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DE19654528A1 - Cascade gyroscope device for providing propulsion force by gravitational field deflection - Google Patents

Cascade gyroscope device for providing propulsion force by gravitational field deflection

Info

Publication number
DE19654528A1
DE19654528A1 DE19654528A DE19654528A DE19654528A1 DE 19654528 A1 DE19654528 A1 DE 19654528A1 DE 19654528 A DE19654528 A DE 19654528A DE 19654528 A DE19654528 A DE 19654528A DE 19654528 A1 DE19654528 A1 DE 19654528A1
Authority
DE
Germany
Prior art keywords
cascade
gravitational field
propulsion force
field deflection
gyroscope device
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Withdrawn
Application number
DE19654528A
Other languages
German (de)
Inventor
Peter Dr Kuemmel
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to DE19654528A priority Critical patent/DE19654528A1/en
Publication of DE19654528A1 publication Critical patent/DE19654528A1/en
Withdrawn legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/409—Unconventional spacecraft propulsion systems
    • 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
    • F03G—SPRING, WEIGHT, INERTIA OR LIKE MOTORS; MECHANICAL-POWER PRODUCING DEVICES OR MECHANISMS, NOT OTHERWISE PROVIDED FOR OR USING ENERGY SOURCES NOT OTHERWISE PROVIDED FOR
    • F03G7/00—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for
    • F03G7/10—Alleged perpetua mobilia
    • F03G7/125—Alleged perpetua mobilia creating a thrust by violating the principle of momentum conservation
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/02—Rotary gyroscopes

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Testing Of Balance (AREA)

Abstract

The device, as in DE P 40 20 888.5, uses counter-rotating masses for each cascade stage, to provide an asymmetrical modification/deflection of the gravitational field. The two-dimensional core mass is rotated at a maximum rate about a roll axis (1) and a perpendicular axis (2), with a counter-rotation in a third perpendicular direction (P) shortly before reaching the maximum loading limit.

Description

Der erfindungsgemäße Schubdraller stellt eine neue Version des Kaskaden­ rotors P 40 20 888.5 dar, vgl. Lit. Nr. 10. Im Schubdraller, Fig. 1, soll pro Kaskade, nämlich einer dreidimensional rotierten Kernmasse, der durch Präzession zustande gekommenen Nickachsenrotation mit maxi­ maler Drehkraft entgegen rotiert werden. Die in Fig. 1 dargestellte Version des erfindungsgemäßen Schubdrallers von der Dimension einer Kaskade, wird in einer Weise angetrieben, daß die Rollachsenrotation der Kernmasse um die Rollachse 1, Fig. 2, kurz vor der Belastbarkeitsgrenze mit maxima­ len Drehzahlen erfolgt. Die Rotation um die Gierachse 2, Fig. 2, soll auch mit maximalen Drehzahlen erfolgen. Der nach der Dreifingerregel durch die Rotationen der Roll- und Gierachse zustande gekommenen Nickachsenrotation als Präzessionswirkung um die Nickachse 3, Fig. 2, soll erfindungsgemäß ebenfalls mit maximalen Drehzahlen entgegen gewirkt werden. Die Richtung der entgegen zu rotierenden Drehkraft ist in Fig. 2 mit dem Pfeil P verdeutlicht. In den Getriebekästen 4 und 5, Fig. 2, wird diese Drehkraft erzeugt. Alle dreidimensional und künstlich erfolgenden Rotationen sollen mit maximalen Drehzahlen, die unmittelbar vor der Belastbarkeit des Materials liegen, ausgeführt werden. Somit wird maximaler Drall als Produkt von rotierender Masse und erfolgender Drehzahlerzielt. Je mehr Rotationsenergie durch die neue, erfindungsge­ mäße Methode in das System des Schubdrallers investiert wird, desto größer wird der erzielte Schub als Vortrieb gemäß Lit. Nr. 10.The thrust twist according to the invention represents a new version of the cascade rotor P 40 20 888.5, cf. No. 10. In the thrust twister, Fig. 1, per cascade, namely a three-dimensionally rotated core mass, is to be rotated counter to the pitch axis rotation caused by precession with maximum torque. The version of the thrust twist according to the invention shown in Fig. 1 of the dimension of a cascade is driven in such a way that the roll axis rotation of the core mass about the roll axis 1 , Fig. 2, takes place shortly before the load limit with maximum speeds. The rotation around the yaw axis 2 , FIG. 2, should also take place at maximum speeds. The pitch axis rotation, which occurs according to the three-finger rule through the rotations of the roll and yaw axis, as a precession effect around the pitch axis 3 , FIG. 2, is also to be counteracted according to the invention with maximum speeds. The direction of the rotational force to be rotated is illustrated by the arrow P in FIG. 2. This torque is generated in the gear boxes 4 and 5 , FIG. 2. All three-dimensional and artificial rotations should be carried out at maximum speeds that are immediately before the material can be loaded. Thus, maximum swirl is achieved as a product of rotating mass and speed. The more rotational energy is invested in the thrust twist system by the new method according to the invention, the greater the thrust achieved as propulsion according to Ref. No. 10.

Literaturliterature

  • 1. KESSLER, A., Impulsgenerator, Offenlegungsschrift 2 6133 442, Anm. v. 29/03/76 in München1. KESSLER, A., pulse generator, laid-open specification 2 6133 442, note from 29/03/76 in Munich
  • 2. KRANICH, M., wie 1,2. KRANICH, M., as 1,
  • 3. KÜMMEL, P., Negative Schwerkraft durch Rotation I, qual. Analyse, 1970, ISBN 3 921 291-00-3,3. KÜMMEL, P., Negative gravity through rotation I, qual. Analysis, 1970, ISBN 3 921 291-00-3,
  • 4. KÜMMEL, P., Negative Schwerkraft durch Rotation II, quant. Analyse, 1971, ISBN: 3 921 291-01-1,4. KÜMMEL, P., Negative gravity through rotation II, quant. Analysis, 1971, ISBN: 3 921 291-01-1,
  • 5. KÜMMEL, P., Antigravitation durch Ablenken von Schwerewellen, 1973, ISBN: 3 921 291-02-X,5. KÜMMEL, P., Antigravity by Deflecting Gravity Waves, 1973, ISBN: 3 921 291-02-X,
  • 6. KÜMMEL, P., Zur Ellipsenbildung beim Foucault-Pendel, 1981, ISBN: 0720-9614, P 17-23,6. KÜMMEL, P., On the ellipse formation at the Foucault pendulum, 1981, ISBN: 0720-9614, P 17-23,
  • 7. KÜMMEL, P., Patentanmeldung zum Thema: Schubkreisel, P 32 34800,2, der Nummer 1775472 v. 20 09 82,7. KÜMMEL, P., patent application on the subject: Schubkreisel, P 32 34800.2, the number 1775472 BC 20 09 82.
  • 8. KÜMMEL, P., Patentanmeldung zum Thema: Kaskadenschubpräzessor, (11), DE 35 23 160, A1, (51), Int. Cl. 4, 64 G1/28, B 64 G1/40, v. 28 06 85,8. KÜMMEL, P., patent application on the subject: cascade thrust processor, (11), DE 35 23 160, A1, (51), Int. Cl. 4, 64 G1 / 28, B 64 G1 / 40, v. 28 06 85,
  • 9. KÜMMEL, P., Schubpräzessor, 1990, 189 pp, 100 Abbildungen, ISSN: 3 921 291-03-8,9. KÜMMEL, P., thrust processor, 1990, 189 pp, 100 figures, ISSN: 3 921 291-03-8,
  • 10. KÜMMEL, P., Patentanmeldung: Kaskadenrotor, P 40 20 888.5, Int. Cl. 5, G 01 C 19/02.10. KÜMMEL, P., patent application: Kaskadenrotor, P 40 20 888.5, Int. Cl. 5, G 01 C 19/02.

Claims (1)

Schubdraller, gemäß P 40 20 888.5 dadurch gekennzeichnet, daß durch zwei­ dimensional und mit maximalen Drehzahlen angetriebene Kernmassen eine Präzession um die dritte Achse zustande kommt, der eine Rotation mit maximalen, kurz vor der Belastungsgrenze liegenden, Drehzahlen gemäß Pfeil P in Fig. 2, entgegengesetzt wird.Thrust twist, in accordance with P 40 20 888.5, characterized in that a precession about the third axis occurs due to two dimensional masses driven at maximum speeds, which is a rotation with maximum speeds shortly before the load limit according to arrow P in Fig. 2, is opposed.
DE19654528A 1996-12-28 1996-12-28 Cascade gyroscope device for providing propulsion force by gravitational field deflection Withdrawn DE19654528A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE19654528A DE19654528A1 (en) 1996-12-28 1996-12-28 Cascade gyroscope device for providing propulsion force by gravitational field deflection

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19654528A DE19654528A1 (en) 1996-12-28 1996-12-28 Cascade gyroscope device for providing propulsion force by gravitational field deflection

Publications (1)

Publication Number Publication Date
DE19654528A1 true DE19654528A1 (en) 1998-07-02

Family

ID=7816326

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19654528A Withdrawn DE19654528A1 (en) 1996-12-28 1996-12-28 Cascade gyroscope device for providing propulsion force by gravitational field deflection

Country Status (1)

Country Link
DE (1) DE19654528A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008044097A1 (en) * 2006-10-10 2008-04-17 Erke Erke Arastirmalari Ve Muhendislik A.S. Gyroscopic apparatus
WO2014185846A1 (en) * 2013-05-16 2014-11-20 Melender Jani Device and method for gyroscopic propulsion

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008044097A1 (en) * 2006-10-10 2008-04-17 Erke Erke Arastirmalari Ve Muhendislik A.S. Gyroscopic apparatus
EA014602B1 (en) * 2006-10-10 2010-12-30 Эрке Эрке Араштырмалары Ве Мюхендислик А. Ш. Gyroscopic device
US8047090B2 (en) 2006-10-10 2011-11-01 Erke Erke Arastirmalari Ve Muhendislik A.S. Method of generating rotation about an output axis and motor for generating rotation about an output axis
CN101506040B (en) * 2006-10-10 2012-05-23 艾尔克能源研究和工程股份公司 Method and motor for producing rotation about an output axis
AP2540A (en) * 2006-10-10 2012-12-20 Erke Erke Arastirmalari Ve Muhandislik As Method of generating rotation about an output axisand motor for generating rotation about an output axis
WO2014185846A1 (en) * 2013-05-16 2014-11-20 Melender Jani Device and method for gyroscopic propulsion

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