WO2009019326A1 - Diminution de la couche limite des effets aerodynamiques - Google Patents
Diminution de la couche limite des effets aerodynamiques Download PDFInfo
- Publication number
- WO2009019326A1 WO2009019326A1 PCT/FR2007/001353 FR2007001353W WO2009019326A1 WO 2009019326 A1 WO2009019326 A1 WO 2009019326A1 FR 2007001353 W FR2007001353 W FR 2007001353W WO 2009019326 A1 WO2009019326 A1 WO 2009019326A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- electrons
- electronic
- gases
- flow
- ions
- 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.)
- Ceased
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15D—FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
- F15D1/00—Influencing flow of fluids
- F15D1/02—Influencing flow of fluids in pipes or conduits
- F15D1/06—Influencing flow of fluids in pipes or conduits by influencing the boundary layer
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15D—FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
- F15D1/00—Influencing flow of fluids
- F15D1/10—Influencing flow of fluids around bodies of solid material
- F15D1/12—Influencing flow of fluids around bodies of solid material by influencing the boundary layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C2230/00—Boundary layer controls
- B64C2230/12—Boundary layer controls by using electromagnetic tiles, fluid ionizers, static charges or plasma
-
- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/10—Drag reduction
Definitions
- Circulations of gases or liquids close to the walls slow down and oppose the flow creating different flow gradients between the center of the flows and the peripheral edges.
- This observation takes the names of drag, shape, profile on the elbows for example, friction on the surfaces of the pipes.
- Interference dragging by changing the pressure or velocity of these fluids inside the duct pipes greatly modifies the flow behavior inside the cavities of the ducts, which is the subject of a correction and flow regulation of liquid or gaseous fluids by the present patent application.
- the dragging forces that oppose flow movements are corrected by a nanotechnology-based method that modifies the adhesion forces that bind fluids and gases to the walls of the ducts.
- the release of the electromagnetic and adhesion forces such as the Van der Waals forces and the polar quantum forces created by the turbulent circulation turbulence of the molecules, give homogeneous fluxes on all the sections of the fluid ducts, whatever the flow rates. the pressures.
- the fluids themselves are free of cohesive forces, tension with the walls that made them less fluid.
- the electronic forces create surface tensions between the molecules themselves and the walls that slow down the fluidity. These forces contribute to turbulence in the flow of gaseous or liquid fluids and in contact with the walls, creating the creation of boundary layers, reducing the flow cross section.
- the variable flow of the fluids in speed or in density varies the flows in proportions breaking any expected linearity of operation, making the operation unstable, unpredictable, chaotic.
- the present application responds directly to these fluctuating problems of the electronic charge nature of fluids and gases applied to the forces of migrating ions and electrons on moving molecules.
- the agitated molecules undergo frictional, frictional, shearing and sliding forces between them and on the wall surfaces of the objects they encounter such as
- the fluctuations of the ions and electrons are of the same order inside the ducts, the pipes, the conduits of the fluids made by all types of materials, for example non-limiting examples of tubes of polymer plastics ig or aluminum, copper, of metal non-limiting examples of products used.
- the nanotechnology-wide world allows by the present process a homogenization, a regularity of the fluidity of the flows of the fluids and the gases on the solid surfaces whatever the flow regimes demanded or usefully undergone, by the apposition at least one electronic component
- the present invention specifically relates to the surface of the moving object or wall of the conduit (s) or tubing used to conduct liquid or gaseous fluids.
- transistors drive the movement of electrons by the polarities and functions of their electron-storage insulating components and the conductors that make it possible to
- the present process by a new electronic component allows an electronic circulation which is to attract absorbing the surplus of electrons and ions, to consume the electrons which agglutinate in mass by the friction on the fluids and the gases and on the walls.
- the apparatus is voracious in ions and electrons by two essential qualities which are an avidity to attract the electrons and the ions by the incense of copper or precious metal like gold having a strong valence of ability to attract electrons and the second quality by the voracity of the electricity piezo which is the transience of eating the energy of ions and electrons, piezo composed of silicas / quartz of different natures oscillating in high frequency by quartz like the diamond or close to it.
- the free ions and electrons migrate to this electronic component that attracts and consumes them by the electricity piezo releasing accumulated and stagnant electrical charges on fluids or flowing gases.
- the electronic component is thus the amalgam of silica / quartz of nature to operate in piezo electricity supplemented with metals or component in lack of electrons and ions attracting them naturally.
- This electronic component called eCRT Electronic Convector Real Time
- metal powders such as titanium, aluminum powder made according to very precise reports by the man of art
- the apparatus is molded according to demand and places available, it varies from a few grams to several hundred grams. Uses on masses to clean important can go to several kilos.
- This molded component can have several composition variants that differ in percentages of different silicas and different metals depending on the specific reactivity required. This component or these components are placed on the pipes or on the moving surfaces with respect to the fluids or gases concerned.
- the component can also be placed inside the ducts in the center of the flows or on the edges of the flows concerned for the desired corrections.
- This product is designed to work without a specific conductor, without an unnecessary electrical wire, because the electronic permeability of air, space or components is sufficient for electronic ion exchange possible in these conditions of nanoscale scales.
- the ionic electron affinity differentials do not require a conducting wire because the ions or electrons jump from component to component of empty ionic or electronic space according to electronic affinity and electron valence gradients specific to each material, until the energy absorption of the electricity piezo product "eCRT" which after attracting these ions and electrons consumes electronic energy in mechanical vibration form.
- the device may be coated with a thin layer of plastic, polymer or paper, cardboard, cosmetic packaging or technical packaging to isolate it from water for example or chemical attack.
- the flows of ions and electrons in the wires are similar to the fluids in the pipes and do not lack similar chaotic functions, which are corrected in the same way. Phase inversions appear to thwart the flow. Corrective frames identify the electronic chaos "over-modulations of multilevel" to delete. These parasitic phenomena create chaotic electron flow functions as in fluids that are well known and this affects in the audio field the sound qualities, which are corrected by this method and devices. Noise alterations due to parasites are now eradicated, cleaned.
- Components and applications of the present method are used to correct and regulate all uses of electrons, moving ions in motion in electronic physics to suppress complex and multi-level phase interference from the computer world to that of the audio-visual and the world of fluids and / or gases in movements useful in the mechanical, aeronautical and space industries, the navy, as well as in the world of food, and also in the world medical. All these applications have a common reason, the self-induced effects of the polarizations of the charges of forces in ionic and electronic movements described in parts as they were stated by Laplace, Maxwell, Lorenz, Van der Walls, and Gauss among others.
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physical Or Chemical Processes And Apparatus (AREA)
- Vibration Prevention Devices (AREA)
- Circuit For Audible Band Transducer (AREA)
- Details Of Audible-Bandwidth Transducers (AREA)
- Apparatuses For Generation Of Mechanical Vibrations (AREA)
- Surface Acoustic Wave Elements And Circuit Networks Thereof (AREA)
- Piezo-Electric Transducers For Audible Bands (AREA)
- Electrophonic Musical Instruments (AREA)
- Stringed Musical Instruments (AREA)
- Soundproofing, Sound Blocking, And Sound Damping (AREA)
Abstract
Description
Claims
Priority Applications (24)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| BRPI0721915-6A BRPI0721915A2 (pt) | 2007-08-08 | 2007-08-08 | Processo de limpar os gases e os fluídos que circulam no interior ou no exterior de objetos de cargas de íons ou de elétrons acumulados por atrito nos fluxos de circulação dos movimentos e aparelho sendo um componente eletrônico. |
| EP07823405A EP2176125A1 (fr) | 2007-08-08 | 2007-08-08 | Diminution de la couche limite des effets aerodynamiques |
| US12/672,483 US20110116202A1 (en) | 2007-08-08 | 2007-08-08 | Reducing the boundary layer of aerodynamic effects |
| CN200780100181A CN101827750A (zh) | 2007-08-08 | 2007-08-08 | 减小空气动力学效应的边界层 |
| JP2010519484A JP2010535992A (ja) | 2007-08-08 | 2007-08-08 | 空気力学的効果の境界層の低減 |
| PCT/FR2007/001353 WO2009019326A1 (fr) | 2007-08-08 | 2007-08-08 | Diminution de la couche limite des effets aerodynamiques |
| CA2695389A CA2695389A1 (fr) | 2007-08-08 | 2007-08-08 | Diminution de la couche limite des effets aerodynamiques |
| KR1020107005133A KR20100061468A (ko) | 2007-08-08 | 2007-08-08 | 공기 역학적 효과의 경계층을 감소시키는 장치 및 방법 |
| CN2008801023677A CN102164818A (zh) | 2007-08-08 | 2008-03-03 | 具有三种关联功能的电子元件 |
| BRPI0815087-7A2A BRPI0815087A2 (pt) | 2007-08-08 | 2008-03-03 | Processo, e aparelho ou componente eletrônico. |
| CA2695310A CA2695310A1 (fr) | 2007-08-08 | 2008-03-03 | Composant electronique a trois fonctions associees |
| JP2010519485A JP2011503838A (ja) | 2007-08-08 | 2008-03-03 | 3つの関連する機能を具備した電子部品 |
| KR1020107005006A KR20100063711A (ko) | 2007-08-08 | 2008-03-03 | 3가지 관련 기능을 가진 전자 컴포넌트 |
| EP08775616A EP2484123A2 (fr) | 2007-08-08 | 2008-03-03 | Composant electronique a trois fonctions associees |
| PCT/FR2008/000273 WO2009019331A2 (fr) | 2007-08-08 | 2008-03-03 | Composant electronique a trois fonctions associees |
| US12/672,477 US20120155758A1 (en) | 2007-08-08 | 2008-03-03 | Electronic component with three associated functions |
| PCT/FR2008/000307 WO2009019332A2 (fr) | 2007-08-08 | 2008-03-10 | Chevalet acoustique de transduction electromagnetique |
| KR1020107004652A KR20100057830A (ko) | 2007-08-08 | 2008-03-10 | 전자기 변환 음향 브릿지 |
| CA2695391A CA2695391A1 (fr) | 2007-08-08 | 2008-03-10 | Chevalet acoustique de transduction electromagnetique |
| JP2010519486A JP2011504303A (ja) | 2007-08-08 | 2008-03-10 | 電磁変換音響ブリッジ |
| CN2008801022871A CN101970293A (zh) | 2007-08-08 | 2008-03-10 | 电磁转换声桥 |
| US12/672,481 US20110110541A1 (en) | 2007-08-08 | 2008-03-10 | Electromagnetic transduction acoustic bridge and related methods |
| BRPI0815083-4A2A BRPI0815083A2 (pt) | 2007-08-08 | 2008-03-10 | Processo e aparelho sendo um cavalete acústico de transdução. |
| EP08775641A EP2176124A2 (fr) | 2007-08-08 | 2008-03-10 | Chevalet acoustique de transduction electromagnetique |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/FR2007/001353 WO2009019326A1 (fr) | 2007-08-08 | 2007-08-08 | Diminution de la couche limite des effets aerodynamiques |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2009019326A1 true WO2009019326A1 (fr) | 2009-02-12 |
Family
ID=39323855
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/FR2007/001353 Ceased WO2009019326A1 (fr) | 2007-08-08 | 2007-08-08 | Diminution de la couche limite des effets aerodynamiques |
| PCT/FR2008/000273 Ceased WO2009019331A2 (fr) | 2007-08-08 | 2008-03-03 | Composant electronique a trois fonctions associees |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/FR2008/000273 Ceased WO2009019331A2 (fr) | 2007-08-08 | 2008-03-03 | Composant electronique a trois fonctions associees |
Country Status (8)
| Country | Link |
|---|---|
| US (3) | US20110116202A1 (fr) |
| EP (3) | EP2176125A1 (fr) |
| JP (3) | JP2010535992A (fr) |
| KR (3) | KR20100061468A (fr) |
| CN (3) | CN101827750A (fr) |
| BR (3) | BRPI0721915A2 (fr) |
| CA (3) | CA2695389A1 (fr) |
| WO (2) | WO2009019326A1 (fr) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2009136011A1 (fr) * | 2008-03-03 | 2009-11-12 | Claude Annie Perrichon | Transparence des optiques et des vitrages |
| WO2010136656A1 (fr) * | 2009-05-25 | 2010-12-02 | Claude Annie Perrichon | Nettoyage de la pollution electromagnetique |
| WO2011018559A3 (fr) * | 2009-08-14 | 2012-08-23 | Claude Annie Perrichon | Autogyre securise stabilise |
| WO2015185806A1 (fr) * | 2014-06-04 | 2015-12-10 | Buendia José | Optimisation de la traînée d'un aéronef |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101827750A (zh) * | 2007-08-08 | 2010-09-08 | 皮赛詹绅股份有限公司 | 减小空气动力学效应的边界层 |
| WO2012076766A2 (fr) * | 2010-12-06 | 2012-06-14 | Claude Annie Perrichon | Technologie piezo integree dans les organes mecanique electrique capot |
| WO2012093206A2 (fr) * | 2011-01-04 | 2012-07-12 | Claude Annie Perrichon | Ajustement mecanique par champ electromagnetique |
| CN103101616A (zh) * | 2011-11-14 | 2013-05-15 | 中国航空工业集团公司沈阳空气动力研究所 | 一种双晶片压电片式振动扰流片装置 |
| WO2013107944A2 (fr) * | 2012-01-17 | 2013-07-25 | Jose Buendia | Regulation des nappes tourbillonnaires |
| WO2014108605A1 (fr) * | 2013-01-11 | 2014-07-17 | Jose Buendia | Regulation thermique par variation du gradient hydrometrique |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2946541A (en) * | 1955-04-11 | 1960-07-26 | John R Boyd | Airfoil fluid flow control system |
| US4080643A (en) * | 1977-04-21 | 1978-03-21 | Dayton-Granger Aviation, Inc. | Aircraft static discharger |
| JPH01288218A (ja) * | 1988-05-17 | 1989-11-20 | Nippon Steel Corp | 発熱体 |
| JPH07284988A (ja) * | 1994-04-20 | 1995-10-31 | Nippon Steel Corp | 高窒素オーステナイト・ステンレス鋼用被覆アーク溶接棒 |
| JPH11276134A (ja) * | 1998-03-26 | 1999-10-12 | Isis:Kk | 食品の鮮度維持方法及び装置 |
| US6198618B1 (en) * | 1998-05-19 | 2001-03-06 | Murata Manufacturing Co., Ltd. | Conductive paste and ceramic electronic part including the same |
| US20020125376A1 (en) * | 2000-02-16 | 2002-09-12 | Karniadakis George Em | Method and apparatus for reducing turbulent drag |
| JP2003171615A (ja) * | 2001-12-06 | 2003-06-20 | Mitsuboshi Belting Ltd | 塗料配合物及び塗膜作製方法 |
| EP1767344A2 (fr) * | 2005-09-19 | 2007-03-28 | The Boeing Company | Recouvrement parafoudre pour une surface étendue |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0413920Y2 (fr) * | 1989-10-17 | 1992-03-30 | ||
| JPH0541297U (ja) * | 1991-10-30 | 1993-06-01 | 京セラ株式会社 | コイル付圧電レシーバー |
| JP2950052B2 (ja) * | 1992-10-15 | 1999-09-20 | トヨタ自動車株式会社 | 圧電素子用導電性ペースト |
| JP4302857B2 (ja) * | 2000-05-16 | 2009-07-29 | 北陸電気工業株式会社 | 圧電発音器 |
| US6671380B2 (en) * | 2001-02-26 | 2003-12-30 | Schlumberger Technology Corporation | Acoustic transducer with spiral-shaped piezoelectric shell |
| EP1548702A1 (fr) * | 2003-12-24 | 2005-06-29 | Interuniversitair Microelektronica Centrum Vzw | Procédé de réglage ultrarapide d'une cellule magnétique et dispositifs associés |
| FR2869754A1 (fr) * | 2004-04-29 | 2005-11-04 | Francois Giry | Acoustique de faible niveau et haute definition |
| CN101502196A (zh) * | 2006-06-02 | 2009-08-05 | 克洛德·安妮·佩里西恩 | 激活电子的管理 |
| CN101827750A (zh) * | 2007-08-08 | 2010-09-08 | 皮赛詹绅股份有限公司 | 减小空气动力学效应的边界层 |
-
2007
- 2007-08-08 CN CN200780100181A patent/CN101827750A/zh active Pending
- 2007-08-08 KR KR1020107005133A patent/KR20100061468A/ko not_active Withdrawn
- 2007-08-08 BR BRPI0721915-6A patent/BRPI0721915A2/pt not_active IP Right Cessation
- 2007-08-08 JP JP2010519484A patent/JP2010535992A/ja active Pending
- 2007-08-08 CA CA2695389A patent/CA2695389A1/fr not_active Abandoned
- 2007-08-08 WO PCT/FR2007/001353 patent/WO2009019326A1/fr not_active Ceased
- 2007-08-08 EP EP07823405A patent/EP2176125A1/fr not_active Withdrawn
- 2007-08-08 US US12/672,483 patent/US20110116202A1/en not_active Abandoned
-
2008
- 2008-03-03 US US12/672,477 patent/US20120155758A1/en not_active Abandoned
- 2008-03-03 CA CA2695310A patent/CA2695310A1/fr not_active Abandoned
- 2008-03-03 JP JP2010519485A patent/JP2011503838A/ja active Pending
- 2008-03-03 KR KR1020107005006A patent/KR20100063711A/ko not_active Withdrawn
- 2008-03-03 EP EP08775616A patent/EP2484123A2/fr not_active Withdrawn
- 2008-03-03 WO PCT/FR2008/000273 patent/WO2009019331A2/fr not_active Ceased
- 2008-03-03 CN CN2008801023677A patent/CN102164818A/zh active Pending
- 2008-03-03 BR BRPI0815087-7A2A patent/BRPI0815087A2/pt not_active IP Right Cessation
- 2008-03-10 KR KR1020107004652A patent/KR20100057830A/ko not_active Withdrawn
- 2008-03-10 EP EP08775641A patent/EP2176124A2/fr not_active Withdrawn
- 2008-03-10 US US12/672,481 patent/US20110110541A1/en not_active Abandoned
- 2008-03-10 CA CA2695391A patent/CA2695391A1/fr not_active Abandoned
- 2008-03-10 BR BRPI0815083-4A2A patent/BRPI0815083A2/pt not_active IP Right Cessation
- 2008-03-10 CN CN2008801022871A patent/CN101970293A/zh active Pending
- 2008-03-10 JP JP2010519486A patent/JP2011504303A/ja active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2946541A (en) * | 1955-04-11 | 1960-07-26 | John R Boyd | Airfoil fluid flow control system |
| US4080643A (en) * | 1977-04-21 | 1978-03-21 | Dayton-Granger Aviation, Inc. | Aircraft static discharger |
| JPH01288218A (ja) * | 1988-05-17 | 1989-11-20 | Nippon Steel Corp | 発熱体 |
| JPH07284988A (ja) * | 1994-04-20 | 1995-10-31 | Nippon Steel Corp | 高窒素オーステナイト・ステンレス鋼用被覆アーク溶接棒 |
| JPH11276134A (ja) * | 1998-03-26 | 1999-10-12 | Isis:Kk | 食品の鮮度維持方法及び装置 |
| US6198618B1 (en) * | 1998-05-19 | 2001-03-06 | Murata Manufacturing Co., Ltd. | Conductive paste and ceramic electronic part including the same |
| US20020125376A1 (en) * | 2000-02-16 | 2002-09-12 | Karniadakis George Em | Method and apparatus for reducing turbulent drag |
| JP2003171615A (ja) * | 2001-12-06 | 2003-06-20 | Mitsuboshi Belting Ltd | 塗料配合物及び塗膜作製方法 |
| EP1767344A2 (fr) * | 2005-09-19 | 2007-03-28 | The Boeing Company | Recouvrement parafoudre pour une surface étendue |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2009136011A1 (fr) * | 2008-03-03 | 2009-11-12 | Claude Annie Perrichon | Transparence des optiques et des vitrages |
| WO2009136012A1 (fr) * | 2008-03-03 | 2009-11-12 | Claude Annie Perrichon | Organisation electronique pour les performances dynamiques chimiques et mecaniques |
| WO2010136656A1 (fr) * | 2009-05-25 | 2010-12-02 | Claude Annie Perrichon | Nettoyage de la pollution electromagnetique |
| WO2011018559A3 (fr) * | 2009-08-14 | 2012-08-23 | Claude Annie Perrichon | Autogyre securise stabilise |
| CN102811904A (zh) * | 2009-08-14 | 2012-12-05 | 克洛德·安妮·佩里西恩 | 稳定的安全旋翼飞机 |
| JP2013501675A (ja) * | 2009-08-14 | 2013-01-17 | ぺリション、クロード、アニー | 安定化された安全なジャイロプレーン |
| WO2015185806A1 (fr) * | 2014-06-04 | 2015-12-10 | Buendia José | Optimisation de la traînée d'un aéronef |
Also Published As
| Publication number | Publication date |
|---|---|
| JP2011503838A (ja) | 2011-01-27 |
| EP2484123A2 (fr) | 2012-08-08 |
| EP2176124A2 (fr) | 2010-04-21 |
| US20110116202A1 (en) | 2011-05-19 |
| KR20100063711A (ko) | 2010-06-11 |
| JP2010535992A (ja) | 2010-11-25 |
| EP2176125A1 (fr) | 2010-04-21 |
| CN101827750A (zh) | 2010-09-08 |
| US20120155758A1 (en) | 2012-06-21 |
| CN102164818A (zh) | 2011-08-24 |
| CA2695310A1 (fr) | 2009-02-12 |
| US20110110541A1 (en) | 2011-05-12 |
| CN101970293A (zh) | 2011-02-09 |
| BRPI0815083A2 (pt) | 2015-02-03 |
| CA2695389A1 (fr) | 2009-02-12 |
| KR20100061468A (ko) | 2010-06-07 |
| BRPI0721915A2 (pt) | 2014-02-25 |
| KR20100057830A (ko) | 2010-06-01 |
| CA2695391A1 (fr) | 2009-02-12 |
| WO2009019331A3 (fr) | 2012-08-30 |
| BRPI0815087A2 (pt) | 2015-02-03 |
| WO2009019331A2 (fr) | 2009-02-12 |
| JP2011504303A (ja) | 2011-02-03 |
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