CN1822909A - Method for the production of a semi-finished product for a wing-shaped element - Google Patents
Method for the production of a semi-finished product for a wing-shaped element Download PDFInfo
- Publication number
- CN1822909A CN1822909A CNA2004800197993A CN200480019799A CN1822909A CN 1822909 A CN1822909 A CN 1822909A CN A2004800197993 A CNA2004800197993 A CN A2004800197993A CN 200480019799 A CN200480019799 A CN 200480019799A CN 1822909 A CN1822909 A CN 1822909A
- Authority
- CN
- China
- Prior art keywords
- former
- sheet material
- sheet
- semi
- panel
- 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 26
- 239000011265 semifinished product Substances 0.000 title claims abstract description 12
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 11
- 238000003825 pressing Methods 0.000 claims abstract description 9
- 238000005452 bending Methods 0.000 claims abstract description 3
- 239000000463 material Substances 0.000 claims description 24
- 238000007688 edging Methods 0.000 claims description 9
- 238000007493 shaping process Methods 0.000 claims description 5
- 238000000137 annealing Methods 0.000 claims description 4
- 238000005096 rolling process Methods 0.000 claims description 4
- 238000001125 extrusion Methods 0.000 claims description 2
- 238000010438 heat treatment Methods 0.000 claims description 2
- 239000002184 metal Substances 0.000 claims description 2
- 229910052751 metal Inorganic materials 0.000 claims description 2
- 229910000831 Steel Inorganic materials 0.000 claims 1
- 229910045601 alloy Inorganic materials 0.000 claims 1
- 239000000956 alloy Substances 0.000 claims 1
- 239000010935 stainless steel Substances 0.000 claims 1
- 229910001220 stainless steel Inorganic materials 0.000 claims 1
- 239000010959 steel Substances 0.000 claims 1
- 230000015572 biosynthetic process Effects 0.000 abstract 1
- 230000002950 deficient Effects 0.000 description 4
- 230000000694 effects Effects 0.000 description 2
- 239000002994 raw material Substances 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 1
- 230000014509 gene expression Effects 0.000 description 1
- 239000003550 marker Substances 0.000 description 1
- 239000000047 product Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D53/00—Making other particular articles
- B21D53/78—Making other particular articles propeller blades; turbine blades
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49336—Blade making
- Y10T29/49339—Hollow blade
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49616—Structural member making
- Y10T29/49622—Vehicular structural member making
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Bending Of Plates, Rods, And Pipes (AREA)
- Shaping Of Tube Ends By Bending Or Straightening (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
Abstract
A method for the production of a semi-finished product (13) for a wing-shaped element (15) having, in cross-section, a front edge (2), a rear edge (14) and an arched bottom wall (3) and an arched top wall (4) that extend some distance apart between the front edge (2) and the rear edge (14), comprises the following steps: bending the sheet (1) with the formation of two panels (3, 4) as well as a curved region (2) which the panels (3, 4) adjoin, placing a former (10) in the bent sheet (1) with the front edge of the former (9) positioned in the curved region (2), forcing the pressure member (8) towards a rubber cushion (7) with the bent sheet (1) enclosed between them and deforming said sheet between the former (10) and the rubber cushion (7), placing the shaped sheet (F) in a rubber press provided with a bottom block having a cavity (16) which has a shape that at least approximately corresponds to the external shape of one of the walls (3, 4) of the shaped sheet (P), pressing the shaped sheet (F) with former (10) between the bottom block (11) and a rubber mat (12), removing the semi-finished product (13) from the rubber press.
Description
Technical field
The present invention relates to the half-finished manufacture method of wing-shaped element and the manufacture method of wing-shaped element itself.This wing-shaped element forms with various form.The so-called blade that is fixed on the aircraft wing wing flap is mentioned as an example.
Background technology
The various manufacture methods of this wing-shaped element have been behaved known.At first to mention extruding of element.In this case, element needn't be made of separated portions, quick like this and relative less expensive.But its defective is that dimensional tolerance is very poor.Especially under the situation of less relatively thickness, this defective can occur.According to another kind of known method, element is by the sheet material manufacturing.After the preform sheet material, sheet material stretches on the stretching straightener, is used to form the parts (section bar) with bottom and top.Axle is included in the preformed sheet material.The integral body of Xing Chenging is clipped in longitudinal end and stretches then thus.Its defective of this known method is that the surface that is obtained has scrambling.
Summary of the invention
The purpose of this invention is to provide a kind of process of semi-finished that is used to make wing-shaped element, it does not have these defectives.Described purpose reaches by a kind of half-finished manufacture method of wing-shaped element, wherein these semi-finished product have the arc diapire and the arc roof of leading edge, back edge and extension spaced from each other between leading edge and back edge in cross section, and this method comprises the steps:
-metal sheet is provided,
-bent sheet, forming the curved region of two panels and panel institute adjacency,
-the shape that provides former, its outside to have the inner surface of the parts (section bar) after finishing,
-former is placed in the bent sheet, make the leading edge of former be positioned at curved region,
-edging machine that is provided with opposed pressing piece and rubber blanket is provided,
-former is fixed on the pressing piece,
-promote pressing piece to rubber blanket, wherein bent sheet is enclosed between them, and makes described sheet material distortion between former and rubber blanket,
-take off the former that has the shaping sheet material from edging machine,
-they are placed in the rubber press that is provided with bottom biock, this bottom biock has its shape and is similar to corresponding cavity at least with the outer shape of a wall of shaping sheet material,
-extrusion molding sheet material, wherein former between bottom biock and rubber mat plate,
-take off semi-finished product from rubber press.
Adopt the method according to this invention, semi-finished product are shaped by being exerted pressure thereon by rubber element.In conjunction with the former that is used as axle and has suitable profile, can obtain shape very accurately by this method, this shape has the surface of aircraft because of the required smoothness of aerodynamics reason.
Preferably, after bent sheet or before or two panel-shaped cambers meanwhile.In order to obtain firm relatively curved element, arc can be towards same direction.But, arc also can be toward each other back to direction.
Curved panel and as selecting to make the panel embowment can be by rolling forming or by rolling realization.The back edge of element can form the parts (section bar) that are fixed on roof and the diapire.In addition, wing-shaped element can be accepted heat treatment, for example stress relief annealing or solution annealing.
The invention still further relates to the wing-shaped element of making according to this method, according to said method, this element for example can form blade.
Please refer to disclosed wing-shaped element among the US-A 4531270.This element is made by flat relatively parts (section bar), and wherein these parts comprise two panels that form an integral body, and wherein finally the arc of wall with the bigger material thickness preproduction in part.This element is by folding panel mutually simply and acquisition thus, and element manufacturing is after this finished.Here the element that relates to is the form of turbine blade.
Description of drawings
Exemplary embodiment below with reference to the accompanying drawings illustrates in greater detail the present invention.
Fig. 1 has shown curved and the arc sheet material, and this sheet material is as the raw material of the method according to this invention.
Fig. 2 has shown the element in the edging machine.
Fig. 3 has shown the effect after handling in edging machine.
Fig. 4 has shown the perspective view of the rubber press of the rubber press that has axle.
Fig. 5 has shown the product that obtains after the rubber compacting.
Fig. 6 has shown the wing-shaped element after finishing.
The specific embodiment
When implementing the method according to this invention, employed raw material are the bent sheet 1 shown in Fig. 1, and it has carried out bending, make to form crooked leading edge 2, depression curved panel 3 and protrude curved panel 4.This bent sheet 1 is placed in the edging machine 5 shown in Fig. 2, and this edging machine has base 6 and the pressing piece 8 that has rubber blanket 7, and wherein pressing piece can move up and down and former 10 is fixed thereon by support 9.This former 10 or axle 10 also are shown among Fig. 4 with perspective view.It has the shape of the inner surface of the wing-shaped element after finishing, and that is to say, has the end face and the bottom surface of leading edge, back edge and arc.This former can be prismatic and twisted shape.
When extruding bent sheet 1 in edging machine, the leading edge of former 10 is pushed in the curved region 2 of sheet material 1.In this way, under the even inside pressure effect of rubber blanket 7, this curved region is further crooked around the leading edge of former 10.As a result, curved panel 3 and 4 is more approaching mutually, as shown in Figure 3.
The sheet material 1 that further is shaped is placed in the rubber press then by this way, and the rubber press 11 of this forcing press is shown among Fig. 4, and its interior shape is corresponding with the leading edge and the curved surfaces of wing-shaped element.The sheet material 1 that has shape shown in Fig. 3 now is placed in the rubber press 11 with axle 10.Rubber mat plate 12 is placed in this above integral body then, and after this, the sheet material 1 that wherein has axle 10 is extruded between rubber press 11 and rubber mat plate 12 by the forcing press (not shown).
After the rubber compacting, obtain the semi-finished product 13 shown in Fig. 5, it has curved front edge 2, protrudes arc top surface 4 and depression lower arcuate surface 3.At last, whole parts (section bar) by reference marker 14 expressions are fixed to the free rear end of wall 4,3.Therefore, these parts have body 15, and this body has relative to each other downward-sloping side 16,17, and they are oriented consistent with the bearing of trend of roof 4 and diapire 3.Parts 14 are fixed on the semi-finished product 13 by the rivet 18 that passes roof 4, body 15 and diapire 3, and after this wing-shaped element 15 is made and finished.As selection, wall 4,3 also can, for example directly fixed to one another by bonding, riveted joint etc.
Claims (15)
1, the manufacture method of the semi-finished product (13) of a kind of wing-shaped element (15), wherein these semi-finished product have the arc diapire (3) and the arc roof (4) of leading edge (2), back edge (14) and extension spaced from each other between leading edge (2) and back edge (14) in cross section, and this method comprises the steps:
-metal sheet (1) is provided,
-bent sheet (1), forming the curved region (2) of two panels (3,4) and panel (3,4) institute adjacency,
-the shape that provides former (10), its outside to have the inner surface of the element (15) after finishing,
-former (10) is placed in the bent sheet (1), make the leading edge of former (10) be positioned at curved region (2),
-edging machine (5) that is provided with opposed pressing piece (8) and rubber blanket (7) is provided,
-former (10) is fixed on the pressing piece (8),
-promote pressing piece (8) to rubber blanket (7), wherein bent sheet (1) is enclosed between them, and makes described sheet material distortion between former (10) and rubber blanket (7),
-take off the former (10) that has shaping sheet material (1 ') from edging machine (5),
-shaping sheet material (1 ') is placed in the rubber press that is provided with bottom biock, this bottom biock has its shape and is similar to corresponding cavity (16) at least with the outer shape of a described wall (3,4) of shaping sheet material (1 '),
-extrusion molding sheet material (1 '), wherein former (10) is positioned between bottom biock (11) and the rubber mat plate (12),
-take off semi-finished product (13) from rubber press.
2, method according to claim 1, wherein bent sheet (1) afterwards or before or meanwhile two panels (3,4) form arc.
3,, comprise by rolling forming curved according to the described method of one of front claim
Qu Suoshu curved region (2), and as selecting to make panel (3,4) embowment.
4, according to the described method of one of front claim, comprise by the described curved region of rolling bending (2), and as selecting to make panel (3,4) embowment.
5,, comprise using being fixed to roof according to the described method of one of front claim
(3) and the parts (14) on the diapire (4) constitute back edge, form wing-shaped element (15) thus.
6, according to the described method of one of front claim, comprise heat treatment step, for example the stress relief annealing or the solution annealing of semi-finished product (13).
7, by the wing-shaped element of making according to the described method of one of front claim
(15), it is formed blade.
8, element according to claim 7 (15), it is by method manufacturing according to claim 5, and wherein parts (14) have the body (19) that extends between panel (3,4).
9, element according to claim 8 (15), wherein panel (3,4) and body (19) are by rivet (18), bonding etc. fixed to one another.
10, according to Claim 8 or 9 described elements (15), wherein body (19) each other back to surface (16,17) relative to each other tilt to extend according to the bearing of trend of panel (3,4).
11, element according to claim 7 (15), wherein panel (3,4) is directly fixed to one another.
12,, comprise sheet material (1) with the thickness in 0.8 to the 2.0mm scope according to the described element of one of claim 7 to 12 (15).
13,, comprise sheet material (1) with the thickness in 1.4 to the 1.6mm scopes according to the described element of one of claim 7 to 12 (15).
14,, comprise sheet material (1) with near the thickness of 1.6mm according to the described elements in one of claim 12 or 13 (15).
15,, comprise the sheet material that constitutes by Al, Ti, Sc, Cu, Mg, Li and/or their alloy and/or steel and/or stainless steel according to the described element of one of claim 7 to 11 (15).
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| NL1023896 | 2003-07-11 | ||
| NL1023896A NL1023896C2 (en) | 2003-07-11 | 2003-07-11 | Method for manufacturing a semi-finished product for a wing-shaped element. |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1822909A true CN1822909A (en) | 2006-08-23 |
| CN100404158C CN100404158C (en) | 2008-07-23 |
Family
ID=34056982
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNB2004800197993A Expired - Fee Related CN100404158C (en) | 2003-07-11 | 2004-07-08 | Method for the production of a semi-finished product for a wing-shaped element |
Country Status (10)
| Country | Link |
|---|---|
| US (1) | US20060150413A1 (en) |
| EP (1) | EP1644147B1 (en) |
| JP (1) | JP2007528789A (en) |
| CN (1) | CN100404158C (en) |
| BR (1) | BRPI0412338A (en) |
| CA (1) | CA2531793A1 (en) |
| DE (1) | DE602004016336D1 (en) |
| NL (1) | NL1023896C2 (en) |
| RU (1) | RU2347638C2 (en) |
| WO (1) | WO2005005077A1 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112238195A (en) * | 2020-10-23 | 2021-01-19 | 浙江三新科技有限公司 | Manufacturing method of wing-shaped blade for fan |
| CN113231540A (en) * | 2021-05-10 | 2021-08-10 | 南通大通宝富风机有限公司 | Method for accurately controlling size of blades of axial flow fan and mixed flow fan |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA2757910C (en) * | 2009-05-28 | 2018-01-16 | Societe Lorraine De Construction Aeronautique | Fabrication method for a composite structural panel for the trailing edge of an aircraft element |
| KR101197089B1 (en) | 2011-04-19 | 2012-11-07 | 한국과학기술원 | The forging device of asymmetry axial product |
| US9428164B2 (en) | 2013-02-28 | 2016-08-30 | Bendix Commercial Vehicle Systems Llc | Valve assembly |
| CN106424440B (en) * | 2016-11-29 | 2018-06-29 | 中国直升机设计研究所 | A kind of helicopter inlet sheet metal component forming method |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3045327A (en) * | 1957-03-04 | 1962-07-24 | Stalker Corp | Fabrication of blades for compressors, turbines and the like |
| US3057393A (en) * | 1957-06-03 | 1962-10-09 | Stalker Corp | Fabrication of blade blanks |
| GB856473A (en) * | 1959-04-01 | 1960-12-14 | John Oliver Creek | Method and apparatus for forming sheet metal blade sections |
| DE1137710B (en) * | 1960-05-23 | 1962-10-11 | Westinghouse Electric Corp | Device for shaping profiled bodies, in particular profiled blades |
| US4531270A (en) * | 1984-06-13 | 1985-07-30 | United Technologies Corporation | Method for the manufacture of metal vanes for turbomachinery |
| JPH08290497A (en) * | 1995-04-20 | 1996-11-05 | Nippon Steel Corp | Wing type honeycomb panel and its manufacture |
| JPH10272527A (en) * | 1997-03-31 | 1998-10-13 | Hitachi Ltd | Manufacture of streamline louver made of steel sheet |
| JP2000326030A (en) * | 1999-05-24 | 2000-11-28 | Hitachi Ltd | Method of manufacturing hollow member |
| JP2001259742A (en) * | 2000-03-16 | 2001-09-25 | Hitachi Ltd | Method for manufacturing hollow member |
| US6675624B2 (en) * | 2000-07-13 | 2004-01-13 | Fokker Aerostructures B.V. | Method and device for producing a double-curved sheet-like object by means of stretch-forming |
-
2003
- 2003-07-11 NL NL1023896A patent/NL1023896C2/en not_active IP Right Cessation
-
2004
- 2004-07-08 DE DE602004016336T patent/DE602004016336D1/en not_active Expired - Fee Related
- 2004-07-08 EP EP04748719A patent/EP1644147B1/en not_active Expired - Lifetime
- 2004-07-08 BR BRPI0412338-7A patent/BRPI0412338A/en not_active IP Right Cessation
- 2004-07-08 RU RU2006100307/02A patent/RU2347638C2/en not_active IP Right Cessation
- 2004-07-08 CA CA002531793A patent/CA2531793A1/en not_active Abandoned
- 2004-07-08 CN CNB2004800197993A patent/CN100404158C/en not_active Expired - Fee Related
- 2004-07-08 US US10/563,368 patent/US20060150413A1/en not_active Abandoned
- 2004-07-08 JP JP2006520130A patent/JP2007528789A/en active Pending
- 2004-07-08 WO PCT/NL2004/000493 patent/WO2005005077A1/en active Application Filing
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112238195A (en) * | 2020-10-23 | 2021-01-19 | 浙江三新科技有限公司 | Manufacturing method of wing-shaped blade for fan |
| CN113231540A (en) * | 2021-05-10 | 2021-08-10 | 南通大通宝富风机有限公司 | Method for accurately controlling size of blades of axial flow fan and mixed flow fan |
Also Published As
| Publication number | Publication date |
|---|---|
| RU2347638C2 (en) | 2009-02-27 |
| RU2006100307A (en) | 2006-07-10 |
| WO2005005077A1 (en) | 2005-01-20 |
| EP1644147B1 (en) | 2008-09-03 |
| BRPI0412338A (en) | 2006-09-05 |
| CN100404158C (en) | 2008-07-23 |
| CA2531793A1 (en) | 2005-01-20 |
| NL1023896C2 (en) | 2005-01-12 |
| US20060150413A1 (en) | 2006-07-13 |
| JP2007528789A (en) | 2007-10-18 |
| DE602004016336D1 (en) | 2008-10-16 |
| EP1644147A1 (en) | 2006-04-12 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104870118B (en) | Punch components, its manufacture method and manufacture device | |
| CN104364074B (en) | For forming adjustable die and the method for tubular torsion beam parts | |
| CN1644264A (en) | High-pressure forming method in tubular member for lowering forming pressure | |
| KR101579028B1 (en) | Method for manufacturing closed-structure part and apparatus for the same | |
| CN1827289A (en) | Forging and rotary extrusion forming process for aluminium alloy wheel | |
| CN114173951B (en) | Method for producing press-formed article | |
| KR101443990B1 (en) | Bent member and method for manufacturing same | |
| KR20120054055A (en) | Curved closed-section structural component and method for manufacturing same | |
| CN1822909A (en) | Method for the production of a semi-finished product for a wing-shaped element | |
| CN109689243A (en) | Method and apparatus for producing the molding especially board member with flange | |
| JP3824850B2 (en) | Multistage press forming method | |
| CN113874134B (en) | Method for manufacturing press member and die for shape correction | |
| CN206382845U (en) | A kind of shape synchronous forming system | |
| KR102545155B1 (en) | Press formimg method | |
| WO2019069631A1 (en) | Torsion beam manufacturing method and torsion beam manufacturing device | |
| KR102545162B1 (en) | Press forming method | |
| CN1247342C (en) | Automotive plate mfg. method | |
| CN1528538A (en) | Fixed roll radian-change bending-point position cold-bending shaping process | |
| KR101234112B1 (en) | Method reducing spri ngback of body panel of motor vehicle using Upform method | |
| JP7476935B2 (en) | Manufacturing method of press-molded products | |
| CN1247336C (en) | Integrated forming manufacture method of seamless pipe for gas insulating equipment | |
| RU2313416C2 (en) | Method for making hollow thin-wall parts | |
| WO2021241024A1 (en) | Press-forming method | |
| CN214645829U (en) | Z-shaped partition frame forming compression roller mechanism | |
| JP7522994B2 (en) | Method for manufacturing press parts, sheet material for press molding, die for preformed shape molding, and program |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20080723 Termination date: 20100708 |