FR3034333A1 - Procede de formation d'orifices dans une piece a paroi mince fabriquee par construction additive de poudres metalliques, et piece a paroi mince ainsi obtenue - Google Patents
Procede de formation d'orifices dans une piece a paroi mince fabriquee par construction additive de poudres metalliques, et piece a paroi mince ainsi obtenue Download PDFInfo
- Publication number
- FR3034333A1 FR3034333A1 FR1552931A FR1552931A FR3034333A1 FR 3034333 A1 FR3034333 A1 FR 3034333A1 FR 1552931 A FR1552931 A FR 1552931A FR 1552931 A FR1552931 A FR 1552931A FR 3034333 A1 FR3034333 A1 FR 3034333A1
- Authority
- FR
- France
- Prior art keywords
- piece
- thin piece
- forming
- metal powders
- thin
- 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.)
- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
- B22F5/04—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine blades
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
- B22F10/20—Direct sintering or melting
- B22F10/28—Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM]
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
- B22F10/30—Process control
- B22F10/36—Process control of energy beam parameters
- B22F10/366—Scanning parameters, e.g. hatch distance or scanning strategy
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
- B22F10/30—Process control
- B22F10/38—Process control to achieve specific product aspects, e.g. surface smoothness, density, porosity or hollow structures
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F12/00—Apparatus or devices specially adapted for additive manufacturing; Auxiliary means for additive manufacturing; Combinations of additive manufacturing apparatus or devices with other processing apparatus or devices
- B22F12/40—Radiation means
- B22F12/41—Radiation means characterised by the type, e.g. laser or electron beam
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/186—Film cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/10—Manufacture by removing material
- F05D2230/13—Manufacture by removing material using lasers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/30—Manufacture with deposition of material
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/30—Manufacture with deposition of material
- F05D2230/31—Layer deposition
- F05D2230/311—Layer deposition by torch or flame spraying
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P10/00—Technologies related to metal processing
- Y02P10/25—Process efficiency
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Automation & Control Theory (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- General Engineering & Computer Science (AREA)
- Health & Medical Sciences (AREA)
- Toxicology (AREA)
- General Health & Medical Sciences (AREA)
- Optics & Photonics (AREA)
- Architecture (AREA)
- Powder Metallurgy (AREA)
- Welding Or Cutting Using Electron Beams (AREA)
- Laser Beam Processing (AREA)
Abstract
L'invention concerne un procédé de formation d'au moins un orifice dans une pièce à paroi mince fabriquée par une construction additive de poudres métalliques au moyen d'un faisceau haute énergie, caractérisé en ce qu'il comprend une étape de délimitation d'au moins une zone non fusionnée par ledit faisceau haute énergie définie par une trajectoire (9) fermée formant un motif (21, 22, 23) présentant au moins deux côtés (31, 32) adjacents formant un angle (α) saillant entre eux, ladite zone non fusionnée formant ledit orifice (8).
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1552931A FR3034333A1 (fr) | 2015-04-03 | 2015-04-03 | Procede de formation d'orifices dans une piece a paroi mince fabriquee par construction additive de poudres metalliques, et piece a paroi mince ainsi obtenue |
PCT/FR2016/050752 WO2016156758A1 (fr) | 2015-04-03 | 2016-04-01 | Procédé de formation d'orifices dans une pièce à paroi mince fabriquée par construction additive de poudres métalliques, et pièce à paroi mince ainsi obtenue |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1552931A FR3034333A1 (fr) | 2015-04-03 | 2015-04-03 | Procede de formation d'orifices dans une piece a paroi mince fabriquee par construction additive de poudres metalliques, et piece a paroi mince ainsi obtenue |
Publications (1)
Publication Number | Publication Date |
---|---|
FR3034333A1 true FR3034333A1 (fr) | 2016-10-07 |
Family
ID=53541757
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1552931A Withdrawn FR3034333A1 (fr) | 2015-04-03 | 2015-04-03 | Procede de formation d'orifices dans une piece a paroi mince fabriquee par construction additive de poudres metalliques, et piece a paroi mince ainsi obtenue |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR3034333A1 (fr) |
WO (1) | WO2016156758A1 (fr) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109277567A (zh) * | 2018-10-16 | 2019-01-29 | 北京星航机电装备有限公司 | 一种异形深腔薄壁舱体的激光近净成形方法 |
CN109622963B (zh) * | 2019-01-09 | 2021-06-15 | 贵州航越科技有限公司 | Slm工艺条件下薄壁零件的制造方法 |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5683600A (en) * | 1993-03-17 | 1997-11-04 | General Electric Company | Gas turbine engine component with compound cooling holes and method for making the same |
US20070007699A1 (en) * | 2003-09-11 | 2007-01-11 | Extrude Hone Corporation | Layered manufactured articles having small-width fluid conduction vents and methods of making same |
US20080223835A1 (en) * | 2007-03-15 | 2008-09-18 | Honeywell International, Inc. | Methods of forming fan-shaped effusion holes in combustors |
US20110123312A1 (en) * | 2009-11-25 | 2011-05-26 | Honeywell International Inc. | Gas turbine engine components with improved film cooling |
US20130280091A1 (en) * | 2012-04-24 | 2013-10-24 | Mark F. Zelesky | Gas turbine engine airfoil impingement cooling |
WO2015069411A1 (fr) * | 2013-11-11 | 2015-05-14 | United Technologies Corporation | Refroidissement de l'extrémité d'une aube de turbine d'un moteur à turbine à gaz |
-
2015
- 2015-04-03 FR FR1552931A patent/FR3034333A1/fr not_active Withdrawn
-
2016
- 2016-04-01 WO PCT/FR2016/050752 patent/WO2016156758A1/fr not_active Application Discontinuation
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5683600A (en) * | 1993-03-17 | 1997-11-04 | General Electric Company | Gas turbine engine component with compound cooling holes and method for making the same |
US20070007699A1 (en) * | 2003-09-11 | 2007-01-11 | Extrude Hone Corporation | Layered manufactured articles having small-width fluid conduction vents and methods of making same |
US20080223835A1 (en) * | 2007-03-15 | 2008-09-18 | Honeywell International, Inc. | Methods of forming fan-shaped effusion holes in combustors |
US20110123312A1 (en) * | 2009-11-25 | 2011-05-26 | Honeywell International Inc. | Gas turbine engine components with improved film cooling |
US20130280091A1 (en) * | 2012-04-24 | 2013-10-24 | Mark F. Zelesky | Gas turbine engine airfoil impingement cooling |
WO2015069411A1 (fr) * | 2013-11-11 | 2015-05-14 | United Technologies Corporation | Refroidissement de l'extrémité d'une aube de turbine d'un moteur à turbine à gaz |
Also Published As
Publication number | Publication date |
---|---|
WO2016156758A1 (fr) | 2016-10-06 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
MX2015017087A (es) | Metodo para producir una junta de soldadura. | |
AR108267A1 (es) | Tubería de acero con alto contenido de manganeso con resistencia a la erosión-corrosión de la zona de soldadura por extensión y método para realizarla | |
MA54718A (fr) | Procédé pour la production d'une tôle d'acier à haute résistance ayant une ductilité et une aptitude au formage améliorées et tôle d'acier ainsi obtenue | |
SG11201810258TA (en) | Laser cutting and machining method for plated steel plate, laser cut-and-machined product, thermal cutting and machining method, thermal cut-and-machined product, surface-treated steel plate, laser cutting method, and laser machining head | |
MY183229A (en) | Method of welding overlapped portion, method of manufacturing overlap-welded member, overlap-welded member, and automotive part | |
EA201650080A3 (ru) | 3d печатающее устройство для изготовления объемного продукта | |
MA53357A (fr) | Procédé de production d'une tôle d'acier revêtue haute résistance présentant une résistance, une ductilité et une aptitude au formage améliorées | |
ZA201803918B (en) | Method for producing a pre-coated metal sheet, with removal of the coating by means of an inclined laser beam, and corresponding metal sheet | |
MA48958A (fr) | Procede de fabrication de pieces d'acier a haute resistance mecanique et ductilite amelioree, et pieces obtenues par ce procede | |
FR3034333A1 (fr) | Procede de formation d'orifices dans une piece a paroi mince fabriquee par construction additive de poudres metalliques, et piece a paroi mince ainsi obtenue | |
PT2176178E (pt) | Forno e processo oxi-combustível para a fusão de matérias vitrificáveis | |
EP3385401A4 (fr) | Acier haute résistance présentant d'excellentes propriétés de capacité antifissures fragiles et de résistance d'amorçage de fissures fragiles de partie de soudage, et son procédé de production | |
MA49585A (fr) | Procédé de production d'une tôle d'acier présentant une résistance, une ductilité et une aptitude au formage améliorées | |
MX2018004069A (es) | Metodo para fabricar un componente soldado, y uso del componente. | |
EA202192805A1 (ru) | Композитный металлический компонент и способ его изготовления | |
MX2015004377A (es) | Metodo de soldadura de combinacion para realizar simultaneamente soldadura de arco de tungsteno y soldadura de arco sumergido. | |
ITUA20162552A1 (it) | Lingottiera, in particolare per la produzione in continuo di lingotti e barre in metallo prezioso tramite forni a tunnel. | |
FR3032898B1 (fr) | Procede de forgeage a haute temperature d'une piece metallique preformee | |
UA116510C2 (uk) | Титановий виливок для гарячої прокатки і спосіб його виготовлення | |
FR3024160B1 (fr) | Procede d'elaboration d`une piece en alliage metallique | |
MY174275A (en) | Methods of making explosive compositions of anfo and heavy anfo | |
UA102031U (ru) | Способ изготовления биметаллов электродуговой сваркой плавким электродом с использованием технологических пазов | |
FR3087379B1 (fr) | Procede de fabrication d’une piece, piece et procede de determination d’un code associe a une piece | |
RU2014110297A (ru) | Способ изготовления наплавленного биметаллического режущего инструмента | |
FR3051697B1 (fr) | Procede de fabrication d'une piece constituee au moins partiellement d'un alliage metallique, et methode d'optimisation. |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 2 |
|
PLSC | Publication of the preliminary search report |
Effective date: 20161007 |
|
RS | Complete withdrawal |
Effective date: 20161017 |
|
CD | Change of name or company name |
Owner name: SAFRAN HELICOPTER ENGINES, FR Effective date: 20170727 |