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 - Non-positive-displacement machines or engines, e.g. steam turbines with pressure/velocity transformation exclusively in rotor, e.g. the rotor rotating under the influence of jets issuing from the rotor
F01D 5/18 - Hollow bladesHeating, heat-insulating, or cooling means on blades
G05B 19/4093 - Numerical control [NC], i.e. automatically operating machines, in particular machine tools, e.g. in a manufacturing environment, so as to execute positioning, movement or co-ordinated operations by means of programme data in numerical form characterised by part programming, e.g. entry of geometrical information as taken from a technical drawing, combining this with machining and material information to obtain control information, named part programme, for the NC machine
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 - Engines of impulse type, i.e. turbines with jets of high-velocity liquid impinging on bladed or like rotors, e.g. Pelton wheelsParts or details peculiar thereto
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 - Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor
F02K 3/068 - Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low-pressure outputs, for augmenting jet thrust, e.g. of double-flow type being characterised by a short axial length relative to diameter
F01D 5/18 - Hollow bladesHeating, heat-insulating, or cooling means on blades
F01D 5/04 - Blade-carrying members, e.g. rotors for radial-flow machines or engines
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 - Digital differential analysers, i.e. computing devices for differentiation, integration or solving differential or integral equations, using pulses representing incrementsOther incremental computing devices for solving difference equations wherein pulses represent unitary increments only
B29C 67/00 - Shaping techniques not covered by groups , or
B22F 3/105 - Sintering only by using electric current, laser radiation or plasma
G05B 15/02 - Systems controlled by a computer electric
B29C 64/153 - Processes of additive manufacturing using only solid materials using layers of powder being selectively joined, e.g. by selective laser sintering or melting
B29C 64/165 - Processes of additive manufacturing using a combination of solid and fluid materials, e.g. a powder selectively bound by a liquid binder, catalyst, inhibitor or energy absorber
B29C 64/20 - Apparatus for additive manufacturingDetails thereof or accessories therefor
B29C 64/386 - Data acquisition or data processing for additive manufacturing
B33Y 50/02 - Data acquisition or data processing for additive manufacturing for controlling or regulating additive manufacturing processes
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 - Wind motors with rotation axis substantially parallel to the air flow entering the rotor having stationary wind-guiding means, e.g. with shrouds or channels
F01D 1/02 - Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor
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.
patents
