Test data acquisition virtualization platform for civil aero-engine

By constructing a decentralized virtualization platform for aero-engine test data acquisition, and employing multi-node, multi-replica, and intelligent exchange equipment, the problems of aging existing system equipment and high network latency were solved, enabling efficient acquisition and management of test data and improving system reliability and resource utilization efficiency.

CN121364071APending Publication Date: 2026-01-20AECC COMML AIRCRAFT ENGINE CO LTD
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Patent Information

Application Number
CN202410963469.9
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2024-07-17
Publication Date
2026-01-20

AI Technical Summary

Technical Problem

The existing aero-engine data acquisition system is outdated and difficult to maintain and upgrade, suffers from high network latency, lacks interconnectivity of test equipment, and cannot effectively utilize and mine a large amount of accumulated test data.

Method used

It employs a data acquisition system, a virtualized complete machine test bench, and intelligent switching equipment. Through cloud technology and virtualization mirroring technology, it achieves multi-node and multi-copy, constructs a decentralized network topology, and uses Cat 6e network cables and intelligent stacking technology to achieve proactive risk avoidance and automatic backup, supporting the simultaneous preparation of multiple test environments.

Benefits of technology

It improves the accuracy of experimental data acquisition and communication efficiency, ensures network reliability and data security, realizes unified management and efficient utilization of computing resources, and supports big data computing and comprehensive management business.

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Abstract

The invention provides a test data acquisition virtualization platform for a civil aero-engine. The platform comprises a data acquisition system, a first virtualized complete machine test bed and a second virtualized complete machine test bed, the data acquisition system comprises an acquisition terminal, a node service station and a total service station; the acquisition terminal acquires simulation test data generated by the first virtualized complete machine test bed and the second virtualized complete machine test bed; the acquisition terminal is connected with the node service station through the intelligent switching equipment; the node service stations are connected with the total service station through intelligent switching equipment; and the node service stations are mutually connected through the intelligent switching equipment.
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Description

TECHNICAL FIELD

[0001] The present application relates to the field of aero-engines, in particular to data acquisition of civil aero-engines. BACKGROUND

[0002] With the continuous development of engine research and development work, the number and types of test parameters required for engine testing are increasing. However, the existing data acquisition system for aero-engines has many defects.

[0003] Firstly, the existing data acquisition system for aero-engines has a backward architecture, a high degree of association between software and hardware, a physical platform that cannot be replicated, no backup when a single hardware device fails, and no quick recovery. Moreover, the device is used continuously for a long time, data is stored in an independent physical host, there is no data backup solution, and data will be lost once the physical host fails. Therefore, it is necessary to build an advanced data acquisition, storage, analysis, and processing system platform to realize the overall packaging of measurement and control, data acquisition, and other business systems, decouple the business host software and hardware while ensuring normal operation of the business system; after migration, the business system is uniformly managed under the new platform, providing more computing resources for the business host and improving the efficiency of business software operation.

[0004] Secondly, the existing network structure is complex and is outsourced to different suppliers according to different protocols. The protocols are numerous, and different network devices are used, which are not compatible and cannot be managed uniformly. It is difficult to troubleshoot problems one by one, and the network line used is a 5-class ordinary network line without shielding and anti-interference. In future use, it is easy to cause uncontrollable connection problems due to line aging, and the complex connection hinders the sustainable expansion of the machine.

[0005] Thirdly, the existing data acquisition system platform for aero-engines is relatively single, being a single node and single copy, and the resources cannot be integrated, so the reliability and high performance requirements cannot be met. Each test bench is independent, and the computing resources are not formed into a unified management platform, so the unified management and distribution of computing resources cannot be realized. The test bench can only perform test preparation for a certain type of engine, which is inefficient. Moreover, there is no mature backup system, the stability is not high, and it cannot bear the big data computing business based on test data and the comprehensive management business of each test bench.

[0006] Fourthly, the existing platform is based on single hardware construction, the software system is unstable, any single computer cannot provide sufficient computing power and storage capacity, the existing collection system is asynchronous discrete large file data, the existing relational database cannot process massive data. The platform architecture is not designed according to the distributed high-reliability architecture, cannot support horizontal expansion, so that any single or multiple server hardware failure or software error will affect the availability and reliability of the system, and cannot efficiently utilize the computing and storage resources in the heterogeneous cluster.

[0007] In summary, a new type of test data acquisition virtualization platform for civil aviation engines is urgently needed to solve the problems of existing test data acquisition system equipment aging and difficult maintenance and upgrade, high network latency of test data acquisition system, non-connection of each tester, and inability to effectively utilize and mine accumulated large amounts of test data. SUMMARY

[0008] In order to solve the problems of existing test data acquisition system equipment aging and difficult maintenance and upgrade, high network latency of test data acquisition system, non-connection of each tester, and inability to effectively utilize and mine accumulated large amounts of test data, the present application provides a test data acquisition virtualization platform for civil aviation engines.

[0009] The test data acquisition virtualization platform for civil aviation engines provided by the present application comprises a data acquisition system, a first virtualized whole-machine test bench and a second virtualized whole-machine test bench.

[0010] The data acquisition system comprises an acquisition terminal, a node service station and a total service station; the acquisition terminal acquires analog test data generated by the first virtualized whole-machine test bench and the second virtualized whole-machine test bench; the acquisition terminal is connected with the node service station through intelligent switching equipment; the node service station is connected with the total service station through intelligent switching equipment; the node service stations are connected with each other through intelligent switching equipment.

[0011] In one embodiment, the first virtualized whole-machine test bench or the second virtualized whole-machine test bench uses cloud technology and virtualization image technology to replace the original single-node single-copy with multiple-node multiple-copy to realize active risk avoidance, reactive fault tolerance and active management, create multiple virtual machines in the test, carry different test environments, and prepare different test environments at the same time.

[0012] In one embodiment, the acquisition terminal transmits the data generated by each virtual machine to the node server through the intelligent switching equipment.

[0013] In one embodiment, the acquisition terminals are connected through a test bench.

[0014] In one embodiment, the data acquisition system is in communication connection with a cloud space.

[0015] In one embodiment, the node service station comprises a node server and a database server; the node server is connected to the database server; the database server stores all data in the node server; the node service station collects and integrates the data collected by the acquisition terminal in the node area.

[0016] In one embodiment, the total service station comprises a total server, a total data server and a backup data server; the total server stores data in the total data server and backs up in the backup data server; the total service station is used for collecting and integrating all test data.

[0017] In one embodiment, the intelligent switching device has an intelligent stacking technology module, a cloud management module, a VXLAN feature, a network flow analysis module and an operation and maintenance module.

[0018] In one embodiment, the intelligent switching device is connected to the network through a 10GB network broadband.

[0019] In one embodiment, a super six category network cable is used in the data acquisition system.

[0020] The test data acquisition virtualization platform for civil aviation engine of the present application has the following advantages:

[0021] Firstly, a new generation of industrial internet construction technology is adopted to redefine the network topology structure of the test bench, and a decentralized architecture is adopted, and the switching devices are distributed in each node, so that when the switching device of any node in the loop fails, other nodes still maintain interconnection, and the reliability of the test network is maximized.

[0022] Secondly, the present application uses multiple nodes and multiple copies instead of the original single node and single copy to realize active risk avoidance, reactive fault tolerance and active management, and different test environments can be prepared at the same time. The platform also has the function of automatic backup configuration, which greatly improves the accuracy of the test.

[0023] Thirdly, the node servers of the present application can communicate with each other, so that when the total server cannot be connected to a certain node server, the information in the server can be obtained through other servers.

[0024] Fourthly, the present application improves the network bandwidth, so that the communication speed and efficiency can be greatly improved. BRIEF DESCRIPTION OF DRAWINGS

[0025] The above summary of the application and the following detailed description of the application will be better understood when read in conjunction with the accompanying drawings. It is noted that the figures are presented for the purpose of illustrating the application claimed and described herein. In the drawings, like reference numerals refer to identical or similar elements throughout.

[0026] Figure 1 Fig. 1 shows a general architecture diagram of a test data acquisition virtualization platform for civil aviation engines according to an embodiment of the present application;

[0027] Figure 2 Fig. 2 shows a topology diagram of a data acquisition system according to an embodiment of the present application;

[0028] Figure 3 Fig. 3 shows a functional diagram of an intelligent switching device according to an embodiment of the present application. DETAILED DESCRIPTION

[0029] The specific features and advantages of the present application will be described in detail in the following detailed description of the application, which is sufficient to enable any person skilled in the art to understand the technical content of the present application and to implement it, and according to the description, claims and drawings disclosed in the specification, those skilled in the art can easily understand the related purposes and advantages of the present application. Although the description of the present application will be introduced in combination with the preferred embodiments, it does not mean that the features of the present application are limited to the embodiments. On the contrary, the purpose of introducing the application in combination with the embodiments is to cover other options or modifications that can be extended based on the claims of the present application. In order to provide a deep understanding of the present application, many specific details will be included in the following description. The present application can also be implemented without using these details. In addition, in order to avoid confusion or obscure the focus of the present application, some specific details will be omitted in the description.

[0030] In the description of the present application, it should be noted that unless otherwise explicitly specified and limited, the terms "mounting", "connection", "connection" should be understood broadly, for example, it can be fixedly connected, or it can be detachably connected, or integrally connected; it can be mechanically connected, or it can be electrically connected; it can be directly connected, or it can be indirectly connected through an intermediate medium, or it can be connected inside two elements. For those skilled in the art, the specific meaning of the above terms in the present application can be understood according to the specific circumstances.

[0031] In addition, in the following description, "up", "down", "left", "right", "top", "bottom", "horizontal", "vertical" should be understood as the orientation shown in the paragraph and the related drawings. Such relative terms are only used for convenience of description, and they do not mean that the devices described should be manufactured or operated in a particular orientation, so they should not be understood as limiting the present application.

[0032] It is to be understood that, while the terms "first," "second," "third," etc. can be used herein to describe various elements, components, channels, regions, layers and / or sections, these elements, components, channels, regions, layers and / or sections should not be limited by these terms as these terms are only used to distinguish one element, component, channel, region, layer and / or section from another element, component, channel, region, layer and / or section. Also, the terms "first," "second," "third," etc. are only used to describe different elements, components, channels, regions, layers and / or sections and do not imply relative importance of the elements, components, channels, regions, layers and / or sections.

[0033] As used in this application and the claims, the terms "comprises", "comprising", "includes", "including" or the like are not intended to exclude a combination of e.g. elements, components, steps, or the like, that can be

[0034] Some embodiments use numerical descriptors of amounts of ingredients, attributes, etc. It should be understood that such numerical descriptors used in the description of embodiments can in some examples be modified by the modifier "about," "approximately," or "generally." Unless otherwise stated, "about," "approximately," or "generally" indicates that a deviation of ±20% is allowed. Accordingly, numerical parameters such as those outlined in the application and claims are approximations, and may, in some embodiments, vary depending upon the desired characteristics sought to be obtained in light of the particular

[0035] Also, the use of certain words or terms in various places in the specification is merely intended to add clarity and under no circumstances should be used to limit the meaning of the description. For example, while the term "including" can mean "comprising A or B" or "comprising A, B, or C," the term "comprising" can mean "including, without limitation" A, B, or C, or "comprising at least A, B, or C." In addition, the term "coupled" means directly or indirectly connected, without necessarily being in physical contact, and the term "current" means generally an electrical current, unless otherwise indicated.

[0036] Figure 1The figure shows a general architecture diagram of a test data acquisition virtualization platform for civil aviation engines according to an embodiment of the present application. The test data acquisition virtualization platform for civil aviation engines comprises a data acquisition system 101, a first virtualized whole-machine test bench 102, and a second virtualized whole-machine test bench 103. The data acquisition system 101 is in communication connection with a cloud space. The first virtualized whole-machine test bench 102 and the second virtualized whole-machine test bench 103 complete simulation tests through cloud technology and virtualization image technology.

[0037] Figure 2 The figure shows a topology diagram of a data acquisition system according to an embodiment of the present application. The data acquisition system 101 comprises acquisition terminals 201, node service stations 202, and a general service station 203. The acquisition terminals are in communication connection through test benches. The acquisition terminals acquire simulation test data generated by the first virtualized whole-machine test bench and the second virtualized whole-machine test bench. The acquisition terminals are connected with the node service stations through intelligent switching devices. The node service stations are connected with the general service station through intelligent switching devices, and the node service stations are connected with each other through intelligent switching devices.

[0038] In one embodiment, the node service station 202 comprises a node server and a database server. The node service station 202 can collect and integrate data collected by the acquisition terminals in the node area. The database server can store all data in the node server.

[0039] In one embodiment, the general service station 203 comprises a general server, a general data server, and a backup data server. The general service station is used for collecting and integrating all test data. The general server can store data in the general data server and can also backup in the backup data server.

[0040] Figure 3 The figure shows a functional diagram of an intelligent switching device according to an embodiment of the present application. The intelligent switching device has an intelligent stacking technology module 301, a cloud management module 302, a VXLAN feature module 303, a network flow analysis module 304, and an operation and maintenance module 305.

[0041] The intelligent stacking technology module 301 is used to logically change multiple switching devices supporting stacking features into one switching device, which participates in data forwarding as a whole.

[0042] The cloud management module 302 is used to automatically connect to a management control system and ensure the safety of the management channel through bidirectional certificate authentication.

[0043] The VXLAN feature module 303 can realize the fusion deployment of multiple service networks or tenant networks on the same physical network, meet the data bearing requirements of different services / customers, save the network construction cost, and improve the network resource utilization efficiency.

[0044] The network flow analysis module 304 is used for collecting specified data flow in real time, uploading data to a network flow collector, and helping users to optimize the network structure and adjust resource deployment in time.

[0045] The operation and maintenance module 305 supports RMON, multiple log hosts, port flow statistics, and network quality analysis, and facilitates network optimization and reconstruction.

[0046] In an embodiment, the intelligent switching device is connected with the network through a 10GB network broadband. By improving the network bandwidth, the communication speed and efficiency can be greatly improved.

[0047] In an embodiment, the network cable used in the data acquisition system is a super six category network cable. Therefore, the network cable has good shielding and anti-interference ability and good safety.

[0048] The first virtualization whole machine test bench and the second virtualization whole machine test bench can complete simulation tests, use cloud technology and virtualization image technology, use multiple nodes and multiple copies instead of the original single node and single copy to realize active risk avoidance, reactive fault tolerance and active management, create multiple virtual machines in the test, load different test environments, and can simultaneously prepare different test environments. The test data acquisition virtualization platform also has the function of automatically backing up the configuration, greatly improving the accuracy of the test. The data generated by the first virtualization whole machine test bench and the second virtualization whole machine test bench during the simulation test can be collected through the acquisition terminal. The acquisition terminals can communicate with each other through the test bench. The acquisition terminal can transmit the data generated by each virtual machine to the node server through the intelligent switching device. The database server can store all the data in the node. The node service station can transmit all the data in the node to the total server through the intelligent switching device. The total server can store the data in the total data server and can back up the data in the standby data server, thereby preventing data loss. The node service stations also communicate with each other through the intelligent switching device. Therefore, when the total service station and a node service station cannot communicate, the node server can communicate with the node server and obtain the required information through other node servers. The required information in the node server can be transmitted to the total service station through other servers.

[0049] Different protocol devices connected to the same switching device can use the VXLAN technology of the intelligent switching device. VXLAN is different from the traditional IP packet in that a label is added to the header of the traditional IP packet. All switching devices in the network system need to be able to process the labeled packet, and a mapping relationship between the label and the area is established. The next time the switching device receives a labeled data on the link, it knows that the data packet corresponds to the ECS area, and similarly, the labeled data packet belongs to the JB industrial control area.

[0050] Thus, the problems of multiple protocols between devices, non-interoperability, incompatibility, and inability to implement unified management are solved. If a device fails, the corresponding interface and line of the failed device can be quickly found from the management interface of the intelligent switching device, thereby confirming whether the failure is caused by the network, and simplifying the troubleshooting difficulty.

[0051] After network reconstruction, network digitization can be achieved. Through digitization, the network state is perceived, the whole network state is abstractly modeled in the digital world, and is uniformly placed in the cloud, so that the cloud unified management and real-time state visualization of the whole network can be achieved. By introducing new technologies such as artificial intelligence and big data, intelligence can be further introduced, intelligent balanced scheduling of network resources and cloud resources can be achieved, network intelligent operation and maintenance can be achieved, and troubleshooting efficiency can be greatly improved; security intelligent defense can be achieved, and security protection capability can be comprehensively improved. Thus, a stable, reliable, efficient and easy-to-maintain environment is provided for aero-engine testing.

[0052] A high-availability server cluster is built to provide a hardware foundation for cloud platform construction, integrate the computing resources of the whole machine test bed to form a unified management platform, and realize unified management and distribution of computing resources; meet the reliability and high-performance requirements of test business, and meet the scalability and generality requirements of future complex test business; be able to bear the big data computing business based on test data and the comprehensive management business of each test bed, as well as other digital test business in the future.

[0053] The high-availability server cluster can be expanded across hundreds of interconnected physical machines and storage devices, thereby forming a complete virtual infrastructure. There is no need to permanently allocate servers, storage space or network bandwidth for each application. Instead, hardware resources are dynamically allocated to the required bits when needed. The highest priority application always gets the resources it needs, so there is no need to waste money on excess resources that are only needed during peak times.

[0054] After building a high-availability server cluster, the servers of each test stand are no longer independent, and the computing resources form a unified management platform, realizing unified management and distribution of computing resources. A test environment with multiple replicas and multiple nodes can be realized. Multiple physical environments and multiple virtual environments are matched, and each virtual environment can be separately corresponding, and multiple-to-multiple realizes the optimal configuration of the test environment. Different test demands are met, and the test efficiency is improved by making good configuration in advance before the test.

[0055] By using edge data center technology, the computing power is improved, the data warehouse is constructed, and the bottom layer architecture is constructed for data analysis. The test data calculation and analysis platform is responsible for obtaining the original data of the whole machine test stand and the core machine test from the data acquisition and control system, effectively pre-processing the test data, facilitating subsequent data analysis, providing fast multi-dimensional query, and combining with various professional business data models to realize fast comparison and query. The efficiency of aero-engine test data analysis is improved, and the test data of civil aircraft engines is analyzed efficiently and effectively by supporting self-defined data analysis methods, further improving the efficiency of civil aircraft engine test.

[0056] Building a platform to improve computing power and equipment storage can provide a bottom layer architecture for building a test data calculation and analysis platform. The data analysis platform is designed according to a distributed high-reliability architecture, which supports horizontal expansion, so that any single or multiple servers that fail or have software errors will not affect the availability and reliability of the system. At the same time, through node virtualization and supplemented by automatic load balancing technology, the computing and storage resources in the heterogeneous cluster can be used most efficiently, reducing hardware investment. On this basis, a distributed multi-dimensional database cluster and a high-speed write cluster are built to store civil aircraft engine whole machine data information uniformly, realizing centralized and unified standard management of test data. Currently, test data is stored in binary single file format, which cannot guarantee the reliability and integrity of the data, providing a foundation and guarantee for the subsequent establishment of a stable and reliable data storage and management platform with backup, fault tolerance, and disaster recovery mechanisms.

[0057] Those skilled in the art will appreciate that various illustrative components, modules, blocks, units, circuits, systems and steps described in connection with the embodiments disclosed herein can be implemented by hardware, software (including firmware, resident software, microcode, etc.), or a combination thereof. To clearly illustrate the interchangeability of hardware and software, various illustrative components, modules, blocks, units, circuits, systems and steps are generally described above in their functional form. Whether such functionality is implemented in hardware or software depends on the specific application and design constraints imposed on the overall system. Skilled persons can implement the described functionality in different ways for each specific application, but such implementation decisions should not be interpreted as causing a departure from the scope of the present application.

[0058] Aspects of the application can be embodied in one or more computer-readable media having computer program code embodied therein.

[0059] Computer readable program code can be embodied in any of a number of forms. Referring to FIG. 6, computer program code embodied in one or more forms of computer readable media can be used to implement the present application. Aspects of the present application are directed to computer program code embodied in one or more computer readable media having computer program code embodied thereon for carrying out aspects of the present application.

[0060] Computer program code embodied on a computer readable medium can be used to carry out any of the processes described herein. Aspects of the present application are directed to computer program code embodied in one or more computer readable media having computer program code embodied thereon for carrying out aspects of the present application. The computer readable medium can be a machine-readable storage medium having stored thereon one or more computer program components embodied in computer readable program code. Examples of a machine-readable storage medium include a floppy disk, a ZIP® disk, a 35 mm film, a tape, a magnetic hard disk, a solid state hard disk, a magnetic tape, or any other magnetic medium, a CD-ROM, any other optical medium, a DVD, any other

[0061] Those skilled in the art will appreciate that information and signals can be represented using any of a variety of different technologies and techniques. For example, data, instructions, commands, information, signals, bits, symbols, and chips that can be referenced throughout the above description can be represented by voltages, currents, electromagnetic waves, magnetic fields or particles, optical fields or particles, or any combination thereof.

[0062] The steps of a method or algorithm described in connection with the embodiments disclosed herein can be embodied directly in hardware, in a software module executed by a processor, or in a combination of the two. A software module can reside in RAM memory, flash memory, ROM memory, EPROM memory, EEPROM memory, registers, hard disk, a removable disk, a CD-ROM, or any other form of storage medium known in the art. An exemplary storage medium is coupled to the processor such that the processor can read information from, and write information to, the storage medium. In the alternative, the storage medium can be integral to the processor. The processor and the storage medium can reside in an application-specific integrated circuit (ASIC). Alternatively, the processor and the storage medium can reside as discrete components in a user terminal.

[0063] In one or more exemplary embodiments, the functions described can be implemented in hardware, software, firmware, or any combination thereof. If implemented in software as a computer program product, the functions can be stored on or transmitted over as one or more instructions or code on a computer-readable medium. Computer-readable media includes both computer storage media and communication media including any medium that facilitates transfer of a computer program from one place to another. A storage media can be any available media that can be accessed by a computer. By way of example, and not limitation, such computer-readable media can comprise RAM, ROM, EEPROM, CD-ROM or other optical disk storage, magnetic disk storage or other magnetic storage devices, or any other medium that can be used to carry or store desired program code in the form of instructions or data structures and that can be accessed by a computer. Also, any connection is properly termed a computer-readable medium. For example, if the software is transmitted from a website, server, or other remote source using a coaxial cable, fiber optic cable, twisted pair, digital subscriber line (DSL), or wireless technologies such as infrared, radio, and microwave, then the coaxial cable, fiber optic cable, twisted pair, DSL, or wireless technologies such as infrared, radio, and microwave are included in the definition of medium. Disk and disc, as used herein, include compact disc (CD), laser disc, optical disc, digital versatile disc (DVD), floppy disk and Blu-ray® disc where disks usually reproduce data magnetically, while discs reproduce data optically with lasers. Combinations of the above should also be included within the scope of computer-readable media.

[0064] The terminology and phraseology employed herein are for descriptive purposes and should not be regarded as limiting. The use of such terminology and phraseology does not exclude any equivalent of the features described (or include where such are not excluded) and it is recognized that various modifications are possible within the scope of the claims. Other modifications, variations, and alternatives are also possible. Accordingly, the claims should be regarded as encompassing all such equivalents.

[0065] For the same reasons, it should be noted that the foregoing description of embodiments of the application is sometimes in terms of implementing aspects of one or more applications, and occasionally will describe features that would be useful in some implementations more than others. The skilled artisan will recognize that not all implementations need implement all features or implementations of one or more applications. Thus, the skilled artisan will recognize that, in some contexts, where subclaims are present in the claims below and they do not have the word "means" associated with them, the claims can be understood to be implementing structural circuity claims, as opposed to means-plus-function claims that refer to actions that are performed by a specified apparatus. Conversely, where subclaims refer to specified apparatuses configured to perform specified actions, the claims can be understood to be implementing means-plus-function claims.

[0066] Also, it is noted that, as used herein, "include," "includes" and "including" are open-ended words, and specifically do not exclude additional unrecited elements, features, or steps. Similarly, "comprises", "comprising", "comer" and "comer" are open-ended words, and specifically do not exclude additional unrecited elements, features, or steps.

Claims

1. A test data acquisition virtualization platform for civil aeroengines, characterized in that, The platform comprises: a data acquisition system comprising acquisition terminals, node service stations and a general service station; a first virtualized whole-machine test bench; and a second virtualized whole-machine test bench; The acquisition terminals acquire analog test data generated by the first virtualized whole-machine test bench and the second virtualized whole-machine test bench; the acquisition terminals are connected to the node service stations through intelligent switching devices; the node service stations are connected to the general service station through intelligent switching devices; the node service stations are connected to each other through intelligent switching devices.

2. The test data acquisition virtualization platform for civil aviation engines of claim 1, wherein, The first virtualized whole-machine test bench or the second virtualized whole-machine test bench uses cloud technology and virtualization image technology to replace the original single-node single-copy with multiple-node multiple-copies to realize active risk avoidance, reactive fault tolerance and active management, create multiple virtual machines in the test, load different test environments, and prepare different test environments at the same time.

3. The test data acquisition virtualization platform for civil aeroengines of claim 2, wherein, The acquisition terminals transmit data generated by each virtual machine to the node servers through the intelligent switching devices.

4. The test data acquisition virtualization platform for civil aviation engines of claim 1, wherein, The acquisition terminals are connected to each other through the test benches.

5. The test data acquisition virtualization platform for civil aviation engines of claim 1, wherein, The data acquisition system is connected to the cloud space.

6. The test data acquisition virtualization platform for civil aviation engines of claim 1, wherein, The node service stations comprise node servers and database servers; the node servers are connected to the database servers; The database servers store all data in the node servers; the node service stations integrate and collect data collected by the acquisition terminals in the node area.

7. The test data acquisition virtualization platform for civil aviation engines of claim 1, wherein, The general service station comprises a general server, a general data server and a backup data server; the general server stores data in the general data server and backs up in the backup data server; the general service station is used for integrating and collecting all test data.

8. The test data acquisition virtualization platform for civil aviation engines of claim 1, wherein, The intelligent switching devices have intelligent stacking technology modules, cloud management modules, VXLAN features, network flow analysis modules and operation and maintenance modules.

9. The test data acquisition virtualization platform for civil aviation engines of claim 1, wherein, The intelligent switching devices are connected to the network through 10GB network broadband.

10. The test data acquisition virtualization platform for civil aviation engines of claim 1, wherein, Category 6a network cables are used in the data acquisition system.

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