CN114118725A - Multi-state configuration method of assembly tool - Google Patents

Multi-state configuration method of assembly tool Download PDF

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Publication number
CN114118725A
CN114118725A CN202111316774.1A CN202111316774A CN114118725A CN 114118725 A CN114118725 A CN 114118725A CN 202111316774 A CN202111316774 A CN 202111316774A CN 114118725 A CN114118725 A CN 114118725A
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China
Prior art keywords
machine
information
derivative
tool
target machine
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Pending
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CN202111316774.1A
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Chinese (zh)
Inventor
邹秋芽
韩波
王波
王梅
张睿
韩志斌
张伟
王家麟
刘剑超
胡高林
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Shaanxi Aircraft Industry Co Ltd
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Shaanxi Aircraft Industry Co Ltd
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Priority to CN202111316774.1A priority Critical patent/CN114118725A/en
Publication of CN114118725A publication Critical patent/CN114118725A/en
Pending legal-status Critical Current

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    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06Q—INFORMATION AND COMMUNICATION TECHNOLOGY [ICT] SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES, NOT OTHERWISE PROVIDED FOR
    • G06Q10/00—Administration; Management
    • G06Q10/06—Resources, workflows, human or project management; Enterprise or organisation planning; Enterprise or organisation modelling
    • G06Q10/063—Operations research, analysis or management
    • G06Q10/0631—Resource planning, allocation, distributing or scheduling for enterprises or organisations
    • G06Q10/06315—Needs-based resource requirements planning or analysis
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06Q—INFORMATION AND COMMUNICATION TECHNOLOGY [ICT] SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES, NOT OTHERWISE PROVIDED FOR
    • G06Q10/00—Administration; Management
    • G06Q10/06—Resources, workflows, human or project management; Enterprise or organisation planning; Enterprise or organisation modelling
    • G06Q10/063—Operations research, analysis or management
    • G06Q10/0631—Resource planning, allocation, distributing or scheduling for enterprises or organisations
    • G06Q10/06316—Sequencing of tasks or work
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06Q—INFORMATION AND COMMUNICATION TECHNOLOGY [ICT] SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES, NOT OTHERWISE PROVIDED FOR
    • G06Q50/00—Systems or methods specially adapted for specific business sectors, e.g. utilities or tourism
    • G06Q50/04—Manufacturing
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P90/00—Enabling technologies with a potential contribution to greenhouse gas [GHG] emissions mitigation
    • Y02P90/30—Computing systems specially adapted for manufacturing

Abstract

The invention discloses a multi-state configuration method of an assembly fixture, which belongs to the technical field of aviation manufacturing, and provides the multi-state configuration method of the assembly fixture.

Description

Multi-state configuration method of assembly tool
Technical Field
The application belongs to the technical field of aviation manufacturing, and particularly relates to a multi-state configuration method of an assembly tool.
Background
Once the airplane is designed and sized, the modified airplane based on the designed and sized airplane (namely, the reference airplane) can be derived, the structure of the derived airplane is locally modified relative to the reference airplane to meet different task requirements, the external geometric dimension and the internal structure of the airplane are locally modified, and the relative position relationship of the geometric dimension and the structure is mostly ensured through an assembly tool. The geometry and relative positioning of the structures of each remodelling machine is generally referred to as a state of the remodelling machine. Because the output ratio needs to be considered in the aircraft manufacturing process, most of tools for assembling derivative models with low yield adopt a method of additionally processing the assembly of a reference machine to realize the assembly and the manufacture of the machine, only a small part of the tools are special tools for the derivative models, after the derivative models are produced, the tools need to be restored to the state of the reference machine or the states of other derivative models, when the derivative models are more, the states of the tools are more, how to express the states in the assembly tool is the key for the correctness of the tool state conversion drawing, if the state expression is not clear, the state conversion error is easily caused, the product quality accident is caused, and the smooth implementation of the subsequent added tools is also influenced.
Disclosure of Invention
The problem that management of the technical state of an assembly tool of a derivative model in a reference model is unclear in the related art is solved. The application provides a multi-state configuration method of an assembly tool, which comprises the following technical scheme:
a method of multi-state configuration of an assembly fixture, the method comprising:
when a determining instruction is received, determining a plurality of derivative machines corresponding to a reference machine according to a preset requirement, wherein the plurality of derivative machines are sequenced according to a preset sequence;
determining the assembly requirements of each of the derivative machines;
judging whether the corresponding derivative machines need to be added with parts or not according to the sorting structure and the assembly requirements of each derivative machine in sequence;
when the derivative machine needs to add parts, tool part management information of the derivative machine is added in assembly tool information of the reference machine, wherein the tool part management information of the derivative machine comprises an identifier of the derivative machine and indication information of the tool part information;
tool component information of the derivative machine is added to the tool component management information of the derivative machine;
and determining the applicable machine types of all the tool components in the assembly tool information after the tool component information of the derivative machine is added.
Optionally, the method further comprises:
when an information deleting instruction is received, deleting the tooling component information of a target machine, wherein the information deleting instruction carries the identification of the target machine and the tooling component information to be deleted, and the target machine is at least one of the reference machine and the derivative machine;
and determining the applicable machine type of the corresponding tool component according to the deleted tool component information.
Optionally, the method further comprises:
when an information replacement instruction is received, replacing tooling component information of a target machine, wherein the information replacement instruction carries an identifier of the target machine and tooling component information to be replaced, and the target machine is at least one of the reference machine and the derivative machine;
and determining the applicable machine type of the corresponding tool component according to the replaced tool component information.
Optionally, the method further comprises:
when an information adding instruction is received, tool component information of a target machine is added, wherein the information adding instruction carries an identifier of the target machine and tool component information to be added, and the target machine is at least one of the reference machine and the derivative machine;
and determining the applicable machine type of the corresponding tool component according to the increased tool component information.
Optionally, the method further comprises:
when a state transition instruction is received, comparing tooling component information of a first target machine with tooling component information of a second target machine, wherein the state transition instruction is used for indicating the transition from the first target machine to the second target machine, the first target machine is a reference machine, the second target machine is a derivative machine, or the first target machine is a derivative machine, the second target machine is a reference machine, or the first target machine is a derivative machine, and the second target machine is another derivative machine;
when the tooling component information of the first target machine is the same as the tooling component information of the second target machine, the operation is finished;
when the tooling component information of the first target machine is different from the tooling component information of the second target machine, determining the same information of the tooling component information of the first target machine and the tooling component information of the second target machine;
outputting the information except the same information in the tooling component information of the first target machine;
and outputting the information except the same information in the tooling component information of the second target machine.
Optionally, the tool component information includes a size parameter, preparation material information, and position information of the tool component.
Optionally, the reference machine corresponds to 7-8 derivation machines.
Optionally, the determining, according to preset requirements, multiple kinds of derivative machines corresponding to the reference machine includes:
and determining various derivative machines corresponding to the reference machine according to the requirements of the scientific research plan.
The application provides a multi-state configuration method of an assembly fixture, the assembly fixture in the multi-state can realize the good management of the state, the method can clearly reflect the position and the quantity of components corresponding to each state and the interrelation of other states, so that the time of process equipment and the occurrence of errors are reduced when the fixture object performs state conversion, the model changing efficiency of the fixture is improved, the occurrence of model changing errors of the process equipment caused by unclear technical states is avoided, and the quality cost is reduced.
Drawings
Fig. 1 is a flowchart of a multi-state configuration method of an assembly fixture provided in the present application.
Detailed Description
The application provides a multi-state configuration method of an assembly tool, which is used for an electronic device, for example, the electronic device may be a computer, as shown in fig. 1, and the method includes:
and 110, when the determining instruction is received, determining a plurality of derivative machines corresponding to the reference machine according to a preset requirement, wherein the plurality of derivative machines are sequenced according to a preset sequence.
And step 120, determining the assembly requirement of each type of derivative machine.
And step 130, judging whether the corresponding derivative machines need to add parts or not according to the assembly requirements of each derivative machine in sequence according to the sorting structure.
And 140, when the derivative machine needs to add parts, adding tool part management information of the derivative machine in the assembly tool information of the reference machine, wherein the tool part management information of the derivative machine comprises an identifier of the derivative machine and indication information of the tool part information.
And 150, adding the tool component information of the derivative machine in the tool component management information of the derivative machine.
And step 160, determining the applicable models of all tool components in the assembly tool information after the tool component information of the derivative machine is added.
The application provides a multi-state configuration method of an assembly fixture, the assembly fixture in the multi-state can realize the good management of the state, the method can clearly reflect the position and the quantity of components corresponding to each state and the interrelation of other states, so that the time of process equipment and the occurrence of errors are reduced when the fixture object performs state conversion, the model changing efficiency of the fixture is improved, the occurrence of model changing errors of the process equipment caused by unclear technical states is avoided, and the quality cost is reduced.
The application provides another multi-state configuration method of an assembly tool, which is used for an electronic device, for example, the electronic device may be a computer, and the method includes:
and step 210, when the determination instruction is received, determining a plurality of derivative machines corresponding to the reference machine according to the requirements of the scientific research plan, and sequencing the plurality of derivative machines according to a preset sequence.
After a brand-new airplane is successfully developed, in order to exert the platform advantages of the airplane, the platform is taken as a reference airplane, and development and planning of a plurality of derivative airplane types are sequentially developed according to the requirements of customers and the emergency degree of the requirements,
the reference machine corresponds to 7-8 derivation machines.
If the reference model is XX, AA, BB, CC, DD, EE, FF, GG, HH and other models can be derived, most of the structures of the derived models are the same as the reference model, and only parts of the derived models are different.
Step 220, determining the assembly requirements of each type of derivative machine.
And (4) according to the design pattern of the derivative model, providing the assembly requirement of the model, namely a tooling order form, and definitely assembling on the basis of the assembly tooling of the reference machine.
And step 230, sequentially judging whether the corresponding derivative machines need to add parts according to the assembly requirements of each derivative machine according to the sorting structure.
Whether the tooling components of the reference machine are suitable for the derivative machine or not and whether the adaptability improvement is needed or not can be met through the assembly requirement.
And 240, when the derivative machine needs to add parts, adding tool part management information of the derivative machine in the assembly tool information of the reference machine, wherein the tool part management information of the derivative machine comprises an identifier of the derivative machine and indication information of the tool part information.
The identification of the tool components of the derivative machine is realized by special numbering of the tool components, and the tool components below the tool components are collected.
And step 250, adding the tool component information of the derivative machine in the tool component management information of the derivative machine.
The tool component information comprises the size parameters, the preparation material information, the quantity information and the position information of the tool component.
And step 260, determining the applicable machine types of all the tool parts in the assembly tool information after the tool part information of the derivative machine is added.
And 270, deleting the tooling component information of the target machine when the information deleting instruction is received.
The information deleting instruction carries an identifier of the target machine and information of the tool parts to be deleted, and the target machine is at least one of a reference machine and a derivative machine.
And step 280, determining the applicable machine type of the corresponding tool component according to the deleted tool component information.
And 290, replacing the tooling component information of the target machine when the information replacement instruction is received.
The information replacement instruction carries an identifier of the target machine and information of the tool parts to be replaced, and the target machine is at least one of a reference machine and a derivative machine.
And 310, determining an applicable model of the corresponding tool component according to the replaced tool component information.
And step 320, when the information adding instruction is received, adding the tool component information of the target machine.
The information adding instruction carries an identifier of a target machine and information of the tool parts to be added, and the target machine is at least one of a reference machine and a derivative machine.
And 330, determining the applicable machine type of the corresponding tool component according to the increased tool component information.
And 340, comparing the tooling component information of the first target machine with the tooling component information of the second target machine when the state conversion instruction is received.
The state transition instruction is used for indicating the transition from the first target machine to the second target machine, wherein the first target machine is a reference machine, and the second target machine is a derivative machine, or the first target machine is the derivative machine and the second target machine is the reference machine, or the first target machine is the derivative machine and the second target machine is another derivative machine.
And 350, when the tooling component information of the first target machine is the same as the tooling component information of the second target machine, finishing the operation.
And step 360, when the tooling component information of the first target machine is different from the tooling component information of the second target machine, determining the same information of the tooling component information of the first target machine and the tooling component information of the second target machine.
And step 370, outputting the information except the same information in the tooling component information of the first target machine.
And 380, outputting the information except the same information in the tooling component information of the second target machine.
The tooling part information of a first target model records part numbers 1, 2, 3, 4, 5, 6, 7, 8, 9, 10 and 11 as part numbers used by the first target model, the tooling part information of a second target model records part numbers 1, 2, 3, 4, 5, 6, 7, 9, 10, 11, 13, 14 and 15 as part numbers used by the second target model, the part numbers shared by the first and second target models are 1, 2, 3, 4, 5, 6, 7, 9, 10 and 11, the tooling part number 8 in the first target model and the tooling part number 13, 14 and 15 in the second target model are special parts of the first and second target models by comparing the part numbers used by the first and second target models with the part number shared by the first and second target models, the first target model removes the tooling part number 8, and the second target model installs the part number 13, 14. The tooling components of 15 can complete the assembly tooling state conversion from the first target machine to the second target machine.
The invention provides a multi-state configuration method of an assembly tool, the assembly tool in multiple states can realize good management of the states, and the method can clearly reflect the positions and the number of components corresponding to each state and the interrelation with other states, so that the time and errors of process equipment are reduced when the tool real object performs state conversion, the model changing efficiency of the tool is improved, the occurrence of model changing errors of the process equipment caused by unclear technical states is avoided, and the quality cost is reduced.
The method mainly solves the problem that the technical state management of the assembly fixture of the derivative model in the reference model is unclear, the states of a plurality of derivative models exist in the assembly fixture drawing corresponding to one component or part of the current reference model, and the special parts of part of the derivative models are intersected, so that the relations between the reference model and the derivative models and between the derivative models are very complex. The design of the tool is carried out according to the development sequence of the machine types, when the number of derived machine types is more and more, a customer cannot order the order according to the development sequence of the airplane, the customer can selectively order among the machine types, the required sequence is inconsistent with the development sequence, the state conversion of the tool is irregular, if the technical state of the assembly tool is not uniformly managed, the state of a real object is difficult to quickly and accurately card during the machine type conversion, namely, the model needs to be dismounted and the model needs to be mounted, the design interference can be effectively avoided through the method, and the model changing efficiency and the model changing quality of the tool are improved.
The foregoing merely represents embodiments of the present application, which are described in greater detail and detail, and therefore should not be construed as limiting the scope of the invention. It should be noted that, for a person skilled in the art, several variations and modifications can be made without departing from the concept of the present application, which falls within the scope of protection of the present application.

Claims (8)

1. A multi-state configuration method of an assembly tool is characterized by comprising the following steps:
when a determining instruction is received, determining a plurality of derivative machines corresponding to a reference machine according to a preset requirement, wherein the plurality of derivative machines are sequenced according to a preset sequence;
determining the assembly requirements of each of the derivative machines;
judging whether the corresponding derivative machines need to be added with parts or not according to the sorting structure and the assembly requirements of each derivative machine in sequence;
when the derivative machine needs to add parts, tool part management information of the derivative machine is added in assembly tool information of the reference machine, wherein the tool part management information of the derivative machine comprises an identifier of the derivative machine and indication information of the tool part information;
tool component information of the derivative machine is added to the tool component management information of the derivative machine;
and determining the applicable machine types of all the tool components in the assembly tool information after the tool component information of the derivative machine is added.
2. The method of claim 1, further comprising:
when an information deleting instruction is received, deleting the tooling component information of a target machine, wherein the information deleting instruction carries the identification of the target machine and the tooling component information to be deleted, and the target machine is at least one of the reference machine and the derivative machine;
and determining the applicable machine type of the corresponding tool component according to the deleted tool component information.
3. The method of claim 1, further comprising:
when an information replacement instruction is received, replacing tooling component information of a target machine, wherein the information replacement instruction carries an identifier of the target machine and tooling component information to be replaced, and the target machine is at least one of the reference machine and the derivative machine;
and determining the applicable machine type of the corresponding tool component according to the replaced tool component information.
4. The method of claim 1, further comprising:
when an information adding instruction is received, tool component information of a target machine is added, wherein the information adding instruction carries an identifier of the target machine and tool component information to be added, and the target machine is at least one of the reference machine and the derivative machine;
and determining the applicable machine type of the corresponding tool component according to the increased tool component information.
5. The method of claim 1, further comprising:
when a state transition instruction is received, comparing tooling component information of a first target machine with tooling component information of a second target machine, wherein the state transition instruction is used for indicating the transition from the first target machine to the second target machine, the first target machine is a reference machine, the second target machine is a derivative machine, or the first target machine is a derivative machine, the second target machine is a reference machine, or the first target machine is a derivative machine, and the second target machine is another derivative machine;
when the tooling component information of the first target machine is the same as the tooling component information of the second target machine, the operation is finished;
when the tooling component information of the first target machine is different from the tooling component information of the second target machine, determining the same information of the tooling component information of the first target machine and the tooling component information of the second target machine;
outputting the information except the same information in the tooling component information of the first target machine;
and outputting the information except the same information in the tooling component information of the second target machine.
6. The method of claim 1,
the tool component information comprises the size parameters, the preparation material information and the position information of the tool component.
7. The method of claim 1, wherein the reference machine corresponds to 7 to 8 derivative machines.
8. The method according to claim 1, wherein the determining the plurality of kinds of derivative machines corresponding to the reference machine according to preset requirements comprises:
and determining various derivative machines corresponding to the reference machine according to the requirements of the scientific research plan.
CN202111316774.1A 2021-11-08 2021-11-08 Multi-state configuration method of assembly tool Pending CN114118725A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202111316774.1A CN114118725A (en) 2021-11-08 2021-11-08 Multi-state configuration method of assembly tool

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202111316774.1A CN114118725A (en) 2021-11-08 2021-11-08 Multi-state configuration method of assembly tool

Publications (1)

Publication Number Publication Date
CN114118725A true CN114118725A (en) 2022-03-01

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Application Number Title Priority Date Filing Date
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Country Status (1)

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