Method of dynamic energy-saving superconductive propeller interaction with a fluid medium

Abstract

In a propeller system a process of dynamic energy-saving superconductive propeller interaction with a fluid medium comprises providing a perforation on the working blade surfaces having the different pressures, with an element possibility of the dynamic fluid medium flow connection between said blade perforations; and modulating a value of said connection of the blade so-called “breathing surfaces” in dependence on a change of a value of at least one controlled characteristic influencing a dynamic energy efficiency of a propeller process such that a dynamic structure-energetically optimization of said modulated surface-energy interaction is provided.

1 . A propeller system for providing a process of dynamic energy-saving superconductive propeller interaction with a fluid medium comprises at least one propeller having at least two blades having at least two working blade surfaces each; at least one perforation on each from the working blade surfaces having at least one perforation hole; at least one blade energy optimizer having at least one control block connected with at least one modulator which structurally connected with at least two portion of at least one created shunt passage having at least one communication with the perforation on each from the working blade surfaces of at least one blade; modulator is configured for modulating a value of a connection providing by flowing the fluid medium between said perforations through the created shunt passage under an action of a difference of the pressures generating on each from the working blade surfaces with the perforation, relatively during the process of the interaction of the perforated blades of the rotating propeller with the fluid medium such that a dynamic structure-energetically optimization, in an energy-effective manner, of said modulated surface-energy interaction is provided. 
     
     
         2 . A propeller system as defined in  claim 1 ; wherein the blade energy optimizer is provided for optimizing a value of at least one parameter of said modulating in dependence on a change of a value of at least one controlled characteristic influencing the dynamic surface-energy interaction efficiency, which comprises minimizing a boundary layer of the fluid medium on the working blade surfaces with the perforation during the process of the modulated surface-energy interaction of the perforated blades of the rotating propeller with the fluid medium. 
     
     
         3 . A propeller system as defined in  claim 1 ; wherein the propeller system does not have a propeller drive and structurally connected with a working mechanism; and the blade energy optimizer is provided for optimizing a value of at least one parameter of said modulating in dependence on a change of a value of at least one controlled characteristic influencing an energy efficiency of the working mechanism during the modulated surface-energy interaction of the perforated blades of the passive rotating propeller with a medium flow providing by a medium flow source, which structurally not connected with the propeller system. 
     
     
         4 . A propeller system as defined in  claim 1 ; wherein the propeller system comprises at least one propeller drive and structurally connected with a mobile apparatus; and the blade energy optimizer is provided for optimizing a value of at least one parameter of said modulating in dependence on a change of a value of at least one controlled characteristic influencing a dynamic energy efficiency of a process of a movement of the mobile apparatus under an energy action of a modulated medium flow-drawn providing by the modulated surface- energy interaction of the perforated blades of the active rotating propeller with the fluid medium during said process. 
     
     
         5 . A propeller system as defined in  claim 1 ; wherein the propeller system comprises at least one propeller drive and structurally not connected with an object which energy interacting with a propeller medium flow; and the blade energy optimizer is provided for optimizing a value of at least one parameter of said modulating in dependence on a change of a value of at least one controlled characteristic influencing an energy efficiency of a process of medium flow transporting said object under an energy action of a modulated medium flow providing by the modulated surface-energy interaction of the perforated blades of the active rotating propeller with the fluid medium during said process. 
     
     
         6 . A propeller system as defined in  claim 3 ,  4  or  5 ; wherein the propeller system comprises at least one additional modulator of said blade energy optimizer and at least one additional perforation on each from the perforated working blade surfaces; and the additional modulator is structurally connected with at least one additional portion of at least one additional created shunt passage having at least one communication with the additional perforation on each from the perforated working blade surfaces of at least one blade; the blade energy optimizer with said additional modulator is provided for additional optimizing a value of at least one parameter of additional modulating in dependence on a change of a value of at least one controlled characteristic influencing the dynamic surface-energy interaction efficiency, which comprises minimizing a boundary layer of the fluid medium on the working blade surfaces with the additional perforation during the process of the additional modulated surface-energy interaction of the perforated blades of the rotating propeller with the fluid medium. 
     
     
         7 . A propeller system as defined in  claim 1 ; wherein the modulator is configured for providing a predetermined frequency of the modulating. 
     
     
         8 . A propeller system as defined in  claim 1 ; wherein the modulator is configured for providing a predetermined range of the modulating. 
     
     
         9 . A propeller system as defined in  claim 1 ; wherein the modulator is configured for providing a predetermined law of the modulating. 
     
     
         10 . A propeller system as defined in  claim 1 ; wherein the modulator is configured for providing a predetermined “drop-shaped” form of a law of the modulating. 
     
     
         11 . A propeller system as defined in  claim 1 ; wherein the modulator is configured for providing a predetermined comparative phase of the modulating. 
     
     
         12 . A propeller system as defined in  claim 1 ; wherein the blade energy optimizer with at least one modulator is configured for providing a predetermined comparative phase of the modulating a value of a perforated blade surfaces connection to a predetermined phase shift comparatively a comparative phase of an independent predetermined periodic process, which is dynamically connected with the process of the modulated surface-energy interaction of the perforated blades of the rotating propeller with the fluid medium. 
     
     
         13 . A propeller system as defined in  claim 1 , comprises at least two propellers; and the blade energy optimizer with at least one modulator in each propeller is configured for providing a predetermined comparative phase of the modulating a value of a perforated blade surfaces connection in each propeller, relatively to a predetermined phase shift between the predetermined comparative phases of each said modulating dynamically connected with the process of the modulated surface-energy interaction of the perforated blades of the rotating propeller with the fluid medium in each said propeller. 
     
     
         14 . A propeller system as defined in  claim 1 ; wherein the control block of said blade energy optimizer is configured for providing at least one modulation discrete input; at least one optimization parametric discrete input; and also—at least one optimization modulation discrete output that connected with at least one optimization modulation discrete input of said modulator. 
     
     
         15 . A propeller system as defined in  claim 1 ; wherein the connection between said blade perforations providing by flowing the fluid medium through the created shunt passage comprises at least one filter. 
     
     
         16 . A propeller system as defined in  claim 1 ; wherein the modulator comprises at least one valve block having at least one immovable valve element and at least one movable valve element connected with a drive; and it is configured for providing said modulated connection through at least one passing channel of the immovable valve element and at least one passing channel of the movable valve element by a dynamic superposition of said passing channels during the process of the modulating. 
     
     
         17 . A propeller system as defined in  claim 16 ; wherein the modulator is configured for providing a regime of a non-modulated connection of a predetermined value by a fixed superposition of said passing channels during the process of the interaction of the perforated blades of the rotating propeller with the fluid medium such that a fixed structure-energetically optimizing control, in an energy-effective manner, of said surface-energy interaction is provided. 
     
     
         18 . A propeller system as defined in  claim 1  or  6 ; wherein the perforation is provided on the working blade surface by a realization of at least one perforation hole in a material of a body of the blade from outside of said working blade surface directly and having at least one communication with the created shunt passage. 
     
     
         19 . A propeller system as defined in  claim 1  or  6 ; wherein the perforation is provided on the working blade surface by a realization of at least one perforation hole in a material of a body from outside of at least one perforated constructive element additional fixed on the working blade surface and having at least one communication with the created shunt passage. 
     
     
         20 . A propeller system as defined in  claim 1  or  6 ; wherein said perforation on a working blade surface has at least two zones of a given form and a given size, which are provided on a given part of the working blade surface. 
     
     
         21 . A propeller system as defined in  claim 20 ; wherein the modulator is a multi-channel modulator comprising at least one controllable multi- channel zone commutator connected with at least two zones of the perforation on a working blade surface by at least two portions of created shunt passages having at least one communication with a perforation zone each on the perforated working blade surfaces of at least one propeller blade. 
     
     
         22 . A propeller system as defined in  claim 21 ; wherein the controllable multi-channel zone commutator is configured for providing a symmetrical regime of at least two connections with multi-channel modulator of at least two zones of the perforations each on the different perforated working blade surfaces of a propeller blade. 
     
     
         23 . A propeller system as defined in  claim 21 ; wherein the controllable multi-channel zone commutator is configured for providing a dissymmetrical regime of at least two connections with multi-channel modulator of at least two zones of the perforations each on the different perforated working blade surfaces of a propeller blade. 
     
     
         24 . A propeller system as defined in  claim 21 ; wherein the controllable multi-channel zone commutator is configured for providing a partial regime of at least one connection with multi-channel modulator of at least two zones of the perforations on the different perforated working blade surfaces of a propeller blade. 
     
     
         25 . A propeller system as defined in  claim 1 ; wherein the modulator is configured for providing at least one outside pressure service input. 
     
     
         26 . A process dynamic energy-saving superconductive propeller interaction with a fluid medium further comprises providing a perforation having at least one perforation hole on every from the working blade surfaces having the different pressures of at least one propeller blade with an element possibility of at least one dynamic fluid medium flow connection between said blade surface perforations with the different pressures; and modulating a value of said connection by a given dynamic periodical change of a value of at least one parameter dynamically connected with a dynamic process of said connection in dependence on a change of a value of at least one controlled characteristic influencing a dynamic energy efficiency of a propeller process such that a dynamic structure-energetically optimization, in an energy-effective manner, of said modulated surface-energy interaction is provided.