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33 results about "Energy system design" patented technology

Impact-resistance optimization design method of multilevel energy absorption of railroad train

The invention discloses an impact-resistance optimization design method of multilevel energy absorption of a railroad train. A one-dimensional longitudinal flexible dynamic model which can accuratelyreflects critical responses of the railroad train in a crash process is established, and mainly consists of a coupler contact end part unit, a rigid connection unit, a coupler spring element and a train body rod element. Main technology of the method includes longitudinal load-deformation feature extraction of a single-section train body, global optimization method-based reverse calculation of mechanical properties of stiffness and damping parameters of the simplified nonlinear train body rod element, establishment of a one-dimensional longitudinal flexible dynamic model of a whole-array formation and train energy absorption system parameter optimization process building. The method increases an accuracy rate of the one-dimensional simplified model on predicting train formation dynamic-response information, also greatly saves single-analysis machine time, solves the problem that synchronous optimization of energy absorption parameters of whole-formation trains is always limited by too-long consumed single-analysis time in the past, and can be used for crash energy system design and parameter optimization of a train design stage.
Owner:CHINA RAILWAYS CORPORATION

Calculating method for determining cooling and heating load of building in hot-summer and cold-winter zone by utilizing pivot element decoupling method

ActiveCN104866702ASimple processLarge heating and cooling loadSpecial data processing applicationsResting timeRest time
The invention discloses a calculating method for determining cooling and heating load of a building in a hot-summer and cold-winter zone by utilizing a pivot element decoupling method. Factors influencing the cooling and heating load of the building are divided into two main types: the self attribute parameter and the operation attribute parameter of the building. The calculation is conducted by the following steps: according to the indoor comprehensive heat dissipation power, calculating the benchmark of the cooling and heating load; according to the work and rest time in the building, calculating the radiation coefficient and the temperature difference coefficient; according to the orientation, the window-wall ratio, the external wall heat resistance and the window heat resistance of the building, calculating the correction factors of the orientation, the window-wall ratio, the external wall heat resistance and the window heat resistance in sequence; according to the coupling influence of the self attribute parameter and the operation attribute parameter, calculating the coupling influence factor; finally calculating the average cold and hot power of unit area of the building in summer (winter) and the cooling (heating) capacity in various time periods of a typical day. The calculating method can meet the precision requirements of engineering application, quickly and economically calculate the cooling and heating load of the typical building in the hot-summer and cold-winter zone, guide the distributed energy system design, and provide reference for system operation and optimization.
Owner:SOUTHEAST UNIV

Data correction method of high-altitude propeller wind tunnel test for influence of Reynolds number

The invention provides a data correction method of a high-altitude propeller wind tunnel test for influence of Reynolds number. The data correction method comprises the following steps: according to the similarity criterion of an advance ratio and a tip Mach number, experimental parameters of the high-altitude propeller scale model wind tunnel test are determined; the wind tunnel test of the propeller scale model is carried out; a tension coefficient experimental value C<T,exp> and a power coefficient experimental value C<P,exp> are measured; the tension coefficient experimental value and thepower coefficient experimental value are corrected; and a corrected propeller propulsion efficiency is calculated according to a propeller propulsion efficiency formula. The invention takes into account the difference between the Reynolds number experimental value under the condition of the equal advance ratio and the equal tip Mach number and the Reynolds number under the real working condition of the high-altitude propeller; more accurate aerodynamic performance experimental data such as the high-altitude propeller tension coefficient, the power coefficient and the propulsion efficiency is obtained by using the proposed correction method; so reliable basic data is provided for designing a propulsion system and an energy system of a high-altitude low-dynamic aircraft.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

A method for design of photoelectric micro power system based on model analysis

The present invention discloses a method for design of photoelectric micro power system based on model analysis and pertains to the technical field of photoelectricity. According to the node composition and functional requirements of the integrated photoelectric micro power sensor, the present invention divides the sensor into four parts: energy conversion subsystem, energy storage subsystem, energy management subsystem and sensor nodes. The energy parameters of these four parts are analyzed. According to the power supply method to sensor nodes from the photoelectric micro power system, a design model for the relations between different energy parameters of the photoelectric micro power system is established. According to the functional requirements of the photoelectric micro power and the environmental features of the areas where micro power is used, system design parameters are determined. From system design parameters and micro power design model, the area of photovoltaic cell and the cell circuit of micro power system are determined, thus completing the design of integrated sensor photoelectric micro power system. The present invention uses a design model to greatly simplify system design process and establish a universal design method for the design of photoelectric micro power system.
Owner:BEIJING INSTITUTE OF TECHNOLOGYGY

Spacecraft energy system design method

The invention relates to a spacecraft energy system design method. The method comprises the following steps: S1, constructing a general spacecraft power supply and distribution system model; s2, inputting prior on-orbit data into a recurrent neural network (RNN) for data generalization, and realizing refined mining of prior empirical data; s3, constructing an actual spacecraft power supply and distribution system model; s4, in a ground design stage, classifying energy balance according to a spacecraft task sequence, establishing sub-samples, and generating a ground test case; s5, correcting the modelable state of the actual spacecraft power supply and distribution system model by adopting a data mining method according to the actual ground test data of the spacecraft, and performing data fitting on the non-modeled state of the actual spacecraft power supply and distribution system model; and S6, in an in-orbit operation stage, performing in-orbit high-precision correction on the actual spacecraft power supply and distribution system model by adopting a data mining method according to the in-orbit measured data. The method has the beneficial effects that the spacecraft energy subsystem is designed according to the operating environment, the task sequence, the working state of each single machine and the previous on-orbit data.
Owner:INNOVATION ACAD FOR MICROSATELLITES OF CAS +1

Acquisition method and system for collaborative optimization comprehensive energy system design scheme

The invention discloses a collaborative optimization comprehensive energy system design scheme obtaining method and system, and the method comprises the steps: determining the types and number of alternative equipment, and taking the total amount as the number of equipment during optimization; according to the number and the type of the equipment, determining the number and the type of variables including an equipment sequence, equipment capacity and operation parameters by using a unified model; based on the unified model of the equipment, expressing the structure of the comprehensive energysystem as a chain structure; performing simulating in a chain operation mode of a chain structure to obtain operation data, and solving variables to obtain a sorting result of equipment in the chain structure by taking a structure sequence, installed capacity and control parameters of the equipment as the variables and taking primary energy consumption, energy supply cost and carbon emission as targets; and obtaining a system design result according to the solving result. The invention discloses an integrated design method, and aims to fundamentally solve the problem of independent optimization failure caused by multi-equipment multi-working-condition, complex and variable structure and multi-energy-flow operation strong coupling.
Owner:SHANDONG UNIV

Solar rotor unmanned aerial vehicle design method based on self-adjusting search pigeon flock intelligence

The invention discloses a solar rotor unmanned aerial vehicle design method based on self-adjusting search pigeon flock intelligence. The method comprises the steps that 1, solar array modeling is conducted; 2, modeling the rotor unmanned aerial vehicle and a power system; 3, designing an MPPT controller based on a self-adjusting search pigeon inspired optimization algorithm; 4, designing an energy management strategy based on a finite-state machine; 5, optimizing the design of the solar rotor energy system; and step 6, flight control system parameter optimization based on a self-adjusting search pigeon inspired optimization algorithm. The invention provides a complete and normative solar rotor unmanned aerial vehicle design method and a process framework. A self-adjusting search pigeon inspired optimization algorithm is designed and applied to design of an MPPT controller, the tracking capability of the maximum power point of a solar array is improved, a cascade PID flight control system is decomposed into a plurality of channels according to the characteristics of the cascade PID flight control system, the self-adjusting search pigeon inspired optimization algorithm is adopted in a layered mode for optimization, the optimization problem is greatly simplified, and the maximum power point tracking capability of the solar array is improved. And the reliability of design results is improved.
Owner:BEIHANG UNIV

Correction method of high-altitude propeller wind tunnel test data for the influence of Reynolds number

The invention provides a data correction method of a high-altitude propeller wind tunnel test for influence of Reynolds number. The data correction method comprises the following steps: according to the similarity criterion of an advance ratio and a tip Mach number, experimental parameters of the high-altitude propeller scale model wind tunnel test are determined; the wind tunnel test of the propeller scale model is carried out; a tension coefficient experimental value C<T,exp> and a power coefficient experimental value C<P,exp> are measured; the tension coefficient experimental value and thepower coefficient experimental value are corrected; and a corrected propeller propulsion efficiency is calculated according to a propeller propulsion efficiency formula. The invention takes into account the difference between the Reynolds number experimental value under the condition of the equal advance ratio and the equal tip Mach number and the Reynolds number under the real working condition of the high-altitude propeller; more accurate aerodynamic performance experimental data such as the high-altitude propeller tension coefficient, the power coefficient and the propulsion efficiency is obtained by using the proposed correction method; so reliable basic data is provided for designing a propulsion system and an energy system of a high-altitude low-dynamic aircraft.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

Premixing device and micro gas turbine

The invention relates to the field of energy system design and discloses a premixing device and a micro gas turbine. The premixing device is used for mixing fuel and air, wherein the fuel comprises pilot-stage fuel and primary-stage fuel. The premixing device comprises a shell. The shell comprises a front plate, a rear plate and a plurality of rotational flow blades connected with the front plateand the rear plate. The multiple rotational flow blades are evenly arranged in the circumferential direction of the front plate to form an air inlet, and the center of the front plate is provided witha pilot-stage fuel inlet. A primary-stage fuel inlet is formed in the edge of the end face of the end, connected with the rotational flow blades, of the rear plate, and a mixed gas outlet is formed in the other end of the rear plate. The primary-stage fuel is sprayed in towards an upper plate, more distributed around the interior of the shell and less distributed in the middle of the shell, the pilot-stage fuel is sprayed in towards a lower plate, less distributed around the interior of the shell and more distributed in the middle of the shell, therefore, uniformity of mixing of the pilot-stage fuel, the primary-stage fuel and the air can be improved through the premixing device, the structure is simple, and operation is convenient.
Owner:新奥能源动力科技(上海)有限公司

Temperature difference power generation control method and control device based on building outer wall

The invention relates to a building outer wall thermoelectric power generation control method and device based on solar radiation daily variation, belongs to the field of building new energy and energy conservation, and solves the problems that in the prior art, a building outer envelope structure thermoelectric power generation technology purely utilizes indoor and outdoor temperature difference, the power generation efficiency is low, and the power generation amount is uneven. According to the application, a plurality of thermoelectric power generation units are arranged on the building outer wall, and through hourly solar radiation analysis of the building outer wall, the maximum average temperature difference between the thermoelectric power generation units in a shadow area and a direct radiation area of the building outer wall and the minimum lead length are taken as control targets; and the building outer wall shadow area thermoelectric power generation unit and the direct incidence area thermoelectric power generation unit are connected in series to form an optimized thermoelectric power generation unit group. Through the power generation control method and device, the building outer wall temperature difference power generation efficiency and the hourly stability of the power generation amount can be remarkably improved, the method and device can be widely applied to the building new energy field such as building outer wall power generation, and support is provided for urban distributed energy system design.
Owner:CHANGAN UNIV

Correction method of high-altitude propeller wind tunnel test data for the influence of tip Mach number

The invention provides a high-altitude propeller wind tunnel test data correction method aiming at the influence of a tip Mach number, which comprises the following steps of: determining test parameters of a wind tunnel test of a high-altitude propeller scaling model according to an advance ratio and a Reynolds number similarity criterion; performing the wind tunnel test on the propeller scaling model to obtain a tension coefficient test value C<T, exp> and a power coefficient test value C<p, exp>; and correcting the tension coefficient test value and the power coefficient test value, and calculating according to a propeller propulsion efficiency formula to obtain a corrected propeller propulsion efficiency. According to the high-altitude propeller wind tunnel test data correction method,the difference between a tip Mach number test value under the conditions of equal advance ratio and equal Reynolds number and a tip Mach number under the real working condition of a high-altitude propeller is considered, and the provided high-altitude propeller wind tunnel test data correction method is utilized to obtain accurate aerodynamic performance test data such as a tension coefficient, apower coefficient, a propulsion efficiency and the like of the high-altitude propeller, so that reliable basic data are provided for the design of a propulsion system and an energy system of a high-altitude low-dynamic aircraft.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

A method for design of photoelectric micro power system based on model analysis

The present invention discloses a method for design of photoelectric micro power system based on model analysis and pertains to the technical field of photoelectricity. According to the node composition and functional requirements of the integrated photoelectric micro power sensor, the present invention divides the sensor into four parts: energy conversion subsystem, energy storage subsystem, energy management subsystem and sensor nodes. The energy parameters of these four parts are analyzed. According to the power supply method to sensor nodes from the photoelectric micro power system, a design model for the relations between different energy parameters of the photoelectric micro power system is established. According to the functional requirements of the photoelectric micro power and theenvironmental features of the areas where micro power is used, system design parameters are determined. From system design parameters and micro power design model, the area of photovoltaic cell and the cell circuit of micro power system are determined, thus completing the design of integrated sensor photoelectric micro power system. The present invention uses a design model to greatly simplify system design process and establish a universal design method for the design of photoelectric micro power system.
Owner:BEIJING INSTITUTE OF TECHNOLOGYGY

A shock resistance optimization design method for multi-stage energy absorption of rail trains

The invention discloses an impact-resistance optimization design method of multilevel energy absorption of a railroad train. A one-dimensional longitudinal flexible dynamic model which can accuratelyreflects critical responses of the railroad train in a crash process is established, and mainly consists of a coupler contact end part unit, a rigid connection unit, a coupler spring element and a train body rod element. Main technology of the method includes longitudinal load-deformation feature extraction of a single-section train body, global optimization method-based reverse calculation of mechanical properties of stiffness and damping parameters of the simplified nonlinear train body rod element, establishment of a one-dimensional longitudinal flexible dynamic model of a whole-array formation and train energy absorption system parameter optimization process building. The method increases an accuracy rate of the one-dimensional simplified model on predicting train formation dynamic-response information, also greatly saves single-analysis machine time, solves the problem that synchronous optimization of energy absorption parameters of whole-formation trains is always limited by too-long consumed single-analysis time in the past, and can be used for crash energy system design and parameter optimization of a train design stage.
Owner:CHINA RAILWAYS CORPORATION

A Method for Calculating Building Loads in Hot Summer and Cold Winter Regions Using Principal Component Decoupling

ActiveCN104866702BSimple processLarge heating and cooling loadSpecial data processing applicationsCold seasonEngineering
The invention discloses a calculation method for determining building cooling and heating loads in hot summer and cold winter regions by using a principal component decoupling method, and divides factors affecting building cooling and heating loads into two categories: building own attribute parameters and operating attribute parameters. Calculation is carried out according to the following steps: Calculate the benchmark of cooling and heating load based on the indoor comprehensive heat dissipation power; calculate the radiation coefficient and temperature difference coefficient based on the building’s work and rest time; Calculate their correction coefficients in turn; calculate the coupling influence coefficient according to the coupling influence of its own attribute parameters and operating attribute parameters; finally calculate the average cooling and heating power per unit area of ​​the building in summer (winter) season and the cooling ( heat) amount. The invention can not only meet the precision requirements of engineering applications, but also quickly and economically calculate the cooling and heating loads of typical buildings in hot summer and cold winter regions, guide the design of distributed energy systems, and provide a basis for system operation optimization.
Owner:SOUTHEAST UNIV
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