DE102008063415A1 - Rotor blade for use as element in drive units for example drive turbines, is connected to rotor and works in connection with gaseous environment medium, where rotor converts centrifugal energy at rotating rotor into up thrust - Google Patents

Rotor blade for use as element in drive units for example drive turbines, is connected to rotor and works in connection with gaseous environment medium, where rotor converts centrifugal energy at rotating rotor into up thrust Download PDF

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Publication number
DE102008063415A1
DE102008063415A1 DE200810063415 DE102008063415A DE102008063415A1 DE 102008063415 A1 DE102008063415 A1 DE 102008063415A1 DE 200810063415 DE200810063415 DE 200810063415 DE 102008063415 A DE102008063415 A DE 102008063415A DE 102008063415 A1 DE102008063415 A1 DE 102008063415A1
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DE
Germany
Prior art keywords
rotor
thrust
works
connection
drive
Prior art date
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Withdrawn
Application number
DE200810063415
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German (de)
Inventor
Manfred Senft
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Individual
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Individual
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Priority to DE200810063415 priority Critical patent/DE102008063415A1/en
Publication of DE102008063415A1 publication Critical patent/DE102008063415A1/en
Withdrawn legal-status Critical Current

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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
    • F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H99/00—Subject matter not provided for in other groups of this subclass

Abstract

The rotor blade is connected to a rotor and works in connection with a gaseous environment medium. The rotor converts centrifugal energy at the rotating rotor into an up thrust independently of environment media. The centrifugal force produces a thrust toward the driving axle of the rotor.

Description

Die Erfindung betrifft ein Rotorblatt für die Verwendung als Element in Antriebseinheiten wie z. B. Antriebs-Turbinen.The The invention relates to a rotor blade for use as an element in drive units such. B. drive turbines.

Rotoren werden derzeit verwendet bei Hubschraubern, in Düsenstrahltriebwerken von Flugzeugen etc.rotors are currently used in helicopters, in aircraft jet engines Etc.

Die beschriebenen Anwendungen mit Rotoren funktionieren aber nur in Verbindung mit einem gasförmigen Umgebungsmedium. Beim Hubschrauber-Rotor ist es die Luft in der sich der Rotor des Hubschraubers dreht. Das gleiche beim Flugzeug-Propellerantrieb.The However, described applications with rotors only work in Compound with a gaseous Surrounding medium. When helicopter rotor, it is the air in the the rotor of the helicopter turns. The same with the aircraft propeller drive.

Bei den Düsenstrahltriebwerken das Plasma des verbrennenden Treibstoffes.at the jet engines the plasma of the burning fuel.

Die im Patentanspruch 1 angegebene Erfindung ist ein Rotor, der unabhängig von Umgebungsmedien die Zentrifugalkräfte am sich drehenden Rotor in Schub umwandelt.The in claim 1 invention is a rotor which is independent of Surrounding media, the centrifugal forces on the rotating rotor converted into thrust.

Er funktioniert also auch im Vakuum.He So it works in a vacuum.

Dieses Ergebnis wird durch folgende Lösung erreicht:
An den äusseren Enden des Rotors sind Masse-Elemente (2 Permanentmagnete beweglich auf einer Achse in sich abstossender Anordnung) angebracht, die bei Drehung des Rotors mit ausreichender Drehzahl so wirken, daß die Rotor-Enden aus der Rotationsebene herausgedrückt werden.This result is achieved by the following solution:
At the outer ends of the rotor mass elements (2 permanent magnets movable on an axis in repelling arrangement) are mounted, which act on rotation of the rotor at a sufficient speed so that the rotor ends are pushed out of the plane of rotation.

Die Zentrifugalkräfte bewirken dann einen Schub in Richtung der Antriebsachse des Rotors.The centrifugal then cause a thrust in the direction of the drive axis of the rotor.

Das gleiche was bei den konventionellen Rotoren durch die oben beschriebenen Medien (Luft, Plasma) bewirkt wird und beim Hubschrauber-Rotor durch Einstellung des Anstellwinkels des Rotorblattes ausgelöst wird.The same thing with the conventional rotors by the ones described above Media (air, plasma) is effected and the helicopter rotor through Adjustment of the angle of attack of the rotor blade is triggered.

Erreichte Vorteile:Achieved benefits:

Die mit der Erfindung erzielten Vorteile bestehen insbesondere darin, daß mit diesem Rotorprinzip Antriebsturbinen gebaut werden können, die lediglich einen Antriebsmotor (z. B.: Elektromotor) benötigen und dann in jeder Umgebung Schub entwickeln können.The particular advantages of the invention are that with This rotor principle drive turbines can be built, the only need a drive motor (eg: electric motor) and then in any environment Can develop thrust.

Für die Entwicklung des Schubes wird dann z. B. also lediglich elektrischer Strom benötigt.For the development the thrust is then z. B. So only electrical power needed.

Anwendungsbeispiele:Application examples:

  • – Antrieb von Satelliten, Raumsonden und anderen Raumfahrzeugen- Drive of satellites, spacecraft and other spacecraft
  • – Antrieb von Booten und UBooten.- Drive of boats and submarines.
  • – Antrieb aller anderen Arten von Fahrzeugen, die durch Schub angetrieben werden können.- Drive all other types of vehicles powered by thrust can be.

Es zeigenIt demonstrate

1 Das Rotorblatt
Im Beispiel eine Aluminiumschiene. Breite 15 mm, Dicke 2 mm, Länge 360 mm 1 The rotor blade
In the example an aluminum rail. Width 15 mm, thickness 2 mm, length 360 mm

2 Ein zusammengebautes Magnetelement 2 An assembled magnetic element

3 Rotorblatt mit montierten Magnetelementen 3 Rotor blade with mounted magnetic elements

4 Explosionszeichnung eines Magnetelementes
Im Beispiel bestehend aus:
1 Rundmessing, Durchmesser 5 mm, Länge 22 mm, M3 Innengewinde
2 Messingschrauben M3 Länge 10 mm
1 Messingscheibe Innendurchmesser 3 mm, Aussendurchmesser 9 mm
2 Neodym Ring-Magnet ⌀ 15–5 × 3 mm (5 mm Innendurchmesser) 4 Exploded view of a magnetic element
In the example consisting of:
1 round brass, diameter 5 mm, length 22 mm, M3 internal thread
2 brass screws M3 length 10 mm
1 brass disc inside diameter 3 mm, outside diameter 9 mm
2 neodymium ring magnet ⌀ 15-5 × 3 mm (5 mm inner diameter)

Claims (1)

Auf das Bauprinzip: Rotorblatt für Antriebe mit Schuberzeugung durch MagnetelementeOn the construction principle: rotor blade for drives with thrust generation by magnetic elements
DE200810063415 2008-12-31 2008-12-31 Rotor blade for use as element in drive units for example drive turbines, is connected to rotor and works in connection with gaseous environment medium, where rotor converts centrifugal energy at rotating rotor into up thrust Withdrawn DE102008063415A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE200810063415 DE102008063415A1 (en) 2008-12-31 2008-12-31 Rotor blade for use as element in drive units for example drive turbines, is connected to rotor and works in connection with gaseous environment medium, where rotor converts centrifugal energy at rotating rotor into up thrust

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE200810063415 DE102008063415A1 (en) 2008-12-31 2008-12-31 Rotor blade for use as element in drive units for example drive turbines, is connected to rotor and works in connection with gaseous environment medium, where rotor converts centrifugal energy at rotating rotor into up thrust

Publications (1)

Publication Number Publication Date
DE102008063415A1 true DE102008063415A1 (en) 2010-07-01

Family

ID=42220791

Family Applications (1)

Application Number Title Priority Date Filing Date
DE200810063415 Withdrawn DE102008063415A1 (en) 2008-12-31 2008-12-31 Rotor blade for use as element in drive units for example drive turbines, is connected to rotor and works in connection with gaseous environment medium, where rotor converts centrifugal energy at rotating rotor into up thrust

Country Status (1)

Country Link
DE (1) DE102008063415A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2568166A1 (en) 2011-09-09 2013-03-13 Nordex Energy GmbH Wind energy assembly rotor blade with a thick profile trailing edge

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2568166A1 (en) 2011-09-09 2013-03-13 Nordex Energy GmbH Wind energy assembly rotor blade with a thick profile trailing edge

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Legal Events

Date Code Title Description
ON Later submitted papers
OR8 Request for search as to paragraph 43 lit. 1 sentence 1 patent law
8110 Request for examination paragraph 44
8105 Search report available
R120 Application withdrawn or ip right abandoned
R120 Application withdrawn or ip right abandoned

Effective date: 20141230