WO1984001982A1 - Application d'une force excentrique centrifuge unidirectionnelle - Google Patents

Application d'une force excentrique centrifuge unidirectionnelle Download PDF

Info

Publication number
WO1984001982A1
WO1984001982A1 PCT/US1983/001723 US8301723W WO8401982A1 WO 1984001982 A1 WO1984001982 A1 WO 1984001982A1 US 8301723 W US8301723 W US 8301723W WO 8401982 A1 WO8401982 A1 WO 8401982A1
Authority
WO
WIPO (PCT)
Prior art keywords
spinning
wheel
liquid
mass
eccentrically placed
Prior art date
Application number
PCT/US1983/001723
Other languages
English (en)
Inventor
Friedrich O W Arntz
Original Assignee
Friedrich O W Arntz
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 Friedrich O W Arntz filed Critical Friedrich O W Arntz
Priority to AU22063/83A priority Critical patent/AU2206383A/en
Publication of WO1984001982A1 publication Critical patent/WO1984001982A1/fr

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
    • F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H99/00—Subject matter not provided for in other groups of this subclass
    • 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
    • F03G3/00—Other motors, e.g. gravity or inertia motors

Definitions

  • This invention relates to a new transport conveyance propelling device. It is common in transport conveyances other than surface mode to have them held aloft by effects of rocket or jet engine thrust or airplane engine use in conjunction with the option of aerodynamics.
  • Figure 1 is a cross-sectional frontview of the apparatus in vertical orientation.
  • Figure 2 is a cross section sideview along a line coinciding with the longitudinal axis centerline of the main drive shaft, in vertical orientation.
  • Figure 3 is a partly schematic cross-sectional side-view of the apparatus in horizontal orientation.
  • FIG. 4 is a schematic cross-sectional front view of the apparatus having an additional, optional means of function; that is a pressurized gas ejecting component.
  • the apparatus illustrated comprises a wheel 6 affixed to a wheel shaft 1 which is supported by shaft bearing 2 which are mounted on a support structure 4.
  • shaft drive unit 3 Affixed to wheel shaft 1 and engaged with it is shaft drive unit 3, a means to turn wheel shaft 1, that could be either a hydraulic motor-, electric motor-. or combustion engine motor or steam turbine drive mode.
  • aforesaid wheel drive is hydraulic wherein 26 are the hydraulic supply respectively return lines from hydraulic pump 16 to shaft drive unit 3.
  • 17 is in this case the drive motor for 16.
  • 23 is an arrow denoting the direction of the wheel revolu ⁇ tions.
  • 15 are encapsulation boreholes wheel 6 is equipped with, within a reinforced thickened circular segment 46 along the essentially halfway outer perimeter area of it.
  • 36 is the actual one-directional centrifugal eccentric force applicator unit and is a composite of mass-medium fluid encapsulating segment 7, mass- medium fluid introduction segment 8 and structural guide cage from unit 5 which frame is affixed at it's outer perimeter at appropriate points with guide support wheel 12.
  • 12 are freewheeling on circular guidetracks 29 whereby the composite unit, that is 36 has it's orientation controlled by hydraulic orientation positioning unit 9 which is activated by actuator unit 10 thereby influencing degrees of direction of propulsion on command.
  • Mass- medium-fluid introduction segment unit 8 receives it's mass-medium-fluid 19 by way of having it's mass-medium- fluid ducted from high-pressure recirculating pump 20 through stationary supply line 25 and flexible supply line 13 to mass-medium-fluid distribution header 47. From 47 fluid 19 is pushed into injectorheads 27. 27 are independently supported and held in appropriate alignment by sheathed, hollow guide nipples 43 around which are placed compression springs 31 of appropriate compression which serve to keep 27 pressed against 46
  • wheel 6 slides through 7 and 8 segments with each revolution and thereby it has a certain defined part of it at it's outer perimeter, the location of which is constantly changing with respect to the wheel itself in phased sequence, loaded up with an eccentrically placed mass, wherein- which the thusly placed eccentric weight is kept constant in fixed position, with respect to orientation towards vertical containment assembly vessel frame 14 or as the case may be towards containment assembly vessel frame 42 in the case of ' horizontal drive main shaft orientation, within the revolving wheel.
  • Horizontal containment assembly vessel 42 wherein 6 revolves in an essentially horizontal plane, is equipped with a circular drain collector 35 located underneath wheel 6.
  • 37 is a seal for 1.
  • assembly vessel 14 18 is a funnel shaped drain collector, collecting the ejected portion of 19 and the. smaller interface leakage portion of 19 for recirculation purposes by recirculation pump 20, which is driven by recirculation pump motor 21.
  • 22 is a cooling temperature exchanger component for 19 if 19 is to be liquid mercury or sodium metal. In the event of using molten liquid metal such as molten tin, 22 would be a heating unit.
  • 32 are compression springs for 28 and 30.
  • FIG. 38 is a compressed gas injection segment unit optionally attached to 36 behind 7 for the purpose of a faster and more precisely defined process - of ejection of 19 after the propellant cycle. 38 obtains it's compressed gas supply by flexible supply line 39 from gas compressor 40 driven by gas compressor motor 41. 45 are guide sheaths for guide nipples 44 of 28 and 30. 33 are compressed air release vents for 30 of suitable duct diameter dimension.
  • the propelling drive apparatus in essence is a one-directional sling-shot type operating device wherein however the induced G-forces are directed and channelled into one predetermined direction.
  • the induced G-forces are directed and channelled into one predetermined direction.

Abstract

Dans un engin de transport, tel qu'un avion ou une fusée, piloté en vol par un équipage, l'engin est maintenu en vol et est propulsé premièrement par l'effet aérodynamique et/ou deuxièmement par l'effet d'une poussée ou propulsion au moyen d'une fusée ou d'un réacteur ou d'un moteur d'avion. L'objectif de cette invention consistant à maintenir l'engin de transport propulsé en vol est atteint par l'application d'une force excentrique centrifuge unidirectionnelle. Le procédé consiste à placer une certaine masse (19) en un certain point sur le périmètre d'une roue en rotation (6), cette masse (19) étant placée en une position fixe (8) par rapport à l'ossature structurale (14) de l'engin, et elle y est maintenue dans une position fixe par rapport à l'orientation dans l'ossature de l'engin malgré les révolutions de la roue (6). La masse (19) est placée sur le périmètre de la roue approximativement le long d'une ligne imaginaire reliant le point central de la roue et un point imaginaire dans la direction de déplacement de l'engin. Plusieurs de ces entraînements de propulsion d'engins peuvent être agencés ensemble de manière à améliorer la maniabilité.
PCT/US1983/001723 1982-11-12 1983-11-07 Application d'une force excentrique centrifuge unidirectionnelle WO1984001982A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU22063/83A AU2206383A (en) 1982-11-12 1983-11-07 One directional centrifugal excentric force applicator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA415454 1982-11-12

Publications (1)

Publication Number Publication Date
WO1984001982A1 true WO1984001982A1 (fr) 1984-05-24

Family

ID=4123933

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US1983/001723 WO1984001982A1 (fr) 1982-11-12 1983-11-07 Application d'une force excentrique centrifuge unidirectionnelle

Country Status (2)

Country Link
EP (1) EP0125291A1 (fr)
WO (1) WO1984001982A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1998042982A2 (fr) * 1997-03-25 1998-10-01 Kolb, Alfred Dispositif et procede pour generer une force orientee a partir d'un mouvement de rotation

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR330710A (fr) * 1903-02-20 1903-08-24 Giacomo Casada Moteur basé sur l'application du principe d'archimède
US3584515A (en) * 1969-01-09 1971-06-15 Laszlo B Matyas Propulsion apparatus
US3756086A (en) * 1970-07-28 1973-09-04 Alister R Mc Propulsion system
US4002086A (en) * 1972-06-06 1977-01-11 Rolf Bertil Reinhall Device for automatic correction of unbalance in rapidly rotating machine elements
DE2752757A1 (de) * 1977-11-25 1979-06-28 Josef Gulaif Vakuum-kondensations-temperaturaustausch-vierkreislauf-waermekraftmaschine

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR330710A (fr) * 1903-02-20 1903-08-24 Giacomo Casada Moteur basé sur l'application du principe d'archimède
US3584515A (en) * 1969-01-09 1971-06-15 Laszlo B Matyas Propulsion apparatus
US3756086A (en) * 1970-07-28 1973-09-04 Alister R Mc Propulsion system
US4002086A (en) * 1972-06-06 1977-01-11 Rolf Bertil Reinhall Device for automatic correction of unbalance in rapidly rotating machine elements
DE2752757A1 (de) * 1977-11-25 1979-06-28 Josef Gulaif Vakuum-kondensations-temperaturaustausch-vierkreislauf-waermekraftmaschine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1998042982A2 (fr) * 1997-03-25 1998-10-01 Kolb, Alfred Dispositif et procede pour generer une force orientee a partir d'un mouvement de rotation
WO1998042982A3 (fr) * 1997-03-25 1998-12-17 Kolb Alfred Dispositif et procede pour generer une force orientee a partir d'un mouvement de rotation

Also Published As

Publication number Publication date
EP0125291A1 (fr) 1984-11-21

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