Simulation solving method, device and computer equipment of aero-engine

Abstract

The application relates to an aero-engine simulation solving method, device and computer equipment. The method comprises the following steps: acquiring system running function information, system structure data and system correlation information between each structural system of an aero-engine, and constructing a sub-simulation running model of each structural system; identifying data interaction correlation information and running interaction correlation information between each structural system, thereby constructing simulation interaction information between each structural system, performing simulation correlation processing on each structural system, obtaining a joint simulation model of the aero-engine, generating a joint simulation result of the aero-engine through the joint simulation model based on demand input data of the aero-engine, and identifying running solving data of the aero-engine through a joint simulation solving algorithm. The method can improve the simulation efficiency and simulation convergence robustness of the aero-engine.

Description

TECHNICAL FIELD

[0001] The present application relates to the technical field of aero-engine modeling simulation, and in particular to a simulation solving method and device for an aero-engine and a computer device. BACKGROUND

[0002] In the working process of research and development, improvement, optimization, adjustment, design, transformation and experiment of an aero-engine, in order to reduce cost loss, safety risk and operation effect, the aero-engine is often modeled for simulation and simulation to perform the working process. Therefore, how to improve the modeling accuracy of the constructed aero-engine model and the simulation operation accuracy of the model is the current research focus.

[0003] The traditional aero-engine simulation modeling method is to construct an entire aero-engine model by single system simulation modeling. However, single system modeling cannot simulate the entire aero-engine operation process, and the simulation result obtained in the simulation process also has a large deviation, thereby the simulation accuracy of the aero-engine is poor. SUMMARY

[0004] Therefore, it is necessary to provide a simulation solving method and device for an aero-engine, a computer device, a computer readable storage medium and a computer program product in view of the above technical problems.

[0005] In a first aspect, the present application provides a simulation solving method for an aero-engine, comprising:

[0006] obtaining system operation function information of each structural system of the aero-engine, system structure data of each structural system, and system association information between each structural system, and constructing a sub-simulation operation model of each structural system based on the system operation function information of each structural system and the system structure data of each structural system;

[0007] based on the system association information between each structural system, identifying data interaction association information between each structural system and operation interaction association information between each structural system, and constructing simulation interaction information between each structural system based on the data interaction association information between each structural system and the operation interaction association information between each structural system;

[0008] based on the simulation interaction information between each structural system, performing simulation association processing on each structural system to obtain a joint simulation model of the aero-engine, and collecting demand input data of the aero-engine;

[0009] Based on the demand input data, a joint simulation result of the aero-engine is generated through the joint simulation model of the aero-engine, and based on the joint simulation result, operation solving data of the aero-engine is identified through a joint simulation solving algorithm.

[0010] Optionally, the sub-simulation operation model of each structure system is constructed based on the system operation function information of each structure system and the system structure data of each structure system, and the method comprises the following steps:

[0011] Based on the system structure data of each structure system, a system structure model of each structure system is constructed through a three-dimensional modeling program, and for each structure system, structure operation data of each operation function type is identified based on the system operation function information of the structure system.

[0012] Based on the structure operation data of each operation function type, the structure operation data of each operation function type is converted into structure operation parameters of each operation function type through a data parameter conversion program, and the system structure model of the structure system is adjusted based on the structure operation parameters of each operation function type to obtain the sub-simulation operation model of the structure system.

[0013] Optionally, the data interaction association information between the structure systems and the operation interaction association information between the structure systems are identified based on the system association information between the structure systems, and the method comprises the following steps:

[0014] Based on the system association information between the structure systems, association information of each association type between the structure systems is identified, and an interaction type to which each association type belongs is queried in an association database.

[0015] Based on the association information of each association type corresponding to the data interaction type, data interaction information between the structure systems and data transmission information between the structure systems are identified, and the data interaction information between the structure systems and the data transmission information between the structure systems are taken as the data interaction association information between the structure systems.

[0016] Based on the association information of each association type corresponding to the operation interaction type, operation interaction modes between the structure systems and operation interaction processes between the structure systems are identified, and the operation interaction modes between the structure systems and the operation interaction processes between the structure systems are taken as the operation interaction association information between the structure systems.

[0017] Optionally, the simulation interaction information between the structure systems is constructed based on the data interaction association information between the structure systems and the operation interaction association information between the structure systems, and the simulation interaction information between the structure systems comprises:

[0018] The simulation operation interaction flow between the structure systems is constructed based on the operation interaction mode between the structure systems and the operation interaction flow between the structure systems.

[0019] The simulation data interaction flow between the structure systems is constructed based on the data interaction information between the structure systems and the data transmission information between the structure systems.

[0020] The simulation operation interaction flow between the structure systems and the simulation data interaction flow between the structure systems are taken as the simulation interaction information between the structure systems.

[0021] Optionally, the simulation association processing of the structure systems is performed based on the simulation interaction information between the structure systems, and a joint simulation model of the aero-engine is obtained, and the simulation association processing of the structure systems comprises:

[0022] The physical connection information between the structure systems is collected, and the model connection processing of the sub-simulation operation model of the structure systems is performed based on the physical connection information between the structure systems, and a joint three-dimensional structure model of the aero-engine is obtained.

[0023] The simulation interaction parameters between the structure systems in the joint three-dimensional structure model are constructed based on the simulation interaction information between the structure systems, and the simulation interaction parameters between all the structure systems are used to adjust the joint three-dimensional structure model, and a joint simulation model of the aero-engine is obtained.

[0024] Optionally, the joint simulation solving algorithm comprises the system simulation solving algorithm of each structure system and the system association solving algorithm between each structure system, and the operation solving data of the aero-engine is identified based on the joint simulation result by using the joint simulation solving algorithm, and the operation solving data of the aero-engine comprises:

[0025] The joint simulation result is split into the system simulation result of each structure system.

[0026] The system association solving sequence between the structure systems and the system algorithm solving sequence corresponding to the system simulation solving algorithm of each structure system are identified based on the simulation interaction information between the structure systems, and the system simulation solving data of each structure system is calculated by using the system simulation solving algorithm of each structure system according to the simulation solving sequence of each structure system based on the system simulation result of each structure system.

[0027] Based on the system simulation solution data of each structural system, the operation solution data of the aero-engine is calculated according to the system correlation solution algorithm between each structural system.

[0028] In a second aspect, the present application further provides a simulation solution device of an aero-engine, comprising:

[0029] An acquisition module is configured to acquire system operation function information of each structural system of an aero-engine, system structure data of each structural system, and system correlation information between each structural system, and construct a sub-simulation operation model of each structural system based on the system operation function information of each structural system and the system structure data of each structural system.

[0030] A construction module is configured to identify data interaction correlation information between each structural system and operation interaction correlation information between each structural system based on the system correlation information between each structural system, and construct simulation interaction information between each structural system based on the data interaction correlation information between each structural system and the operation interaction correlation information between each structural system.

[0031] An acquisition module is configured to acquire system operation function information of each structural system of an aero-engine, system structure data of each structural system, and system correlation information between each structural system, and construct a sub-simulation operation model of each structural system based on the system operation function information of each structural system and the system structure data of each structural system.

[0032] An identification module is configured to generate a joint simulation result of the aero-engine by the joint simulation model of the aero-engine based on the demand input data, and identify operation solution data of the aero-engine by a joint simulation solution algorithm based on the joint simulation result.

[0033] Optionally, the acquisition module is specifically configured to:

[0034] Based on the system structure data of each structural system, a system structure model of each structural system is constructed by a three-dimensional modeling program, and for each structural system, structural operation data of each operation function type is identified based on the system operation function information of the structural system.

[0035] Based on the structural operation data of each operation function type, the structural operation data of each operation function type is converted into structural operation parameters of each operation function type by a data parameter conversion program, and the system structure model of the structural system is adjusted based on the structural operation parameters of each operation function type to obtain the sub-simulation operation model of the structural system.

[0036] Optionally, the construction module is specifically configured to:

[0037] Based on the system association information between each of the structure systems, identify the association information of each association type between each of the structure systems, and query the interaction type to which each association type belongs in the association database;

[0038] Based on the association information of each association type corresponding to the data interaction type, identify the data interaction information between each of the structure systems and the data transmission information between each of the structure systems, and take the data interaction information between each of the structure systems and the data transmission information between each of the structure systems as the data interaction association information between each of the structure systems;

[0039] Based on the association information of each association type corresponding to the operation interaction type, identify the operation interaction mode between each of the structure systems and the operation interaction process between each of the structure systems, and take the operation interaction mode between each of the structure systems and the operation interaction process between each of the structure systems as the operation interaction association information between each of the structure systems.

[0040] Optionally, the construction module is specifically used for:

[0041] Based on the operation interaction mode between each of the structure systems and the operation interaction process between each of the structure systems, construct the simulation operation interaction process between each of the structure systems;

[0042] Based on the data interaction information between each of the structure systems and the data transmission information between each of the structure systems, construct the simulation data interaction process between each of the structure systems;

[0043] Take the simulation operation interaction process between each of the structure systems and the simulation data interaction process between each of the structure systems as the simulation interaction information between each of the structure systems.

[0044] Optionally, the acquisition module is specifically used for:

[0045] Acquire the physical connection information between each of the structure systems, and based on the physical connection information between each of the structure systems, perform model connection processing on the sub-simulation operation model of each of the structure systems to obtain the joint three-dimensional structure model of the aero-engine;

[0046] Based on the simulation interaction information between each of the structure systems, construct the simulation interaction parameters between each of the structure systems in the joint three-dimensional structure model, and adjust the simulation interaction parameters between all structure systems to adjust the joint three-dimensional structure model to obtain the joint simulation model of the aero-engine.

[0047] Optionally, the identification module is specifically used for:

[0048] splitting the joint simulation result into system simulation results of each structural system;

[0049] identifying a system correlation solving sequence between each structural system and a system algorithm solving sequence corresponding to each system simulation solving algorithm of each structural system based on simulation interaction information between each structural system, and calculating system simulation solving data of each structural system through each system simulation solving algorithm of each structural system according to the simulation solving sequence of each structural system based on the system simulation result of each structural system;

[0050] calculating the operation solving data of the aero-engine according to the system correlation solving algorithm between each structural system based on the system simulation solving data of each structural system.

[0051] In a third aspect, the present application provides a computer device. The computer device comprises a memory and a processor, the memory stores a computer program, and the processor implements the steps of the method in any one of the first aspect when executing the computer program.

[0052] In a fourth aspect, the present application provides a computer readable storage medium. The computer readable storage medium stores a computer program, and the computer program implements the steps of the method in any one of the first aspect when executed by a processor.

[0053] In a fifth aspect, the present application provides a computer program product. The computer program product comprises a computer program, and the computer program implements the steps of the method in any one of the first aspect when executed by a processor.

[0054] The aforementioned simulation solution method, apparatus, and computer equipment for aero-engines acquire system operation function information, system structure data, and system correlation information between various structural systems of the aero-engine. Based on the system operation function information and system structure data of each structural system, a sub-simulation operation model of each structural system is constructed. Based on the system correlation information between the structural systems, data interaction correlation information and operation interaction correlation information between the structural systems are identified. Based on the data interaction correlation information and operation interaction correlation information between the structural systems, simulation interaction information between the structural systems is constructed. Based on the simulation interaction information between the structural systems, simulation correlation processing is performed on each structural system to obtain a joint simulation model of the aero-engine, and the demand input data of the aero-engine is collected. Based on the demand input data, the joint simulation result of the aero-engine is generated through the joint simulation model, and based on the joint simulation result, the operation solution data of the aero-engine is identified through a joint simulation solution algorithm. This scheme involves simulating and modeling each structural system separately based on its operational function information, structural data, and interrelationship information. It then identifies the simulation interaction information between these systems and constructs a joint simulation model of the aero-engine based on this interaction information. This not only avoids the large simulation deviations inherent in single-system modeling but also improves the simulation accuracy by identifying the simulation data and results of each system during aero-engine operation simulation. Finally, in actual simulation, the scheme uses a distributed and progressive solution algorithm to solve the joint simulation results of the aero-engine. This avoids the significant increase in the number of equations and the resulting increase in difficulty and long solution times associated with unified modeling. Therefore, this approach effectively improves both the simulation accuracy and the simulation efficiency and convergence robustness of the aero-engine. Attached Figure Description

[0055] To more clearly illustrate the technical solutions in the embodiments or related technologies of this application, the accompanying drawings used in the description of the embodiments or related technologies will be briefly introduced below. Obviously, the accompanying drawings described below are only some embodiments of this application. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0056] Figure 1A flowchart of a simulation solving method of an aero-engine in an embodiment;

[0057] Figure 2 A flowchart of a simulation solving example of an aero-engine in an embodiment;

[0058] Figure 3 A block diagram of a simulation solving device of an aero-engine in an embodiment;

[0059] Figure 4 An internal structure diagram of a computer device in an embodiment. DETAILED DESCRIPTION

[0060] In order to make the purposes, technical solutions and advantages of the present application clearer, the present application is further described in detail below with reference to the drawings and embodiments. It should be understood that the specific embodiments described herein are only used to explain the present application and not to limit the present application.

[0061] The simulation solving method of an aero-engine provided by the embodiment of the present application can be applied to the application environment of aero-engine multi-system joint simulation. The method can be applied to a terminal, a server, or a system including a terminal and a server, and is realized through the interaction of the terminal and the server. The terminal can be, but is not limited to, various personal computers, notebook computers, medium-sized computers, etc. The terminal identifies the simulation interaction information between the structure systems after simulating and modeling each structure system by using the system running function information, the system structure data, and the system association information of each structure system, and finally constructs a joint simulation model of the aero-engine capable of simulating and interacting data jointly based on the simulation interaction information. The joint simulation model not only avoids the problem of large simulation deviation of single system modeling, but also can identify the simulation running data and the simulation running result of each system when the aero-engine is running, thereby improving the simulation accuracy of the aero-engine. Finally, the joint simulation result of the aero-engine is distributedly solved and jointly progressively solved by using the constructed joint simulation solving algorithm in the actual simulation process, which avoids the problem of significantly increased solving difficulty and long solving time and difficulty in convergence caused by the large number of solving equations after unified modeling, thereby improving the simulation accuracy, efficiency, and convergence robustness of the aero-engine.

[0062] In an exemplary embodiment, as shown in Figure 1 A simulation solving method of an aero-engine is provided. The method is applied to a terminal as an example, and includes the following steps S101 to S104. Wherein:

[0063] In step S101, system operation function information of each structural system of the aero-engine, system structure data of each structural system, and system association information between the structural systems are acquired, and based on the system operation function information of each structural system and the system structure data of each structural system, a sub-simulation operation model of each structural system is constructed.

[0064] In this embodiment, the terminal acquires, in response to an information uploading operation of the staff, the system operation function information of each structural system of the aero-engine, the system structure data of each structural system, and the system association information between the structural systems. The system structure of each system is a device structure that constitutes the aero-engine. The system structure includes an air intake system, a compression system, a combustion chamber system, a turbine system, an exhaust system, and a fuel supply system. The system operation function information includes system functions of each system structure and system operation information of each system structure, and the system structure data is system three-dimensional structure data of each system structure, which can be obtained by the staff performing three-dimensional scanning on each system structure. The system association information between each system structure includes association information of each association type. The association type is used to represent data interaction association and operation interaction association between two system structures. The association type includes but is not limited to a data transmission direction type, a data format conversion type, a data transmission restriction type, an operation function interaction type, an operation mode interaction type, and an operation flow interaction type. The association type belonging to the data interaction type includes but is not limited to the data transmission direction type, the data format conversion type, and the data transmission restriction type, and the association type belonging to the operation interaction type includes but is not limited to the operation function interaction type, the operation mode interaction type, and the operation flow interaction type. The specific identification will be described in detail later. Finally, the terminal constructs a sub-simulation operation model of each structural system based on the system operation function information of each structural system and the system structure data of each structural system. Each sub-simulation operation model can simulate the operation process of the structural system.

[0065] In step S102, based on the system association information between the structural systems, data interaction association information between the structural systems and operation interaction association information between the structural systems are identified, and based on the data interaction association information between the structural systems and the operation interaction association information between the structural systems, simulation interaction information between the structural systems is constructed.

[0066] In this embodiment, the terminal identifies the data interaction association information between the structural systems and the operation interaction association information between the structural systems based on the system association information between the structural systems, and constructs the simulation interaction information between the structural systems based on the data interaction association information between the structural systems and the operation interaction association information between the structural systems. The data interaction association information includes the data interaction information between the structural systems and the data transmission information between the structural systems, and the operation interaction association information includes the operation interaction mode between the structural systems and the operation interaction process between the structural systems. The specific identification process will be described in detail later. The constructed simulation interaction information between the systems is the simulation operation interaction process between the structural systems and the simulation data interaction process between the structural systems. The specific construction process will be described in detail later.

[0067] In step S103, based on the simulation interaction information between the structural systems, the terminal performs simulation association processing on the structural systems to obtain a joint simulation model of the aero-engine, and collects the demand input data of the aero-engine.

[0068] In this embodiment, the terminal performs simulation association processing on the structural systems based on the simulation interaction information between the structural systems to obtain a joint simulation model of the aero-engine, and collects the demand input data of the aero-engine. The simulation association processing process is to associate the simulation operation processes of the structural systems to ensure that the joint simulation process between the structural systems can be realized in the simulation operation process. The specific association processing process will be described in detail later. Then, the terminal collects the demand input data of the aero-engine, which is the data information corresponding to the simulated operation condition, the simulated operation mode, and the simulated operation process of the aero-engine required by the staff. The data information is the data information uploaded to the terminal by the staff, which can be changed according to the adjustment of the staff.

[0069] In step S104, based on the demand input data, the terminal generates a joint simulation result of the aero-engine through the joint simulation model of the aero-engine, and identifies the operation solving data of the aero-engine through a joint simulation solving algorithm based on the joint simulation result.

[0070] In this embodiment, the terminal generates a joint simulation result of the aero-engine through the joint simulation model of the aero-engine based on the demand input data, and identifies the operation solving data of the aero-engine through a joint simulation solving algorithm based on the joint simulation result. The joint simulation solving algorithm includes the system simulation solving algorithm of each structural system and the system association solving algorithm between each structural system, and the solving mode of the system association solving algorithm and the solving mode of the system simulation solving algorithm will be described in detail later.

[0071] Based on the above scheme, by simulating and modeling each structural system respectively from the system operation function information, system structure data and system association information of each structural system, identifying the simulation interaction information between each structural system, and finally, based on the simulation interaction information, constructing a joint simulation model of the aero-engine which can simulate and interact data respectively, not only avoids the problem of large simulation deviation of single system modeling, but also through the joint simulation model, when the aero-engine operation simulation is carried out, the simulation running data and simulation running result of each system can be identified respectively, thereby improving the simulation accuracy of the aero-engine. Finally, in the actual simulation process, the joint simulation result of the aero-engine is distributed and solved by the joint simulation solving algorithm constructed in the scheme, and is solved by joint progressive solving, which avoids the problem that the solving equation increases greatly after unified modeling, which causes the solving difficulty to increase significantly and is difficult to converge, thereby improving the simulation accuracy of the aero-engine while effectively improving the simulation efficiency and simulation convergence robustness of the aero-engine.

[0072] Optionally, based on the system operation function information of each structural system and the system structure data of each structural system, a sub-simulation running model of each structural system is constructed, including: based on the system structure data of each structural system, constructing a system structure model of each structural system through a three-dimensional modeling program, and for each structural system, based on the system operation function information of the structural system, identifying the structural running data of each running function type; based on the structural running data of each running function type, converting the structural running data of each running function type into the structural running data of each running function type through a data parameter conversion program, and adjusting the system structure model of the structural system based on the structural running data of each running function type to obtain a sub-simulation running model of the structural system.

[0073] In this embodiment, the terminal constructs a system structure model of each structural system based on the system structure data of each structural system through a three-dimensional modeling program, and for each structural system, identifies structural operation data of each operation function type based on system operation function information of the structural system. The three-dimensional modeling program is a structural modeling method based on modeling languages such as Modelica, C / C++, Fortran, and Python. Then, the terminal converts the structural operation data of each operation function type into structural operation parameters of each operation function type based on the structural operation data of each operation function type through a data parameter conversion program, and adjusts the system structure model of the structural system based on the structural operation parameters of each operation function type to obtain a sub-simulation operation model of the structural system. The data parameter conversion program stores data conversion instructions between the structural operation data of different operation function types and the structural operation parameters, and then the terminal generates the structural operation parameters of each operation function type through the data conversion instructions of each operation function type. Each operation function type is a function type corresponding to each operation function included in each structural system. For example, the operation functions of the fuel supply system include fuel supply function, fuel adjustment function, and fuel protection function, and the operation function types of the fuel supply system include fuel supply function type, fuel adjustment function type, and fuel protection function type.

[0074] Based on the above scheme, the three-dimensional structure modeling is performed on each structural system, and the structural operation data of each structural system is split and converted to generate a sub-simulation operation model of each structural system, thereby improving the operation practicality and simulation accuracy of the constructed sub-simulation operation model.

[0075] Optionally, based on the system association information between the structural systems, the data interaction association information between the structural systems and the operation interaction association information between the structural systems are identified, including: based on the system association information between the structural systems, identifying association information of each association type between the structural systems, and querying an interaction type to which each association type belongs in an association database; based on the association information of each association type corresponding to the data interaction type, identifying data interaction information between the structural systems and data transmission information between the structural systems, and taking the data interaction information between the structural systems and the data transmission information between the structural systems as the data interaction association information between the structural systems; based on the association information of each association type corresponding to the operation interaction type, identifying an operation interaction mode between the structural systems and an operation interaction process between the structural systems, and taking the operation interaction mode between the structural systems and the operation interaction process between the structural systems as the operation interaction association information between the structural systems.

[0076] In this embodiment, the terminal identifies the association information of each association type between the structural systems based on the system association information between the structural systems, and queries the interaction type to which each association type belongs in the association database. The association database stores the interaction type range corresponding to the data interaction type and the interaction type range corresponding to the running interaction type. Then the terminal identifies the association type corresponding to the data interaction type and the association type corresponding to the running interaction type through range query.

[0077] Then, the terminal identifies the data interaction information between the structural systems and the data transmission information between the structural systems based on the association information of the association type corresponding to the data interaction type, and takes the data interaction information between the structural systems and the data transmission information between the structural systems as the data interaction association information between the structural systems. Each association type corresponding to the data interaction type includes the association type for data transmission and the association type for data interaction. The terminal processes the association information of the association type for data transmission to obtain the data interaction information between the structural systems, and then processes the association information of the association type for data interaction to obtain the data transmission information between the structural systems.

[0078] The terminal identifies the running interaction mode between the structural systems and the running interaction process between the structural systems based on the association information of the association type corresponding to the running interaction type, and takes the running interaction mode between the structural systems and the running interaction process between the structural systems as the running interaction association information between the structural systems. Each association type corresponding to the running interaction type includes the association type for interaction mode and the association type for interaction process. The terminal processes the association information of the association type for interaction mode to obtain the running interaction mode between the structural systems, and then processes the association information of the association type for interaction process to obtain the running interaction process between the structural systems.

[0079] Based on the above scheme, the association information is split into the association information of each association type through data query, and the association information of each association type is summarized according to the data interaction type and the running interaction type respectively to obtain the running interaction association information between the structural systems and the data interaction association information between the structural systems, which improves the comprehensiveness and accuracy of identifying the running interaction association information between the structural systems and the data interaction association information.

[0080] Optionally, based on the data interaction association information between the structure systems and the operation interaction association information between the structure systems, simulation interaction information between the structure systems is constructed, including: based on the operation interaction mode between the structure systems and the operation interaction process between the structure systems, simulation operation interaction processes between the structure systems are constructed; based on the data interaction information between the structure systems and the data transmission information between the structure systems, simulation data interaction processes between the structure systems are constructed; the simulation operation interaction processes between the structure systems and the simulation data interaction processes between the structure systems are taken as the simulation interaction information between the structure systems.

[0081] In this embodiment, the terminal constructs simulation operation interaction processes between the structure systems based on the operation interaction mode between the structure systems and the operation interaction process between the structure systems. The construction mode is to convert the operation interaction mode and the operation interaction process between the structure systems into operation processes (including operation interaction sequence, operation interaction process, operation interaction range, etc.) between the structure systems by modeling languages corresponding to languages such as Modelica, C / C++, Fortran, and Python, to obtain the simulation operation interaction processes between the structure systems.

[0082] Then, the terminal constructs simulation data interaction processes between the structure systems based on the data interaction information between the structure systems and the data transmission information between the structure systems. Then, the terminal takes the simulation operation interaction processes between the structure systems and the simulation data interaction processes between the structure systems as the simulation interaction information between the structure systems. The construction mode is to convert the data interaction information between the structure systems and the data transmission information between the structure systems into data transmission processes (including data transmission direction, data transmission limitation, data transmission format conversion and adjustment, etc.) between the structure systems by modeling languages corresponding to languages such as Modelica, C / C++, Fortran, and Python, to obtain the simulation data interaction processes between the structure systems.

[0083] Based on the above scheme, through the construction of the simulation operation interaction processes between the structure systems and the simulation data interaction processes, the actuality and accuracy of the simulation interaction between the structure systems are ensured.

[0084] Optionally, based on the simulation interaction information between the structure systems, the structure systems are simulated and associated to obtain a joint simulation model of the aero-engine, including: collecting physical connection information between the structure systems, and based on the physical connection information between the structure systems, performing model connection processing on the sub-simulation running models of the structure systems to obtain a joint three-dimensional structure model of the aero-engine; based on the simulation interaction information between the structure systems, constructing simulation interaction parameters between the structure systems in the joint three-dimensional structure model, and adjusting the simulation interaction parameters between all the structure systems to adjust the joint three-dimensional structure model to obtain the joint simulation model of the aero-engine.

[0085] In this embodiment, the terminal collects the physical connection information between the structure systems, and based on the physical connection information between the structure systems, performs model connection processing on the sub-simulation running models of the structure systems to obtain a joint three-dimensional structure model of the aero-engine. The physical connection information includes connection information such as connection points between two structure systems, connection modes of the connection points, and connection angles of the connection points.

[0086] Then, based on the simulation interaction information between the structure systems, the terminal constructs simulation interaction parameters between the structure systems in the joint three-dimensional structure model, and adjusts the simulation interaction parameters between all the structure systems to adjust the joint three-dimensional structure model to obtain the joint simulation model of the aero-engine. The terminal predefines parameter conversion strategies corresponding to the simulation data interaction process and the simulation running interaction process, thereby converting the simulation interaction processes into simulation interaction parameters, and improving the conversion efficiency of the simulation interaction parameters.

[0087] Based on the above scheme, after the structure connection by the physical connection information, the simulation running interaction process and the simulation data interaction process are converted, and finally the joint simulation model of the aero-engine is constructed, thereby improving the construction efficiency and actuality of the joint simulation model.

[0088] Optionally, the joint simulation solving algorithm comprises a system simulation solving algorithm of each structural system and a system correlation solving algorithm between each structural system. Based on the joint simulation result, the operation solving data of the aero-engine is identified by the joint simulation solving algorithm, comprising: splitting the joint simulation result into system simulation results of each structural system; identifying the system correlation solving sequence between each structural system and the system algorithm solving sequence corresponding to the system simulation solving algorithm of each structural system based on the simulation interaction information between each structural system, and calculating the system simulation solving data of each structural system by the system simulation solving algorithm of each structural system according to the simulation solving sequence of each structural system based on the system simulation results of each structural system; and calculating the operation solving data of the aero-engine according to the system correlation solving algorithm between each structural system based on the system simulation solving data of each structural system.

[0089] In this embodiment, the terminal splits the joint simulation result into system simulation results of each structural system. Then, the terminal identifies the system correlation solving sequence between each structural system and the system algorithm solving sequence corresponding to the system simulation solving algorithm of each structural system based on the simulation interaction information between each structural system, and calculates the system simulation solving data of each structural system by the system simulation solving algorithm of each structural system according to the simulation solving sequence of each structural system based on the system simulation results of each structural system. Finally, the terminal calculates the operation solving data of the aero-engine according to the system correlation solving algorithm between each structural system based on the system simulation solving data of each structural system.

[0090] Specifically, the joint simulation model comprises M subsystem models, N equations to be solved, N>M, M>=1, the ith subsystem model comprises Ni equations to be solved, i=1, 2, 3, …, M, Ni>=0, N>= Suppose that the simulation calculation at the kth time has been completed, the N equations to be solved at the k+1 time are solved according to the following steps, k>=0.

[0091] S1. The calculation sequence is sorted according to the connection relationship of the subsystem models in the joint simulation model, and the calculation sequence of the M subsystem models is obtained, and the step S2 is transferred.

[0092] S2. According to the given calculation sequence, each subsystem is solved and calculated in turn, and the equations to be solved of each subsystem model are solved and calculated by using the corresponding solver of each subsystem according to the latest input data and the current simulation data of each subsystem, and the model interaction interface data is updated; after the solving and calculation of all subsystem models are completed, the step S3 is transferred.

[0093] S3. According to the calculation results of the solving of each subsystem model, the remaining N-1 simulation to be solved of the joint simulation model is solved, if the solving result is convergent, go to S4; if the solving result is not convergent, go to step S2.

[0094] S4. Output the running solving data at the k+1 time.

[0095] S4. Output the running solving data at the k+1 time.

[0096] Based on the above scheme, the originally mutually coupled high-dimensional equation groups to be solved are decomposed into multiple subsystem models according to different subsystems, and then solved by the required solvers of each subsystem, and then the solving equations between the subsystems are solved, and the whole joint simulation model is solved. In this process, on the one hand, the correctness of the whole solving simulation calculation result is ensured, because all the solving equations are satisfied; on the other hand, through the decomposition and separate solving of the equations to be solved, the effect of dimension reduction calculation is realized, which can reduce the difficulty and calculation amount of the whole solving, and improve the simulation calculation efficiency.

[0097] The application also provides a simulation solving example of an aero-engine, as shown in Figure 2 The specific processing process includes the following steps:

[0098] Step S201, obtaining system running function information of each structural system of the aero-engine, system structure data of each structural system, and system association information between each structural system.

[0099] Step S202, based on the system structure data of each structural system, constructing a system structure model of each structural system through a three-dimensional modeling program, and for each structural system, identifying structural running data of each running function type based on the system running function information of the structural system.

[0100] Step S203, based on the structural running data of each running function type, converting the structural running data of each running function type into structural running parameters of each running function type through a data parameter conversion program, and adjusting the system structure model of the structural system based on the structural running parameters of each running function type to obtain a sub-simulation running model of the structural system.

[0101] Step S204, identifying the association information of each association type between each structural system based on the system association information between each structural system, and querying the interaction type to which each association type belongs in the association database.

[0102] In step S205, the data interaction information between the structure systems and the data transmission information between the structure systems are identified based on the association information of each association type corresponding to the data interaction type, and the data interaction information between the structure systems and the data transmission information between the structure systems are taken as the data interaction association information between the structure systems.

[0103] In step S206, the operation interaction mode between the structure systems and the operation interaction process between the structure systems are identified based on the association information of each association type corresponding to the operation interaction type, and the operation interaction mode between the structure systems and the operation interaction process between the structure systems are taken as the operation interaction association information between the structure systems.

[0104] In step S207, the simulation operation interaction process between the structure systems is constructed based on the operation interaction mode between the structure systems and the operation interaction process between the structure systems.

[0105] In step S208, the simulation data interaction process between the structure systems is constructed based on the data interaction information between the structure systems and the data transmission information between the structure systems.

[0106] In step S209, the simulation operation interaction process between the structure systems and the simulation data interaction process between the structure systems are taken as the simulation interaction information between the structure systems.

[0107] In step S210, the physical connection information between the structure systems is collected, and the model connection processing is performed on the sub-simulation operation model of each structure system based on the physical connection information between the structure systems, so as to obtain the joint three-dimensional structure model of the aero-engine.

[0108] In step S211, the simulation interaction parameters between the structure systems in the joint three-dimensional structure model are constructed based on the simulation interaction information between the structure systems, and the simulation interaction parameters between all the structure systems are used to adjust the joint three-dimensional structure model, so as to obtain the joint simulation model of the aero-engine.

[0109] In step S212, the demand input data of the aero-engine is collected.

[0110] In step S213, the joint simulation result is split into the system simulation results of each structure system.

[0111] Step S214, based on the simulation interaction information between each of the structure systems, identifying a system correlation solving sequence between each of the structure systems, and a system algorithm solving sequence corresponding to each system simulation solving algorithm of each of the structure systems, and based on the system simulation results of each of the structure systems, calculating system simulation solving data of each of the structure systems through the system simulation solving algorithm of each of the structure systems in accordance with the simulation solving sequence of each of the structure systems.

[0112] Step S215, based on the system simulation solving data of each of the structure systems, calculating the operation solving data of the aero-engine in accordance with the system correlation solving algorithm between each of the structure systems.

[0113] It should be understood that, although each of the steps in the flowchart involved in the embodiments described above is shown in sequence according to the arrow, these steps are not necessarily executed in the order indicated by the arrow. Unless otherwise specified herein, the execution of these steps is not strictly limited in sequence, and these steps can be executed in other orders. Moreover, at least part of the steps in the flowchart involved in the embodiments described above can include multiple steps or stages, which are not necessarily executed at the same time, but can be executed at different times, and the execution sequence of these steps or stages is not necessarily sequential, but can be executed alternately or alternately with at least part of other steps or steps or stages in other steps.

[0114] Based on the same inventive concept, the embodiments of the present application also provide an aero-engine simulation solving device for implementing the simulation solving method of the aero-engine involved above. The implementation scheme for solving problems provided by the device is similar to the implementation scheme described in the above method, so the specific limitations in one or more aero-engine simulation solving device embodiments provided below can refer to the limitations of the aero-engine simulation solving method described above, which will not be repeated here.

[0115] In one exemplary embodiment, as shown in Figure 3 An aero-engine simulation solving device is provided, comprising: an acquisition module 310, a construction module 320, an acquisition module 330 and an identification module 340, wherein:

[0116] The acquisition module 310 is configured to acquire system operation function information of each structure system of the aero-engine, system structure data of each of the structure systems, and system correlation information between each of the structure systems, and based on the system operation function information of each of the structure systems and the system structure data of each of the structure systems, construct a sub-simulation running model of each of the structure systems;

[0117] The constructing module 320 is configured to identify data interaction correlation information between the structure systems and operation interaction correlation information between the structure systems based on the system correlation information between the structure systems, and construct simulation interaction information between the structure systems based on the data interaction correlation information between the structure systems and the operation interaction correlation information between the structure systems.

[0118] The collecting module 330 is configured to perform simulation correlation processing on the structure systems based on the simulation interaction information between the structure systems to obtain a joint simulation model of the aero-engine, and collect demand input data of the aero-engine.

[0119] The identifying module 340 is configured to generate a joint simulation result of the aero-engine by the joint simulation model of the aero-engine based on the demand input data, and identify operation solving data of the aero-engine by a joint simulation solving algorithm based on the joint simulation result.

[0120] Optionally, the obtaining module 310 is specifically configured to:

[0121] construct a system structure model of each structure system by a three-dimensional modeling program based on system structure data of the structure system, and identify structure operation data of each operation function type for each structure system based on system operation function information of the structure system;

[0122] convert the structure operation data of each operation function type into structure operation parameters of each operation function type by a data parameter conversion program based on the structure operation data of each operation function type, and adjust the system structure model of the structure system based on the structure operation parameters of each operation function type to obtain a sub-simulation operation model of the structure system.

[0123] Optionally, the constructing module 320 is specifically configured to:

[0124] identify correlation information of each correlation type between the structure systems based on the system correlation information between the structure systems, and query an interaction type to which each correlation type belongs in a correlation database;

[0125] identify data interaction information between the structure systems and data transmission information between the structure systems based on the correlation information of each correlation type corresponding to the data interaction type, and take the data interaction information between the structure systems and the data transmission information between the structure systems as the data interaction correlation information between the structure systems;

[0126] The operation interaction modes between the structure systems and the operation interaction processes between the structure systems are identified based on the association information of each association type corresponding to the operation interaction type, and the operation interaction modes between the structure systems and the operation interaction processes between the structure systems are taken as operation interaction association information between the structure systems.

[0127] Optionally, the construction module 320 is specifically configured to:

[0128] The simulation operation interaction processes between the structure systems are constructed based on the operation interaction modes between the structure systems and the operation interaction processes between the structure systems.

[0129] The simulation data interaction processes between the structure systems are constructed based on the data interaction information between the structure systems and the data transmission information between the structure systems.

[0130] The simulation operation interaction processes between the structure systems and the simulation data interaction processes between the structure systems are taken as simulation interaction information between the structure systems.

[0131] Optionally, the collection module 330 is specifically configured to:

[0132] The physical connection information between the structure systems is collected, and the model connection processing is performed on the sub-simulation operation models of the structure systems based on the physical connection information between the structure systems, so as to obtain a joint three-dimensional structure model of the aero-engine.

[0133] The simulation interaction parameters between the structure systems in the joint three-dimensional structure model are constructed based on the simulation interaction information between the structure systems, and the simulation interaction parameters between all the structure systems are used to adjust the joint three-dimensional structure model, so as to obtain a joint simulation model of the aero-engine.

[0134] Optionally, the identification module 340 is specifically configured to:

[0135] The joint simulation result is split into system simulation results of the structure systems.

[0136] The system association solving sequences between the structure systems and the system algorithm solving sequences corresponding to the system simulation solving algorithms of the structure systems are identified based on the simulation interaction information between the structure systems, and the system simulation solving data of each structure system is calculated by the system simulation solving algorithm of each structure system in accordance with the simulation solving sequence of each structure system based on the system simulation result of each structure system.

[0137] Based on the system simulation solution data of each structural system, the operation solution data of the aero-engine is calculated according to the system correlation solution algorithm between each structural system.

[0138] The modules in the simulation solution device of the aero-engine can be implemented by software, hardware, or a combination thereof. The modules can be embedded in or independent of the processor in the computer device in hardware form, or stored in the memory in the computer device in software form, so that the processor can call and execute the operations corresponding to the modules.

[0139] In an exemplary embodiment, a computer device, which can be a terminal, has an internal structure as shown in Figure 4 The computer device includes a processor, a memory, an input / output interface, a communication interface, a display unit, and an input device. The processor, the memory, and the input / output interface are connected through a system bus, and the communication interface, the display unit, and the input device are connected to the system bus through the input / output interface. The processor of the computer device is configured to provide computing and control capabilities. The memory of the computer device includes a non-volatile storage medium and an internal memory. The non-volatile storage medium stores an operating system and a computer program. The internal memory provides an environment for the operating system and the computer program in the non-volatile storage medium to run. The input / output interface of the computer device is configured to exchange information between the processor and external devices. The communication interface of the computer device is configured to perform wired or wireless communication with external terminals. The wireless communication can be achieved through WIFI, mobile cellular network, NFC (Near Field Communication), or other technologies. The computer program is executed by the processor to implement a simulation solution method for an aero-engine. The display unit of the computer device is configured to form a visually visible picture, which can be a display screen, a projection device, or a virtual reality imaging device. The display screen can be a liquid crystal display screen or an electronic ink display screen. The input device of the computer device can be a touch layer overlaid on the display screen, or a key, trackball, or touchpad arranged on the shell of the computer device, or an external keyboard, touchpad, or mouse, etc.

[0140] Those skilled in the art can understand that Figure 4 The structure shown in the above description is only a block diagram of part of the structure related to the scheme of the present application, and does not limit the computer device to which the scheme of the present application is applied. The specific computer device can include more or fewer components than those shown in the figure, or combine certain components, or have a different arrangement of components.

[0141] In one exemplary embodiment, a computer device is provided, comprising a memory and a processor, the memory having stored therein a computer program, the processor implementing the steps of the simulation solving method of an aero-engine when executing the computer program.

[0142] In one embodiment, a computer readable storage medium is provided, having stored thereon a computer program, the computer program implementing the steps of the simulation solving method of an aero-engine when executed by a processor.

[0143] In one embodiment, a computer program product is provided, comprising a computer program, the computer program implementing the steps of the simulation solving method of an aero-engine when executed by a processor.

[0144] It should be noted that the user information (including but not limited to user equipment information, user personal information, etc.) and data (including but not limited to data for analysis, stored data, displayed data, etc.) involved in the present application are all information and data authorized by the user or fully authorized by all parties, and the collection, use and processing of related data need to comply with relevant regulations.

[0145] Those skilled in the art can understand that all or part of the processes in the above-mentioned embodiment methods can be completed by instructing the relevant hardware through a computer program. The computer program can be stored in a non-volatile computer readable storage medium, and when the computer program is executed, the processes of the above-mentioned embodiments of the methods can be included. Any reference to memory, database or other medium used in the embodiments provided in the present application can include at least one of non-volatile and volatile memory. Non-volatile memory can include read-only memory (ROM), magnetic tape, floppy disk, flash memory, optical storage, high-density embedded non-volatile memory, resistive memory (ReRAM), magnetoresistive random access memory (MRAM), ferroelectric memory (FRAM), phase change memory (PCM), graphene memory, etc. Volatile memory can include random access memory (RAM) or external cache memory, etc. As an illustration but not limitation, RAM can be in various forms, such as static random access memory (SRAM) or dynamic random access memory (DRAM), etc. The database involved in the embodiments provided in the present application can include at least one of a relational database and a non-relational database. The non-relational database can include a distributed database based on a block chain, etc., without being limited thereto. The processor involved in the embodiments provided in the present application can be a general-purpose processor, a central processing unit, a graphics processing unit, a digital signal processor, a programmable logic device, a data processing logic device based on quantum computing, etc., without being limited thereto.

[0146] Any combination of the technical features of the above embodiments can be made. In order to make the description simple, all possible combinations of the technical features in the above embodiments are not described, however, as long as the combination of the technical features does not exist, it should be considered as the scope of the present application.

[0147] The above embodiments only express several implementation manners of the present application, and the description is more specific and detailed, but it should not be understood as a limitation on the scope of the patent of the present application. It should be pointed out that for ordinary skilled in the art, without departing from the concept of the present application, a number of modifications and improvements can be made, which are within the scope of protection of the present application. Therefore, the protection scope of the present application should be subject to the appended claims.

Claims

1. A method of simulation solution of an aeroengine, characterized in that, The method comprises: obtaining system operation function information of each structural system of an aero-engine, system structure data of each structural system, and system association information between each structural system, and constructing a sub-simulation operation model of each structural system based on the system operation function information of each structural system and the system structure data of each structural system; based on the system association information between each structural system, identifying association information of each association type between each structural system, and querying an interaction type to which each association type belongs in an association database; based on the association information of each association type corresponding to a data interaction type, identifying data interaction information between each structural system and data transmission information between each structural system, and taking the data interaction information between each structural system and the data transmission information between each structural system as data interaction association information between each structural system; based on the association information of each association type corresponding to a running interaction type, identifying a running interaction mode between each structural system and a running interaction process between each structural system, and taking the running interaction mode between each structural system and the running interaction process between each structural system as running interaction association information between each structural system; based on the data interaction association information between each structural system and the running interaction association information between each structural system, constructing simulation interaction information between each structural system; based on the simulation interaction information between each structural system, performing simulation association processing on each structural system to obtain a joint simulation model of the aero-engine, and collecting demand input data of the aero-engine; based on the demand input data, generating a joint simulation result of the aero-engine through the joint simulation model of the aero-engine, and identifying operation solving data of the aero-engine through a joint simulation solving algorithm based on the joint simulation result.

2. The method of claim 1, wherein, The method comprises: based on the system structure data of each structural system, constructing a system structure model of each structural system through a three-dimensional modeling program, and identifying structural operation data of each operation function type for each structural system based on the system operation function information of the structural system; based on the structural operation data of each operation function type, converting the structural operation data of each operation function type into structural operation parameters of each operation function type through a data parameter conversion program, and adjusting the system structure model of the structural system based on the structural operation parameters of each operation function type to obtain a sub-simulation operation model of the structural system.

3. The method of claim 1, wherein, The method comprises: Based on the operation interaction mode between each structure system and the operation interaction process between each structure system, a simulation operation interaction process between each structure system is constructed; Based on the data interaction information between each structure system and the data transmission information between each structure system, a simulation data interaction process between each structure system is constructed; The simulation operation interaction process between each structure system and the simulation data interaction process between each structure system are taken as simulation interaction information between each structure system.

4. The method of claim 3, wherein, Based on the simulation interaction information between each structure system, the structure systems are simulated and associated to obtain a joint simulation model of the aero-engine, including: Physical connection information between each structure system is collected, and based on the physical connection information between each structure system, model connection processing is performed on the sub-simulation operation model of each structure system to obtain a joint three-dimensional structure model of the aero-engine; Based on the simulation interaction information between each structure system, simulation interaction parameters between each structure system in the joint three-dimensional structure model are constructed, and all simulation interaction parameters between the structure systems are used to adjust the joint three-dimensional structure model to obtain the joint simulation model of the aero-engine.

5. The method of claim 1, wherein, The joint simulation solving algorithm includes each system simulation solving algorithm of each structure system and system association solving algorithm between each structure system, and based on the joint simulation result, the operation solving data of the aero-engine is identified through the joint simulation solving algorithm, including: The joint simulation result is split into system simulation results of each structure system; Based on the simulation interaction information between each structure system, system association solving sequences between each structure system and system algorithm solving sequences corresponding to each system simulation solving algorithm of each structure system are identified, and based on the system simulation results of each structure system, each structure system is calculated through each system simulation solving algorithm of each structure system in the simulation solving sequence of each structure system; Based on the system simulation solving data of each structure system, the operation solving data of the aero-engine is calculated according to the system association solving algorithm between each structure system.

6. An aeroengine simulation solving apparatus, characterized by, The device includes: An acquisition module is configured to acquire system operation function information of each structure system of an aero-engine, system structure data of each structure system, and system association information between each structure system, and based on the system operation function information of each structure system and the system structure data of each structure system, a sub-simulation operation model of each structure system is constructed; The construction module is configured to: identify, based on system correlation information between the structure systems, correlation information of each correlation type between the structure systems, and query, in a correlation database, an interaction type to which each correlation type belongs; identify, based on the correlation information of each correlation type corresponding to a data interaction type, data interaction information between the structure systems and data transmission information between the structure systems, and take the data interaction information between the structure systems and the data transmission information between the structure systems as data interaction correlation information between the structure systems; identify, based on the correlation information of each correlation type corresponding to a running interaction type, a running interaction mode between the structure systems and a running interaction process between the structure systems, and take the running interaction mode between the structure systems and the running interaction process between the structure systems as running interaction correlation information between the structure systems; and construct simulation interaction information between the structure systems based on the data interaction correlation information between the structure systems and the running interaction correlation information between the structure systems. The acquisition module is configured to: perform simulation correlation processing on the structure systems based on the simulation interaction information between the structure systems, to obtain a joint simulation model of the aero-engine, and acquire demand input data of the aero-engine. The identification module is configured to: generate a joint simulation result of the aero-engine by the joint simulation model of the aero-engine based on the demand input data, and identify running solution data of the aero-engine by a joint simulation solution algorithm based on the joint simulation result.

7. The apparatus of claim 6, wherein, The acquisition module is specifically configured to: construct, based on system structure data of each structure system, a system structure model of each structure system by a three-dimensional modeling program, and identify, for each structure system, structure running data of each running function type based on system running function information of the structure system; convert, based on the structure running data of each running energy supply type, the structure running data of each running function type into structure running parameters of each running function type by a data parameter conversion program, and adjust the system structure model of the structure system based on the structure running parameters of each running function type, to obtain a sub-simulation running model of the structure system. 8.A computer device, comprising a memory and a processor, wherein the memory stores a computer program, and the computer device is configured to perform the method according to any one of claims 1-7. The processor executes the computer program to implement the steps of the method in any one of claims 1 to 5.

9. A computer readable storage medium having stored thereon a computer program, characterized in that, The computer program is executed by the processor to implement the steps of the method in any one of claims 1 to 5.

10. A computer program product comprising a computer program, characterized in that, The computer program is executed by the processor to implement the steps of the method in any one of claims 1 to 5.

Images