic implants according to claim 1 processing method it is characterised in that:
In described step 2, the datum line angular range in arranged on left and right sides type face is 90 °~150 °.
3. a kind of Streamlined thin-wall metallic implants according to claim 1 processing method it is characterised in that:
In described step 2, the radius of connecting arc R is more than support plate head radius.
4. a kind of Streamlined thin-wall metallic implants according to claim 1 processing method it is characterised in that:
In described step 2, the arc length of connecting arc R is consistent with support plate head arc length.
5. a kind of Streamlined thin-wall metallic implants according to claim 1 processing method it is characterised in that:
In described step 2, arranged on left and right sides type face is connected by connecting arc R and becomes tangent state.
6. a kind of Streamlined thin-wall metallic implants according to claim 1 processing method it is characterised in that:
In described step 2, the radius span of connecting arc R is 5~20mm.
7. a kind of Streamlined thin-wall metallic implants according to claim 1 processing method it is characterised in that:
In described step 3, support plate tail end adopts argon arc welding to weld.
CN201611118350.3A 2016-12-07 2016-12-07 A kind of processing method of Streamlined thin-wall metallic implants Active CN106392501B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201611118350.3A CN106392501B (en) 2016-12-07 2016-12-07 A kind of processing method of Streamlined thin-wall metallic implants

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611118350.3A CN106392501B (en) 2016-12-07 2016-12-07 A kind of processing method of Streamlined thin-wall metallic implants

Publications (2)

Publication Number Publication Date
CN106392501A true CN106392501A (en) 2017-02-15
CN106392501B CN106392501B (en) 2018-08-24

Family

ID=58084033

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201611118350.3A Active CN106392501B (en) 2016-12-07 2016-12-07 A kind of processing method of Streamlined thin-wall metallic implants

Country Status (1)

Country Link
CN (1) CN106392501B (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112975296A (en) * 2021-03-08 2021-06-18 哈尔滨汽轮机厂有限责任公司 Manufacturing method of 300 MW-grade F-grade reburning combustion chamber transition section liner rear sealing ring
CN113953771A (en) * 2021-11-12 2022-01-21 中国航发贵州黎阳航空动力有限公司 Machining method of wide-edge metal plate hollow support plate-shaped fairing
CN114951428A (en) * 2022-04-02 2022-08-30 佛山市南海建泰铝制品有限公司 Aluminum profile edge folding forming method and system applying same
CN113953771B (en) * 2021-11-12 2024-07-09 中国航发贵州黎阳航空动力有限公司 Processing method of hollow supporting plate-shaped fairing with band width edge sheet metal

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH071568A (en) * 1993-06-17 1995-01-06 Dainippon Printing Co Ltd Mold
CN103522021A (en) * 2013-10-31 2014-01-22 上海交通大学 Spinning forming process of extra-high-voltage shielding cover
CN103817944A (en) * 2014-01-22 2014-05-28 上虞市美思工艺品有限公司 Manufacturing method of magazine box containing binding strip
CN105081070A (en) * 2014-05-07 2015-11-25 哈尔滨飞机工业集团有限责任公司 Method for forming high inner flange of lip component in reverse drawing manner
CN106001235A (en) * 2016-07-01 2016-10-12 中航飞机股份有限公司西安飞机分公司 Forming method and forming mold of semi-closed sheet part

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH071568A (en) * 1993-06-17 1995-01-06 Dainippon Printing Co Ltd Mold
CN103522021A (en) * 2013-10-31 2014-01-22 上海交通大学 Spinning forming process of extra-high-voltage shielding cover
CN103817944A (en) * 2014-01-22 2014-05-28 上虞市美思工艺品有限公司 Manufacturing method of magazine box containing binding strip
CN105081070A (en) * 2014-05-07 2015-11-25 哈尔滨飞机工业集团有限责任公司 Method for forming high inner flange of lip component in reverse drawing manner
CN106001235A (en) * 2016-07-01 2016-10-12 中航飞机股份有限公司西安飞机分公司 Forming method and forming mold of semi-closed sheet part

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112975296A (en) * 2021-03-08 2021-06-18 哈尔滨汽轮机厂有限责任公司 Manufacturing method of 300 MW-grade F-grade reburning combustion chamber transition section liner rear sealing ring
CN113953771A (en) * 2021-11-12 2022-01-21 中国航发贵州黎阳航空动力有限公司 Machining method of wide-edge metal plate hollow support plate-shaped fairing
CN113953771B (en) * 2021-11-12 2024-07-09 中国航发贵州黎阳航空动力有限公司 Processing method of hollow supporting plate-shaped fairing with band width edge sheet metal
CN114951428A (en) * 2022-04-02 2022-08-30 佛山市南海建泰铝制品有限公司 Aluminum profile edge folding forming method and system applying same
CN114951428B (en) * 2022-04-02 2022-12-13 佛山市南海建泰铝制品有限公司 Aluminum profile edge folding forming method and system applying same

Also Published As

Publication number Publication date
CN106392501B (en) 2018-08-24

Similar Documents

Publication Publication Date Title
CN103752685B (en) The process for stamping of multi-station efficient high-precision automobile panel
CN109570920B (en) Machining method for base body of wave-lobe diffuser
CN106424355A (en) Annular thin-wall part molding die and molding method
CN204035335U (en) A kind of automobile side coaming stamping die
CN105328020A (en) Stamping tool for front ring in flame tube and working method of stamping tool
CN112719021B (en) Flexible side pressing block composite tool for sheet metal part rubber bag forming and use method
CN106392501A (en) Machining method for streamline thin-wall metal support plate
CN103212634B (en) The method for designing of rubber shaping male bend limit multistep mould and forming surface thereof
CN106881422A (en) Oil filling pipe entrance point moulding process
CN107774801B (en) Metal Sheets for Body-manufacturing progressive die Fast design method
CN103406449B (en) Drawing die for covering parts of automobiles
CN112588956A (en) Method for forming double-curved-surface skin opening frame
CN104826937A (en) Tailcone forming mould and forming method of tailcone forming mould
CN112828168B (en) Digital conversion manufacturing method for craftsman skill of magnesium-aluminum alloy automobile covering part die
CN105921587A (en) Forming machining method and device for three branch pipes side by side
CN109465376A (en) The forging method of wind tower doorframe
CN214919793U (en) Adjustable flaring die
CN109127909A (en) Hole extruding formed punch, formed punch design method and anti-deforming structure
CN106903490A (en) A kind of auto parts and components production method
CN204052605U (en) Before in burner inner liner, punch forming frock used by circle
CN113579046A (en) Method for molding drawing technical surface of outer plate of front side wall of automobile
CN207205183U (en) The superplastic forming of the thicker face split casting such as a kind of/diffusion joint forming mould
CN206854457U (en) The punch-forming mold of motor rotor rack
CN101722570A (en) Processing method of mould of cambered special-shaped brick
CN109530540A (en) A kind of car roof product rear portion tailgate avoids part punching press new method

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant
CP03 Change of name, title or address
CP03 Change of name, title or address

Address after: 550014 No. 1111 Liyang Road, Baiyun District, Guiyang City, Guizhou Province

Patentee after: Chinese Hangfa Guizhou Liyang aero Power Co. Ltd.

Address before: 561102 Baiyun Town, Pingba County, Anshun City, Guizhou Province

Patentee before: Guizhou Liyang Aerospace Power Co., Ltd.