Graphical self-adaptive identification and generation method for specification parameters of pipeline assembly of hydraulic system

Abstract

The invention belongs to the technical field of aviation technology electromechanical systems, and relates to a 28MPa pressure level airplane hydraulic system pipeline assembly specification parameter self-adaptive identification and generation method. Comprising the steps that a pipeline assembly graph module, a hydraulic drive actuator graph module, a pipeline connector graph module, an oil tank graph module and a module attribute parameter matcher are arranged; setting module attribute parameters; starting from any actuator, sequentially establishing crosslinking between the hydraulic actuator graphic module and the oil tank graphic module by using the pipeline assembly graphic module and the pipeline connector graphic module; determining the association between the graphic module and the attribute parameter matcher; according to an onboard pipeline arrangement scheme, connecting a pipeline assembly graph module with a hydraulic actuator graph module, an oil tank graph module and each pipeline connector graph module; pipeline attribute parameters are set, and an attribute parameter sensor automatically sets and confirms pipeline specification attributes according to the logic; and rechecking the setting and confirmation results.

Description

Technical Field

[0001] The present invention belongs to the technical field of aviation technology electromechanical systems, and relates to a method for adaptively identifying and generating specification parameters of a pipeline component of a 28MPa pressure-level aircraft hydraulic system. Background Art

[0002] The 28MPa pressure level aircraft hydraulic system needs to serve a large number of system users, such as ailerons, rudders, elevators, flaps, spoilers and other flight control system users, nose wheel turning, brakes, landing gear retraction and extension and other landing gear system users. During the hydraulic system design process, the flow requirements of system users will be iteratively updated as the design gradually deepens. Different functional pipelines have different limiting flow rates. The change in flow will select different pipeline specifications according to the flow rate limit. After the pipelines are intersected, the change in flow will also affect the change in pipeline specifications. The hydraulic system uses multiple independent energy systems, and the total number of pipelines is thousands. The setting of pipeline specification attributes will consume a lot of human resources and is prone to errors. Summary of the invention

[0003] Purpose of the invention: To provide a method for graphically adaptively identifying and generating specification parameters of a 28MPa pressure-level aircraft hydraulic system piping component, so as to solve the problem of low efficiency and easy error in setting parameters of the 28MPa pressure-level hydraulic system piping specifications during the iteration of the system solution.

[0004] Technical solution:

[0005] A method for graphically adaptively identifying and generating specification parameters of a 28MPa pressure-level aircraft hydraulic system pipeline component, comprising:

[0006] Step 1: Set a pipeline component graphic module, a hydraulic drive actuator graphic module, a pipeline connector graphic module, a fuel tank graphic module, and a module attribute parameter matcher, wherein the pipeline component graphic module, the hydraulic drive actuator graphic module, the pipeline connector graphic module, and the fuel tank graphic module have an attribute setting function, and the attribute parameter matcher has a calculation and logic judgment function;

[0007] Step 2: Set module attribute parameters;

[0008] Step 3, starting from any actuator, using the pipeline component graphic module and the pipeline connector graphic module to sequentially establish the cross-linking between the hydraulic actuator graphic module and the fuel tank graphic module; determining the association between the pipeline component graphic module, the hydraulic drive actuator graphic module, the pipeline connector graphic module, the fuel tank graphic module and the attribute parameter matcher;

[0009] Step 4: Graphic drawing: According to the onboard pipeline layout plan, connect the pipeline component graphic module with the hydraulic actuator graphic module, the fuel tank graphic module, and each pipeline connector graphic module;

[0010] Step 5: Automatic identification: Set the pipeline attribute parameters. The attribute parameter sensor automatically sets and confirms the pipeline specification attributes according to the logic of step 3.

[0011] Step 6: Review the settings and confirmation results.

[0012] Furthermore, the attribute parameters configured by the pipeline component graphic module include: pipeline material attribute parameters, which are divided into three types: stainless steel 2169 material, stainless steel 1Cr18Ni10Ti material, and aluminum alloy 6061 material; pipeline pressure type parameters, which are divided into three types: supply pressure, i.e. 28MPa, oil suction, i.e. 2MPa, and oil return, i.e. 14MPa; pipeline specification parameters, which are used for the selection of specification parameters of different pipe diameters.

[0013] Further, the hydraulic actuator graphic module is configured with hydraulic flow parameters.

[0014] Furthermore, the pipeline connector graphic module is configured with confluence and diversion options.

[0015] Furthermore, step three specifically includes:

[0016] Step 31: Determine the actual pipe specification of the pipe assembly graphic module having one end connected to the actuator graphic module and the other end connected to the pipe connector graphic module;

[0017] Step 32: Determine the actual pipeline specification of the pipeline assembly graphic module with both ends connected to the pipeline connector graphic module;

[0018] Step 33: Determine the actual pipe specification of the pipe assembly graphic module that is connected to the fuel tank graphic module at one end and to the pipe connector graphic module at the other end.

[0019] Furthermore, step 31 specifically includes:

[0020] Step 311: the pipeline component graphic module is connected to the hydraulic actuator graphic module, the attribute parameter matcher is automatically activated, and the flow division / confluence information of the pipeline connector graphic module is extracted, and it is in a state of waiting for logic judgment;

[0021] Step 312: Set the pressure type parameter of the pipeline component graphic module, and the attribute parameter matcher calculates the theoretical pipeline specifications according to the corresponding maximum flow rate and the flow parameter of the hydraulic actuator graphic module, which is in a state to be compared; specifically:

[0022] Determine the maximum flow rate according to the pressure type parameter of the pipeline component graphic module, determine the ratio of the flow parameter of the hydraulic actuator graphic module to the maximum flow rate of the pipeline component graphic module as the pipeline cross-sectional area, and determine the pipeline diameter according to the pipeline cross-sectional area as the theoretical pipeline specification;

[0023] Step 313: Set the pipeline material attribute parameters. The attribute parameter matcher compares the corresponding optional specifications of the material with the calculated theoretical pipeline specifications, and selects the closest value greater than the calculated result as the actual pipeline specification.

[0024] Furthermore, step 32 specifically includes:

[0025] Step 321: extracting the flow splitting / converging information of the flow parameter attributes of the pipeline connector graphic modules at both ends of the pipeline component graphic module;

[0026] Step 322: If both ends of the pipeline component graphic module are connected to the split flow, the flow attribute of the end close to the hydraulic drive actuator graphic module is used as the flow of the current pipeline component graphic module;

[0027] Determine the maximum flow rate according to the pressure type parameter of the pipeline component graphic module; determine the ratio of the flow rate of the current pipeline component graphic module to the maximum flow rate of the pipeline component graphic module as the pipeline cross-sectional area, and determine the pipeline diameter according to the pipeline cross-sectional area as the theoretical pipeline specification;

[0028] Set the pipeline material attribute parameters. The attribute parameter matcher compares the corresponding optional specifications of the material with the calculated theoretical pipeline specifications, and selects the closest value greater than the calculated result as the actual pipeline specification.

[0029] Step 323: when one end of the pipeline component graphic module is connected to a confluence, the attribute parameter matcher calculates the sum of the flow rates of the branch pipelines corresponding to the confluence port as the flow rate of the current pipeline;

[0030] Determine the maximum flow rate according to the pressure type parameter of the pipeline component graphic module; determine the ratio of the flow rate of the current pipeline component graphic module to the maximum flow rate of the pipeline component graphic module as the pipeline cross-sectional area, and determine the pipeline diameter according to the pipeline cross-sectional area as the theoretical pipeline specification;

[0031] Set the pipeline material attribute parameters. The attribute parameter matcher compares the corresponding optional specifications of the material with the calculated theoretical pipeline specifications, and selects the closest value that is greater than the calculated result as the actual pipeline specification.

[0032] Furthermore, step 33 specifically includes:

[0033] Step 331: extracting the flow parameter attribute of the pipeline connector graphic module at one end of the pipeline component graphic module away from the fuel tank graphic module;

[0034] Step 332: Determine whether the current pipeline component graphic module is split or converged when it is away from one end of the fuel tank graphic module; in the case of split flow, the flow of the pipeline component graphic module connected to the current pipeline component graphic module is used as the flow of the current pipeline; in the case of convergence, calculate the sum of the flow of each split pipeline corresponding to the convergence port as the flow of the current pipeline;

[0035] Step 333: determining the maximum flow rate according to the pressure type parameter of the pipeline component graphic module; determining the ratio of the flow rate of the current pipeline component graphic module to the maximum flow rate of the pipeline component graphic module as the pipeline cross-sectional area, and determining the pipeline diameter according to the pipeline cross-sectional area as the theoretical pipeline specification;

[0036] Step 334: Set the pipeline material attribute parameters. The attribute parameter matcher compares the corresponding optional specifications of the material with the calculated theoretical pipeline specifications, and selects the closest value greater than the calculated result as the actual pipeline specification.

[0037] Beneficial effects:

[0038] The method provides a method for graphically automatically identifying and generating the pipeline specification parameters of the aircraft hydraulic system at a pressure level of 28MPa. By setting a pipeline component graphic module, a hydraulic drive actuator graphic module, a pipeline connector graphic module, and a module attribute parameter matcher, the modules are graphically connected using pipeline component modules. Through the user and pipeline connector flow and flow in the pipeline connected by the pipeline module graphic, the restricted flow rate is automatically generated according to the pipeline function classification, the pipeline specifications are automatically calculated according to the flow rate and the restricted flow rate, the pipeline specifications can be selected by comparing the materials, and the pipeline specification parameters are determined. The method has simple modules, simplified steps, easy operation, and improved work efficiency. DETAILED DESCRIPTION

[0039] The present invention provides a method for graphically adaptively identifying and generating specification parameters of a 28MPa pressure-level aircraft hydraulic system pipeline component, which includes setting aircraft modules and their respective regions; setting user modules according to the location of system users; setting pipeline modules, configuring pipeline material attribute parameters, usage function classification, pipeline specification parameters, etc.; using lines to dynamically associate system users and hydraulic energy, and using a graphical method to dynamically identify and generate hydraulic system pipeline specification parameters. The method comprises the following steps:

[0040] Step 1: Set the pipeline component graphic module, hydraulic drive actuator graphic module, pipeline connector graphic module, fuel tank graphic module, and module attribute parameter matcher. The pipeline component graphic module, hydraulic drive actuator graphic module, pipeline connector graphic module, and fuel tank graphic module have attribute setting functions, and the attribute parameter matcher has calculation and logic judgment functions.

[0041] Step 2: Module attribute parameter settings:

[0042] The attribute parameters configured in the pipeline component graphic module include: pipeline material attribute parameters, which are divided into three types: stainless steel 2169 material, stainless steel 1Cr18Ni10Ti material, and aluminum alloy 6061 material; pipeline pressure type parameters, which are divided into three types: supply pressure, i.e. 28MPa, oil suction, i.e. 2MPa, and oil return, i.e. 14MPa; pipeline specification parameters, which are used to select specification parameters of different pipe diameters.

[0043] The hydraulic actuator graphic module is configured with hydraulic flow parameters.

[0044] The pipeline connector graphic module is configured with confluence and diversion options.

[0045] Step 3, establishing the association between the three modules and the attribute parameter matcher: starting from any actuator, using the pipeline component graphic module and the pipeline connector graphic module to sequentially establish the cross-linking between the hydraulic actuator graphic module and the fuel tank graphic module; determining the association between the pipeline component graphic module, the hydraulic drive actuator graphic module, the pipeline connector graphic module, the fuel tank graphic module and the attribute parameter matcher;

[0046] Step 31: Determine the actual pipe specification of the pipe assembly graphic module having one end connected to the actuator graphic module and the other end connected to the pipe connector graphic module; specifically including:

[0047] Step 311: the pipeline component graphic module is connected to the hydraulic actuator graphic module, the attribute parameter matcher is automatically activated, and the flow division / confluence information of the pipeline connector graphic module is extracted, and it is in a state of waiting for logic judgment;

[0048] Step 312: Set the pressure type parameter of the pipeline component graphic module, and the attribute parameter matcher calculates the theoretical pipeline specifications according to the corresponding maximum flow rate and the flow parameter of the hydraulic actuator graphic module, which is in a state to be compared; specifically:

[0049] Determine the maximum flow rate according to the pressure type parameter of the pipeline component graphic module, determine the ratio of the flow parameter of the hydraulic actuator graphic module to the maximum flow rate of the pipeline component graphic module as the pipeline cross-sectional area, and determine the pipeline diameter according to the pipeline cross-sectional area as the theoretical pipeline specification;

[0050] Step 313: Setting pipeline material attribute parameters, the attribute parameter matcher compares the corresponding optional specifications of the material with the calculated theoretical pipeline specifications, and selects the closest value greater than the calculated result as the actual pipeline specification;

[0051] Step 32: Determine the actual pipeline specifications of the pipeline assembly graphic module with both ends connected to the pipeline connector graphic module, including:

[0052] Step 321: extracting the flow splitting / converging information of the flow parameter attributes of the pipeline connector graphic modules at both ends of the pipeline component graphic module;

[0053] Step 322: If both ends of the pipeline component graphic module are connected to the split flow, the flow attribute of the end close to the hydraulic drive actuator graphic module is used as the flow of the current pipeline component graphic module;

[0054] Determine the maximum flow rate according to the pressure type parameter of the pipeline component graphic module; determine the ratio of the flow rate of the current pipeline component graphic module to the maximum flow rate of the pipeline component graphic module as the pipeline cross-sectional area, and determine the pipeline diameter according to the pipeline cross-sectional area as the theoretical pipeline specification;

[0055] Set the pipeline material attribute parameters. The attribute parameter matcher compares the corresponding optional specifications of the material with the calculated theoretical pipeline specifications, and selects the closest value greater than the calculated result as the actual pipeline specification.

[0056] Step 323: when one end of the pipeline component graphic module is connected to a confluence, the attribute parameter matcher calculates the sum of the flow rates of the branch pipelines corresponding to the confluence port as the flow rate of the current pipeline;

[0057] Determine the maximum flow rate according to the pressure type parameter of the pipeline component graphic module; determine the ratio of the flow rate of the current pipeline component graphic module to the maximum flow rate of the pipeline component graphic module as the pipeline cross-sectional area, and determine the pipeline diameter according to the pipeline cross-sectional area as the theoretical pipeline specification;

[0058] Set the pipeline material attribute parameters. The attribute parameter matcher compares the corresponding optional specifications of the material with the calculated theoretical pipeline specifications, and selects the closest value greater than the calculated result as the actual pipeline specification.

[0059] Step 33: Determine the actual pipe specification of the pipe assembly graphic module, one end of which is connected to the fuel tank graphic module and the other end of which is connected to the pipe connector graphic module; specifically, including:

[0060] Step 331: extracting the flow parameter attribute of the pipeline connector graphic module at one end of the pipeline component graphic module away from the fuel tank graphic module;

[0061] Step 332: Determine whether the current pipeline component graphic module is split or converged when it is away from one end of the fuel tank graphic module; in the case of split flow, the flow of the pipeline component graphic module connected to the current pipeline component graphic module is used as the flow of the current pipeline; in the case of convergence, calculate the sum of the flow of each split pipeline corresponding to the convergence port as the flow of the current pipeline;

[0062] Step 333: determining the maximum flow rate according to the pressure type parameter of the pipeline component graphic module; determining the ratio of the flow rate of the current pipeline component graphic module to the maximum flow rate of the pipeline component graphic module as the pipeline cross-sectional area, and determining the pipeline diameter according to the pipeline cross-sectional area as the theoretical pipeline specification;

[0063] Step 334: Setting pipeline material attribute parameters, the attribute parameter matcher compares the corresponding optional specifications of the material with the calculated theoretical pipeline specifications, and selects the closest value greater than the calculated result as the actual pipeline specification;

[0064] Step 4: Graphic drawing: According to the onboard pipeline layout plan, connect the pipeline component graphic module with the hydraulic actuator graphic module, the fuel tank graphic module, and each pipeline connector graphic module;

[0065] Step 5: Automatic identification: Set the pipeline attribute parameters. The attribute parameter sensor automatically sets and confirms the pipeline specification attributes according to the logic of step 3.

[0066] Step 6. Result review: Check the pipeline specifications according to the flow of the hydraulic actuator graphic module connected to the pipeline component graphic module. If the theoretical pipeline specification is greater than the selected specification or the specification is beyond the material correspondence, an error reminder will be issued. Update the pipeline specifications by modifying the pipeline material properties of the pipeline component graphic module and the flow separation and confluence properties of the pipeline connector graphic module. After confirming that the requirements are met, the reminder information will be automatically cleared.

Claims

1. A graphical adaptive identification and generation method for specification parameters of a 28MPa pressure level aircraft hydraulic system pipeline component, characterized in that: include: Step 1: Set a pipeline component graphic module, a hydraulic drive actuator graphic module, a pipeline connector graphic module, a fuel tank graphic module, and a module attribute parameter matcher, wherein the pipeline component graphic module, the hydraulic drive actuator graphic module, the pipeline connector graphic module, and the fuel tank graphic module have an attribute setting function, and the attribute parameter matcher has a calculation and logic judgment function; Step 2: Set module attribute parameters; Step 3, starting from any actuator, using the pipeline component graphic module and the pipeline connector graphic module to sequentially establish the cross-linking between the hydraulic actuator graphic module and the fuel tank graphic module; determining the association between the pipeline component graphic module, the hydraulic drive actuator graphic module, the pipeline connector graphic module, the fuel tank graphic module and the attribute parameter matcher; Step 4: Graphic drawing: According to the onboard pipeline layout plan, connect the pipeline component graphic module with the hydraulic actuator graphic module, the fuel tank graphic module, and each pipeline connector graphic module; Step 5: Automatic identification: Set the pipeline attribute parameters. The attribute parameter sensor automatically sets and confirms the pipeline specification attributes according to the logic of step 3. Step 6: Review the settings and confirmation results.

2. The method according to claim 1, characterized in that The attribute parameters configured in the pipeline component graphic module include: pipeline material attribute parameters, which are divided into three types: stainless steel 2169 material, stainless steel 1Cr18Ni10Ti material, and aluminum alloy 6061 material; pipeline pressure type parameters, which are divided into three types: supply pressure, i.e. 28MPa, oil suction, i.e. 2MPa, and oil return, i.e. 14MPa; pipeline specification parameters, which are used to select specification parameters of different pipe diameters.

3. The method according to claim 1, characterized in that The hydraulic actuator graphic module is configured with hydraulic flow parameters.

4. The method according to claim 1, characterized in that: The pipeline connector graphic module is configured with confluence and diversion options.

5. The method according to claim 1, characterized in that Step three specifically includes: Step 31: Determine the actual pipe specification of the pipe assembly graphic module having one end connected to the actuator graphic module and the other end connected to the pipe connector graphic module; Step 32: Determine the actual pipeline specification of the pipeline assembly graphic module with both ends connected to the pipeline connector graphic module; Step 33: Determine the actual pipe specification of the pipe assembly graphic module that is connected to the fuel tank graphic module at one end and to the pipe connector graphic module at the other end.

6. The method according to claim 1, characterized in that Step 31 specifically includes: Step 311: the pipeline component graphic module is connected to the hydraulic actuator graphic module, the attribute parameter matcher is automatically activated, and the flow division / confluence information of the pipeline connector graphic module is extracted, and it is in a state of waiting for logic judgment; Step 312: Set the pressure type parameter of the pipeline component graphic module, and the attribute parameter matcher calculates the theoretical pipeline specifications according to the corresponding maximum flow rate and the flow parameter of the hydraulic actuator graphic module, which is in a state to be compared; specifically: Determine the maximum flow rate according to the pressure type parameter of the pipeline component graphic module, determine the ratio of the flow parameter of the hydraulic actuator graphic module to the maximum flow rate of the pipeline component graphic module as the pipeline cross-sectional area, and determine the pipeline diameter according to the pipeline cross-sectional area as the theoretical pipeline specification; Step 313: Set the pipeline material attribute parameters. The attribute parameter matcher compares the corresponding optional specifications of the material with the calculated theoretical pipeline specifications, and selects the closest value greater than the calculated result as the actual pipeline specification.

7. The method according to claim 1, characterized in that Step 32 specifically includes: Step 321: extracting the flow parameter attribute of the pipeline connector graphic modules at both ends of the pipeline component graphic module, the flow splitting / converging information; Step 322: If both ends of the pipeline component graphic module are connected to the split flow, the flow attribute of the end close to the hydraulic drive actuator graphic module is used as the flow of the current pipeline component graphic module; Determine the maximum flow rate according to the pressure type parameter of the pipeline component graphic module; determine the ratio of the flow rate of the current pipeline component graphic module to the maximum flow rate of the pipeline component graphic module as the pipeline cross-sectional area, and determine the pipeline diameter according to the pipeline cross-sectional area as the theoretical pipeline specification; Set the pipeline material attribute parameters. The attribute parameter matcher compares the corresponding optional specifications of the material with the calculated theoretical pipeline specifications, and selects the closest value greater than the calculated result as the actual pipeline specification. Step 323: when one end of the pipeline component graphic module is connected to a confluence, the attribute parameter matcher calculates the sum of the flow rates of the branch pipelines corresponding to the confluence port as the flow rate of the current pipeline; Determine the maximum flow rate according to the pressure type parameter of the pipeline component graphic module; determine the ratio of the flow rate of the current pipeline component graphic module to the maximum flow rate of the pipeline component graphic module as the pipeline cross-sectional area, and determine the pipeline diameter according to the pipeline cross-sectional area as the theoretical pipeline specification; Set the pipeline material attribute parameters. The attribute parameter matcher compares the corresponding optional specifications of the material with the calculated theoretical pipeline specifications, and selects the closest value that is greater than the calculated result as the actual pipeline specification.

8. The method according to claim 1, characterized in that: Step 33 specifically includes: Step 331: extracting the flow parameter attribute of the pipeline connector graphic module at one end of the pipeline component graphic module away from the fuel tank graphic module; Step 332: Determine whether the current pipeline component graphic module is split or converged when it is away from one end of the fuel tank graphic module; in the case of split flow, the flow of the pipeline component graphic module connected to the current pipeline component graphic module is used as the flow of the current pipeline; in the case of convergence, calculate the sum of the flow of each split pipeline corresponding to the convergence port as the flow of the current pipeline; Step 333: determining the maximum flow rate according to the pressure type parameter of the pipeline component graphic module; determining the ratio of the flow rate of the current pipeline component graphic module to the maximum flow rate of the pipeline component graphic module as the pipeline cross-sectional area, and determining the pipeline diameter according to the pipeline cross-sectional area as the theoretical pipeline specification; Step 334: Set the pipeline material attribute parameters. The attribute parameter matcher compares the corresponding optional specifications of the material with the calculated theoretical pipeline specifications, and selects the closest value greater than the calculated result as the actual pipeline specification.