The invention relates to a method for designing, constructing and producing the skeleton of turbine-impeller-reactor wheels which employ simultaneously, in the same wheel, the principles of the turbine, the impeller, and the reactor, and which can also have the function of a hybrid wheel powered by an energetic fluid.
F01D 1/32 - "Machines" ou machines motrices à déplacement non positif, p. ex. turbines à vapeur avec transformation pression-vitesse exclusivement dans le rotor, p. ex. le rotor tournant sous l'action de jets issus de celui-ci
F01D 5/18 - Aubes creusesDispositifs de chauffage, de protection contre l'échauffement ou de refroidissement des aubes
G05B 19/4093 - Commande numérique [CN], c.-à-d. machines fonctionnant automatiquement, en particulier machines-outils, p. ex. dans un milieu de fabrication industriel, afin d'effectuer un positionnement, un mouvement ou des actions coordonnées au moyen de données d'un programme sous forme numérique caractérisée par la programmation de pièce, p. ex. introduction d'une information géométrique dérivée d'un dessin technique, combinaison de cette information avec l'information d'usinage et de matériau pour obtenir une information de commande, appelée programme de pièce, pour la machine à commande numérique [CN]
The invention relates to a method for designing and producing turbines having buckets with calibrated jets, on request, characterised in that the skeletons of the turbines displayed on the screen allow the design and then the production thereof in any dimensions, any materials and any quantities, the construction being carried out with blades designed according to the so-called five-parameter arithmetic principle, the skeleton of the turbine is displayed on the screen by means of "virtual neutral fibres" which are subsequently covered with a material, the turbines being contained, over the entire length thereof, in a circular envelope, which is in principle slightly rounded and has a diameter evolving over the length thereof according to the content of the envelope, and the length of said single-component envelope is shown on a drawing and divided into four zones intersected by temporary virtual disks which each separate the zones according to the functions carried out in said areas, the front edge of said envelope being very thinned-out or, on request, provided with a flange Br for allowing connection to installations, the four zones including: a first zone for (1) for introduction of the fluid, which is an empty space or a space containing valves or inducers, of the corkscrew type, which optionally cause a pre-rotation of the fluid which enters a second zone (2), a pointed shield spreading the stream of fluid in the centre, at the inflow point thereof, and directing it as it spreads, towards the second zone (2), the second zone (2) where the rotation of the fluid is created in channels that wind in spirals and open up at the rear of the second zone (2), rotating the fluid, a third zone (3) containing the rotating wheel provided with buckets with calibrated jets that harness the energy supplied by the jets of fluid leaving the second zone (2), and a fourth zone (4) containing a housing attached to the stationary casing of the turbine and placed after the rotating wheel, said housing containing channels that orient the fluid towards the outlet at the rear of the turbine, and the fluid is guided, as soon as it reaches the second zone (2), by channels contained in tubes that are arranged in continuity face to face, over the entire length of the turbine.
F03B 1/00 - Machines motrices du type "à action", c.-à-d. turbines avec jets de liquide à grande vitesse heurtant des rotors à aubes ou à dispositifs similaires, p. ex. roues PeltonParties constitutives ou détails particuliers les concernant
3.
METHOD FOR CONSTRUCTING THRUSTERS OR MOTORS CONTAINED IN A CYLINDRICAL CASING AND ASSOCIATED THRUSTER OR MOTOR
These new thrusters simultaneously use wheels of the CARPYZ THRA "Turbo Powered Helicopter Reactor" type and wheels of the CARPYZ TaG ''Bucket Turbines'' type or wheels of the CARPYZ TaC ''Scoop Turbines" type, representing real global technological breakthroughs for fluid mechanics. They use, upon vertical take-off of the aircraft, propellers driven by electric motors and temporarily use the required additional high vertical axial thrust that is then supplied by the reactors of the THRA wheels, which also use an energetic fluid. The CARPYZ type thrusters, due to the low diameter and weight afforded thereto, are progressively horizontally inclined and the force of the reactors is progressively replaced by that of the propellers, which then supply the flows required in order for the aircraft to travel horizontally using wings that rely on the lift of the fluid, like airplanes. Photovoltaic wings are then deployed that are like butterfly wings and this economical solution will enable voyages over longer distances. It really is the safe mass market vertical take-off car of the future that can be achieved in less than 10 years by virtue of the new CARPYZ type thrusters, the little things change everything!
F01D 1/02 - "Machines" ou machines motrices à déplacement non positif, p. ex. turbines à vapeur avec des moyens stationnaires de guidage de fluide de travail et un rotor à ailettes ou de structure analogue
F02K 3/068 - Ensembles fonctionnels comportant une turbine à gaz entraînant un compresseur ou un ventilateur soufflant dans lesquels une partie du fluide énergétique passe en dehors de la turbine et de la chambre de combustion l'ensemble fonctionnel comprenant des soufflantes carénées, c.-à-d. des soufflantes à fort débit volumétrique sous basse pression pour augmenter la poussée, p. ex. du type à double flux caractérisé par une longueur axiale courte par rapport au diamètre
F01D 5/18 - Aubes creusesDispositifs de chauffage, de protection contre l'échauffement ou de refroidissement des aubes
F01D 5/04 - Organes de support des aubes, p. ex. rotors pour "machines" ou machines à flux radial
The invention relates to design and production methods for a rotor which is both a turbine and a propeller having blades that are hollow along the entire length thereof and which lead into peripheral circular chambers that operate as an engine (THRA) that can be powered by working fluids.
The invention relates to a machine for the layer-by-layer production of objects, comprising: a circular rotary container arranged in the lower part (B), the inside thereof being provided with independently and vertically motor-driven cylindrical crowns (7); and a stationary part that tops the container. The machine also includes at least one production unit comprising a first station (1) for distributing the layer of product, a second station (2) for evening out the thickness of the layer, a third station (3) for controlling and regulating the temperature of the next layer, a fourth station (4) for solidifying the useful surfaces of the layer of product, a fifth station (5) for controlling and regulating the temperature of the layer that has just been deposited, and a sixth station (6) for treating and impregnating the layer.
G06F 7/66 - Analyseurs différentiels numériques, c.-à-d. dispositifs de calcul pour le calcul différentiel et intégral ou la résolution d'équations différentielles ou intégrales, en utilisant des impulsions représentant des incrémentsAutres dispositifs de calcul incrémentiel pour la résolution d'équations aux différences dans lesquels les impulsions représentent uniquement des incréments unitaires
B29C 67/00 - Techniques de façonnage non couvertes par les groupes , ou
B22F 3/105 - Frittage seul en utilisant un courant électrique, un rayonnement laser ou un plasma
G05B 15/02 - Systèmes commandés par un calculateur électriques
B29C 64/153 - Procédés de fabrication additive n’utilisant que des matériaux solides utilisant des couches de poudre avec jonction sélective, p. ex. par frittage ou fusion laser sélectif
B29C 64/165 - Procédés de fabrication additive utilisant une combinaison de matériaux solides et liquides, p. ex. une poudre avec liaison sélective par liant liquide, catalyseur, inhibiteur ou absorbeur d’énergie
B29C 64/20 - Appareil pour la fabrication additiveDétails ou accessoires à cet effet
B29C 64/386 - Acquisition ou traitement de données pour la fabrication additive
B33Y 50/02 - Acquisition ou traitement de données pour la fabrication additive pour la commande ou la régulation de procédés de fabrication additive
6.
TURBINE COMPRISING AT LEAST TWO HOLLOW 3D WHEELS NESTED INSIDE ONE ANOTHER
Firstly, the turbines direct the fluid tangentially through channels provided around a stationary hollow wheel and the jets are received in buckets in a rotating wheel surrounding the stationary wheel, operating on the Pelton wheel principle. This novel method can be used to construct turbine assemblies that can recover energy from moving fluids, like wind turbines and marine turbines, using a minimum capture surface and obtaining a maximum yield.
F03D 1/04 - Mécanismes moteurs à vent avec axe de rotation sensiblement parallèle au flux d'air pénétrant dans le rotor comportant des moyens fixes de guidage du vent, p. ex. par aubages ou canaux directeurs
F01D 1/02 - "Machines" ou machines motrices à déplacement non positif, p. ex. turbines à vapeur avec des moyens stationnaires de guidage de fluide de travail et un rotor à ailettes ou de structure analogue
The invention relates to a machine for the layer-by-layer production of objects, comprising: a circular rotary container arranged in the lower part (B), the inside thereof being provided with independently and vertically motor-driven cylindrical crowns (7); and a stationary part that tops the container. The machine also includes at least one production unit comprising a first station (1) for distributing the layer of product, a second station (2) for evening out the thickness of the layer, a third station (3) for controlling and regulating the temperature of the next layer, a fourth station (4) for solidifying the useful surfaces of the layer of product, a fifth station (5) for controlling and regulating the temperature of the layer that has just been deposited, and a sixth station (6) for treating and impregnating the layer.
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