FR2527533A1 - VTOL reaction motor aircraft - comprises vertical engine which creates air cushion beneath body of aircraft during take off and landing - Google Patents
VTOL reaction motor aircraft - comprises vertical engine which creates air cushion beneath body of aircraft during take off and landing Download PDFInfo
- Publication number
- FR2527533A1 FR2527533A1 FR8209216A FR8209216A FR2527533A1 FR 2527533 A1 FR2527533 A1 FR 2527533A1 FR 8209216 A FR8209216 A FR 8209216A FR 8209216 A FR8209216 A FR 8209216A FR 2527533 A1 FR2527533 A1 FR 2527533A1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- air cushion
- landing
- vtol
- comprises vertical
- 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- Withdrawn
Links
- 241000243251 Hydra Species 0.000 claims 1
- 210000001015 abdomen Anatomy 0.000 claims 1
- QRXWMOHMRWLFEY-UHFFFAOYSA-N isoniazide Chemical compound NNC(=O)C1=CC=NC=C1 QRXWMOHMRWLFEY-UHFFFAOYSA-N 0.000 claims 1
- 230000035515 penetration Effects 0.000 description 2
- 230000004308 accommodation Effects 0.000 description 1
- 238000005054 agglomeration Methods 0.000 description 1
- 230000002776 aggregation Effects 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 239000000969 carrier Substances 0.000 description 1
- 230000010006 flight Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000000638 solvent extraction Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/001—Flying saucers
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
Abstract
Description
La présente invention concerne l'aéronautique,c'est un appareil aéronef pouvant effectuer un attèrissage et un décollage vertical sur coussin d'air.The present invention relates to aeronautics, it is an aircraft device that can perform a vertical landing and takeoff on an air cushion.
flans les dispositifs de ce genre c'est l'hover craft qui u lui ressemble le plus;et qui sert aux transports maritimes. Mais jusqu'a ce jour aucun aéronef d ce genre n'a existé (exeption faite par l'hélicoptère qui se maut par hélice, lui permettant de monter et descendre verticalement,ainsi que de se déplacer avec peu de passagers à patite vitesse)
L'Aéronaf selon l'invention se caractérise par sa forma aérodynamique circulaire coma un disque conique.D'un profil étudié lui assurant une assise parfaite dans l'air. C'est l'ensemble de ce disque qui constitue ce que l'on appelle sur un avion,une aile.Son bord d'attaque lui assure une pénétration optimum dans l'air,les trajectoires du fluide atmosphérique assurent une constante parfaite et maintient une assiette d'une stabilité parfaite.In devices of this kind, it is the hover craft that most resembles it, and which is used for maritime transport. But to date no aircraft of this kind has existed (except for the helicopter which dies by propeller, allowing it to go up and down vertically, as well as to move with few passengers at speed speed)
The Aeronaf according to the invention is characterized by its circular aerodynamic shape like a conical disc, with a studied profile ensuring a perfect seat in the air. It is the whole of this disc which constitutes what is called on a plane, a wing. Its leading edge ensures an optimum penetration in the air, the trajectories of the atmospheric fluid ensure a perfect constant and maintains a plate of perfect stability.
Par le profil un gain énorme est acquis contre la résistance de l'air,la structure est uniforme est indestructible partiellement. (aucun risque de voir s'arracher un réacteur d'aile).By the profile an enormous gain is acquired against the air resistance, the structure is uniform and partially indestructible. (no risk of having a wing reactor torn off).
Le dispositif de l'invention permet à l'aéronef de décoller verticalement, de stationner an point fixe verticalement,de se poser verticalement,ainsi que de se déplacer dans l'air horizontalement avec une vitesse bien supérieure à celle connue du concorde;ceci dans une stabilité de vol encore jamais atteint jusqu'a ce jour. Ayant également un nombre de passagers important.The device of the invention allows the aircraft to take off vertically, to park at a fixed point vertically, to land vertically, as well as to move in the air horizontally with a speed much higher than that known to concord; this in flight stability never reached until today. Also having a large number of passengers.
Tel qu'il est représ@nté le dispositif comporte:
La structure circulaire et légèrement conique,usiné de façon à laisser plusieurs orifices ouverts pour l'assemblage et les fonctions diverses 14.As shown, the device includes:
The circular and slightly conical structure, machined so as to leave several open holes for assembly and various functions 14.
Un réacteur central 7 lui assure se poussée verticale. Un rotor composé d' hélices à pas variables lui assure sa sustentation par un coussin d'air qui se crée sous le carénage en toute sa forme circulaire 2.A central reactor 7 ensures it is pushed vertically. A rotor made up of variable pitch propellers ensures its lift by an air cushion which is created under the fairing in all its circular shape 2.
Lorsque le coussin d'air est créé sous l'@ l'aéronef, que le réacteur central a ,par sa poussé élevé colui-ci à une altitude déterminé,c'est les réacteurs 3 qui interviennent pour propulser l'aéronef dans une trajectoire horizontale à grande vitesse. When the air cushion is created under the @ the aircraft, that the central reactor has, by its high thrust colui this at a determined altitude, it is the reactors 3 which intervene to propel the aircraft in a trajectory horizontal at high speed.
Lorsque le machine à prise une grande vitesse,les Volets 1 hydrauliques se fermes afin d'assurer une assiette parfaite pour une vitesse plus grande dans l'espace. Un empennage 9 + 12 assure une stabilité et les moyens directionnels dans ltespace. Un aérofrein 8g est conçu pour ralentir l'aéronef, ainsi que l'inversion des forces de propulsions des réacteurs. Lorsque la vitesss se réduit le rotor actionné par ses moteurs C se met en mouvement,pour assurer le coussin d'air qui va sustenter la machine.Le réacteur 7 qui s'est remis en fonctionnement va maintenir selon le désir ,la descente ou le stationnement en altitude désirée.When the machine sets at high speed, the hydraulic Flaps 1 close to ensure a perfect attitude for greater speed in space. A 9 + 12 empennage ensures stability and directional means in space. An 8g airbrake is designed to slow down the aircraft, as well as reversing the propulsion forces of the reactors. When the speed is reduced the rotor actuated by its motors C starts to move, to ensure the air cushion which will support the machine. The reactor 7 which has restarted will maintain, as desired, the descent or parking at desired altitude.
La cellule circulaire 11 permet la réalisation de différentes cabines par cloisonnement,où le logement des passagers. Les logements dans la structure 13 permet le freet,le carburant est logé dans la structure 5,les trains d'attérissages sont aussi logés dans la structure 4.The circular cell 11 allows the realization of different cabins by partitioning, where the accommodation of passengers. The housings in the structure 13 allow the freet, the fuel is housed in the structure 5, the landing gear are also housed in the structure 4.
Les dispositifs,objet de l'invention permettent à cet aéronef des parcours à longues distances très rapide,et d'une sécurité améliorée par rapport aux types d'aéronefs existant.The devices which are the subject of the invention allow this aircraft to travel very long distances very quickly, and with improved safety compared to the types of aircraft existing.
Sa pénétration dans l'air étant plus performante,ainsi que son assise plus conséquente,permot d'obtenir des résultats incomparablent avec ceux connus jusqu'à présent.Its penetration in the air being more efficient, as well as its more substantial seat, allows to obtain incomparable results with those known until now.
Les moyens permettant de se mouvoir aussi bien verticalement,qu'horizonta- lement,élimine de ce fait les approches de terrains à basse altitude,qui produit des nuisances de bruit pour tous les riverains des aéroports.The means making it possible to move both vertically and horizontally, therefore eliminates approaches to terrain at low altitude, which produces noise nuisance for all residents living near airports.
(Plus de manifestations contre le bruit) Codt de revient réduit sur les
Nouveaux aéroports ,plus d'entretient de pistes énormes.(No more noise protests) Reduced cost coding on
New airports, more maintenance of huge runways.
Des vols en charters peuvent s'effectuer dans toutes les destinations possibles,des expéditions peuvent s'effectuer dans tous les coins du globe, dans un maximum de confort.Charter flights can be made to all possible destinations, expeditions can be made to all corners of the globe, in maximum comfort.
En version militaire,la complexité des portes avions s'ammenuisant,des bases peuvent se créer dans le coeur mena des montagnes,sur des platesformes en mer..Le largage des paras peut se faire n'importe où..In the military version, the complexity of aircraft carriers is shrinking, bases can be created in the heart of the mountains, on platforms at sea. The paras can be dropped anywhere.
La sécurité des transports est accrus considérablement. Dans tous les cas l'engin peut se poser dans un champs prés de n'importe qu'akls agglomération. Transport security is increased considerably. In all cases the machine can land in a field near any agglomeration.
Claims (4)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8209216A FR2527533A1 (en) | 1982-05-27 | 1982-05-27 | VTOL reaction motor aircraft - comprises vertical engine which creates air cushion beneath body of aircraft during take off and landing |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8209216A FR2527533A1 (en) | 1982-05-27 | 1982-05-27 | VTOL reaction motor aircraft - comprises vertical engine which creates air cushion beneath body of aircraft during take off and landing |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2527533A1 true FR2527533A1 (en) | 1983-12-02 |
Family
ID=9274384
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8209216A Withdrawn FR2527533A1 (en) | 1982-05-27 | 1982-05-27 | VTOL reaction motor aircraft - comprises vertical engine which creates air cushion beneath body of aircraft during take off and landing |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2527533A1 (en) |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1162303A (en) * | 1956-11-07 | 1958-09-11 | Ring or lenticular wing aerodyne | |
US2876964A (en) * | 1953-07-22 | 1959-03-10 | Streib Homer Frederick | Circular wing aircraft |
FR1336549A (en) * | 1962-10-16 | 1963-08-30 | Airplane suction cup, vertical takeoff and landing | |
FR82526E (en) * | 1962-10-27 | 1964-02-28 | Suction cup plane with vertical take-off and landing | |
US3689011A (en) * | 1969-07-11 | 1972-09-05 | Dorant Torelli | Aircraft |
-
1982
- 1982-05-27 FR FR8209216A patent/FR2527533A1/en not_active Withdrawn
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2876964A (en) * | 1953-07-22 | 1959-03-10 | Streib Homer Frederick | Circular wing aircraft |
FR1162303A (en) * | 1956-11-07 | 1958-09-11 | Ring or lenticular wing aerodyne | |
FR1336549A (en) * | 1962-10-16 | 1963-08-30 | Airplane suction cup, vertical takeoff and landing | |
FR82526E (en) * | 1962-10-27 | 1964-02-28 | Suction cup plane with vertical take-off and landing | |
US3689011A (en) * | 1969-07-11 | 1972-09-05 | Dorant Torelli | Aircraft |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |