Abstract: An energy and hydrogen transport system includes a duct to transfer hydrogen. The duct has a pump or fan driven by an electric motor to pressurize or create a vacuum therein. A double walled container stores hydrogen.

Abstract: Oxidizer and fuel supply system for internal combustion engines, which includes oxygen supplies for the engines, particle filters, oxygen generators using nanofilters, pressurized oxygen bottles and air compressors, O2 loading media, by means of bottles, carboys or interchangeable tanks or hoses, Complementary means of nanomolecular membrane filters that separate O2 from air, performing the separation by means of aspiration or suction from the combustion engine or the suction or impulsion of a pump or compressor driven by an electric motor or mechanically by the combustion engine itself; Storage means for the separated or obtained O2; means for controlling the variable fuel/O2 mixture by means of a processor or an ECU (engine control unit); and as fuel: synthetic fuel, hydrocarbons, alcohols or hydrogen.

Abstract: The lifting, stabilizing and propelling arrangement for vertical take-off and landing aircraft, uses rotating wings, turbines or lift fans, propellers and stabilizers on the trailing edges of the wings and empennages, centrifugal or tangential turbines applied on the sides of the fuselage, on the inlet and outlet edges of the wings, or centrifugal or tangential turbines on the sides of the fuselage and inside the wings, those that carry the fuselage are fixed and produce only lift and those that go in the wings they rotate with them and produce lift during vertical flight and propulsion during horizontal flight, add some horizontal stabilizing fans at the tips of the wings and others for direction in the vertical empennage.

Abstract: The improvements in the energy capture systems of sea, river and wind currents, characterized in that the turbines are helical in shape and the turns or threads have an inclination close to 45°, of a quarter-round or quarter-circle section and are placed together with the shafts of the generators that are covered by a casing. or aerodynamic nacelle in front of or on the other side of the support mast. The upper area of the mast can rotate with the generator and have an aerodynamic profile. They can be installed attached to one end by means of a cable between the two banks of a river, or in a narrowing of the same, or they can be subject to elements or means of fastening consisting of a mast, tree, or with a chain, fixed to the ground. at the bottom of the sea or river. The turbines drive a generator and electrical conduction cables and a security and warning facility are added.

Abstract: The germ protection system for vehicles, hospitals, restaurants, schools, nursing homes, lifts and the like uses: a) A system that prevents germs: bacteria, protozoa, viruses or parasites from being breathed in vehicles or closed premises, lifts or the like, blowing or sucking air, b) An independent air installation that applies air conditioning, fed with turbofan engines, to the individual air blowing nozzles in the ceiling or backrest of the compartments of each passenger, c) An independent air installation using compressors that extracts and compresses the outside air, and apply it to the individual air blowing nozzles in the ceiling or backrest of the compartments of each passenger, d) A system that uses an individual installation to replace oxygen system in case of emergency, e) A system that is valid simultaneously for protection against germs and for breathing in case of emergency.

Abstract: The ultralight two track train that does not derail, made up of one or more ultralight wagons and aerodynamic, oval or semi-oval transverse profiles, characterized in that the wagons carry vertical or inclined wheels or pulley wheels in their lower area and supported by the chassis of the wagons, which rest and roll on a pair of vertical or inclined rails, the channels of the pulley wheels are supported and held on the head of circular, semicircular or semi-oval section of the rails, the heads of the rails being trapped with the pulley wheels, adding pairs of wheels that use a common axis, the rails are coupled and fixed tongue and groove to the sleepers or to some monolithic structures or channels, the sleepers are fixed using the track system on concrete slab, using electrical supply means, propellant means and reducing means of the front, rear and lateral resistance of the wagons, adding wheels with permanent magnets or with electromagnets that are attached, or run close and attracted by the rails.

Abstract: The system for removing the objects from the throat consists of a device formed by a nozzle or a smooth, corrugated, waved or cylindrical tubular element, which is inserted into the mouth and allows a depression to be produced in it, either by extracting the tubular element smooth or cylindrical, or by sucking the air from the mouth with a corrugated tubular element by means of a suction pump constituted by a bellows, bell or chamber in the shape of a deformable spherical cap. The smooth or cylindrical tubular element is inserted into the mouth and once it is adjusted to the lips, it is extracted by sucking a large part of the air, creating a depression that sucks the object that closes the throat. The nozzle and the end of the corrugated tube are held in place with the teeth. Circulating the air through its central area. Valves with a flexible tongue act during the impulsion and extraction of air.

Abstract: The aseptic protective system against germs and dirt for beverage bottles and cans and system for joining beverage cans, consists of applying a protective cover to the end or mouth of the bottles or cans of drinks, whose protective elements are sheets or films, sleeves, caps, lids, stoppers or belts made of biodegradable plastic materials, which protect them from contamination by germs and dirt. attaching or tongue-and-groove joints to groups or rows of cans, the attachments use covers, sheets of tape, bands or a cover of biodegradable material. The groups or rows of cans are constructed in a way that the bottoms of the cans are placed at their ends towards the outside and therefore those carrying the nozzles and opener are protected internally from dirt and contamination. The union is done by tongue and groove, attached or glued, and adding covers or sleeves, tapes or bands of metal sheets.

Abstract: The wind or marine energy capture system uses paragliders, elliptical or rhomboidal kites that are rotated, twisted or with fins on portions of their trailing or leading edges of the major edges and held at their ends by cables or cords, which by the action of the wind or water rotate around its axis and apply the rotational movement to an electric generator or mechanical element to move to the ground. Paragliders or elliptical kites, etc. they are directed by the wind automatically without having to apply any energy to it.

Abstract: The lift, propulsion and stabilising system for vertical takeoff and landing aircraft of the invention consists of applying during vertical flight on, below or in the interior of the fixed-wing aircraft one or more rotors or large fans each one with two or more horizontal blades, said rotors are activated by means of turboshafts, turbofans or turboprops with a mechanical, hydraulic, pneumatic or electrical transmission, and the respective motors. Using lifting and/or stabilising and/or controlling fans and/or oscillating fins and/or air blasts. Placing the horizontal lifters near at least one end of the longitudinal axis and of the transverse axis of the aircraft. Generally said stabilising elements form 90° with one another and with the central application point of the rotor or application of that which results from the lift forces.

Abstract: The lifesaving system for buildings of the present invention includes a tubular device having opened crowns or circular radial curved crowns attached to an inside wall of the tubular device, the crowns having flexible vanes or fins through which inverted bell-shaped elements pass, the elements larger in size than the inner size of the crowns, and are braked or slowed as they move downwards, a foam rubber element added at an end of the tubular device, and an annular element having an outside perimeter forming a tapered cone and curved, and which adapts to a top of a user's chest and is positionable under user's armpits.

Abstract: A lifting arrangement for aircraft fuselages that consists of placing longitudinal vertical or slanted fins or plates on the lower and lateral lower part of the whole fuselage, said fins forming a channel with the underside of the fuselage, including nose, fuselage and tail, open on their lower area. Further adding longitudinal horizontal or laterally slanted fins on the lateral middle or middle-to-low area of the fuselage and with a positive slope up to the nose with said fins arranged in such a way that the upper fins are projected increasingly laterally, and because of this arrangement and their slope up to the nose, the air flow is directed downward and backward.

Abstract: Aerodynamic profile that comprises two zones or main sections: one is the front surface inclined with a positive angle, generating the totality or greater part of the lift, and the other is the rear portion or zone to the front surface, profiled or streamlined, formed by two curved, generally hollow surfaces and, which does not generate lift, but leads the air flow properly reducing drag and avoiding boundary layer separation.

Abstract: A wind energy catchment device comprising a central vertical shaft that rotates, the bottom end of which is secured by means of bearings to a rigid support fixed to the ground, the upper and lower part of the shaft have radial arms secured to it, evenly spaced one from the other, the outer ends of the upper arms are connected by cables or cords with its contiguous outer ends of the lower arms, between the upper and lower radial arms and the central shaft there are rectangular parallelepiped sails secured at their outer vertices. In all cases the furthest external vertical side of these sails or plates is secured and the sails or plates rotates from 90° to 180° with or around their shafts, cables or ropes that connect the ends of the arms, having both internal vertices loose, between the central shaft and two contiguous arms are arranged some parallel cords or mesh that support the sails or plates when they receive the air on the side of the mesh furthest from the wind.

Abstract: The golf ball having either a smooth or dimpled surface is disclosed including a sphere with peripheral channels spaced and intersected at distances on the surface, with part of the air flow on the front over-pressure area communicating with the rear depression of the ball in its forward movement, facilitating aerodynamic air circulation through it, resulting in reduced resistance, thereby facilitating rotation and lift, enhancing the advance of the ball.

Abstract: Lifting arrangement for lateral aircraft surfaces that consists of numerous lateral flutings, grooves, splines, flutes or riblets parallel to each other, arranged on the lateral surfaces of fuselages, fin units, pylons and gondolas of aircraft with a downward slope from the nose to the tail, with the flow of air passing through such flutings, grooves, etc., towards the rear and downwards, generating lifting by reaction, using small planes or fins to support the engines and flight control fins.

Abstract: A lifting arrangement for aircraft fuselages that consists of placing longitudinal vertical or slanted fins or plates on the lower and lateral lower part of the whole fuselage, said fins forming a channel with the underside of the fuselage, including nose, fuselage and tail, open on their lower area. Further adding longitudinal horizontal or laterally slanted fins on the lateral middle or middle-to-low area of the fuselage and with a positive slope up to the nose with said fins arranged in such a way that the upper fins are projected increasingly laterally, and because of this arrangement and their slope up to the nose, the air flow is directed downward and backward.

Abstract: A spherical gear pump that comprises two rotors, or geared spheres, with the teeth arranged around them in a circular band at right angles to their axis of rotation: the pump spheres are covered by close-fitting spherical cases or housings except at the central or most internal part of the connection between the gears on the two spheres, the fluid contained in the cavity created between the most external gears and the case or housing is moved during rotation from the intake to the outlet, one sphere is driven by its shaft and the other is dragged by the gearing between the two.

Abstract: A process for the recovery of the energy from the air in pressurised areas of aircraft that involves linking or moving air from the pressurised areas to the lower areas of the fuselage or lower surfaces of the wings, the horizontal stabilisers, and other aerodynamic profiles, along ducting and/or by discharging through multiple slots or openings flowing downward and rearward with a small inclination against the direction of the air flow, to avoid turbulence. The pressure of the pressurised cabin air conditioning is used. In other cases, it is used the pressure produced at the front of the fuselage, on the leading edges of the wings, the horizontal stabiliser or other aerodynamic profiles. Lift is increased in all cases without further energy requirements.

Abstract: The present invention is direct to an aircraft fuselage lift arrangement which includes an elongated vertically flattened oval cross section fuselage having a longitudinal axis; an upper longitudinal axis along the upper most portion of the fuselage and parallel to the longitudinal axis, a lower longitudinal axis parallel to the longitudinal axis and along the length of the bottom of the fuselage. The fuselage having a conical nose portion at one end and a conical tail portion at its opposite end. The nose portion of the fuselage having an upwardly inclined front wall extending upwardly from the bottom of the fuselage to at least the upper longitudinal axis of the fuselage. The tail portion of the fuselage having a downwardly declining rear wall extending from the upper longitudinal axis to the bottom of the fuselage. The fuselage also having a main landing gear.