FR2862282A1 - Flying device for permitting pilot to move in air, has support structure made of aluminum alloy, with upper part receiving two small jet engines, fuel tank and fuel system, and lower part receiving pilot support and flying control - Google Patents
Flying device for permitting pilot to move in air, has support structure made of aluminum alloy, with upper part receiving two small jet engines, fuel tank and fuel system, and lower part receiving pilot support and flying control Download PDFInfo
- Publication number
- FR2862282A1 FR2862282A1 FR0313304A FR0313304A FR2862282A1 FR 2862282 A1 FR2862282 A1 FR 2862282A1 FR 0313304 A FR0313304 A FR 0313304A FR 0313304 A FR0313304 A FR 0313304A FR 2862282 A1 FR2862282 A1 FR 2862282A1
- Authority
- FR
- France
- Prior art keywords
- pilot
- support
- part receiving
- flying
- aluminum alloy
- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/026—Aircraft not otherwise provided for characterised by special use for use as personal propulsion unit
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
Description
APPAREIL QUI SE DEPLACE DANS l'AIRAPPARATUS THAT MOVES INTO AIR
Ce travail consiste dans l'invention d'un appareil piloté qui se déplace dans l'air, dans n'importe quelle direction. Cette direction peut être modifiée par le déplacement du centre de gravité du pilote et par la poussée des moteurs. This work consists in the invention of a controlled device that moves in the air, in any direction. This direction can be modified by the displacement of the center of gravity of the pilot and by the thrust of the engines.
L'appareil est relativement simple; il permet d'avoir des positions de repos ou de déplacement; il se déplace dans n'importe quelle direction jusqu'à une vitesse déterminée(x). The device is relatively simple; it allows to have rest or displacement positions; it moves in any direction up to a certain speed (x).
L'appareil se compose d'une structure support en alliage d'aluminium sur laquelle se fixe, dans sa partie supérieure,avec un angle déterminé(x) deux ou plusieurs petits réacteurs et dans cette même partie leur système et réservoir de combustible. The apparatus consists of an aluminum alloy support structure on which attaches, in its upper part, with a given angle (x) two or more small reactors and in this same part their system and fuel tank.
Dans sa partie inférieure se place le support du pilote et la commande de vol. La position du pilote pour le décollage et l'atterrissage sera verticale et pour le déplacement horizontale ou assise Les commandes de l'appareil sont similaires à celles du deltaplane pour obtenir les différentes phases de vol. La figure 1 montre le schéma de l'appareil en vol et de ses 20 parties. In its lower part is placed the support of the pilot and the control of flight. The position of the pilot for take-off and landing will be vertical and for horizontal or seated movement The controls of the aircraft are similar to those of the hang-glider to obtain the different phases of flight. Figure 1 shows the diagram of the aircraft in flight and its parts.
La figure 2 montre les différentes phases pour la réalisation du vol. La figure 2a montre l'appareil en état de repos, posé sur le sol. On peut noter la position verticale des réacteurs qui coïncide 25 avec le centre de gravité du pilote. Figure 2 shows the different phases for the realization of the flight. Figure 2a shows the device in the state of rest, placed on the ground. The vertical position of the reactors coinciding with the center of gravity of the pilot can be noted.
Dans cette position s'allument les moteurs et l'ascension verticale débute lorsque la force de poussée dépasse le poids total. In this position the engines come on and the vertical ascent starts when the thrust force exceeds the total weight.
La figure 2b représente l'ascension verticale quand le pilote 30 abandonne la position assise,il peut aussi la maintenir. FIG. 2b represents the vertical ascent when the pilot 30 abandons the seated position, he can also maintain it.
La figure 2c: le pilote déplace son centre de gravité en avant; la force résultant de la poussée (E) s'incline vers l'avant et avec l'aide de la poussée des moteurs et l'utilisation d'un variomètre,l'altitude est maintenue;la composante horizontale(Eh) de la poussée provoque le déplacement horizontal de l'appareil. Figure 2c: the pilot moves his center of gravity forward; the force resulting from the thrust (E) tilts forward and with the help of the thrust of the motors and the use of a variometer, the altitude is maintained, the horizontal component (Eh) of the thrust causes the device to move horizontally.
L'altitude est maintenue avec une valeur de la composante verticale de la poussée (Ev) égale au poids total (p).Pour effectuer les tours à gauche ou à droite, il suffit de déplacer le centre de gravité à gauche ou à droite, et ainsi il se 5 crée une force latérale qui provoque une accélération perpendiculaire à la trajectoire entraînant le tour. The altitude is maintained with a value of the vertical component of the thrust (Ev) equal to the total weight (p) .To perform the left or right turns, simply move the center of gravity to the left or right, and thus a lateral force is created which causes an acceleration perpendicular to the trajectory causing the turn.
La figure 2d montre le déplacement à effectuer pour diminuer la vitesse et la réduire à 0,et ainsi débuter la descente ou se maintenir. Figure 2d shows the movement to be made to reduce the speed and reduce it to 0, and thus start the descent or maintain.
Dans ce cas, en déplaçant le corps et le centre de gravité en arrière, les moteurs se positionnent de manière telle qu'ils entraînent une composante horizontale de la poussée(Eh) en arrière qui effectuera le freinage. In this case, by moving the body and the center of gravity back, the motors are positioned in such a way that they cause a horizontal component of the thrust (Eh) behind which will perform the braking.
Pour effectuer la descente qui permet l'atterrissage: une fois que l'appareil est à la vitesse horizontale zéro, les moteurs sont placés en position verticale; avec la position du centre de gravité et en contrôlant la poussée, la vitesse de descente et l'altitude, l'atterrissage est effectué en maintenant une position similaire à celle de la fig 2b,le corps étant en position verticale ou assise. To perform the descent that allows the landing: once the aircraft is at zero horizontal speed, the engines are placed in a vertical position; with the position of the center of gravity and controlling thrust, descent speed and altitude, the landing is performed by maintaining a position similar to that of Fig 2b, the body being in a vertical or sitting position.
La figure 3 montre une forme plus simple de l'appareil: l'opération de décollage et d'atterrissage s'effectue avec les pieds, grâce à un poids moindre des moteurs, de leurs accessoires et du combustible. Figure 3 shows a simpler form of the aircraft: the take-off and landing is done with the feet, thanks to a lower weight of the engines, their accessories and fuel.
La figure 4 montre le système d'apprentissage proposé : le pilote et son appareil se déplacent le long d'un câble tendu grâce à un petit support mobile; un contrepoids est nécessaire pour permettre l'utilisation d'une plus petite poussée des moteurs et des vitesses moindres adaptées à la phase d'apprentissage jusqu'à ce que la technique de pilotage soit assimilée. Figure 4 shows the proposed learning system: the pilot and his aircraft move along a stretched cable thanks to a small mobile support; a counterweight is necessary to allow the use of a smaller engine thrust and lower speeds adapted to the learning phase until the steering technique is assimilated.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0313304A FR2862282B1 (en) | 2003-11-13 | 2003-11-13 | APPARATUS THAT MOVES INTO THE AIR |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0313304A FR2862282B1 (en) | 2003-11-13 | 2003-11-13 | APPARATUS THAT MOVES INTO THE AIR |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2862282A1 true FR2862282A1 (en) | 2005-05-20 |
FR2862282B1 FR2862282B1 (en) | 2007-02-23 |
Family
ID=34508441
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0313304A Expired - Fee Related FR2862282B1 (en) | 2003-11-13 | 2003-11-13 | APPARATUS THAT MOVES INTO THE AIR |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2862282B1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2011131861A (en) * | 2009-12-25 | 2011-07-07 | Ihi Corp | Vertical takeoff/landing aircraft |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1331882A (en) * | 1962-08-24 | 1963-07-05 | Bell Aerospace Corp | Personal propulsion device |
US3474987A (en) * | 1967-07-24 | 1969-10-28 | Ludwig F Meditz | Helicopter device |
-
2003
- 2003-11-13 FR FR0313304A patent/FR2862282B1/en not_active Expired - Fee Related
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1331882A (en) * | 1962-08-24 | 1963-07-05 | Bell Aerospace Corp | Personal propulsion device |
US3474987A (en) * | 1967-07-24 | 1969-10-28 | Ludwig F Meditz | Helicopter device |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2011131861A (en) * | 2009-12-25 | 2011-07-07 | Ihi Corp | Vertical takeoff/landing aircraft |
Also Published As
Publication number | Publication date |
---|---|
FR2862282B1 (en) | 2007-02-23 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |
Effective date: 20140731 |