DE102011102252A1 - Method for adjustment of wing profile used for e.g. cargo sailor, involves moving one wing profile side to other profile side, so that widening side of profile is bulged, and extended through connecting webs - Google Patents
Method for adjustment of wing profile used for e.g. cargo sailor, involves moving one wing profile side to other profile side, so that widening side of profile is bulged, and extended through connecting webs Download PDFInfo
- Publication number
- DE102011102252A1 DE102011102252A1 DE102011102252A DE102011102252A DE102011102252A1 DE 102011102252 A1 DE102011102252 A1 DE 102011102252A1 DE 102011102252 A DE102011102252 A DE 102011102252A DE 102011102252 A DE102011102252 A DE 102011102252A DE 102011102252 A1 DE102011102252 A1 DE 102011102252A1
- Authority
- DE
- Germany
- Prior art keywords
- profile
- wing
- bulged
- extended
- cargo
- 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
- 230000015572 biosynthetic process Effects 0.000 abstract 1
- 239000004744 fabric Substances 0.000 description 1
- 239000011888 foil Substances 0.000 description 1
- 210000004013 groin Anatomy 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/44—Varying camber
- B64C3/48—Varying camber by relatively-movable parts of wing structures
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H9/00—Marine propulsion provided directly by wind power
- B63H9/04—Marine propulsion provided directly by wind power using sails or like wind-catching surfaces
- B63H9/06—Types of sail; Constructional features of sails; Arrangements thereof on vessels
- B63H9/061—Rigid sails; Aerofoil sails
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- 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
- F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor
- F03D1/06—Rotors
- F03D1/0608—Rotors characterised by their aerodynamic shape
- F03D1/0633—Rotors characterised by their aerodynamic shape of the blades
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2240/00—Components
- F05B2240/20—Rotors
- F05B2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05B2240/31—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor of changeable form or shape
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- 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
- Y02E10/72—Wind turbines with rotation axis in wind direction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Sustainable Energy (AREA)
- Life Sciences & Earth Sciences (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Sustainable Development (AREA)
- Ocean & Marine Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Seal Device For Vehicle (AREA)
Abstract
Description
Stand der Technik ist es, eine Flügelprofilform veränderbar zu machen, indem einzelne Profilteile miteinander verbunden werden. Dadurch wird eine einwandfreie Straklinie nicht erreicht. (siehe Blatt Nr. 4)The prior art is to make a wing profile shape changeable by individual profile parts are joined together. As a result, a perfect Straklinie is not achieved. (see sheet no. 4)
Meine Idee ist es, dieses Problehm dadurch zu lösen, indem die gesamte Profilfläche, das Profil direkt mit den beweglichen Halte-Stegen verbunden werden, und dadurch eine nahtlose Profilfläche bildet, und die Stege gleichzeitig eine statische Funktion haben.My idea is to solve this problem by connecting the entire profile surface, the profile directly to the movable support webs, thereby forming a seamless profile surface and at the same time having a static function.
Durch das Verschieben der einen Profilseite zur Anderen, wölbt sich die breiter werdende Seite, und zieht durch den Verbindungs-Stegen, die gegenüberliegende Seite mit sich. Stufenlos, mit strakenden Linien.By moving the one profile side to the other, the widening side bulges, and pulls through the connecting webs, the opposite side with it. Stepless, with firm lines.
Mit dieser Technik kann aus einem symmetrischen Profil ein asymmetrisches Profil erzeugt werden und Umgekehrt. Bzw. aus einem asynnetrischem Profil ein Spiegelbildliches. (siehe Blatt Nr. 3)With this technique an asymmetric profile can be created from a symmetrical profile and vice versa. Respectively. from an asynnetric profile a mirror image. (see sheet no. 3)
Ein 2. Vorteil im Vergleich zum Stand der Technik, ist die Erreichbarkeit eines sehr geringen Flügelgewichtes, verbunden mit einer Profilform-Stabilität, z. B. durch Segel-Tuch.- bzw. Folienbespannung über ein Leistengerüst.A second advantage compared to the prior art is the accessibility of a very low sash weight, combined with a profile shape stability, for. B. by sail cloth.- or foil covering a groin scaffold.
Anwendungsgebiete wären die Windenergie und die Schiffahrt. Die herkömmliche Praxis auf den Frachtenseglern war es/ist es, einzelne Segel mit viel Aufwand und Mühe zu setzen und zu bergen. Durch die Anwendung von leichten, aerodynamischem, profilverstellbaren Flügeln wäre dieses Problehm gelöst. Fields of application would be wind energy and shipping. The traditional practice on the cargo sailors was / is to set individual sails with much effort and effort and recover. The use of lightweight, aerodynamic, profile-adjustable wings would solve this problem.
Bei einem Sturm bietet ein Profil-Flügel in Windfahnenrichtung weniger Wiederstand als ein Großmast ohne Profilflügel.In a storm, a tread wing offers less resistance in wind direction than a main mast without tread wing.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102011102252A DE102011102252A1 (en) | 2011-05-23 | 2011-05-23 | Method for adjustment of wing profile used for e.g. cargo sailor, involves moving one wing profile side to other profile side, so that widening side of profile is bulged, and extended through connecting webs |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102011102252A DE102011102252A1 (en) | 2011-05-23 | 2011-05-23 | Method for adjustment of wing profile used for e.g. cargo sailor, involves moving one wing profile side to other profile side, so that widening side of profile is bulged, and extended through connecting webs |
Publications (1)
Publication Number | Publication Date |
---|---|
DE102011102252A1 true DE102011102252A1 (en) | 2012-11-29 |
Family
ID=47140271
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE102011102252A Ceased DE102011102252A1 (en) | 2011-05-23 | 2011-05-23 | Method for adjustment of wing profile used for e.g. cargo sailor, involves moving one wing profile side to other profile side, so that widening side of profile is bulged, and extended through connecting webs |
Country Status (1)
Country | Link |
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DE (1) | DE102011102252A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3273053A1 (en) * | 2016-07-20 | 2018-01-24 | Siemens Aktiengesellschaft | Rotor blade with structural elements inside |
-
2011
- 2011-05-23 DE DE102011102252A patent/DE102011102252A1/en not_active Ceased
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3273053A1 (en) * | 2016-07-20 | 2018-01-24 | Siemens Aktiengesellschaft | Rotor blade with structural elements inside |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
R086 | Non-binding declaration of licensing interest | ||
R012 | Request for examination validly filed | ||
R016 | Response to examination communication | ||
R079 | Amendment of ipc main class |
Free format text: PREVIOUS MAIN CLASS: B64C0003480000 Ipc: B63H0009000000 |
|
R079 | Amendment of ipc main class |
Free format text: PREVIOUS MAIN CLASS: B64C0003480000 Ipc: B63H0009000000 Effective date: 20130716 |
|
R002 | Refusal decision in examination/registration proceedings | ||
R125 | Request for further processing filed | ||
R126 | Request for further processing allowed | ||
R002 | Refusal decision in examination/registration proceedings | ||
R125 | Request for further processing filed | ||
R126 | Request for further processing allowed | ||
R003 | Refusal decision now final | ||
R409 | Internal rectification of the legal status completed |