FR2653743B1 - Sous-ensemble de pale d'un propulseur et son procede de fabrication. - Google Patents
Sous-ensemble de pale d'un propulseur et son procede de fabrication.Info
- Publication number
- FR2653743B1 FR2653743B1 FR9013570A FR9013570A FR2653743B1 FR 2653743 B1 FR2653743 B1 FR 2653743B1 FR 9013570 A FR9013570 A FR 9013570A FR 9013570 A FR9013570 A FR 9013570A FR 2653743 B1 FR2653743 B1 FR 2653743B1
- Authority
- FR
- France
- Prior art keywords
- propeller
- manufacturing
- assembly
- blade sub
- blade
- 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.)
- Expired - Fee Related
Links
- 238000004519 manufacturing process Methods 0.000 title 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/0025—Producing blades or the like, e.g. blades for turbines, propellers, or wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C44/00—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles
- B29C44/02—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles for articles of definite length, i.e. discrete articles
- B29C44/12—Incorporating or moulding on preformed parts, e.g. inserts or reinforcements
- B29C44/14—Incorporating or moulding on preformed parts, e.g. inserts or reinforcements the preformed part being a lining
- B29C44/16—Incorporating or moulding on preformed parts, e.g. inserts or reinforcements the preformed part being a lining shaped by the expansion of the material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
- B29C70/86—Incorporated in coherent impregnated reinforcing layers, e.g. by winding
- B29C70/865—Incorporated in coherent impregnated reinforcing layers, e.g. by winding completely encapsulated
-
- 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
- Y10T29/49332—Propeller making
-
- 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
-
- 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
- Y10T29/49337—Composite blade
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Moulding By Coating Moulds (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US07/430,836 US5042968A (en) | 1989-11-02 | 1989-11-02 | Propeller blade subassembly and method for making a propeller blade subassembly |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2653743A1 FR2653743A1 (fr) | 1991-05-03 |
| FR2653743B1 true FR2653743B1 (fr) | 1993-11-19 |
Family
ID=23709263
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR9013570A Expired - Fee Related FR2653743B1 (fr) | 1989-11-02 | 1990-10-31 | Sous-ensemble de pale d'un propulseur et son procede de fabrication. |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US5042968A (fr) |
| CA (1) | CA2028970C (fr) |
| FR (1) | FR2653743B1 (fr) |
| GB (1) | GB2237532B (fr) |
Families Citing this family (53)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5127802A (en) * | 1990-12-24 | 1992-07-07 | United Technologies Corporation | Reinforced full-spar composite rotor blade |
| GB9102665D0 (en) * | 1991-02-07 | 1991-03-27 | Lawson Tancred Sir H | The manufacture of turbine blades for wind turbines |
| US5222297A (en) * | 1991-10-18 | 1993-06-29 | United Technologies Corporation | Composite blade manufacture |
| US5392514A (en) * | 1992-02-06 | 1995-02-28 | United Technologies Corporation | Method of manufacturing a composite blade with a reinforced leading edge |
| US5320494A (en) * | 1992-12-22 | 1994-06-14 | United Technologies Corporation | Helicopter rotor blade having a replaceable anhedral tip |
| FR2699498B1 (fr) * | 1992-12-23 | 1995-03-10 | Eurocopter France | Pale en composite thermoplastique, notamment pour rotor arrière caréné d'hélicoptère, et son procédé de fabrication. |
| FR2699499B1 (fr) * | 1992-12-23 | 1995-03-10 | Eurocopter France | Pale en composite thermoplastique, notamment pour rotor arrière caréné d'hélicoptère, et son procédé de fabrication avec étape d'injection. |
| GB2279114A (en) * | 1993-06-15 | 1994-12-21 | Nuaire Ltd | Fan impeller blade |
| US5462409A (en) * | 1994-03-18 | 1995-10-31 | Mcdonnell Douglas Helicopter Co. | Leading edge weight retention assembly for a helicopter rotor |
| US5433002A (en) * | 1994-05-05 | 1995-07-18 | The United States Of America As Represented By The Secretary Of The Navy | Fabrication process for complex composite parts |
| US6352485B1 (en) | 1994-08-12 | 2002-03-05 | Advanced Composites, Inc. | Fiber reinforced molded products and processes |
| US6267399B1 (en) | 1994-08-22 | 2001-07-31 | Advanced Composites, Inc. | Net shape filament winding manufacturing process, articles made therefrom and composite bicycle fork and other components |
| US5609349A (en) * | 1994-08-22 | 1997-03-11 | Advanced Composites, Inc. | Vehicle Fork |
| US6655707B2 (en) | 1994-08-22 | 2003-12-02 | Advanced Composites, Inc. | Net shape filament winding manufacturing process, articles made therefrom and composite bicycle fork and other components |
| RU2139441C1 (ru) * | 1995-05-10 | 1999-10-10 | Центральный научно-исследовательский институт "Электроприбор" | Способ изготовления ветроколеса ветроэнергетической установки |
| FR2740378B1 (fr) * | 1995-10-30 | 1998-01-02 | Eurocopter France | Procede de fabrication d'une pale a pas variable en materiau composite pour rotor d'helicoptere, et pale a pas variable pouvant etre obtenue par un tel procede |
| EP0861145B1 (fr) * | 1995-11-13 | 2003-06-04 | GMIC, Corp. | Fabrication d'outillage par pulverisation thermique |
| US6155784A (en) * | 1997-01-09 | 2000-12-05 | Cartercopters, Llc. | Variable pitch aircraft propeller |
| US5851459A (en) * | 1997-03-31 | 1998-12-22 | Chen; Jason | Method for manufacturing cranks for bicycles |
| DE19959598A1 (de) * | 1999-12-10 | 2001-06-13 | Rolls Royce Deutschland | Verfahren zum Herstellen einer Schaufel einer Strömungsmaschine |
| FR2855811B1 (fr) * | 2003-06-05 | 2005-08-05 | Eurocopter France | Pale de rotor a pas variable, pour rotors carenes, notamment d'helicopteres |
| GB2403987B (en) * | 2003-07-11 | 2006-09-06 | Rolls Royce Plc | Blades |
| GB2410458B (en) * | 2004-01-27 | 2008-09-03 | David Irving | Moulded composite products with cores |
| SE528006C2 (sv) * | 2004-12-23 | 2006-08-01 | Volvo Aero Corp | Statisk gasturbinkomponent och förfarande för reparation av en sådan komponent |
| US7824592B2 (en) * | 2006-09-22 | 2010-11-02 | General Electric Company | Bond line forming method |
| GB2450937B (en) * | 2007-07-13 | 2009-06-03 | Rolls Royce Plc | Component with tuned frequency response |
| EP2203647A1 (fr) * | 2007-10-04 | 2010-07-07 | Bronswerk Heat Transfer B.V. | Ventilateur |
| US8221084B2 (en) | 2008-02-28 | 2012-07-17 | Textron Innovations Inc. | Single-piece propeller and method of making |
| FI20085570A0 (fi) * | 2008-06-10 | 2008-06-10 | Deep Sea Engineering | Menetelmä teknisten komposiittituotteiden valmistamiseksi käsittäen epoksihartsit ja hiilinanoputket |
| US20100122459A1 (en) * | 2008-11-17 | 2010-05-20 | General Electric Company | Method of making wind turbine blade |
| GB2466793B (en) | 2009-01-07 | 2011-11-09 | Ge Aviat Systems Ltd | Composite spars |
| KR101713882B1 (ko) | 2010-01-14 | 2017-03-09 | 센비온 게엠베하 | 윈드 터빈 로터 블레이드 컴포넌트 및 그것을 만드는 방법 |
| US10137542B2 (en) | 2010-01-14 | 2018-11-27 | Senvion Gmbh | Wind turbine rotor blade components and machine for making same |
| DK2402148T3 (da) * | 2010-06-30 | 2014-10-13 | Siemens Ag | Støbningsfremgangsmåde til fremstilling af et arbejdsemne |
| US20120114897A1 (en) * | 2010-11-05 | 2012-05-10 | Ramesh Thiagarajan | Foam Stiffened Structure and Method of Making the Same |
| FR2970943B1 (fr) | 2011-01-31 | 2014-02-28 | Eurocopter France | Pale et procede de fabrication de ladite pale |
| ITRM20110517A1 (it) * | 2011-09-30 | 2013-03-31 | Enel Green Power Spa | Pala per generatore eolico e metodo di assemblaggio di detta pala |
| EP2599714B1 (fr) | 2011-11-30 | 2014-10-08 | Hamilton Sundstrand Corporation | Pale d'hélice dotée d'un adhésif conforme sur l'interface du longeron |
| US9139287B2 (en) * | 2012-06-26 | 2015-09-22 | Hamilton Sundstrand Corporation | Propeller blade with carbon foam spar core |
| CN103507200A (zh) * | 2012-06-29 | 2014-01-15 | 合肥杰事杰新材料股份有限公司 | 一种微孔泡沫复合材料的制备方法及其产品 |
| US10487675B2 (en) * | 2013-02-18 | 2019-11-26 | United Technologies Corporation | Stress mitigation feature for composite airfoil leading edge |
| KR20140147931A (ko) * | 2013-06-19 | 2014-12-31 | 주식회사 제이에스영테크 | 무인항공기용 날개 및 그 제조방법 |
| US9574544B2 (en) | 2013-12-16 | 2017-02-21 | General Electric Company | Methods of manufacturing rotor blade components for a wind turbine |
| US9709030B2 (en) * | 2013-12-16 | 2017-07-18 | General Electric Company | Methods of manufacturing rotor blade components for a wind turbine |
| US9920629B2 (en) * | 2014-02-20 | 2018-03-20 | Hamilton Sundstrand Corporation | Propeller blade and method |
| RU2566816C2 (ru) * | 2014-03-12 | 2015-10-27 | Общество с ограниченной ответственностью "Альбатрос" | Оптическая система и способ освещения поверхности |
| US20150266572A1 (en) * | 2014-03-21 | 2015-09-24 | Hamilton Sundstrand Corporation | Propeller blade having compliant spar core |
| ES2806262T3 (es) * | 2014-06-30 | 2021-02-17 | Gen Electric | Pala de rotor para una turbina eólica y procedimiento de fabricación de un componente de pala de rotor |
| CN104742048B (zh) * | 2015-04-07 | 2017-03-01 | 中国直升机设计研究所 | 一种桨叶夹持机构 |
| JP2020151876A (ja) * | 2019-03-18 | 2020-09-24 | 三菱重工業株式会社 | 複合材翼の成形方法 |
| CN110450951B (zh) * | 2019-07-30 | 2021-07-02 | 北京航空航天大学 | 扑翼飞行器的机翼及扑翼飞行器 |
| CN112406135B (zh) * | 2020-11-06 | 2022-10-25 | 航天海鹰(镇江)特种材料有限公司 | 一种利用气囊吹胀辅助复合材料螺旋桨叶片成型的方法 |
| US12448897B2 (en) * | 2024-01-31 | 2025-10-21 | Rtx Corporation | Gas turbine engine component formed by CMCS and having a compressed insert with tapered ends |
Family Cites Families (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB720800A (en) * | 1952-05-23 | 1954-12-29 | United Aircraft Corp | Improvements in or relating to aeronautical propeller blades |
| US3923421A (en) * | 1974-12-19 | 1975-12-02 | United Technologies Corp | Lightning protected composite helicopter blade |
| FR2381662A1 (fr) * | 1977-02-28 | 1978-09-22 | Aerospatiale | Pale, notamment pour un rotor d'helicoptere, et son procede de fabrication |
| GB2032832B (en) * | 1978-09-16 | 1982-07-28 | Dowty Rotol Ltd | Foam-containing structures |
| BR8105757A (pt) * | 1980-10-02 | 1982-05-25 | United Technologies Corp | Processo pra a producao de um aerofolio |
| US4648921A (en) * | 1980-10-02 | 1987-03-10 | United Technologies Corporation | Method of making fiber reinforced articles |
| GB2105633B (en) * | 1981-08-28 | 1985-07-31 | Dowty Rotol Ltd | Foam-containing structures |
| US4470862A (en) * | 1982-05-27 | 1984-09-11 | United Technologies Corporation | Manufacture of fiber reinforced articles |
| FR2542695B1 (fr) * | 1983-03-18 | 1985-07-26 | Aerospatiale | Helice multipale a pas variable a pale s en materiaux composites demontables individuellement, procede de fabrication de telles pales et pales ainsi realisees |
| IT1161534B (it) * | 1983-10-26 | 1987-03-18 | Agusta Aeronaut Costr | Longherone per pala di elicottero e metodo per la sua realizzazione |
| FR2574752B1 (fr) * | 1984-12-19 | 1987-02-20 | Aerospatiale | Pale pour rotor d'helicoptere en materiau composite multilongeron a caissons de torsion et son procede de fabrication |
| FR2602739B1 (fr) * | 1986-07-28 | 1988-11-18 | Aerospatiale | Pale en materiaux composites, a structure bilongeron et bicaisson, et a revetement stratifies a sandwich de nid d'abeilles, et son procede de fabrication |
| CN1042692A (zh) * | 1988-11-14 | 1990-06-06 | 通用电气公司 | 反转的飞机螺旋桨叶 |
-
1989
- 1989-11-02 US US07/430,836 patent/US5042968A/en not_active Expired - Fee Related
-
1990
- 1990-10-31 CA CA002028970A patent/CA2028970C/fr not_active Expired - Fee Related
- 1990-10-31 FR FR9013570A patent/FR2653743B1/fr not_active Expired - Fee Related
- 1990-11-02 GB GB9023834A patent/GB2237532B/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| CA2028970C (fr) | 1994-07-26 |
| US5042968A (en) | 1991-08-27 |
| FR2653743A1 (fr) | 1991-05-03 |
| GB2237532B (en) | 1993-06-02 |
| GB9023834D0 (en) | 1990-12-12 |
| CA2028970A1 (fr) | 1991-05-03 |
| GB2237532A (en) | 1991-05-08 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ST | Notification of lapse |