DE102004035902B3 - Ring segment repeller used in wind power technology, aircraft manufacture and in ship building comprises thin-walled circular or elliptical ring segments formed as angle-adjusted repeller elements rotating about a rotational axis - Google Patents
Ring segment repeller used in wind power technology, aircraft manufacture and in ship building comprises thin-walled circular or elliptical ring segments formed as angle-adjusted repeller elements rotating about a rotational axis Download PDFInfo
- Publication number
- DE102004035902B3 DE102004035902B3 DE102004035902A DE102004035902A DE102004035902B3 DE 102004035902 B3 DE102004035902 B3 DE 102004035902B3 DE 102004035902 A DE102004035902 A DE 102004035902A DE 102004035902 A DE102004035902 A DE 102004035902A DE 102004035902 B3 DE102004035902 B3 DE 102004035902B3
- Authority
- DE
- Germany
- Prior art keywords
- repeller
- gyration
- ring
- segment
- horizontal
- 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
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D5/00—Other wind motors
-
- 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
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B10/00—Integration of renewable energy sources in buildings
- Y02B10/30—Wind power
-
- 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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
-
- 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
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/50—Manufacturing or production processes characterised by the final manufactured product
Abstract
Description
Die Nutzung unterschiedlicher Repeller-Formen bei differierender, strömungstechnischer Erfordernisse beispielsweise in Luft bis hin zu flüssigen Medien hat heute eine Vielzahl technologischer Antriebs-Aggregate insbesondere im Hochleistungsbereich hervorgebracht (Windenergie, Flugzeugbau, Schiffsantriebsbau, etc.). Die klassischen Rotorblätter im Windenergiebereich oder die Auftriebsflügel im Flugzeugbau mit ihren Druck- und Saugseiten bis hin zu den Blattspitzen haben den Nachteil der Ausbildung eines strömungsinduzierten Widerstandes durch Druckausgleich an den Flügelblattspitzen. Die Reduzierung bzw. Vermeidung des induzierten Widerstandes ist über die Nutzung von Winglets bzw. Multiwinglets oder auch durch die Nutzung von Split-Wing Loops an den Blattspitzen erfolgreich realisiert worden.The Use of different repeller shapes with different, fluidic Requirements for example in air up to liquid media today has a large number of technological drive units in particular produced in the high-performance sector (wind energy, aircraft construction, marine propulsion, Etc.). The classic rotor blades in the wind energy sector or the buoyancy wings in aircraft construction with their Pressure and suction sides up to the blade tips have the disadvantage the formation of a flow-induced Resistance by pressure equalization at the vane tips. The reduction or avoidance of the induced resistance is over the Use of winglets or multi-winglets or through use from split-wing loops been successfully realized at the blade tips.
Hier
knüpft
die vorliegende Erfindung im ersten Teilschritt an, die dünnwandige,
kreis- oder ellipsenförmige
Ring-Segmente als winkelverstellbare Repeller-Elemente (
Modifikationen
der Repeller-Elemente sind auch nach optischen, ästhetischen Gesichtspunkten mit
einer Innen- und / oder Außenstruktur
möglich (Beispiele
Aufgrund
der physikalischen Symmetrie-Identität zwischen Vorder- und Rückseite
dieses Ring-Segmente-Repeller-Systems erfüllt es auch die Bedingungen
einer strömungsdynamischen
Reziprozität,
die im zweiten Teil der Erfindung durch ein Gyrations-Zentrum zur
Anwendung kommt. Hierbei werden beliebig zahlige Ring-Segmente-Repeller
um ein horizontales wie auch bis hin zu einem vertikalen Gyrationszentrum
mechanisch so zu einer Gyrations-Repeller-Einheit
kreislagig angeordnet und kombiniert, dass die Ring-Segmente-Repeller-Rotations-Achsen
tangential (
Bei
Verwendung verschiedener Gyrations-Repeller-Einheiten durch beliebig
zahlige Ring-Segmente-Repeller in mehrlagigen horizontalen (
Die physikalische Funktionsweise einer Gyrations-Repeller-Einheit ist zu erklären über das Gyrations-Drehmoment durch unterschiedliche Staudruck-Kräfte differierend, rotierender Ring-Segmente-Repeller zusammen mit ihren Gyrations-Führungsstangen-Längen und -Lagen zum Gyrations-Zentrum wie auch über inhomogene Strömungsanteile. Rotationsdynamisch charakteristisch sind dabei die Rotations-Beschleunigungsänderungen der Ring-Segmente-Repeller in Abhängigkeit der Drehposition der Gyrations-Repeller-Einheit zur Strömungsgeschwindigkeit.The physical functioning of a gyration repeller unit to explain about that Gyration torque differing by different dynamic pressure forces, rotating ring segment repeller along with their gyration guide bar lengths and Layers to the gyration center as well as inhomogeneous flow components. Rotational dynamics are characteristic of the rotational acceleration changes of Ring-segment repeller depending the rotational position of the gyration-repeller unit to the flow velocity.
Bezeichnungsliste der Abbildungen:Designation list of pictures:
Ausführungsbeispiele:EXAMPLES
-
1. Ring-Segmente-Repeller mit strömungsphysikalischer
Symmetrie-Identität
zwischen Vorder- und Rückseite
als reziproke Strömungssysteme, dadurch
gekennzeichnet, dass dünnwandige, kreis-
oder ellipsenförmige
Ring-Segmente als winkel-verstellbare Repeller-Elemente (
1(A) ) beliebig zahlig in einer Rotations-Ebene um ihre Drehachse entsprechend angeordnet sind (1(B) ).1. Ring-segment repeller with fluid-physical symmetry identity between front and back as reciprocal flow systems, characterized in that thin-walled, circular or elliptical ring segments as angle-adjustable repeller elements (1 (A) ) are arbitrarily arranged in a rotational plane around their axis of rotation (1 (B) ). -
2. Ring-Segmente-Repeller mit strömungsphysikalischer Symmetrie-Identität zwischen
Vorder- und Rückseite
als reziproke Strömungssysteme nach
Ausführungsbeispiel
1, dadurch gekennzeichnet, dass die Repeller-Elemente auch Innenstrukturen
mit beliebig zahligen Ring-Segmenten enthalten (
2(A) ) und/oder dass die Repeller-Elemente auch Außenstrukturen beliebig zahliger Ring-Segmente aufweisen (2 (B,C)).2. Ring-segment repeller with fluid-physical symmetry identity between front and back as reciprocal flow systems according to Embodiment 1, characterized in that the repeller elements also contain internal structures with any number of ring segments (2 (A) ) and / or that the repeller elements also have external structures of any number of ring segments (2 (B, C)). -
3. Ring-Segmente-Repeller als reziproke Strömungssysteme kombiniert in
Staudruck-Gyrations-Anordnungen nach Ausführungsbeispiel 1 oder 2, dadurch
gekennzeichnet, dass beliebig zahlige Ring-Segmente-Repeller mechanisch
mit Gyrations-Führungsstangen
um ein horizontales wie auch bis hin zu einem vertikalen Gyrations-Zentrum
so zu einer Gyrations-Repeller-Einheit kreislagig angeordnet sind,
dass die Ring-Segmente-Repeller-Drehachsen tangential (
3(A) ) sowie auch bis hin radial (3(B) ) zum Gyrations-Zentrum ausgerichtet sind.3. ring-segment repeller as reciprocal flow systems combined in dynamic pressure gyration arrangements according to embodiment 1 or 2, characterized in that any number of ring-segment repeller mechanically with gyration guide rods to a horizontal as well as to a vertical gyration Center are arranged in a circle to a gyration repeller unit so that the ring-segment-repeller axes of rotation are tangential (3 (A) ) as well as up to radial (3 (B) ) are aligned to the gyration center. -
4. Ring-Segmente-Repeller als reziproke Strömungssysteme kombiniert in
Staudruck-Gyrations-Anordnungen nach Ausführungsbeispiel 3, dadurch gekennzeichnet,
dass verschiedene Gyrations-Repeller-Einheiten durch beliebig zahlige Ring-Segmente-Repeller
mehrlagig horizontal (
4(A) ) wie auch mehrlagig bis hin zu vertikalen Gyrationslagen (4(B) ) der Gyrations-Zentren mechanisch drehbar gekoppelt sind.4. ring-segment repeller as a reciprocal flow systems combined in dynamic pressure gyration arrangements according to Embodiment 3, characterized in that various gyration repeller units by any number of ring segment repeaters multilayer horizontal (4 (A) ) as well as multilayered up to vertical gyration layers (4 (B) ) of the gyration centers are mechanically rotatably coupled. - 5. Für alle weiteren, physikalisch reziproken Repeller-Strömungs-Systeme wie nach Ausführungsbeispiel 3 mit den Repeller-Einheiten in Radial- bis Tangential-Ausrichtungen sowie den Gyrations-Einheiten in Horizontal- bis Vertikal-Ausrichtungen und Ausführungsbeispiel 4 mit den mehrlagigen horizontalen bis vertikalen Gyrations-Repeller-Einheiten entstehen auch Staudruck-Gyrations-Drehmoment-Effekte.5. For all other physically reciprocal repeller flow systems as in the embodiment 3 with the repeller units in radial to tangential orientations and the gyration units in horizontal to vertical orientations and embodiment 4 with the multilayer horizontal to vertical gyration repeller units there are also dynamic pressure gyration torque effects.
Claims (6)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102004035902A DE102004035902B3 (en) | 2004-07-19 | 2004-07-19 | Ring segment repeller used in wind power technology, aircraft manufacture and in ship building comprises thin-walled circular or elliptical ring segments formed as angle-adjusted repeller elements rotating about a rotational axis |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102004035902A DE102004035902B3 (en) | 2004-07-19 | 2004-07-19 | Ring segment repeller used in wind power technology, aircraft manufacture and in ship building comprises thin-walled circular or elliptical ring segments formed as angle-adjusted repeller elements rotating about a rotational axis |
Publications (1)
Publication Number | Publication Date |
---|---|
DE102004035902B3 true DE102004035902B3 (en) | 2006-03-02 |
Family
ID=35745917
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE102004035902A Expired - Fee Related DE102004035902B3 (en) | 2004-07-19 | 2004-07-19 | Ring segment repeller used in wind power technology, aircraft manufacture and in ship building comprises thin-walled circular or elliptical ring segments formed as angle-adjusted repeller elements rotating about a rotational axis |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE102004035902B3 (en) |
Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US199550A (en) * | 1878-01-22 | Improvement in screw-propellers | ||
US1851513A (en) * | 1929-05-17 | 1932-03-29 | Holmstrom Axel | Aircraft and watercraft construction |
US1918747A (en) * | 1932-12-22 | 1933-07-18 | Hammarstrom John | Toy windmill |
US3732994A (en) * | 1970-04-09 | 1973-05-15 | Nippon Steel Corp | Apparatus for changing the charge distribution in a vertical furnace |
US4285635A (en) * | 1978-08-23 | 1981-08-25 | Oy Mercantile Ab | Impeller in a centrifugal blower |
EP0364020B1 (en) * | 1988-10-03 | 1992-12-30 | Josef Moser | Rotor for a wind motor |
DE9419221U1 (en) * | 1994-12-01 | 1995-04-20 | Simhan Krishna Dr | Vertical axis wind turbine |
DE19544400A1 (en) * | 1995-11-29 | 1997-06-05 | En Umwelt Beratung E V I | Wind power rotor blade adjuster in light wind |
US5984629A (en) * | 1993-09-25 | 1999-11-16 | Ksb Aktiengesellscaft | Turbo-machine with reduced abrasive wear |
DE10208588A1 (en) * | 2002-02-27 | 2003-09-11 | Kbe Windpower Gmbh | Wind power generator for generating electricity, has stator windings arranged in cowling and magnet elements arranged in radially outer regions of rotor blades |
DE69432523T2 (en) * | 1993-12-14 | 2003-11-06 | Northrop Grumman Corp | ULTRASONIC WING WITH LAMINARY FLOW |
-
2004
- 2004-07-19 DE DE102004035902A patent/DE102004035902B3/en not_active Expired - Fee Related
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US199550A (en) * | 1878-01-22 | Improvement in screw-propellers | ||
US1851513A (en) * | 1929-05-17 | 1932-03-29 | Holmstrom Axel | Aircraft and watercraft construction |
US1918747A (en) * | 1932-12-22 | 1933-07-18 | Hammarstrom John | Toy windmill |
US3732994A (en) * | 1970-04-09 | 1973-05-15 | Nippon Steel Corp | Apparatus for changing the charge distribution in a vertical furnace |
US4285635A (en) * | 1978-08-23 | 1981-08-25 | Oy Mercantile Ab | Impeller in a centrifugal blower |
EP0364020B1 (en) * | 1988-10-03 | 1992-12-30 | Josef Moser | Rotor for a wind motor |
US5984629A (en) * | 1993-09-25 | 1999-11-16 | Ksb Aktiengesellscaft | Turbo-machine with reduced abrasive wear |
DE69432523T2 (en) * | 1993-12-14 | 2003-11-06 | Northrop Grumman Corp | ULTRASONIC WING WITH LAMINARY FLOW |
DE9419221U1 (en) * | 1994-12-01 | 1995-04-20 | Simhan Krishna Dr | Vertical axis wind turbine |
DE19544400A1 (en) * | 1995-11-29 | 1997-06-05 | En Umwelt Beratung E V I | Wind power rotor blade adjuster in light wind |
DE10208588A1 (en) * | 2002-02-27 | 2003-09-11 | Kbe Windpower Gmbh | Wind power generator for generating electricity, has stator windings arranged in cowling and magnet elements arranged in radially outer regions of rotor blades |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE69914134T2 (en) | Wheel | |
EP2468628B1 (en) | Hybrid rotor | |
DE102004019620B4 (en) | Flow-controlled wind turbine | |
EP2035694B1 (en) | Rotor hub of a wind energy plant | |
WO1992021878A1 (en) | Process and installation for producing useable energy from parallel flows | |
DE19931035A1 (en) | Rotor with split rotor blade | |
CH700332B1 (en) | Wind Turbine. | |
DE102011055515A1 (en) | Propeller arrangement, in particular for watercraft | |
DE7005689U (en) | FAN. | |
EP1714869B1 (en) | Lifting surface with improved separation behaviour under strongly variable angle of incidence | |
DE2652642C2 (en) | ||
DE19941323A1 (en) | Turbo engine with improved phase mixing to pump poli-phase crude oil flow has beads in flow channels to generate turbulent eddy flow to mix liquid and gaseous phases | |
DE102004035902B3 (en) | Ring segment repeller used in wind power technology, aircraft manufacture and in ship building comprises thin-walled circular or elliptical ring segments formed as angle-adjusted repeller elements rotating about a rotational axis | |
AT514149B1 (en) | Wind power module | |
WO2021048230A1 (en) | Ducted-fan engine with at least one torque stage | |
DE202018006760U1 (en) | swirl element | |
DE3047501C2 (en) | Wind turbine | |
DE102007057077A1 (en) | Rotor for use as e.g. ship rotor, has annular rotor blade, where blade position is changed between two of vertices with maximum distance from uplift position into down position | |
CH714302B1 (en) | Aerodynamically optimized rotor blade. | |
AT523720B1 (en) | Turbine for a wind power plant and a wind power plant | |
DE102019005750A1 (en) | Airfoil rotor ring for lift and control of missiles. | |
DE102008051953A1 (en) | Optimized drive system for wind power plant in offshore area, has perforated plate cylinder with air deflector plate and spiral sheet metal provided at inner casing sides, where air deflector plate longitudinally runs at outer casing sides | |
DE102013005917A1 (en) | Rotary discs to increase the efficiency of aerodynamic profiles | |
DE202016001030U1 (en) | wing | |
DE102021004804B3 (en) | Aerodynamic drive unit |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
8100 | Publication of the examined application without publication of unexamined application | ||
8322 | Nonbinding interest in granting licences declared | ||
8364 | No opposition during term of opposition | ||
R119 | Application deemed withdrawn, or ip right lapsed, due to non-payment of renewal fee |
Effective date: 20120201 |