WO1999051491A1 - Objet volant a effet de rotation - Google Patents

Objet volant a effet de rotation Download PDF

Info

Publication number
WO1999051491A1
WO1999051491A1 PCT/YU1998/000013 YU9800013W WO9951491A1 WO 1999051491 A1 WO1999051491 A1 WO 1999051491A1 YU 9800013 W YU9800013 W YU 9800013W WO 9951491 A1 WO9951491 A1 WO 9951491A1
Authority
WO
WIPO (PCT)
Prior art keywords
engine
rotation
platform
flying object
flying
Prior art date
Application number
PCT/YU1998/000013
Other languages
English (en)
Inventor
Srecko Ugrin
Original Assignee
Srecko Ugrin
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 Srecko Ugrin filed Critical Srecko Ugrin
Priority to PCT/YU1998/000013 priority Critical patent/WO1999051491A1/fr
Publication of WO1999051491A1 publication Critical patent/WO1999051491A1/fr

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/001—Flying saucers

Definitions

  • the patent belongs to the field of flying and to a flying objects driven by an engine and used for transport of people and loads and for other purposes. It relates to achievement of effects in tremendous increase of velocity, in minimizing spending of energy, in increasing capability of loading and in enlarging a moved distance without landing.
  • the patent solves four main problems which are present in functioning the flying objects driven by engine, i.e. : 1 ) - a significant reduction of energy spent in motion,
  • the construction of the contemporary kinds of aircraft driven with engine is based on effects of a jet engine and on effects of rotating propellers.
  • the parts of the body of contemporary aircraft remain in fixed position during a flying.
  • a term the body relates here to all walls of the aircraft and a volume closed by them which is suitable for placement an engine, other technical devices, a load and accommodation of a crew and a passengers.
  • the body does not include a propellers and a stream of a jet engine.
  • the body remains in fixed position during a flying, i.e. no one part of the body does not change a position during the flying related to its other parts or related to things located within it while they are not in movement. This fixed position of the body represents an essential constitutive characteristic of the aircraft.
  • the body of the flying object with a rotational effect consists of a base and a three pieces which rotates during a flying about a particular axis of rotation.
  • the three rotating pieces of the body rotate parallel to the base.
  • the full efficiency in flying is reached when the base and three rotating pieces of the body are in position which makes a right angle with a direction of an influence of the attraction of gravity (of earth or other planets).
  • This direction of rotational motion is designed here with a terms: horizontal motion, horizontal rotation, horizontally, horizontal position, etc.
  • the flying object possesses two kinds of motion during a flying, i.e. the motion of flying and the rotational motion.
  • the flying object flies horizontally or in other position.
  • An extraordinary special properties arise in the horizontal motion through effects in a field of velocity, capability in loading, in spending of energy and in capability of covering a greater distances without lending in comparison to effects which belong to the contemporary aircraft.
  • the position of the flying object is not horizontal it spends a greater quantity of energy for the rotation of the three parts of the body than in case when it flies horizontally.
  • the effects of the significant reduction of spent fuel in motion is less than in case of the horizontal motion.
  • the flying object is depicted with a figure of drawing.
  • the parts of the flying object which are chosen to be presented in The Figure represents an essential components of the flying object which are of importance for demonstration the efficiency of the applied patent. These fractions of the figure relate to four pieces of the body, three engines for rotation, jet engine, three wheels needed for a start a motion of the flying object and for lending and to an outlet of a jet engine. f) Detailed description of the patent
  • the body of the flying object consist of four pieces, as it is depicted in The Figure, i.e. of the base marked in the figure with 1, the first platform marked with 4, the second platform marked with 5 and the cover marked with 6.
  • the rotation of the first platform marked with 4 is produced with work of engine marked with the engine 1.
  • the rotation of the second platform marked with 5 is effected with work of engine marked with the engine 2.
  • the cover marked with 6 rotates with action of engine marked as the engine 3.
  • the second platform (5) and the cover (6) rotate in the same direction.
  • the first platform (4) rotates in opposite direction of rotation of the second platform (5) and the cover (6).
  • the attributes of such engines are similar to characteristics of those engines which are customary used for other rotational purposes. They are similar to characteristics the engines for trunks, for other vehicles or for vessels, i.e. to attributes of other kinds of engines of the same category. These engines are designated in the further text as the engines for rotation.
  • a power and a force of the engines for rotation are transmitted over an axis to the rotational pieces of the body.
  • the main construction material is metal.
  • the shape of the base and of the platforms is circle.
  • the cover is shaped in the form of a lateral surface of a cone or as a halves of a sphere or a spherical sector, etc. These three rotating parts of the body rotate regularly with the same speed.
  • the engine 1 is fixed to the base (1), the engine 2 to the first platform (4) and the engine 3 to the second platform (5).
  • the rotation of the second platform (5) has a relative static position in comparison to any chosen point in the base (1) or to an exterior point out of the flying object when it is at state of rest, i.e. a distance between this exterior fixed point and the chosen point in the second platform (5) has constant magnitude and it does not change when the flying object is not in motion.
  • the second platform (5) provides conditions for loading and accommodation of people.
  • the people, the load, the jet engine, the engine 3 and the fuel are placed in the second platform (5).
  • the engine 2 is located on the first platform (4).
  • the achievements of the effects of the flying object depend of the level of the reached speed of the rotational parts of the body.
  • the representing speed of the rotating pieces is the speed of the middle point placed in the middle of the distance between an axis and a rim of the platforms and of the cover, i.e. the speed of the middle point on a radius of the platforms and of the cover.
  • the flying object moves by effects produced with the jet engine marked with 8.
  • the outlet of the jet engine is presented in The Figure with a number 3. Its location can be alternatively placed in other parts of the flying object.
  • the wheels are marked in The Figure with number 2.
  • the cover (6) suspended on the vertical axis marked with 7 slides in the groove on the base
  • the flying object for the use as a space ship can have a larger magnitude of the radius than when the flying object is to be used for other purposes.
  • the main efficiency of the subjected flying object originates from the rotational motion of three parts of the body.
  • the patent relates to this effectiveness. With improvements and developments of functions of technical components and the operations between them the final effects of this flying object can reach utmost results but the difference in efficiency obtained in this way will be always significantly smaller in comparison of the difference which appears with the application the main attributes of the patent. Therefore, the improvements of this kind could not be constituted with such patents by which is possible to annul validity of this patent. They will have a meaning of improvement of this patent. In this respect they can relate to all solutions regarding to functioning of the parts of the flying object and to other alternative solutions but not to main characteristics of the flying object.
  • the engine 1 is placed on the first platform (4), the cover (6) consist of more than one piece, only one engine rotates three rotating pieces of the body, the rotations of three parts of the body is produced with connections between rims and not over an axis, the metal is replaced with an another material, etc.
  • the improvements of the patent should be introduced with acquired experiences in its application. For example, if engine 1 is located on the first platform (4) instead on the base (1) the effects of flying will be greater. However, a more precise experiences in a field of stability and vibration of object are necessary for application of such solution.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vehicle Waterproofing, Decoration, And Sanitation Devices (AREA)

Abstract

Les effets obtenus en vol proviennent d'un régime de rotation approprié de trois des quatre parties du corps de l'objet volant, à savoir: la première plate-forme (4), la seconde plate-forme (5) et le couvercle (6), ainsi que de la rotation de la charge incluse dont le moteur à réaction (8), le carburant, les deux moteurs assurant la rotation (moteur 2 et moteur 3), l'équipage et les passagers. Le moteur à réaction (8), le carburant, la charge et le matériel embarqué dans leur totalité, l'équipage et les passagers sont logés sur la seconde plate-forme (5). La seconde plate-forme (5) et le couvercle (6) tournent dans le sens opposés à celui de la première plate-forme (4). L'objet volant est d'une extrême efficacité en termes de vitesse de déplacement, d'économie d'énergie, de charge et de distance franchie sans atterrissage, efficacité qui dépasse de loin celle d'aéronefs actuels à propulsion à réaction ou autre.
PCT/YU1998/000013 1998-04-08 1998-04-08 Objet volant a effet de rotation WO1999051491A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PCT/YU1998/000013 WO1999051491A1 (fr) 1998-04-08 1998-04-08 Objet volant a effet de rotation

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/YU1998/000013 WO1999051491A1 (fr) 1998-04-08 1998-04-08 Objet volant a effet de rotation

Related Child Applications (2)

Application Number Title Priority Date Filing Date
US09601268 A-371-Of-International 2000-07-29
US10/092,671 Continuation-In-Part US20020088899A1 (en) 2000-07-29 2002-03-07 Flying object with a rotational effect

Publications (1)

Publication Number Publication Date
WO1999051491A1 true WO1999051491A1 (fr) 1999-10-14

Family

ID=25559986

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/YU1998/000013 WO1999051491A1 (fr) 1998-04-08 1998-04-08 Objet volant a effet de rotation

Country Status (1)

Country Link
WO (1) WO1999051491A1 (fr)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR68524E (fr) * 1955-09-15 1958-05-02 Aérodyne à ailes multiples
FR2081263A1 (fr) * 1970-03-25 1971-12-03 Pennacchio Pierre
FR2159158A1 (fr) * 1971-11-08 1973-06-22 Jarraud Jean
FR2235071A1 (en) * 1973-06-27 1975-01-24 Coroneos Max Aerial transport machine - has load surrounded by rotating sphere which counter acts effect of gravity
FR2348852A1 (fr) * 1976-04-22 1977-11-18 Delabie Leon Engin anti-pesanteur
WO1985003053A1 (fr) * 1984-01-09 1985-07-18 Bureau Nilos Systems Engin volant
DE29715430U1 (de) * 1997-04-02 1997-12-11 Kähler, Kai, 20355 Hamburg Luftfahrzeug mit Auftriebsaggregat

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR68524E (fr) * 1955-09-15 1958-05-02 Aérodyne à ailes multiples
FR2081263A1 (fr) * 1970-03-25 1971-12-03 Pennacchio Pierre
FR2159158A1 (fr) * 1971-11-08 1973-06-22 Jarraud Jean
FR2235071A1 (en) * 1973-06-27 1975-01-24 Coroneos Max Aerial transport machine - has load surrounded by rotating sphere which counter acts effect of gravity
FR2348852A1 (fr) * 1976-04-22 1977-11-18 Delabie Leon Engin anti-pesanteur
WO1985003053A1 (fr) * 1984-01-09 1985-07-18 Bureau Nilos Systems Engin volant
DE29715430U1 (de) * 1997-04-02 1997-12-11 Kähler, Kai, 20355 Hamburg Luftfahrzeug mit Auftriebsaggregat

Similar Documents

Publication Publication Date Title
Chaisson The Hubble wars: Astrophysics meets astropolitics in the two-billion-dollar struggle over the Hubble Space Telescope
Gamow Gravity
CN104670447A (zh) 带高效短距滑行或垂直起降飞机装置的航母、舰船、水陆喷气跑道
CN103991534A (zh) 一种垂直起降安全飞机
Dick et al. The golden age of the great passenger airships: Graf Zeppelin and Hindenburg
Hartman Adventures in Research: A History of Ames Research Center, 1940-1965
McGowen Helicopters: an illustrated history of their impact
WO1999051491A1 (fr) Objet volant a effet de rotation
CN209126987U (zh) 平台式喷气跑道
US20020088899A1 (en) Flying object with a rotational effect
US11260962B1 (en) Centrifugal-force-propulsion and control system (CFPandCS) and applications
WO1993014973A3 (fr) Vaisseau spatial en forme de soucoupe volante
CN101700809A (zh) 飞碟
CN1876493A (zh) 用碳纤维复合材料制造的可水、陆起落直升飞机
Hollebone The hovercraft: A history
US5839693A (en) Aircraft refueling system
Vesco et al. Man-Made UFOs, 1944-94: Fifty Years of Suppression
RU2214945C1 (ru) Летательный аппарат черемушкина о.в.
US20030155469A1 (en) Flying object with a rotational effect
RU2042576C1 (ru) Летательный аппарат
CN101797980A (zh) 飞碟
CN206187343U (zh) 一种碟形飞行器
CN108116676A (zh) 一种碟形飞行器
Handler et al. Design factors for an economically viable airship
JPH05187348A (ja) 万有斥力飛行装置

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A1

Designated state(s): RU US

AL Designated countries for regional patents

Kind code of ref document: A1

Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LU MC NL PT SE

121 Ep: the epo has been informed by wipo that ep was designated in this application
DFPE Request for preliminary examination filed prior to expiration of 19th month from priority date (pct application filed before 20040101)
WWE Wipo information: entry into national phase

Ref document number: 09601268

Country of ref document: US

122 Ep: pct application non-entry in european phase