Method of providing power supply of electrodynamic flying vehicles
 High voltage electric drive of alternating current (versions) / 2334349Composition of the electric drive of an alternating current includes the frequency converter, the invention can be used for the launching and control of the work of asynchronous or synchronous electric drives with the working voltage 6...10 kV and power of up to tens of mW. The high-voltage electric drive of the alternating current with the three-phase electric motor contains a source of an adjustable direct current, three-phase bridge thyristor chopper, switching devices connected to the outputs of alternating current of the inverter consistently with the phases of the three-phase winding of the electric motor, sensors of current and voltage and the control devices of the inverter and switching devices. Each switching device contains a capacitor with two outputs and the bidirectional symmetric operated semi-conductor key connected in parallel to it completely. Starting of the switching device in the electric drive is carried out in the manner as it specified in the materials of application for each of the three variants. In the electric drive for each of the variants protection of semi-conductor keys is provided at extraordinary and emergency situations. |
 Duple unregulated voltage converter / 2334347In the duple converter working without a regulated pause with synchronising generator (22), strobe generator (29) is introduced which periodically, for a short period blocks the disconnecting trigger for protection against an overload is executed on transistors (19, 33). During this time protection is transferred into the regime of current limitation, and power transistor keys (1, 2) - in an active mode of operation. The porosity of the pulses of the strobe generator (29) is selected so as to avoid overheating of transistor keys (1, 2). The high-speed protection of the converter makes it possible to connect the converter to the capacitive load and to provide reliable work of transistor keys (1, 2) with overloads and short circuits of output. |
 Thyristor chopper with capacitors in power circuit / 2334346Device is supplied with a block of expanding of the range of regulation, executed on the principle of the transfer of the electric energy saved up in inductance from the source to the receiver. Thus the energy source is the additional winding of the transformer, and using the filter capacitor shunting the power supply. |
 Converter of ac potential into constant one with 9-fold frequency of pulsation / 2334345Converter of the ac potential into a constant one with 9-fold frequency of the pulsation contains a three-phase transformer (1) with the group of secondary windings (2) connected according to the scheme of the first six-phase star, and the group of the secondary windings (3) connected under the scheme of the second six-phase star, and fifteen gates (4...18). Phase conclusions and, in, with the groups of windings 3, which belong to the star of the second six-phase star, are connected by three unidirectional gates (5, 11, 16) which are switched on, accordingly, with phase leads x', y', z' groups of the windings (2), belonging to the reverse star of the first six-phase star, and phase leads x, y, z of the reverse star belonging to the second six-phase star, are connected by three unidirectional gates (13, 18, 8) which have been switched on, accordingly, with phase outputs a', b', c' of the star belonging to the first six-phase star. From the gates of the devices (12, 15, 17, 4, 7, 10) a six-valve anodic star is formed, and from the gates (14, 6, 9) a three-star cathodic star is formed, free electrodes of the gates (12, 17, 7, 4, 10, 15) are connected, accordingly, with phase leads a, b, c, x, y, z of the second six-phase star, free electrodes of gates (6, 9, 14) of three-valve stars are connected, accordingly, to the phase leads a', b', c' of the straight star belonging to the first six-phase star. All the gates of the device are included unidirectional, and the general points (19 and 20), accordingly, the six- and three-valve stars form output leads of the converter to which is connected the load (21). |
 Direct current to alternating current converter / 2333591Invention pertains to electrical engineering, and specifically to invertors for autonomous electrical power supply for different electrical equipment, requiring use of sinusoidal alternating current. The direct current converter has a generator of sinusoidal voltage, a driver-amplifier and a power electronic converter. The sinusoidal voltage generator with frequency f is in the form of a miniature motor-generator, the electric motor of which rotates with a stable velocity proportional to frequency f and the motor-generator controls the electronic breaker-splitter. The electric motor of the motor-generator works on direct or alternating current and can smoothly change speed of rotation. |
 Switching converter circuit / 2333590Converter circuit for switching a number of levels of commutating voltage is proposed. The circuit has n first commutation groups (1.1,..., 1.n) on each phase (R, S, T). The n-th first commutation group (1.n) is formed by the first (2) and the second (3) controlled bidirectional power semiconductor switches, and the commutation groups from the first (1.1) to the (n-1)-th commutation group (1.(n-1)) are formed respectively by the first (2) and the second (3) controlled bidirectional power semiconductor switches and connected to the first (2) and the second (3) controlled bidirectional power semiconductor switches by a capacitor (4). Each of the first n first commutation groups (1.1,..., 1.n) is connected to respectively to the adjacent first commutation group (1.1,..., 1.n), and the first (2) and second (3) controlled bidirectional power semiconductor switches of the first commutation group (1.1) are also interconnected. To achieve the technical outcome, the accumulated electrical energy of the converter circuit n≥1 is reduced, and for this purpose there are p second (5.1,..., 5.p) and p third (6.1,..., 6.p) commutation groups, with, respectively, a first controlled bidirectional power semiconductor switch (7, 8), second controlled bidirectional power semiconductor switch (9, 10) and a capacitor (13, 14), and in this case p≥1. Each of the p second commutation groups (5.1,..., 5.p) are connected respectively to the second adjacent commutation group (5.1,..., 5.p), and each of the p third commutation groups (6.1,..., 6.p) is connected respectively to the adjacent third commutation group (6.1,..., 6.p). Further, the first second (5.1) and the first third (6.1) commutation groups have respectively a third controlled bidirectional power semiconductor switch (11, 12), connected in anti-parallel form to the corresponding second controlled bidirectional power semiconductor switch (9, 10). The first second commutation group (5.1) is connected to the first controlled bidirectional power semiconductor switch (2) of the n-th first commutation group (1.n), and the first third commutation group (6.1) is connected to the second controlled bidirectional power semiconductor switch (3) of the n-th first commutation group (1.n), and capacitor (13) of the p-th second commutation group (5.p) serially connected to capacitor (14) of the p-th third commutation group (6.p). |
 Method of controlling multiphase rectifier / 2333589Invention concerns technique of transformation the electric power of alternating current into the energy of constant current using gated transformer with a smooth regulation of rectified voltage. It's realised by changing outlet voltage of additionally inserted autonomous three-phase bridge voltage inverter with sinusoidal pulse-duration modulation. The inverter's inlets are connected to the chain of constant current of the unit, outlets are connected to the primary winding of the three-phase matching transformer, and at the same time the secondary phase windings of matching transformer are connected sequentially with the net windings of converting transformers. Changing outlet voltage of the autonomous inverter is realised by adjusting either phase or amplitude or both values of modulating sinusoidal voltage. The secondary phase windings of matching transformer are connected to the net windings of converting transformers either directly or through compensator with the fifth and seventh current harmonics in condensers. Gated windings of converting transformers are connected to the rectifying bridges' outlets of alternating current either directly or through the same compensator. Converting transformers of the unit's blocks are performed either on standalone or parallel magnetic conductors. Rectifying bridges of the unit are connected either parallel or sequentially. The invention can be used in aluminium, copper, zinc, chlorine, hydrogen, etc electrolysis plants, for electrothermics and electric transport and in other branches which use constant current. |
 Static converter / 2333587Static converter has four two-conducting switches, power supply, load, and a capacitor, one of the plates of which connected to the second lead of the first switch. The second plate is connected to the second lead of the first switch. The converter also has two reactors. One lead of the reactor is connected to one of the leads of the load, and the other lead of the reactor connected to the other end of the load. The second leads of the first and second reactors are joined together and connected to the other pole of the supply. |
 Alternating voltage/constant voltage converter with twelvefold pulse frequency / 2332776Alternating voltage/constant voltage converter with twelvefold pulse frequency can be used as uncontrolled or controlled alternating voltage/constant voltage converter for electric power supply mainly to high-voltage load and for multilevel voltage inverters. It contains three four-phase gate bridges (1, 2, 3) and transformer phase converter (4) which has five secondary phase windings on each limb of three-phase transformer. These secondary windings form three groups of windings (5, 6, 7). Each group of secondary windings is made up of two opposite equilateral zigzags with mutually reversed phases. Midpoints of these zigzags formed by starts of windings are connected with beginning, and midpoints formed by ends of phase windings are connected with the end of secondary phase winding of transformer limb, which transformer does not contain phase windings forming these zigzags. Four phase winding outputs created in each group are connected with inputs of one of four-phase gate bridges: outputs of winding group (5) - with inputs of bridge (1), group (6) - with inputs of bridge (2), group (7) - with inputs of bridge (3). Among themselves the bridges are connected by outputs with different poles, at that, load (10) is connected to output terminals (8, 9) of bridge (1) and bridge (3) respectively, and tap leads with terminals (11, 12) are made from connection points of bridges (1, 2) and (2, 3). |
 Push-and-pull inverter / 2331961Result is achieved by implementation of two resistor dividers of voltage and two current stabilisers in push-and-pull inverter. For this purpose, two voltage regulator diodes and three resistors are introduced, one of the said resistors being current sensor for two current stabilisers and current limiter at the same time. The said introductions allow for keeping equal magnification current in both inverter sides enabling eliminating of the main push-and-pull inverter drawback such as over-magnification asymmetry, increasing specific power of the proposed inverter, improving transistor switch switching over dynamics, reducing current bump amplitude and, as a result, reducing heating and likelihood of transistor switches disruption. Thus, reliable operation of the said push-and pull inverter within wide range of supplied voltage is ensured. |
 Method and device for wireless transmission of electric power / 2322745The high-frequency electricity is transmitted through one conducting channel formed by the boundary layer of a long-lasting vortex hopper serving as a conductor self-maintaining its structure due to the directed axial flow of electrons and rotation about the channel axis. A traveling wave of the high-frequency current and of the magnetic field at a frequency equal to the rotational speed of the vortex boundary layer is generated in the swirl channel. As a result, the transmitter inductance-capacitance resonance and the reactance maximum of the capacitance charging current are conducted through the resonating channel. The power for maintaining the rotation of the swirl channel is taken from the environment. |
 Electrical energy transmission method and device / 2310964Proposed method used for electrical energy transmission beyond Earth atmosphere in vacuum between space vehicles or planets from Earth to space bodies and vice versa, from space to Earth, as well as from one point on Earth to another through atmosphere and space dispensing with relativistic beam accelerators and lasers includes generation of high-frequency electromagnetic waves and their transmission over conductive channel between electrical energy sources and receivers. High-voltage electromagnetic waves are generated in high-frequency resonance-tuned transformer, amplified in voltage to (0.5-100) x 106 V in quarter-wave resonance-tuned line that has spiral waveguide and natural capacitor at line end by supplying electromagnetic waves from high-voltage resonance-tuned transformer to spiral waveguide input at frequency f0 = 1-1000 kHz synchronized with voltage-wave motion time period Tk from spiral waveguide input to natural capacitor and reflected wave return to spiral waveguide input. Electrical energy is stored in natural capacitor. Conductive channel is organized by emission of streamers and production of electromagnetic radiation flow from end of needle-type conductive channel generator at resonant frequency f0 = 1 - 1000 kHz and voltage V = (0.5-100) x 106 V by connecting natural capacitor thereto. |
 Wireless charging system (variants) / 2306654Device contains, on power supply side, a narrowband high frequency generator with emitting antenna, and on the side of charging block, a receiving antenna, voltage inverter, charge-discharge controller, block of accumulators and/or block of super-capacitors, while the inverter contains at its input a rectifier and impulse voltage multiplexer, containing "n" cascades (where "n"≥2), each of which contains serially coupled first diode, accumulating capacitor, and second diode, coupled in accord with first one, and also MOS-transistor with induced channel, drain of which is connected to gate and to connection point of first diode and accumulating capacitor, point of connection of which with second diode is connected to source of MOS-transistor with induced channel of previous cascade, while interconnected free clamps of first diodes and correspondingly interconnected free clamps of second diodes act as input of impulse voltage multiplexer, output of which is the source of MOS-transistor with induced last cascade channel and connection point of accumulating capacitor and second diode of first cascade, and as a variant - device contains on power supply side a narrowband high frequency generator with emitting antenna, and on the side of charging block - receiving antenna, voltage inverter, charge-discharge controller, block of accumulators and/or block of super-capacitors, while inverter contains at input a rectifier and impulse multiplexer of voltage, containing "n" cascades (where "n"≥2), each of which contains serially connected first diode, accumulating capacitor and second diode, enabled in accord with first one, and also first and second field transistors, while point of connection of first diode and accumulating capacitor is connected to gate of first field transistor and to drain of second field transistor, source of first field transistor is connected to gate of second field transistor, while free clamps of first cascade diodes are combined, free clamps of second cascade diodes are combined and drains of first field transistors are connected to them, source of second field transistor of cascade is connected to point of connection of capacitor and second diode of next cascade, and source of second field transistor of last cascade and point of connection of capacitor and second diode of first cascade act as output of impulse multiplexer of voltage, as input of which interconnected free outputs of first diodes and correspondingly interconnected free outputs of second diodes are used. |
 Wireless charging system with reverse communication / 2306653Claimed system contains high frequency generator at powering side, input of which is connected to control output of controller, and output - to first input of modulator, output of which is connected to antenna and to input of decoder, output of which through an amplifier is connected to input of controller, information output of which is connected to second input of modulator, and on the side of charging block, an antenna connected to output of modulator and to inputs of decoder and inverter, outputs of which are connected respectively to information and energy inputs of charge-discharge controller, which is connected to accumulators block and/or super-capacitors block, while information and control outputs of charge-discharge controller are connected respectively to first input of modulator and to input of generator, output of which is connected to second input of modulator, while inverter contains serially connected rectifier and voltage multiplexer. |
 Method and device for transferring electric energy (variants) / 2273939Transferring of electric energy is performed below ground or below water in resonance mode at resonance frequency 50 Hz - 50 KHz and voltage 1-1000 kV, current density 1-500 A/mm2 along one-wire electric-insulated cable, in particular, multi-wired, with length 1-20000 km with section 0,01-1000 cm2, cable diameter of which exceeds wire diameter in 5-100 times. In accordance to another variant electric energy is transferred below ground or below water in resonance mode along axial-symmetric one-wire wave duct inside hermetic hollow dielectric cylinder-shaped channel in insulating gas atmosphere, in particular, electronic gas under pressure 1-10 kg/cm2. In accordance to yet another variant of method electric energy is transferred along single electro-statically screened and electric-insulated wave duct of surface wave inside the hollow-bodied cylinder-shaped screen and hermetic dielectric channel in atmosphere of insulated gas. High-voltage line may be made below ground or below water in form of one-conductor wave guide with length 1-20000 km, section 0,1-1000 cm, mounted in axial-symmetric manner inside the pipeline with diameter 0,02-10 m made of dielectric material. To increase transferred voltage and power wave guide is made of electric-insulated cable with insulation thickness 3-300 mm, and space between wave guide and pipeline is filled with electric-insulating gas under pressure, for example, electronic gas. High-voltage line is made in form of one-wire wave duct with length 1-20000 km, section 0,01-1000 cm2, mounted in axial-symmetric manner inside the pipeline with diameter 0,02-10 m of dielectric material, and contains electric screen, made in form of multiple electric-insulated from each other non-closed conductive cylinder-shaped covers, total length of which is equal to length of wave guide, and length of each conducting cover is 1-1000 meters. |
 Method and device for electrical energy transmission / 2255406Electrical energy is transmitted in the form of high-frequency resonant waves over circuit set up of high-frequency oscillator and two step-up and one step-down high-frequency Tesla transformers. High-voltage potential and electrical energy are conveyed from internal lead of step-up Tesla transformer high-voltage winding over single-wire line to step-down Tesla transformer; electric current is rectified and transferred to load by connecting low-voltage winding of step-down Tesla transformer to two inputs of single-phase bridge rectifier and two outputs of this rectifier, to load. Reactive-current resonant waves of wavelength λ = 2LAB/n, where n is integer number and 2LAB is electric circuit length between external leads A and B of high-voltage windings of transformers, are transferred from resonance-tuned circuit of low-voltage winding of step-up Tesla transformer to resonant-tuned circuit of low-voltage winding of step-down Tesla transformer over single-wire line and to ground line by connecting external leads A and B of high-voltage windings of step-up and step-down Tesla transformers disposed in close proximity of low-voltage winding lead to ground and converting reactive current to direct current within inverter by inserting the latter between rectifier and load. |
 Method and device for electrical energy transmission / 2255405Proposed device designed for power transmission to ground and flying vehicles has high-frequency generator connected to resonance-tuned circuit of primary winding of high-frequency step-up Tesla transformer, and single-wire transmission line connected on one end to one internal lead of mentioned Tesla transformer high-voltage winding and on other end, to load. Adjacent leads of primary and secondary windings of high-frequency step-up Tesla transformer are interconnected and grounded, Single-wire transmission line is connected to load through one of single-phase bridge rectifier inputs, other input of this rectifier being connected to natural capacitor in the form of ground, water, or insulated body surface. |
 Method for manufacturing optical devices and appropriated devices / 2335035Invention is related to optical devices manufactured by method induced with additive of quantum well (QW) mixing. Method for manufacturing optical device, in which body from which this device is manufactured, contains at least one quantum well (QW), includes stages whereat mixing of doped material is caused with the said, at least, one quantum well, this doped material containing copper (Cu). |
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Method for manufacturing optical devices and appropriated devices / 2335035 Invention is related to optical devices manufactured by method induced with additive of quantum well (QW) mixing. Method for manufacturing optical device, in which body from which this device is manufactured, contains at least one quantum well (QW), includes stages whereat mixing of doped material is caused with the said, at least, one quantum well, this doped material containing copper (Cu). |
 Quadrature photo-receiving device / 2335034Invention is related to optoelectronics and interferometry and intended for measurement of spatial distribution of light intensity in interference field formed by counter luminous fluxes. Quadrature photo-receiving device contains photodetector including four interferentially sensitive photoelectric element, two of which are reference ones. Difference of optical distances from the first photoelectric element to the plane that is perpendicular to measured luminous flux and that limits optically distant surface of photodetector for the first photoelectric element and from i-photoelectric element to this plane is calculated from the proposed formula, signals from odd photoelectric elements of photodetector being supplied to appropriate inlets of the first differential amplifier, and signals from even photoelectric elements of photodetector to appropriate inlets of the second differential amplifier. |
 Transfiguration method of optical emission from distant object and facility for its implementation / 2334305Method is based on dividing of taking from distant object of luminous flux for two current of equal intensity with further forming from it optical beams of wedge shape, tapering in propagation direction and common edge on its tops, located in zone of optical emission converter. Concentrator system for implementation of method contains two elliptic reflector of sulcate shape for supplying of concentrated emission to the extensive emission converter and located between reflectors two reflective plates of parabolic section. The first focal lines of reflectors and plates overlapped in pairs, and the second focal line of reflectors are located in area of extensive emission converter. |
FIELD: electrical engineering.
SUBSTANCE: invention relates to remote transfer and conversion of super-high-frequency energy into DC electrical power. The proposed method consists in fitting an aluminium foil enclosure on over the entire surface of the vehicle airframe skin. The super-high-frequency converter is made in a material representing a mix of two chemical solid-state components with grain size not over 30 to 50 microns, taken in equal proportion but different atomic numbers, and forming, when combined, a dipole solid-state matrix. Note that the said bi-component mix is applied uniformly onto the said skin enclosure, the like poles of the dipole matrix being combined and connected to appropriate terminals of the vehicle flight control components.
EFFECT: higher efficiency power supply.
2 dwg
The invention relates to techniques for transmitting and converting microwave energy into electrical energy direct current, designed to provide balloon-type devices helicopters, airplanes, probes, etc. operating at the application to the apparatus shaped electric field and is used to monitor the condition of thermodynamics of the atmosphere, the detection of emergencies, disasters, natural disasters and other natural and man-made anomalies.
Known methods of energy supply electrodynamic aircraft, namely, that the movement of the apparatus to create the electrical voltage applied to the electrodes of the aircraft, one of which is executed in the form of a thin straight rod, the other in the form of systems consisting of separate elements interconnected electrically, and the power source (the effect of brown) [U.S. patent No. 3187206, NCI 310-5 (copy counterpart attached].
These very promising ways of energy saving, but without the energy recharge their operational capability is limited, and therefore, the time of their stay in space is also limited.
Known processes for the supply of aircraft, consisting in the making of microwave energy, is opriate microwave energy, sent from a terrestrial source, the transformation of this energy into energy DC [microwave ENERGY. Edited EAKNESS. Volume 1. The generation. Transfer, Straightening. Edited Edelivery. Ed. "The world". M., 1971 // passing a beam of electromagnetic waves in free space. Guba, Swearing. S-387 (similar to attached)].
The coefficient of transmission of microwave energy using a parabolic antenna with a diameter of up to 30.5 m is not more than 18% when the transmission distance is 22 feet Therefore, the use of such a channel is expensive and unprofitable.
The most cost-effective of the claimed invention is a power supply system of the aircraft electrodynamic apparatus containing ground source of microwave energy and transmitting antenna form the energy into a narrow beam receiving antenna on an aircraft, inverter microwave energy to the energy DC [microwave ENERGY. Edited EAKNESS. Volume 3. The use of the energy of ultra-high frequencies in medicine, science and technology. Edited Edelivery. Ed. Mir M., 1971. Nutrition aerospace aircraft microwave energy. Brown. P.77-88 (prototype shown)].
The disadvantage of this method is the need to create a receiving antenna on an aircraft large area to extend the service life in ozdok, however, a large area of the receiving antenna generates a large vetrano pressure on the system, and to stabilize its position in the air requires additional energy. In addition, the receiving antenna should be focused in the direction of the radiating antenna.
The method of power supply aerial electrodynamic apparatus is that radiate from an external source of microwave energy, take this energy to Board the aircraft, convert it aboard in energy DC and used to stabilize the power of the elements of the flight control and device control flight modes, which are placed under the dielectric casing of the device, enter the sheath of aluminum foil and put it over the entire surface of the plating apparatus and the inverter microwave energy is made of a material which is a mixture of two chemical semiconductor granulation not more than 30...50 µm, taken in equal proportions, but with different atomic numbers, together forming the dipole semiconductor matrix, with a two-part mixture is applied uniformly in the form of a coating on the surface of the shell thickness in 2...3 times bigger than the size of the granules, with like poles of the dipole matrix unite IU is themselves and connect them to the appropriate terminals of the elements of the flight control apparatus and the device control mode of flight.
The advantage of the proposed technical solution is simple technology of energy supply, allowing to extend the presence of the device in the air long flight. The continuity of the power contact of the transmitting and receiving antennas, regardless of the orientation of the device in space can increase the efficiency of the system due to developed effective surface of the transducer, combining the functions of the receiving antenna.
1 shows a diagram of the power supply system of the aircraft from the ground station microwave (MW) energy that implements the method; figure 2 - cross section of the plating apparatus 1.
The circuit that implements the method, confirms statics his health. The schema contains ground source 1 microwave energy from the antenna 2 of the radiation of microwave energy, the aircraft 3 controls and control (not shown)powered by the battery and inside design of the device 3 under the dielectric casing 4, the shell 5 of the aluminum foil and the inverter 6 of microwave energy into electrical energy, DC, intended for electrical power controls and flight control and other functions of the apparatus 3.
The shell 5 is made of aluminum foil. The proposed material, on the one hand, today is a large electrical conductivity, low weight, and the circular arrangement of the shell 5 on the casing 4 is designed to provide a more complete reflection of energy from the surface of the shell 5 in the Converter 6. The shell 5 or glued to the casing 4, or not fix it another way.
Semiconductor Converter 6 performs the function of simultaneously receiving antenna and transmitter of microwave energy into the energy of DC.
The Converter 6 is made of a semiconductor of a mixture of the two semiconductor components with a grain of not more than 30...50 microns each. One of the components has an atomic number greater than the atomic number of the second component. As components can be, for example, materials gallium (Ga31with atomic number 31 and arsenic (As33with atomic number 33 or other couples: gallium - antimony; cadmium - tellurium, etc. the combination of the two semiconductor components allows you to automatically ensure dipole rectifier matrix, the positive and negative poles of the charges which are connected with the corresponding terminals of the control mechanism and control regime of the flight apparatus 3. This mixture is applied in the form of a coating on the surface of the shell 5, for example, by plasma or flame spraying thickness of about 2...3 times bigger than the size of the grains granulation components. The coating process of the criminal code of the above methods does not violate the structure of the material of the shell 5, since experience shows that these methods can be used for coating any material, even on the paper backing.
The presence of the semiconductor Converter 6 provides efficient conversion of microwave energy into the energy of direct current, and the shell 5 of aluminum foil allows you to increase the power conversion of microwave energy 1.75 times due to direct transmission of microwave energy through a transformer 6 and the reverse passage of microwave energy through a transformer 6, reflected from the material of the shell 5 [see str given similar].
The specified material properties of the shell 5 and inverter 6 together increase the efficiency of the system.
The system
Aircraft 3 starts with the earth's surface due to its own resources, provide self-contained power supply such as a battery. After dialing the desired height unit 3 turns on the system power supply, extending the operational viability of the device 3. With ground source 1 microwave oscillations radiated energy transmitting antenna 2 with the specified parameters. This radiation is supplied to the inverter 6 of the aircraft 3, which is both a transducer and a receiving antenna of microwave energy. Microwave energy is received and converted into Preobrazovatel the 6 sides of the device into electrical energy DC which ensures the supply of the elements of the flight control device 3, and device monitoring mode of flight.
The advantage of the proposed technical solution is simple technology method of power supply, allowing you to extend the presence of the device in the air long flight. The continuity of the power contact of the transmitting and receiving antennas, regardless of the orientation of the device in space can increase the efficiency of the system due to developed effective surface of the Converter.
The way of energy flying electrodynamic machines, namely, that radiate from an external source of microwave energy, take this energy to Board the aircraft, convert it aboard in energy DC and used to stabilize the power of the elements of the flight control and device control flight modes, which are placed under the dielectric casing of the apparatus, characterized in that the injected shell of aluminum foil and put it over the entire surface of the plating apparatus and the inverter microwave energy is made of a material which is a mixture of two chemical semiconductor granulation not more than 30...50 MK is, taken in equal proportions, but with different atomic numbers, together forming the dipole semiconductor matrix, with a two-part mixture is applied uniformly in the form of a coating on the surface of the shell thickness in 2...3 times bigger than the size of the granules, with like poles of the dipole matrix unite among themselves and connect them to the appropriate terminals of the elements of the flight control apparatus and the device control mode of flight.