DE102016001111A1 - Luftwiederstadschirm - Google Patents
Luftwiederstadschirm Download PDFInfo
- Publication number
- DE102016001111A1 DE102016001111A1 DE102016001111.4A DE102016001111A DE102016001111A1 DE 102016001111 A1 DE102016001111 A1 DE 102016001111A1 DE 102016001111 A DE102016001111 A DE 102016001111A DE 102016001111 A1 DE102016001111 A1 DE 102016001111A1
- Authority
- DE
- Germany
- Prior art keywords
- air resistance
- air
- energy consumption
- ultrasonic
- reduce
- 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- Withdrawn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
Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D35/00—Vehicle bodies characterised by streamlining
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- 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
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- 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
- F15D1/002—Influencing flow of fluids by influencing the boundary layer
- F15D1/0065—Influencing flow of fluids by influencing the boundary layer using active means, e.g. supplying external energy or injecting fluid
- F15D1/007—Influencing flow of fluids by influencing the boundary layer using active means, e.g. supplying external energy or injecting fluid comprising surfaces being moved by external supplied energy
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- 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
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- 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
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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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/10—Drag reduction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Apparatuses For Generation Of Mechanical Vibrations (AREA)
- Catching Or Destruction (AREA)
- Transducers For Ultrasonic Waves (AREA)
Abstract
Benuzug der Luftwiederstandschirm ermöglicht, um der Luftwiederstand zu reduziren. Dadurch gekennzeichnet, dass die Luftwiderstandsenkung durch Ultraschallwellen erfolgt. Dabei besteht der Luftwiderstandschirm aus mehreren Ultraschall-Emmitern.Operation of the air resistance screen allows to reduce the air resistance. Characterized in that the air resistance reduction is effected by ultrasonic waves. The air resistance screen consists of several ultrasonic emitters.
Description
Aktuell existieren unterschiedliche Erd- und Lufttransportmittel. Die Entwicklung dieser Technik bewegt sich in Richtung der Sicherheit und muss dabei praktisch und ökonomisch sein. Im Bereich der Ökonomie treffen wir auf großen Energieverbrauch. Eine der Hauptschwierigkeiten des großen Energieverbrauchs stellt der Luftwiderstand dar. Die letzten Entwicklungen der stromlinienförmigen Transportmittel erlauben dieses Hindernis bis zu einem gewissen Grad zu mindern. Allerdings bleibt der Energieverbrauch bei der Überwindung des Luftwiderstandes noch zu hoch. Um die Ökonomie zu steigern, soll die Wirkung des Luftwiderstandes auf das Transportmittel zum Minimum gebracht werden.Currently, there are different means of transporting earth and air. The development of this technique is moving in the direction of safety and must be practical and economical. In the field of economics we meet with great energy consumption. Air resistance is one of the main difficulties of high energy consumption. The recent developments of the streamlined means of transport allow to reduce this obstacle to a certain extent. However, the energy consumption in overcoming the air resistance remains too high. In order to increase the economy, the effect of air resistance on the means of transport should be minimized.
Der die im Patentanspruch 1 angegebenen Erfindung liegt das Problem zugrunde, nämlich den bei den Transportmitteln durch den Luftwiderstand verursachten Energieverbrauch zu reduzieren.The indicated in claim 1 invention is based on the problem, namely to reduce the energy consumption caused by the air resistance in the transport.
Dieses Problem wird durch die im Patentanspruch 1 aufgeführten Merkmale gelöstThis problem is solved by the features listed in claim 1
Die mit der Erfindung erzielten Vorteile bestehen insbesondere darin, dass durch die Minderung des Lüftwiederstandes, der Energiverbrauch erheblich reduziert wird.The advantages achieved by the invention are, in particular, that considerably reduced energy consumption through the reduction of the Lüftwiederstandes.
Ein Ausfuhrungsbeispiel der Erfindung ist in der Zeichnung dargestellt und wird im Folgenden nacher beschrieben. Es zeigen dass der Luftwiederstandsschirm besteht aus mehreren sechseckigen Piezo Elementen (
Claims (2)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102016001111.4A DE102016001111A1 (en) | 2016-02-02 | 2016-02-02 | Luftwiederstadschirm |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102016001111.4A DE102016001111A1 (en) | 2016-02-02 | 2016-02-02 | Luftwiederstadschirm |
Publications (1)
Publication Number | Publication Date |
---|---|
DE102016001111A1 true DE102016001111A1 (en) | 2017-08-17 |
Family
ID=59410119
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE102016001111.4A Withdrawn DE102016001111A1 (en) | 2016-02-02 | 2016-02-02 | Luftwiederstadschirm |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE102016001111A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20210094630A1 (en) * | 2019-09-30 | 2021-04-01 | Subaru Corporation | Airflow adjusting apparatus |
-
2016
- 2016-02-02 DE DE102016001111.4A patent/DE102016001111A1/en not_active Withdrawn
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20210094630A1 (en) * | 2019-09-30 | 2021-04-01 | Subaru Corporation | Airflow adjusting apparatus |
US11639203B2 (en) * | 2019-09-30 | 2023-05-02 | Subaru Corporation | Airflow adjusting apparatus |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
R086 | Non-binding declaration of licensing interest | ||
R119 | Application deemed withdrawn, or ip right lapsed, due to non-payment of renewal fee |