BRPI0412338A - method for producing a semi-finished product for a wing shaped element, and wing shaped element - Google Patents
method for producing a semi-finished product for a wing shaped element, and wing shaped elementInfo
- Publication number
- BRPI0412338A BRPI0412338A BRPI0412338-7A BRPI0412338A BRPI0412338A BR PI0412338 A BRPI0412338 A BR PI0412338A BR PI0412338 A BRPI0412338 A BR PI0412338A BR PI0412338 A BRPI0412338 A BR PI0412338A
- Authority
- BR
- Brazil
- Prior art keywords
- semi
- sheet
- finished product
- shaped element
- conformer
- Prior art date
Links
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
"MéTODO PARA A PRODUçãO DE UM PRODUTO SEMI-ACABADO PARA UM ELEMENTO EM FORMA DE ASA, E, ELEMENTO EM FORMA DE ASA". Um método para a produção de um produto semi-acabado (13) para um elemento em forma de asa (15) tendo, em seção transversal, uma borda dianteira (2), uma borda traseira (14) e uma parede de fundo arqueada (3) e uma parede de topo arqueada (4) que se estendem alguma distância separadamente entre a borda dianteira (2) e a borda traseira (14), inclui as etapas seguintes de: dobrar a folha (1) com a formação de dois painéis (3, 4) como também uma região curvada (2), em que os painéis (3, 4) se juntam, colocar um conformador (10) na folha dobrada (1) com a borda dianteira do conformador (9) posicionada na região curvada (2), forçar o membro de pressão (8) em direção a uma almofada de borracha (7) com a folha dobrada (1) encerrada entre eles e deformar dita folha entre o conformador (10) e a almofada de borracha (7), colocar a folha conformada (F) em uma prensa de borracha provida com um bloco de fundo tendo uma cavidade (16), que tem uma forma que corresponde pelo menos aproximadamente à forma externa de uma das paredes (3, 4) da folha conformada (P), pressionar a folha conformada (F) com o conformador (10) entre o bloco de fundo (11) e um tapete de borracha (12), remover o produto semi-acabado (13) da prensa de borracha."METHOD FOR PRODUCING A SEMI-FINISHED PRODUCT FOR A WING ELEMENT, AND, WING ELEMENT". A method for producing 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) extending some distance separately between the front edge (2) and the rear edge (14), includes the following steps of: folding the sheet (1) to form two panels (3, 4) as well as a curved region (2), in which the panels (3, 4) join, place a conformer (10) on the folded sheet (1) with the front edge of the conformer (9) positioned in the region. bent (2), force the pressure member (8) towards a rubber pad (7) with the folded sheet (1) enclosed therebetween and deform said sheet between the conformer (10) and the rubber pad (7 ), place the shaped sheet (F) in a rubber press provided with a bottom block having a cavity (16), which has a shape corresponding at least to near the outer shape of one of the walls (3, 4) of the shaped sheet (P), pressing the shaped sheet (F) with the conformer (10) between the bottom block (11) and a rubber mat (12), remove the semi-finished product (13) from the rubber press.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NL1023896A NL1023896C2 (en) | 2003-07-11 | 2003-07-11 | Method for manufacturing a semi-finished product for a wing-shaped element. |
PCT/NL2004/000493 WO2005005077A1 (en) | 2003-07-11 | 2004-07-08 | Method for the production of a semi-finished product for a wing-shaped element |
Publications (1)
Publication Number | Publication Date |
---|---|
BRPI0412338A true BRPI0412338A (en) | 2006-09-05 |
Family
ID=34056982
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0412338-7A BRPI0412338A (en) | 2003-07-11 | 2004-07-08 | method for producing a semi-finished product for a wing shaped element, and 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) |
Families Citing this family (6)
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 |
CN112238195B (en) * | 2020-10-23 | 2022-07-26 | 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 |
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
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 |
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 |
CN1822909A (en) | 2006-08-23 |
DE602004016336D1 (en) | 2008-10-16 |
EP1644147A1 (en) | 2006-04-12 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B08F | Application fees: application dismissed [chapter 8.6 patent gazette] |
Free format text: REFERENTE AS 6A, 7A E 8A ANUIDADES. |
|
B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] |
Free format text: REFERENTE AO DESPACHO 8.6 PUBLICADO NA RPI 2159 DE 22/05/2012. |