Requirement and calculation model association verification method and system, storage medium and equipment

A technology of computing models and verification methods, which is applied in manufacturing computing systems, design optimization/simulation, instruments, etc., can solve problems such as data incompatibility, error-prone updates, and delays in time, and achieve the effect of reducing error probability and workload

Pending Publication Date: 2022-08-05
XIAN AEROSPACE PROPULSION INST +1
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Problems solved by technology

[0004] The purpose of the present invention is to solve the technical problems of large workload, error-prone and untimely update caused by data incompatibility between the demand model and various calculation models in the scheme design process of the current liquid rocket engine system, and propose a demand and calculation model Associating the verification method, system, storage medium and equipment to realize the association of the design paramete

Method used

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  • Requirement and calculation model association verification method and system, storage medium and equipment
  • Requirement and calculation model association verification method and system, storage medium and equipment
  • Requirement and calculation model association verification method and system, storage medium and equipment

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Embodiment Construction

[0032] see figure 1 , the present embodiment provides a method for verifying an association between a requirement and a computing model, and the method includes the following steps:

[0033] S1. Build the demand model of the liquid rocket engine in the demand model modeling software, and the demand model includes design parameters and performance parameters;

[0034] Various calculation models of the liquid rocket engine are constructed in the corresponding modeling software, and the various calculation models include input parameters, output variables and calculation formulas. Specifically, the various calculation models are a parameter calculation model, a static calculation model, a reliability calculation model, and a dynamic calculation model.

[0035] S2. Perform a first association between the design parameters in the requirement model and the input parameters in the calculation model, and store the first association relationship as an xml file.

[0036] Perform a sec...

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Abstract

The invention relates to a demand and calculation model association verification method and system, a storage medium and equipment, and aims to solve the technical problems of large workload, error proneness and untimely updating caused by data non-intercommunication between a demand model and various calculation models in a scheme design process of a current liquid rocket engine system. The method comprises the following steps: 1, constructing a demand model and a plurality of calculation models; 2, establishing association between the demand model and the calculation model; 3, updating design parameters of the demand model to the calculation model; 4, solving the calculation model; 5, comparing the calculation result of the calculation model with the performance parameters of the demand model, and if the requirement is met, ending; and if the requirements are not met, adjusting the calculation model or the demand model, and returning to the step 3 until the requirements are met. The system comprises a demand model module, a calculation model module, a variable association module, a parameter reference module and a demand verification module.

Description

technical field [0001] The invention relates to a design method of a liquid rocket engine system, in particular to a method, system, storage medium and equipment for verifying the correlation between requirements and calculation models of a liquid rocket engine system. Background technique [0002] The design of the liquid rocket engine system is a multi-task and multi-model process. Different tasks correspond to different models, which mainly include demand models and various calculation models. There is a data correlation between the models, such as the propellant type, specific impulse, mixing ratio, engine thrust, total system weight, system reliability and other parameters in the demand model will be used in subsequent calculation models. At present, there is no relationship between the demand model and various design calculation models, the data is not interoperable, and the various models are separated from each other. When one of the parameters is modified, it is ne...

Claims

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Application Information

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IPC IPC(8): G06F30/15G06F30/20G06F119/02
CPCG06F30/15G06F30/20G06F2119/02Y02P90/30
Inventor 李晨沛王天飞胡海峰陈宏玉张晨曦李舒欣周康周晨初刘占一张睿文周雯
Owner XIAN AEROSPACE PROPULSION INST
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