WO2009102227A3 - The direction acceleration principle, the direction acceleration devices and the direction acceleration devices systems - Google Patents

The direction acceleration principle, the direction acceleration devices and the direction acceleration devices systems Download PDF

Info

Publication number
WO2009102227A3
WO2009102227A3 PCT/RO2008/000002 RO2008000002W WO2009102227A3 WO 2009102227 A3 WO2009102227 A3 WO 2009102227A3 RO 2008000002 W RO2008000002 W RO 2008000002W WO 2009102227 A3 WO2009102227 A3 WO 2009102227A3
Authority
WO
WIPO (PCT)
Prior art keywords
acceleration
principle
devices
direction acceleration
base
Prior art date
Application number
PCT/RO2008/000002
Other languages
French (fr)
Other versions
WO2009102227A2 (en
Inventor
Dumitru Ionescu
Original Assignee
Dumitru Ionescu
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 Dumitru Ionescu filed Critical Dumitru Ionescu
Priority to PCT/RO2008/000002 priority Critical patent/WO2009102227A2/en
Publication of WO2009102227A2 publication Critical patent/WO2009102227A2/en
Publication of WO2009102227A3 publication Critical patent/WO2009102227A3/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03HPRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H99/00Subject matter not provided for in other groups of this subclass
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40Arrangements or adaptations of propulsion systems
    • B64G1/408Nuclear spacecraft propulsion
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40Arrangements or adaptations of propulsion systems
    • B64G1/409Unconventional spacecraft propulsion systems

Abstract

The invention refers to raise theoretical some complex movements which generated well determined direction and sense accelerations, resulting an acceleration direction principle, and on the base of the principle it describes an acceleration direction device and with the help of many of these devices, it can conceive devices systems with direction acceleration. The actual theoretical physics on the base of relativity theory studies space, time and body mass in movement in physical inertness systems, without accelerate movement. The direction acceleration principle results from an acceleration general movement of a body and the analyse was extended to two or more bodies with synchronical movement. The terrestrial, naval and aerospace will be the areas with maximal practicability. On the base of the theoretical principle from the present invention, it can conceive many constructive solutions, but I opt for the constructive solution from Fig. 2 a, b which has to the base the theoretical principle from Fig. If where Formule (I). This device is compound from body 1 where are assembly two atomic reactors RA and RA' with identical parameters. In the reactor RA, the toroidal plasm 2, the working fluid from the cooler instalation 4, turbine 8 and current generator is spinning all of them in the same sense but to simplifying the draw i figured only the angular speed ϖ 1. The reactor RA' is identical with the other reactor and for all the elements in rotation enumerate subsequent i figurated only the angular speed ϖ 2 equal, parallel and contrary with angular speed ϖ 1. For all these mass founded in own rotation with angular speeds ϖ 1 or ϖ 2 to produce mass effects all this device is spinning with angular speed ϖ 0 perpendiculary on these two vectors i mean Formule (II) Term of applications can be used a single direction acceleration device or more devices resulting direction acceleration devices systems. In Fig. 3 to a airship is applied a system with three identical devices disposed in the corner of the echilateral triangle which developed the draught force necessary to the flight and a fourth device who produce gravitational local effects upon the men who are inside the ship, for them the subdued acceleration to be maintain to a comfortable level.
PCT/RO2008/000002 2008-02-12 2008-02-12 The direction acceleration principle, the direction acceleration devices and the direction acceleration devices systems WO2009102227A2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PCT/RO2008/000002 WO2009102227A2 (en) 2008-02-12 2008-02-12 The direction acceleration principle, the direction acceleration devices and the direction acceleration devices systems

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/RO2008/000002 WO2009102227A2 (en) 2008-02-12 2008-02-12 The direction acceleration principle, the direction acceleration devices and the direction acceleration devices systems

Publications (2)

Publication Number Publication Date
WO2009102227A2 WO2009102227A2 (en) 2009-08-20
WO2009102227A3 true WO2009102227A3 (en) 2013-08-01

Family

ID=39870587

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/RO2008/000002 WO2009102227A2 (en) 2008-02-12 2008-02-12 The direction acceleration principle, the direction acceleration devices and the direction acceleration devices systems

Country Status (1)

Country Link
WO (1) WO2009102227A2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018095505A1 (en) * 2016-11-22 2018-05-31 Nurgaliyev Zhan B Gravity propulsion based on gravity induction principle

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4509899A (en) * 1983-03-28 1985-04-09 Frederick Larry J Traversing blade-rotary propeller
RU2120061C1 (en) * 1997-07-10 1998-10-10 Илья Иванович Лаптев Plasma engine
US6279314B1 (en) * 1998-12-30 2001-08-28 Societe Nationale D'etude Et De Construction De Moteurs D'aviation-S.N.E.C.M.A. Closed electron drift plasma thruster with a steerable thrust vector
US20040240998A1 (en) * 2001-08-06 2004-12-02 Eric Ashworth Fluid flow control mechanism
WO2007084092A1 (en) * 2006-01-20 2007-07-26 Yuriy Makarovych Lykhovyd Method for producing a thrust force by coriolis forces , a 'gydroturbine ' device for carrying out said method and a transport means based on the 'hydroturbine device'

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4509899A (en) * 1983-03-28 1985-04-09 Frederick Larry J Traversing blade-rotary propeller
RU2120061C1 (en) * 1997-07-10 1998-10-10 Илья Иванович Лаптев Plasma engine
US6279314B1 (en) * 1998-12-30 2001-08-28 Societe Nationale D'etude Et De Construction De Moteurs D'aviation-S.N.E.C.M.A. Closed electron drift plasma thruster with a steerable thrust vector
US20040240998A1 (en) * 2001-08-06 2004-12-02 Eric Ashworth Fluid flow control mechanism
WO2007084092A1 (en) * 2006-01-20 2007-07-26 Yuriy Makarovych Lykhovyd Method for producing a thrust force by coriolis forces , a 'gydroturbine ' device for carrying out said method and a transport means based on the 'hydroturbine device'

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
GORELENKOV N N ET AL: "Toroidal plasma thruster for deep space flights", AIAA JOURNAL AIAA USA, vol. 41, no. 5, May 2003 (2003-05-01), pages 774 - 784, XP008098164, ISSN: 0001-1452 *
HALL T W: "ARTIFICIAL GRAVITY AND THE ARCHITECTURE OF ORBITAL HABITATS", JOURNAL OF THE BRITISH INTERPLANETARY SOCIETY, BRITISH INTERPLANETARY SOCIETY, LONDON, GB, vol. 52, no. 7/08, 1 July 1999 (1999-07-01), pages 290 - 300, XP000828681, ISSN: 0007-084X *

Also Published As

Publication number Publication date
WO2009102227A2 (en) 2009-08-20

Similar Documents

Publication Publication Date Title
Saroj et al. Sliding mode controller design for Twin Rotor MIMO system with a nonlinear state observer
WO2009102227A3 (en) The direction acceleration principle, the direction acceleration devices and the direction acceleration devices systems
Fan et al. Nonlinear observer design for current estimation based on underwater vehicle dynamic model
Isa et al. Motion simulation for propeller-driven USM underwater glider with controllable wings and rudder
CN112607055A (en) Multistage double-super no-drag control method and system in gravitational wave detection displacement mode
Provatidis Design of a propulsion cycle for endless sliding on frictional ground using rotating masses
CN111677810B (en) Passive vibration isolation system for optical payload
Park et al. Cable Suspension and Balance System with Low Support Interference and Vibration for Effective Wind Tunnel Tests
Cristallini The gun tackle revisited
Melnik On-board algorithm for nanosatellite orientation and stabilization system
Lyubimov et al. Attitude control of small spacecraft with allowance made for failures in the system for decreasing angular momentums of flywheels
Li et al. Robust control approach for novel stabilized platform with series elastic actuator
Bernstein Geometry, kinematics, statics and dynamics
Bezglasnyi Realization of program motion of a gyrostat with variable inertia moments
Xiaoguang et al. Numerical investigation on a cable-driven flight simulator with high-G acceleration capability
Li et al. Robust stabilization control for the floated sensor inertial platform
Tombe The Centrifugal Force Argument
Pandey et al. Shear-free gravitational collapse of dust cloud and dark energy
Ming et al. The deployment dynamics of a new mixed space web
Tuveri et al. A Mesh Based Approach for Unconventional Unmanned Airship Added Masses Computation
Alyushin et al. Mathematical model of Stewart platform motion
Zhang et al. Study on Flux-Pinned Interaction between High-Temperature Superconductor and Permanent Magnet and Flux-Pinning’s Self-Stability
Weijie et al. Disturbance estimation and compensation for drag-free satellite based on frequency domain disturbance observer
Shahadat et al. Development of three-axis active vibration isolator using displacement cancellation technique
Sinha A Re-Look at the Classical Laws of Motion

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 08766992

Country of ref document: EP

Kind code of ref document: A2

NENP Non-entry into the national phase

Ref country code: DE

32PN Ep: public notification in the ep bulletin as address of the adressee cannot be established

Free format text: NOTING OF LOSS OF RIGHTS PURSUANT TO RULE 112(1) EPC

122 Ep: pct application non-entry in european phase

Ref document number: 08766992

Country of ref document: EP

Kind code of ref document: A2