CN112668783A

CN112668783A - Data processing method, device and equipment based on airplane and readable storage medium

Info

Publication number: CN112668783A
Application number: CN202011603990.XA
Authority: CN
Inventors: 潘浩文
Original assignee: Icalc Holdings Ltd
Current assignee: Icalc Holdings Ltd
Priority date: 2020-12-29
Filing date: 2020-12-29
Publication date: 2021-04-16
Anticipated expiration: 2040-12-29
Also published as: CN112668783B

Abstract

The application discloses a data processing method, a device, equipment and a readable storage medium based on an airplane, wherein the method comprises the following steps: acquiring a property right transfer request sent by first equipment; calling an intelligent contract, and generating accident breakage rates respectively corresponding to the components, the engine and the energy supply equipment through virtual asset breakage data respectively corresponding to the components, the engine and the energy supply equipment carried in the intelligent contract and the property right transfer request; generating virtual asset breakage rates respectively corresponding to the components, the engine and the energy supply equipment through historical maintenance data respectively corresponding to the components, the engine and the energy supply equipment, and virtual asset breakage data respectively corresponding to the components, the engine and the energy supply equipment, which are carried in the intelligent contract and the property right transfer request; and generating a virtual asset evaluation reference value of the airplane according to the accident breakage rate, the virtual asset breakage rate and the airplane navigation data. By the method and the device, the evaluation efficiency and accuracy of the virtual asset value of the article can be improved.

Description

Data processing method, device and equipment based on airplane and readable storage medium

Technical Field

The present application relates to the field of computer technologies, and in particular, to a data processing method, apparatus, device, and readable storage medium based on an aircraft.

Background

The property right transfer refers to transferring the article mortgage authority of the article to a second user by a first user with the property right of the article, so that the virtual property data corresponding to the application virtual property data are acquired to the second user.

When a first user has a requirement for transferring the property right of an article, a second user usually evaluates the virtual asset value of the article through manual experience, and the method not only needs to consume a large amount of manpower, but also needs to consume a large amount of time, and the evaluation efficiency is not high; meanwhile, the mode depends on manual accumulated experience, centralized authority influence is large, and the accuracy of evaluation on the virtual asset value of the article is not high.

Disclosure of Invention

The embodiment of the application provides a data processing method, a data processing device, data processing equipment and a readable storage medium based on an airplane, and the evaluation efficiency and accuracy of the virtual asset value of an article can be improved.

An embodiment of the present application provides an aircraft-based data processing method, including:

acquiring a property right transfer request sent by first equipment; the first equipment is corresponding to a user who has ownership for the airplane; the object right transfer request is used for requesting to transfer the object affiliation authority of the airplane to the second equipment, and the first equipment has the object use authority of the airplane after the object affiliation authority is transferred;

calling an intelligent contract, and generating accident breakage rates respectively corresponding to the components, the engine and the energy supply equipment through virtual asset breakage data respectively corresponding to the components, the engine and the energy supply equipment carried in the intelligent contract and the property right transfer request; the components are parts that make up the aircraft; the energy supply equipment supplies energy to the airplane;

generating virtual asset breakage rates respectively corresponding to the components, the engine and the energy supply equipment through historical maintenance data respectively corresponding to the components, the engine and the energy supply equipment, and virtual asset breakage data respectively corresponding to the components, the engine and the energy supply equipment, which are carried in the intelligent contract and the property right transfer request;

generating a virtual asset evaluation reference value aiming at the airplane according to the accident breakage rate respectively corresponding to the component, the engine and the energy providing equipment, the virtual asset breakage rate respectively corresponding to the component, the engine and the energy providing equipment and airplane navigation data carried by the object right transfer request; the virtual asset assessment reference value is used for assessing and referencing the virtual asset value of the airplane and is used for responding to the property right transfer request to provide the first device with virtual asset data which is smaller than or equal to the virtual asset value of the airplane.

An aspect of an embodiment of the present application provides an aircraft-based data processing apparatus, including:

the request acquisition module is used for acquiring a property right transfer request sent by first equipment; the first equipment is corresponding to a user who has ownership for the airplane; the object right transfer request is used for requesting to transfer the object affiliation authority of the airplane to the second equipment, and the first equipment has the object use authority of the airplane after the object affiliation authority is transferred;

the contract calling module is used for calling an intelligent contract;

the accident data generation module is used for generating accident breakage rates corresponding to the components, the engine and the energy supply equipment respectively through virtual asset breakage data corresponding to the components, the engine and the energy supply equipment respectively carried in the intelligent contract and the property right transfer request; the components are parts that make up the aircraft; the energy supply equipment supplies energy to the airplane;

the asset data generation module is used for generating virtual asset breakage rates respectively corresponding to the components, the engine and the energy supply equipment through historical maintenance data respectively corresponding to the components, the engine and the energy supply equipment and virtual asset breakage data respectively corresponding to the components, the engine and the energy supply equipment which are carried in the intelligent contract and the property right transfer request;

the reference value generation module is used for generating a virtual asset evaluation reference value aiming at the airplane according to the accident breakage rate respectively corresponding to the component, the engine and the energy supply equipment, the virtual asset breakage rate respectively corresponding to the component, the engine and the energy supply equipment and airplane navigation data carried by the property right transfer request; the virtual asset assessment reference value is used for assessing and referencing the virtual asset value of the airplane and is used for responding to the property right transfer request to provide the first device with virtual asset data which is smaller than or equal to the virtual asset value of the airplane.

Wherein, the object right transfer request also comprises user information; the user information is information of a user who has ownership for the airplane;

the device also includes:

the credibility generation module is used for triggering an intelligent contract based on the material right transfer request and generating a credibility evaluation value aiming at user information through the intelligent contract and the user information;

and the credibility matching module is used for matching the credibility evaluation value with a credibility threshold, executing and calling an intelligent contract when the matching result and the user information meet the credibility condition, and generating accident damage rates corresponding to the component, the engine and the energy supply equipment through virtual asset damage data corresponding to the component, the engine and the energy supply equipment carried in the intelligent contract and the property right transfer request.

The virtual asset reduction data comprises equipment virtual asset reduction data corresponding to the energy supply equipment, component virtual asset reduction data corresponding to the components and engine virtual asset reduction data corresponding to the engine; the accident breakage rate comprises an equipment accident breakage rate corresponding to the energy supply equipment, a component accident breakage rate corresponding to the component and an engine accident breakage rate corresponding to the engine;

the accident data generation module is also specifically used for generating an equipment accident breakage rate through the intelligent contract and the equipment virtual asset breakage data;

the accident data generation module is also specifically used for generating a component accident breakage rate through the intelligent contract and the component virtual asset breakage data;

and the accident data generation module is also specifically used for generating an engine accident breakage rate through the intelligent contract and the engine virtual asset breakage data.

The accident data generation module is further specifically used for traversing the equipment virtual asset depreciation data through the intelligent contract;

the accident data generation module is further specifically used for acquiring the equipment type of the energy supply equipment by intelligently enclosing the equipment accident certification data of the energy supply equipment in the equipment virtual asset breakage data if the equipment accident certification data of the energy supply equipment exists in the equipment virtual asset breakage data, acquiring a first accident breakage rate matched with the equipment type in the block chain full database, and taking the first accident breakage rate as the equipment accident breakage rate; the equipment accident certification data refers to the certification data that the equipment has no accident;

the accident data generation module is further specifically configured to, if the equipment accident proof data does not exist in the equipment virtual asset breakage data, acquire equipment accident occurrence data in the equipment virtual asset breakage data through intelligent closure, acquire a second accident breakage rate, which is obtained by matching the equipment type and the equipment accident occurrence data, in the block chain full database, and use the second accident breakage rate as the equipment accident breakage rate; the equipment accident occurrence data refers to historical data of accidents of the energy supply equipment;

the accident data generation module is further specifically configured to, if there is no equipment accident proof data and no equipment accident occurrence data in the equipment virtual asset breakage data, obtain a third accident breakage rate matched with the equipment type in the block chain full database through the intelligent contract, and use the third accident breakage rate as the equipment accident breakage rate.

The historical maintenance data comprises equipment historical maintenance data corresponding to the energy supply equipment, assembly virtual asset breakage data corresponding to the assembly and engine historical maintenance data corresponding to the engine; the virtual asset breakage rate comprises an equipment virtual asset breakage rate corresponding to the energy supply equipment, a component virtual asset breakage rate corresponding to the component and an engine virtual asset breakage rate corresponding to the engine;

the asset data generation module is specifically used for generating the virtual asset breakage rate of the equipment through the intelligent contract, the virtual asset breakage data of the equipment and the historical maintenance data of the equipment;

the asset data generation module is further specifically used for generating a component virtual asset breakage rate through the intelligent contract, the component virtual asset breakage data and the component historical maintenance data;

and the asset data generation module is also specifically used for generating the engine virtual asset breakage rate through the intelligent contract and the engine virtual asset breakage data.

The asset data generation module is further specifically used for traversing virtual asset depreciation data of the equipment and historical maintenance data of the equipment through an intelligent contract;

the asset data generation module is further specifically used for acquiring a proof existence breakage rate matched with the navigation authority proof data and the maintenance proof data in the block chain full-scale database through an intelligent contract if the navigation authority proof data exists in the equipment virtual asset breakage data and the maintenance proof data exists in the equipment historical maintenance data, and taking the proof existence breakage rate as the equipment virtual asset breakage rate;

the asset data generation module is further specifically configured to, if navigation authority certification data exists in the equipment virtual asset breakage data and maintenance certification data does not exist in the equipment historical maintenance data, obtain a first certification loss breakage rate matched with the maintenance certification data in the block chain full database through an intelligent contract, and use the first certification loss breakage rate as the equipment virtual asset breakage rate;

the asset data generation module is further specifically configured to, if no navigation authority certification data exists in the equipment virtual asset breakage data and maintenance certification data exists in the equipment historical maintenance data, obtain a second certification loss breakage rate matched with the navigation authority certification data in the block chain full database through an intelligent contract, and use the second certification loss breakage rate as the equipment virtual asset breakage rate;

and the asset data generation module is further specifically configured to, if no navigation authority certification data exists in the equipment virtual asset breakage data and no maintenance certification data exists in the equipment historical maintenance data, obtain a third certification loss breakage rate matched with the navigation authority certification data and the maintenance certification data in the block chain full database through an intelligent contract, and use the third certification loss breakage rate as the equipment virtual asset breakage rate.

The reference value generation module is further specifically used for determining the airplane accident breakage rate according to the component accident breakage rate, the engine accident breakage rate and the equipment accident breakage rate;

the reference value generation module is further specifically used for determining the aircraft virtual asset breakage rate according to the component virtual asset breakage rate, the engine virtual asset breakage rate and the equipment virtual asset breakage rate;

the reference value generation module is further specifically used for generating maintenance remaining duration according to the aircraft navigation data;

the reference value generation module is further specifically configured to determine the aircraft accident breakage rate, the aircraft virtual asset breakage rate, and the maintenance remaining duration as virtual asset evaluation reference values for the aircraft.

The reference value generation module is further specifically used for acquiring an accident assessment matrix associated with the airplane; elements in the accident assessment matrix are used for representing accident assessment reference proportions corresponding to the component accident breakage rate, the engine accident breakage rate and the equipment accident breakage rate respectively;

the reference value generation module is further specifically used for multiplying the component accident breakage rate by the accident assessment reference proportion corresponding to the component accident breakage rate to obtain a target component accident breakage rate;

the reference value generation module is further specifically used for multiplying the engine accident breakage rate by the accident assessment reference proportion corresponding to the engine accident breakage rate to obtain a target engine accident breakage rate;

the reference value generation module is further specifically used for multiplying the equipment accident breakage rate by the accident assessment reference proportion corresponding to the equipment accident breakage rate to obtain a target equipment accident breakage rate;

and the reference value generation module is further specifically used for performing addition operation processing on the target component accident breakage rate, the target engine accident breakage rate and the target equipment accident breakage rate to obtain the airplane accident breakage rate.

The reference value generation module is further specifically used for acquiring an asset evaluation matrix associated with the aircraft; elements in the asset assessment matrix are used for representing asset assessment reference proportions corresponding to the assembly virtual asset breakage rate, the engine virtual asset breakage rate and the equipment virtual asset breakage rate respectively;

the reference value generation module is further specifically used for multiplying the component virtual asset breakage rate by an asset evaluation reference proportion corresponding to the component virtual asset breakage rate to obtain a target component virtual asset breakage rate;

the reference value generation module is further specifically used for multiplying the engine virtual asset breakage rate by an asset evaluation reference proportion corresponding to the engine virtual asset breakage rate to obtain a target engine virtual asset breakage rate;

the reference value generation module is further specifically configured to multiply the equipment virtual asset breakage rate by an asset assessment reference proportion corresponding to the equipment virtual asset breakage rate to obtain a target equipment virtual asset breakage rate;

and the reference value generation module is further specifically used for performing addition operation processing on the target component virtual asset breakage rate, the target engine virtual asset breakage rate and the target equipment virtual asset breakage rate to obtain the aircraft virtual asset breakage rate.

Wherein, the device still includes:

the matrix acquisition module is used for acquiring an initial accident assessment matrix and an initial asset assessment matrix;

the breakage rate acquisition module is used for acquiring the sample assembly accident breakage rate, the sample engine accident breakage rate and the sample equipment accident breakage rate of the sample airplane;

the prediction data generation module is used for generating a prediction accident breakage rate of the airplane through the initial accident evaluation matrix, the sample assembly accident breakage rate, the sample engine accident breakage rate and the sample equipment accident breakage rate;

the prediction data generation module is also used for generating a virtual asset prediction rate of the airplane through the initial asset evaluation matrix, the sample assembly accident breakage rate, the sample engine accident breakage rate and the sample equipment accident breakage rate;

the matrix adjusting module is used for obtaining the tag accident breakage rate of the airplane and the tag virtual asset breakage rate of the airplane, and adjusting the initial accident assessment matrix through predicting the accident breakage rate and the tag accident breakage rate to obtain an accident assessment matrix;

and the matrix adjusting module is also used for adjusting the initial asset evaluation matrix by predicting the virtual asset breakage rate and the tag virtual asset breakage rate to obtain the asset evaluation matrix.

The reference value generation module is further specifically used for acquiring an airplane historical navigation cycle corresponding to the airplane, a maintenance navigation time corresponding to the airplane and an airplane type corresponding to the airplane from the airplane navigation data through an intelligent contract; the historical navigation period of the airplane is the total period of navigation by using the airplane; the maintenance navigation cycle refers to a cycle of navigating by using the airplane after the performance of the airplane is recovered and maintained; the maintenance navigation time is the time for navigating by using the airplane after the performance of the airplane is recovered and maintained;

the reference value generation module is further specifically used for acquiring a maintenance remaining duration set; the maintenance remaining duration set comprises a mapping relation between the configuration data group and the configuration maintenance remaining duration; the configuration data set is a data set consisting of configuration of airplane type, configuration of maintenance navigation duration, configuration of maintenance navigation period and configuration of historical navigation period;

the reference value generation module is specifically used for matching a target data group consisting of the type of the airplane, the maintenance navigation time, the maintenance navigation period and the historical navigation period of the airplane with the maintenance residual time set through an intelligent contract, and acquiring a configuration data group matched with the target data group from the maintenance residual time set to serve as a target configuration data group;

the reference value generation module is further specifically configured to use the configured remaining repair duration having the mapping relationship with the target configuration data set as the remaining repair duration of the aircraft.

Wherein, the request for transferring the property right further comprises applying for a virtual property value;

the device also includes:

the data sending module is used for sending the property right transfer request and the virtual asset evaluation reference value to the second equipment so that the second equipment determines the virtual asset value of the airplane based on the property right transfer request and the virtual asset evaluation reference value, and returns a property right transfer confirmation message according to the application virtual asset value when the virtual asset value is greater than or equal to the application virtual asset value;

and the account sending module is used for sending the equipment account corresponding to the first equipment to the second equipment according to the property right transfer confirmation message so that the second equipment obtains the virtual asset data corresponding to the application virtual asset numerical value in the equipment account corresponding to the second equipment and transfers the virtual asset data to the equipment account corresponding to the first equipment.

An aspect of an embodiment of the present application provides a computer device, including: a processor and a memory;

the memory stores a computer program that, when executed by the processor, causes the processor to perform the method in the embodiments of the present application.

An aspect of the embodiments of the present application provides a computer-readable storage medium, in which a computer program is stored, where the computer program includes program instructions, and the program instructions, when executed by a processor, perform the method in the embodiments of the present application.

In one aspect of the application, a computer program product or computer program is provided, the computer program product or computer program comprising computer instructions stored in a computer readable storage medium. The processor of the computer device reads the computer instructions from the computer-readable storage medium, and the processor executes the computer instructions to cause the computer device to perform the method provided by one aspect of the embodiments of the present application.

In the embodiment of the application, a user with an engine ownership can send relevant data (such as virtual asset damage data corresponding to components, engines and energy supply equipment respectively; historical maintenance data corresponding to the components, the engines and the energy supply equipment respectively; aircraft navigation data of the aircraft and the like) of the aircraft for carrying out the object right transfer to a block chain through first equipment, and an anti-tampering mechanism of the block chain can ensure that the relevant data are not tampered, so that the real validity of the relevant data of the aircraft is guaranteed, the reliability guarantee of the data can be further provided for the evaluation of the virtual asset value of the aircraft according to the relevant data, and the evaluation of the virtual asset value of the aircraft can be more accurate; meanwhile, the related data can be automatically calculated through the block chain, and the virtual asset assessment reference value can be quickly and accurately obtained, so that the second equipment can quickly and accurately determine the virtual asset assessment reference value of the airplane according to the virtual asset assessment reference value. In conclusion, the method and the device can improve the efficiency and the accuracy of the evaluation of the virtual asset value of the object (such as an airplane).

Drawings

In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts.

Fig. 1 is a diagram of a network architecture provided by an embodiment of the present application;

FIG. 2 is a schematic view of a scenario provided by an embodiment of the present application;

FIG. 3 is a schematic flow chart diagram illustrating a method for aircraft-based data processing according to an embodiment of the present disclosure;

FIG. 4 is a block diagram of a method for generating a virtual asset assessment reference for an aircraft according to an embodiment of the present disclosure;

FIG. 5 is a schematic structural diagram of an aircraft-based data processing apparatus according to an embodiment of the present disclosure;

fig. 6 is a schematic structural diagram of a computer device according to an embodiment of the present application.

Detailed Description

The technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application, and it is obvious that the described embodiments are only a part of the embodiments of the present application, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present application.

Please refer to fig. 1, which is a schematic diagram of a network architecture according to an embodiment of the present application. The block chain is a novel application mode of computer technologies such as distributed data storage, point-to-point transmission, a consensus mechanism and an encryption algorithm, and is mainly used for sorting data according to a time sequence and encrypting the data into an account book, so that the data cannot be falsified or forged, and meanwhile, the data can be verified, stored and updated. The blockchain is essentially a decentralized database, each node in the database stores an identical blockchain, and the blockchain network divides the nodes into core nodes, data nodes and light nodes, wherein the core nodes are responsible for the consensus of the whole blockchain network, that is, the core nodes are the consensus nodes in the blockchain network. The process of writing the transaction data into the account book in the blockchain network can be that the client sends the transaction data to the data node or the light node, then the transaction data is transmitted between the data node or the light node in the blockchain network in a baton mode until the consensus node receives the transaction data, the consensus node packs the transaction data into a block and performs consensus with other consensus nodes, and after the consensus passes, the block carrying the transaction data is written into the account book.

It is to be understood that the blockchain system may include an intelligent contract, and the intelligent contract may be understood in the blockchain system as a code that each node (including a common node) of the blockchain can understand and execute, and may execute any logic and obtain a result. The user can invoke the intelligent contract already deployed on the blockchain by initiating a transaction service request through the client, and then the data node or the light node on the blockchain can send the transaction service request to the consensus node, and each consensus node on the blockchain can respectively run the intelligent contract. It should be understood that the blockchain may include one or more intelligent contracts, where the intelligent contracts may be distinguished by identification numbers (IDs) or names, and a transaction service request initiated by a client may also carry the identification numbers or names of the intelligent contracts, so as to specify the intelligent contracts that the blockchain needs to run, after the intelligent contracts are run and an execution result is obtained, each common identification node may mutually verify whether the execution result is consistent (that is, perform common identification), and if so, the execution result may be stored in a respective local account book, and the execution result is returned to the client.

As shown in fig. 1, the network architecture may include a cluster of core nodes (consensus nodes) 1000, a cluster of data nodes or light nodes 100, and a cluster of user terminals (clients) 10. As shown in fig. 1, the core node cluster 1000 may include a core node 1000a, core nodes 1000b, …, and a core node 1000n, the data node cluster 100 may specifically include a data node 100a, data nodes 100b, …, and a data node 100n, and the user terminal cluster 10 may specifically include a user terminal 10a, user terminals 10b, …, and a user terminal 10 n.

As shown in fig. 1, the user terminal 10a, the user terminal 10b, …, and the user terminal 10n may be respectively in network connection with the data node 100a, the data node 100b, …, and the data node 100n, so that the user terminal may interact data with the data node through the network connection; the data node 100a, the data node 100b, …, and the data node 100n may be respectively in network connection with the core node 1000a, the core node 1000b, …, and the core node 1000n, so that the data node may perform data interaction with the core node through the network connection; the

data nodes

100a, 100b, …, and 100n are connected to each other so that data interaction can be performed between the data nodes, and the

core nodes

1000a, 1000b, …, and 1000n are connected to each other so that data interaction can be performed between the core nodes.

Taking the user terminal 10a, the data node 100a, and the core node 1000a as an example, the data node 100a may receive a transaction service request (the transaction service request carries an ID or a name of an intelligent contract) sent by the user terminal 10a, and then the data node 100a may send the transaction service request to the core node 1000a through the data node cluster 100; the core node 1000a may run the intelligent contract, execute the transaction service through the intelligent contract, obtain an execution result, store the execution result in a memory pool (such as a transaction pool), and generate a new block according to the execution result; subsequently, the core node 1000a may send the newly generated blocks to other core nodes in the blockchain network where the newly generated blocks are located according to node identifiers of other core nodes (i.e., common nodes) in the blockchain network, check (i.e., perform common identification) the newly generated blocks by the other core nodes, and add the newly generated blocks to the blockchain stored in the newly generated blocks after the check is completed (i.e., store the execution result into the blockchain after the common identification passes). Each core node in the blockchain network has a node identifier corresponding thereto, and each core node in the blockchain network may store node identifiers of other core nodes in the blockchain network, so that the generated block is broadcast to other core nodes in the blockchain network according to the node identifiers of the other core nodes, and data stored in all the core nodes in the blockchain network are consistent.

The method for transferring the property right of the airplane can be provided based on the characteristic that the block chain cannot be tampered or forged, so that data in the business of transferring the property right of the airplane can be safe, the reliability guarantee of the data can be further provided for the evaluation of the virtual asset value of the airplane, and the evaluation efficiency and accuracy of the virtual asset value of the airplane can be improved. Taking the core node 1000a, the data node 100a, the user terminal 10a, and the user terminal 10b as an example to describe the specific method provided in the present application, the user terminal 10a may send a ownership transfer request (transaction service request) for requesting an airplane to perform ownership transfer to the core node 1000a through the data node 100a, where the ownership transfer request may be a transfer request initiated by a user a having an airplane ownership, the ownership transfer request may be a transfer request of an airplane's belonging right, and the belonging right may be a belonging right for an object mortgage right; the property right transfer request may include virtual asset related data of the airplane (e.g., airplane flight data, virtual asset damage data corresponding to the component, the engine, and the energy supply device, respectively, historical maintenance data corresponding to the component, the engine, and the energy supply device, respectively, a temporary use contract of the airplane, etc.) and a requested virtual asset value of the user a (e.g., 5 ten thousand yuan); subsequently, the core node 1000a may generate a block for the virtual asset associated data, and after the block passes the consensus, the block may be linked to the belonging block chain, thereby ensuring that the virtual asset associated data cannot be tampered with, and ensuring the real validity of the virtual asset associated data.

Further, the core node 1000a may invoke an intelligent contract, and may generate accident breakage rates corresponding to the component, the engine, and the energy providing device, respectively, according to the intelligent contract and the virtual asset breakage data corresponding to the component, the engine, and the energy providing device, respectively; virtual asset damage rates respectively corresponding to the components, the engine and the energy supply equipment can be generated through the intelligent contract and the historical maintenance data respectively corresponding to the components, the engine and the energy supply equipment and the virtual asset damage data respectively corresponding to the components, the engine and the energy supply equipment; further, the virtual asset assessment reference value of the airplane can be generated according to the accident damage rates respectively corresponding to the component, the engine and the energy supply equipment, the virtual asset damage rates respectively corresponding to the component, the engine and the energy supply equipment and the airplane navigation data.

Further, the core node 1000a may transmit the virtual asset assessment reference value to the user terminal 10b, so that the user terminal 10b may determine the virtual asset value of the airplane based on the virtual asset assessment reference value, where the user terminal 10b may be a user terminal corresponding to a provider of the virtual asset data. It should be understood that the user terminal 10b may determine the virtual asset worth value of the airplane based on the virtual asset evaluation reference value, and determine whether to transfer virtual asset data corresponding to the application virtual asset value to the user terminal 10a based on the virtual asset worth value. For example, when the user terminal 10b determines that the virtual asset value (e.g., 8 ten thousand yuan) is greater than the application virtual asset value (e.g., 5 ten thousand yuan), the user terminal 10b may generate a physical right transfer confirmation message based on the application virtual asset value (5 ten thousand yuan), and return the physical right transfer confirmation message to the core node 1000a, the core node 1000a may transmit the terminal account corresponding to the user terminal 10a (i.e., the account of the user a) to the user terminal 10b according to the physical right transfer confirmation message, and after receiving the terminal account corresponding to the user terminal 10a, the user terminal 10b may transfer the virtual asset data (5 ten thousand yuan) corresponding to the application virtual asset value to the terminal account corresponding to the user terminal 10a (the account of the user a). It should be appreciated that after the user a successfully obtains the virtual asset data, the user a may send a virtual asset transfer confirmation message to the core node 1000a through the user terminal 10a, and the core node 1000a may transfer the item mortgage authority of the airplane to the user terminal 10b (i.e., to the provider). It should be understood that after the transfer of the airplane's property right is successful, the provider already has the property right (article mortgage authority) for the airplane, and the user a no longer has the article mortgage authority for the airplane; meanwhile, after the transfer of the property right is successful, the user a has no selling right but has a use right for the airplane.

For ease of understanding, please refer to fig. 2 together, and fig. 2 is a schematic view of a scenario provided by an embodiment of the present application. The ue a shown in fig. 2 may be any ue in the ue cluster 10 in the embodiment corresponding to fig. 1, for example, the ue is a ue 10 a; the block link point shown in fig. 2 may be any core node in the core node cluster 1000 in the embodiment corresponding to fig. 1, for example, the core node may be core node 1000 b.

As shown in fig. 2, a user a may apply for a transfer of the right of things (transfer of the right of things for mortgage) for an airplane through a target application (e.g., a goods service platform) in a user terminal a, for example, after the user a selects a goods of the airplane in the goods service platform, the user a may click a "apply for right of things to transfer" control; subsequently, the user terminal a may respond to the trigger operation of the user a to display an information input interface, in which the user a may input relevant data of the airplane (e.g., airplane navigation data, virtual asset damage data corresponding to the airplane component, the engine, and the energy supply device, respectively; historical maintenance data corresponding to the airplane component, the engine, and the energy supply device, respectively; a temporary use contract of the airplane, etc.); the user a can also input user information (such as age, gender, belonging region information, credit assessment records and the like) and apply for a virtual asset value (such as 10 ten thousand yuan) in the information input interface; the virtual asset value application may refer to a virtual asset value that user a desires to apply for through an airplane's ownership transfer request. Subsequently, after the user a finishes inputting the information and clicks the determination control, the user terminal a can respond to the triggering operation of the user a to generate an object right transfer request for the airplane and send the object right transfer request to the block chain node.

Further, the block chain node may trigger an intelligent contract in the block chain based on the weight transfer request, and may evaluate the credit value (credibility) of the user a through the user information, so as to obtain a credibility evaluation value of the user a; when the reliability evaluation value of the user a is greater than or equal to the reliability threshold and the user information satisfies the reliability condition (e.g., the user's age satisfies the property right transfer condition, the user has no bad credit record, the user has full capability, the user's region information belongs to the region for which the block link point is responsible, etc.), the block link point may determine that the user a has the property right transfer authority, and the block link node may generate the block 2001 according to the data related to the airplane and the user information, and uplink the block 2001 to the block link 200.

Further, the blockchain node may generate a virtual asset assessment reference value for the airplane based on the data related to the airplane in the blockchain 200, and send the virtual asset assessment reference value and the weight transfer request to a user terminal B (a user terminal corresponding to a provider of the virtual asset data), where the user terminal B may quickly and accurately calculate the virtual asset value of the airplane to be 15 ten thousand yuan based on the virtual asset assessment reference value. The user terminal B can determine that the virtual asset value is 15 ten thousand yuan greater than the application virtual asset value of 10 ten thousand yuan, and the user terminal B can generate a physical right transfer confirmation message according to the application virtual asset value (10 ten thousand yuan); the user terminal B may return the weight transfer acknowledgement message to the blockchain node. Further, the blockchain node may send the terminal account of the user terminal a (the account of the user a) to the user terminal B based on the weight transfer confirmation message; the user terminal B can transfer the virtual asset data (10 ten thousand yuan) corresponding to the applied virtual asset value to the terminal account of the user terminal a. It should be understood that after the user terminal a successfully acquires the virtual asset data corresponding to the application virtual asset value provided by the user terminal B, the user terminal B may obtain the item mortgage authority of the airplane.

It should be noted that the above-mentioned values of 10 ten thousand yuan, 15 ten thousand yuan, etc. are examples for easy understanding, and are not intended to have actual reference meanings.

For a specific implementation manner of determining the virtual asset assessment reference value of the aircraft based on the relevant data of the aircraft by using the block link points, reference may be made to the description in the embodiment corresponding to fig. 3. It should be understood that the application of the blockchain to the weight transfer of the aircraft can ensure the authenticity of the relevant data of the aircraft, so as to provide reliable data for further calculation of the virtual asset assessment reference value; and the virtual asset evaluation reference value is provided for the virtual asset data provider, so that the virtual asset value of the airplane can be quickly and accurately determined by the virtual asset data provider based on the virtual asset evaluation reference value, and the virtual asset evaluation efficiency and accuracy of the airplane can be improved.

Further, please refer to fig. 3, where fig. 3 is a schematic flowchart of a data processing method based on an aircraft according to an embodiment of the present application. The method may be performed by a block node (e.g., the core node in the embodiment corresponding to fig. 1) or may be performed by both the block node and a user terminal (e.g., the user terminal in the embodiment corresponding to fig. 1). The following will be described as an example of the method being executed by the block chain node, wherein the aircraft-based data processing method at least includes the following steps S101 to S104:

step S101, acquiring a property right transfer request sent by first equipment; the first equipment is corresponding to a user who has ownership for the airplane; the object right transfer request is used for requesting to transfer the object affiliation authority of the airplane to the second device, and the first device has the object use authority of the airplane after the object affiliation authority is transferred.

In this application, the block link node may be a core node in the block chain, the core node may receive a transaction request (e.g., a property right transfer request) sent from a data node or a light node in the block chain, and the data node or the light node may receive the transaction request sent from the user terminal. The transaction request may be a request generated by the user terminal according to a transaction service initiated by the user.

It should be understood that a user (a user having ownership of the airplane) may initiate a rights transfer request for the airplane through the user terminal, where the rights transfer request may be a request to transfer an item affiliation right of the airplane, where the item affiliation right may refer to an item mortgage right. The property right transfer request may include virtual property related data of the airplane input by the user, wherein the virtual property related data may include airplane voyage data of the airplane, virtual property damage data of airplane components (e.g., landing gear, fuselage, etc.), virtual property damage data of an engine, virtual property damage data of an energy supply device, historical maintenance data of the airplane components (e.g., landing gear, fuselage, etc.), historical maintenance data of the engine, historical maintenance data of the energy supply device, temporary use contracts (e.g., lease related data) of the airplane, factory files, and the like; the material right transfer request may further include user information (information of a user having airplane ownership), wherein the user information may include user basic attribute information (e.g., information of a worker and a company of the user, information of a company real control person, information of a company shareholder, information of a company core person, information of a company change, etc.), basic attribute information of a company having an association relationship with the user (e.g., information of an external investment, information of a supplier, information of a core client, information of an external security company, etc.), historical material right transfer data (e.g., information of an asset flow direction of a historical material right transfer, information of a debt, information of a bank debit, information of a credit line, information of a bond financing, etc.), operation warning information (e.g., historical information of an external security, information of a debt), integrity archive information (e.g., information of a past information and integrity of the user), Judicial litigation information (e.g., historical litigation records), rating record information (e.g., credit or tax rating information, default data, company tax payment information, default prediction probability information, etc.), company public opinion information (e.g., negative public opinion information for a company), company financial information (e.g., asset liability information, profit sheets, cash flow sheets), and company financial index analysis data (e.g., company profit probability analysis data, repayment probability analysis data, operation analysis data, cash flow data contrasts, etc.).

It should be appreciated that based on the physical right transfer request, a smart contract in the block chain may be triggered, and through the smart contract and the user information, a confidence evaluation value for the user information may be generated.

Step S102, calling an intelligent contract, and generating accident breakage rates respectively corresponding to the components, the engine and the energy supply equipment through virtual asset breakage data respectively corresponding to the components, the engine and the energy supply equipment carried in the intelligent contract and the property right transfer request; the components are parts that make up the aircraft; the energy supply device supplies energy to the aircraft.

In this application, the user information may further include attribute related information of the user (for example, age, gender, credit record, belonging region information, and the like), and when the reliability evaluation value of the user information is greater than or equal to the reliability threshold value and the basic attribute information also meets the reliability condition (for example, the age of the user meets the property right transfer condition, the user does not have a bad credit record, the user has full behavior capability, the region information of the user belongs to the region in which the block link point is responsible, and the like), the intelligent contract may be invoked to determine the accident damage rates corresponding to the component, the engine, and the energy supply device, respectively, through the intelligent contract.

It should be understood that the accident damage rate may refer to the damage rate (Incident damage) corresponding to an accident (e.g., a fire accident, a water intake accident, etc.) occurring after the assembly (including the landing gear and the body) or the engine or the energy supply device. The equipment accident breakage rate corresponding to the energy supply equipment can be generated through the equipment virtual asset breakage data corresponding to the intelligent contract and the energy supply equipment; generating a component accident breakage rate corresponding to the component through the component virtual asset breakage data corresponding to the intelligent contract and the component; the engine accident breakage rate corresponding to the engine can be generated through the engine virtual asset breakage data corresponding to the engine through the intelligent contract.

The specific method for generating the equipment accident breakage rate corresponding to the energy supply equipment by the intelligent contract comprises the following steps of traversing equipment virtual asset breakage data by the intelligent contract; if the equipment accident certification data of the energy supply equipment exists in the equipment virtual asset breakage data, the equipment type of the energy supply equipment can be obtained by intelligently enclosing the equipment virtual asset breakage data, a first accident breakage rate matched with the equipment type is obtained in a block chain full database, and the first accident breakage rate can be used as the equipment accident breakage rate; the equipment accident certification data refers to the certification data that the equipment has no accident; if the equipment accident proof data does not exist in the equipment virtual asset breakage data, the equipment accident occurrence data can be obtained from the equipment virtual asset breakage data through intelligent closure, a second accident breakage rate matched with the equipment type and the equipment accident occurrence data is obtained from a block chain full database, and the second accident breakage rate can be used as the equipment accident breakage rate; the equipment accident occurrence data refers to historical data of accidents of the energy supply equipment; and if the equipment accident proof data and the equipment accident occurrence data do not exist in the equipment virtual asset breakage data, acquiring a third accident breakage rate matched with the equipment type in the block chain full database through the intelligent contract, and taking the third accident breakage rate as the equipment accident breakage rate.

It should be understood that the above-mentioned energy supply device may refer to an Auxiliary Power Unit (APU) of an aircraft; if the energy supply device has not been in an accident, a user with the airplane ownership can provide accident certification data (Non-included condition) of the energy supply device to prove that the energy supply device has not been in an accident, and according to the accident certification data, a corresponding accident damage rate (for example, the accident damage rate is 0) can be inquired in a block chain total database; if the energy supply device has an accident (e.g., a fire, a falling from a high-rise building, etc.), the owner of the airplane may provide related accident occurrence data (inclusion History), and according to the related accident occurrence data, the corresponding accident damage rate may be queried in the block chain total database (e.g., the corresponding accident damage rate may be queried according to the type of the accident); if the owner of the airplane does not provide the accident certification data of the energy providing equipment and does not provide the related accident occurrence data, the corresponding accident damage rate (when the accident certification data and the related accident occurrence data are not provided, the corresponding accident damage rate) can be inquired in the block chain full database according to the equipment type of the energy providing equipment.

It will be appreciated that the above-described assembly may include the landing gear and fuselage of an aircraft. Similarly, if the fuselage has no accident, the user with the ownership of the airplane can provide accident certification data of the fuselage to prove that the fuselage has no accident, and according to the accident certification data, the corresponding accident breakage rate (for example, the accident breakage rate is 0) can be inquired in the block chain total database; if the airplane body has an accident, the owner of the airplane can provide related accident occurrence data, and the corresponding accident breakage rate can be inquired in the block chain total database according to the related accident occurrence data (for example, the corresponding accident breakage rate can be inquired according to the type of the accident); if the owner of the airplane does not provide the accident certification data of the airplane body or the related accident occurrence data of the airplane body, the corresponding accident breakage rate (when the accident certification data and the related accident occurrence data are not provided, the corresponding accident breakage rate) can be inquired in the block chain total database according to the airplane type of the airplane. Similarly, if the landing gear is not in an accident, the user with the ownership of the airplane can provide accident certification data of the landing gear to prove that the landing gear is not in the accident, and according to the accident certification data, the corresponding accident breakage rate (for example, the accident breakage rate is 0) can be inquired in the block chain total database; if the landing gear has an accident, the aircraft ownership user can provide related accident occurrence data, and according to the related accident occurrence data, the corresponding accident breakage rate can be inquired in the block chain total database (for example, the corresponding accident breakage rate can be inquired according to the type of the accident); if the owner of the aircraft does not provide the accident certification data of the undercarriage and does not provide the related accident occurrence data of the undercarriage, the corresponding accident breakage rate (when the accident certification data and the related accident occurrence data are not provided, the corresponding accident breakage rate) can be inquired in the block chain total database according to the type of the undercarriage.

Similarly, it should be understood that if the engine has not failed to be in an accident, the user with the airplane ownership may provide accident certification data of the engine to prove that the engine has not failed to be in an accident, and according to the accident certification data, the corresponding accident breakage rate (for example, the accident breakage rate is 0) may be queried in the block chain total database; if the engine has an accident, the owner of the airplane can provide related accident occurrence data, and according to the related accident occurrence data, the corresponding accident breakage rate can be inquired in the block chain total database (for example, the corresponding accident breakage rate can be inquired according to the type of the accident); if the owner of the airplane does not provide the accident certification data of the engine and does not provide the related accident occurrence data of the engine, the corresponding accident breakage rate (when the accident certification data and the related accident occurrence data are not provided, the corresponding accident breakage rate) can be inquired in the block chain total database according to the type of the engine.

Step S103, generating virtual asset breakage rates respectively corresponding to the components, the engine and the energy supply equipment through historical maintenance data respectively corresponding to the components, the engine and the energy supply equipment carried in the intelligent contract and the property right transfer request and virtual asset breakage data respectively corresponding to the components, the engine and the energy supply equipment;

in the present application, the virtual asset breakage data may refer to a virtual asset breakage rate corresponding to a case where maintenance certification data and navigation authority certification data (quasi flight certification data or airworthiness certification) of the component, the engine, and the energy supply device are lost. The equipment virtual asset damage rate corresponding to the energy supply equipment can be generated through the intelligent contract, the equipment virtual asset data corresponding to the energy supply equipment and the historical equipment maintenance data corresponding to the energy supply equipment; generating a component virtual asset breakage rate corresponding to the component through the intelligent contract, the component virtual asset data corresponding to the component and the component historical maintenance data corresponding to the component; the engine virtual asset breakage rate corresponding to the engine can be generated through the intelligent contract, the engine virtual asset data corresponding to the engine and the historical engine maintenance data corresponding to the engine.

The specific method for determining the virtual asset breakage rate of the equipment corresponding to the energy supply equipment through the intelligent contract comprises the following steps of traversing equipment virtual asset breakage data and equipment historical maintenance data through the intelligent contract; if navigation authority certification data exists in the equipment virtual asset breakage data and maintenance certification data exists in the equipment historical maintenance data, obtaining a certification breakage rate matched with the navigation authority certification data and the maintenance certification data in the block chain full database through an intelligent contract, and taking the certification breakage rate as the equipment virtual asset breakage rate; if navigation authority certification data exists in the equipment virtual asset breakage data and maintenance certification data does not exist in the equipment historical maintenance data, acquiring a first certification loss breakage rate matched with the maintenance certification data in the block chain full database through an intelligent contract, and taking the first certification loss breakage rate as the equipment virtual asset breakage rate; if the navigation authority certification data does not exist in the equipment virtual asset breakage data and the maintenance certification data exists in the equipment historical maintenance data, acquiring a second certification loss breakage rate matched with the navigation authority certification data in the block chain full database through an intelligent contract, and taking the second certification loss breakage rate as the equipment virtual asset breakage rate; and if the navigation authority certification data does not exist in the equipment virtual asset breakage data and the maintenance certification data does not exist in the equipment historical maintenance data, acquiring a third certification loss breakage rate matched with the navigation authority certification data and the maintenance certification data in the block chain full database through an intelligent contract, and taking the third certification loss breakage rate as the equipment virtual asset breakage rate.

It should be understood that each energy providing device (APU) should have returned Birth certification data (Back to Birth Certificates) from factory, where the returned Birth certification data may include maintenance certification data and quasi-flight certification data (the quasi-flight certification data may also be referred to as airworthiness certification data), and if neither the maintenance certification data nor the quasi-flight certification data is lost, the virtual asset damage rate corresponding to the existence of the certification may be queried from the blockchain full-scale database (the virtual asset damage rate may be queried according to the device type of the energy providing device, for example, the virtual asset damage rate queried according to the device type is 0); if any one of the maintenance certification data and the quasi-flight certification data is lost or both are lost, the virtual asset loss rate (Missing Back to bit Certificates discard) corresponding to the loss certification of any one of the certification data (or both certification data are lost) can be inquired from the block chain total database through the device type. Similarly, it should be understood that each fuselage should have returned Birth certification data (Back to Birth Certificates) from the factory, and if the maintenance certification data and the quasi flight certification data are not lost, the virtual asset damage rate corresponding to the existence of the certification can be queried from the block chain full database (which can be queried according to the airplane type of the airplane, for example, the virtual asset damage rate queried according to the airplane type is 0); if either or both of the maintenance certification data and the quasi-flight certification are lost, the virtual asset loss rate corresponding to the loss of either certification (or both certifications) can be searched from the block chain full database by the airplane type. Similarly, it should be understood that each landing gear should have returned Birth certification data (Back to Birth Certificates) from the factory, and if the maintenance certification data and the quasi flight certification data are not lost, the virtual asset damage rate corresponding to the existence of the certification can be queried from the block chain full database (the virtual asset damage rate can be queried through the landing gear type of the landing gear, for example, the virtual asset damage rate queried through the landing gear type is 0); if either or both of the maintenance certification data and the quasi-flight certification are lost, the virtual asset loss rate corresponding to the loss of either certification (or both certifications) can be queried from the block chain full database according to the type of the landing gear. Similarly, it should be understood that each engine should have returned Birth certification data (Back to Birth Certificates) from the factory, and if the maintenance certification data and the quasi flight certification data are not lost, the virtual asset damage rate corresponding to the existence of the maintenance certification data and the quasi flight certification data can be queried from the block chain full database (which can be queried according to the engine type of the engine, for example, the virtual asset damage rate queried according to the engine type is 0); if either or both of the maintenance certification data and the quasi-flight certification are lost, the corresponding virtual asset loss rate when either certification is lost (or both certifications are lost) can be inquired from the block chain full database through the engine type.

Step S104, generating a virtual asset evaluation reference value aiming at the airplane according to the accident breakage rate respectively corresponding to the component, the engine and the energy supply equipment, the virtual asset breakage rate respectively corresponding to the component, the engine and the energy supply equipment and the airplane navigation data carried by the property right transfer request; the virtual asset assessment reference value is used for assessing and referencing the virtual asset value of the airplane and is used for responding to the property right transfer request to provide the first device with virtual asset data which is smaller than or equal to the virtual asset value of the airplane.

In the application, the airplane accident breakage rate of the airplane can be determined according to the assembly accident breakage rate (including the accident breakage rate of the airplane body and the accident breakage rate of the undercarriage), the engine accident breakage rate and the equipment accident breakage rate; determining the airplane virtual asset breakage rate of the airplane according to the assembly virtual asset breakage rate (including the virtual asset breakage rate of the airplane body and the virtual asset breakage rate of the undercarriage), the engine virtual asset breakage rate and the equipment virtual asset breakage rate; the remaining maintenance duration of the airplane can be generated according to the airplane navigation data; and the aircraft accident breakage rate, the aircraft virtual asset breakage rate and the maintenance remaining time can be determined as the virtual asset evaluation reference values of the aircraft.

Wherein, it should be understood that, as for a specific method for determining the aircraft accident breakage rate of the aircraft, an accident assessment matrix associated with the aircraft can be obtained; elements in the accident assessment matrix are used for representing accident assessment reference proportions corresponding to the component accident breakage rate, the engine accident breakage rate and the equipment accident breakage rate respectively; the accident breakage rate of the component and the accident assessment reference proportion corresponding to the accident breakage rate of the component can be multiplied to obtain the accident breakage rate of the target component; the accident breakage rate of the engine and the accident assessment reference proportion corresponding to the accident breakage rate of the engine can be multiplied to obtain the accident breakage rate of the target engine; the equipment accident breakage rate and the accident assessment reference proportion corresponding to the equipment accident breakage rate can be multiplied to obtain the target equipment accident breakage rate; and then, the accident breakage rate of the target assembly, the accident breakage rate of the target engine and the accident breakage rate of the target equipment can be added for operation processing, so that the accident breakage rate of the airplane is obtained.

It should be appreciated that the incident evaluation matrix described above may be as shown in incident evaluation matrix A1:

accident evaluation matrix A1

For example, four numerical values 1 in the accident assessment matrix a1 can be accident assessment reference specific gravity respectively corresponding to the accident damage rate of the fuselage, the accident damage rate of the landing gear, the accident damage rate of the engine, and the accident damage rate of the equipment.

Taking the accident damage rate of the airplane body as 5%, the accident damage rate of the landing gear as 1%, the accident damage rate of the engine as 6% and the accident damage rate of the equipment as 0% as examples, the accident evaluation matrix a1 can determine that the airplane accident damage rate of the airplane is as follows: the failure rate of an aircraft accident may be 12% when 5% × 1+ 1% × 1+ 6% × 1+ 0% × 1 is 12%.

Optionally, the accident evaluation matrix may also be shown as accident evaluation matrix a 2:

accident evaluation matrix A2

Wherein, the value 2 in the accident assessment matrix a2 can be an accident assessment reference proportion corresponding to the component accident breakage rate; the numerical value 1 can be an accident evaluation reference proportion corresponding to the engine accident breakage rate; the value 3 can be the accident assessment reference weight corresponding to the energy supply equipment. It should be appreciated that the accident assessment reference specific gravities corresponding to the accident breakage rate of the fuselage and the undercarriage are both accident assessment reference specific gravities corresponding to the component accident breakage rate (i.e., numerical value 2).

Wherein, it should be understood that, as a specific method for determining the aircraft virtual asset breakage rate of the aircraft, an asset evaluation matrix associated with the aircraft can be obtained; wherein, the elements in the asset evaluation matrix are used for representing asset evaluation reference proportions corresponding to the component virtual asset breakage rate, the engine virtual asset breakage rate and the equipment virtual asset breakage rate respectively; the component virtual asset breakage rate and the asset evaluation reference proportion corresponding to the component virtual asset breakage rate can be multiplied to obtain the target component virtual asset breakage rate; the virtual asset breakage rate of the engine and the asset evaluation reference proportion corresponding to the virtual asset breakage rate of the engine can be multiplied to obtain the virtual asset breakage rate of the target engine; the virtual asset breakage rate of the equipment and the asset evaluation reference proportion corresponding to the virtual asset breakage rate of the equipment are multiplied to obtain the virtual asset breakage rate of the target equipment; and then, adding the target assembly virtual asset breakage rate, the target engine virtual asset breakage rate and the target equipment virtual asset breakage rate to obtain the airplane virtual asset breakage rate.

It should be appreciated that the above-described asset valuation matrix may be as shown by asset valuation matrix A3:

asset valuation matrix A3

Wherein, for example, the value 1 in the asset assessment matrix a3 can be the asset assessment reference specific gravity corresponding to the virtual asset breakage rate of the airframe; the two numerical values 1.5 can be asset evaluation reference proportions respectively corresponding to the virtual asset breakage rate of the undercarriage and the virtual asset breakage rate of the engine; the value 2 can be the asset assessment reference weight corresponding to the virtual asset breakage rate of the equipment.

Taking the virtual asset breakage rate of the airplane body as 5%, the virtual asset breakage rate of the landing gear as 0, the virtual asset breakage rate of the engine as 0 and the virtual asset breakage rate of the equipment as 1% as examples, the virtual asset breakage rate of the airplane can be determined as follows through the asset evaluation matrix A3: the virtual asset breakage rate of the airplane may be 7% when the ratio is 5% × 1+0 × 1.5+0 × 1.5+ 1% × 2.

Optionally, the asset valuation matrix may also be as shown by asset valuation matrix A4:

asset valuation matrix A4

Wherein, the value 3 in the asset assessment matrix a4 may be an asset assessment reference weight corresponding to the component virtual asset breakage rate; the two values 1 may be an asset assessment reference weight corresponding to the engine virtual asset breakage rate and an asset assessment reference weight corresponding to the energy supply device, respectively. It should be appreciated that the asset assessment reference weight corresponding to the virtual asset breakage rate of the fuselage and the virtual asset breakage rate of the landing gear may each be the asset assessment reference weight corresponding to the component virtual asset breakage rate (i.e., a value of 3).

It should be appreciated that the accident assessment matrix and the asset assessment matrix may be trained to provide greater accuracy in the aircraft accident breakage rate obtained from the accident assessment matrix and the aircraft virtual asset breakage rate obtained from the asset assessment matrix. The training method comprises the specific steps of obtaining an initial accident assessment matrix and an initial asset assessment matrix; then, the sample assembly accident breakage rate, the sample engine accident breakage rate and the sample equipment accident breakage rate of the sample airplane can be obtained; generating a predicted accident breakage rate of the airplane through the initial accident assessment matrix, the sample assembly accident breakage rate, the sample engine accident breakage rate and the sample equipment accident breakage rate; generating a predicted virtual asset breakage rate of the airplane through the initial asset evaluation matrix, the sample assembly accident breakage rate, the sample engine accident breakage rate and the sample equipment accident breakage rate; then, the tag accident breakage rate of the airplane and the tag virtual asset breakage rate of the airplane can be obtained, and the initial accident assessment matrix can be adjusted by predicting the accident breakage rate and the tag accident breakage rate to obtain an accident assessment matrix; and adjusting the initial asset evaluation matrix by predicting the virtual asset breakage rate and the tag virtual asset breakage rate to obtain the asset evaluation matrix. It should be appreciated that a loss value between the tag accident breakage rate and the predicted accident breakage rate may be determined by a loss function, and the initial accident assessment matrix may be adjusted by the loss value; similarly, a loss value between the tag virtual asset breakage rate and the predicted virtual asset breakage rate can be determined through a loss function, and the initial asset evaluation matrix can be adjusted through the loss value.

It should be appreciated that the remaining Time to maintenance (Estimated Green Time) of the aircraft may refer to the remaining Time to the next maintenance of the aircraft. The specific method for determining the remaining maintenance time of the airplane can be that the historical navigation cycle of the airplane corresponding to the airplane, the maintenance navigation cycle corresponding to the airplane, the maintenance navigation time corresponding to the airplane and the airplane type corresponding to the airplane can be obtained in the airplane navigation data through an intelligent contract; the historical navigation period of the airplane can be the total period of navigation by using the airplane; the maintenance navigation cycle may be a cycle of navigating by using the aircraft after the performance of the aircraft is restored and maintained; the maintenance navigation time duration can be the time duration for navigating by using the airplane after the performance of the airplane is recovered and maintained; subsequently, a set of remaining duration of maintenance may be obtained; the maintenance remaining duration set comprises a mapping relation between a configuration data set and configuration maintenance remaining duration; the configuration data set can be a data set consisting of the type of the configured airplane, the duration of the configured maintenance navigation, the period of the configured maintenance navigation and the period of the configured historical navigation; matching a target data group consisting of the type of the airplane, the maintenance navigation time, the maintenance navigation period and the historical navigation period of the airplane with a maintenance residual time set through an intelligent contract, acquiring a configuration data group matched with the target data group from the maintenance residual time set, and taking the configuration data group as the target configuration data group; the configured remaining length of maintenance time having a mapping relationship with the target configuration data set may be used as the remaining length of maintenance time for the aircraft.

It should be understood that the process from takeoff to landing of the airplane may be referred to as a Cycle (Cycle), for example, if the airplane flies straight from city a to city B, the flow from city a to landing in city B may be referred to as a Cycle. The maintenance navigation duration of the airplane can be the total navigation duration (TSLSV) of the airplane after performance recovery and maintenance is carried out; the maintenance navigation Cycle may be a total navigation Cycle (CSLSV) of the aircraft after performance recovery and maintenance; the historical navigation period of the aircraft may refer to a total period (CSN) during which the aircraft navigates from the factory, and the remaining maintenance duration corresponding to the aircraft may be queried according to the type of the aircraft, the maintenance navigation duration (TSLSV) of the aircraft, the maintenance navigation period (CSLSV), and the CSN of the aircraft.

Alternatively, it will be appreciated that the determination of the remaining Time to repair (Estimated Green Time) may also be determined by the maintenance voyage Time (TSLSV) of the aircraft and the next Time to repair of the aircraft. The next maintenance time of the aircraft can be obtained by querying the block chain full database through the aircraft type and the aircraft Serial Number (MSN). For example, the last repair time for an aircraft was 12 months in 2020, 24 am 7:00, by inquiry, the next maintenance time should be 7 in 24 am at 2020 and 12 months at the last maintenance time: after 10 hours of 00 (where 10 hours here refers to the maximum flight time of the aircraft after a repair at 7:00, that is, the aircraft must be repaired next after 10 hours of flight after a 7:00 repair); whereas in 2020, 24 am 7:00, after the maintenance, the aircraft has navigated for 5 hours, where the 5 hours are the maintenance navigation Time (TSLSV), then the maintenance navigation time 5 of the aircraft can be subtracted from the maximum navigation time 10, and the obtained result 5 can be the remaining maintenance time of the aircraft.

It should be noted that, the service hours include the last service time mentioned above, i.e., 12/24/7/am: 00. the maximum flight time 10 hours and the TSLSV 5 hours are examples for easy understanding and are not intended to be actually used.

Optionally, it is understood that the virtual asset assessment reference Value of the aircraft may include a Maintenance Adjusted Base Value (MABV) in addition to the above-mentioned aircraft accident breakage rate, aircraft virtual asset breakage rate, and remaining duration of repair. The maintenance adjustment benchmark value may be a corresponding benchmark value when the aircraft is in a state of not being used after performance recovery maintenance.

A specific method for determining the Maintenance Adjustment Benchmark Value (MABV) of an aircraft may be: the method can acquire the half-life virtual asset value of the airplane, the MABV of the airplane body, the MABV of the undercarriage, the MABV of the energy supply equipment and the MABV of the engine; and then, adding the half-life virtual asset value of the airplane, the MABV of the airplane body, the MABV of the undercarriage, the MABV of the energy supply equipment and the MABV of the engine to obtain the MABV of the airplane. The semi-Life virtual asset Value of the airplane can be a semi-Life Market Value (Half Life Market Value) of the airplane, and the semi-Life Market Value can be obtained by inquiring from a block chain full database according to the airplane type of the airplane.

The specific method for determining the MABV of the fuselage may be as follows: determining a list of performance Maintenance unit cost rates (Airframe HMV rates) of the fuselage according to the type of the aircraft, wherein the list of the Airframe HMV rates includes one or more Airframe HMV rates, and the performance Maintenance unit cost rates may be a billing Rate (for example, a billing Rate for overhaul of the fuselage in one month) when the fuselage is repaired in a larger amount of Maintenance per unit time (i.e., when the fuselage is overhauled); subsequently, a maintenance time limit type corresponding to the airplane type can be obtained (e.g., 6years check, i.e., a maintenance with a large maintenance amount is performed every 6 years; 12years check, i.e., a maintenance with a large maintenance amount is performed every 12 years); according to the type of the repair time limit, the corresponding performance maintenance unit cost Rate (Airframe HMV Rate) of the fuselage can be inquired from the Airframe HMV Rate list. Then, a Half-Life state value (Half Life) of the fuselage can be obtained by inquiring the airplane type in a block chain full database, wherein the Half-Life state value can be a corresponding value when the fuselage is in a state that the fuselage is not maintained according to actual maintenance conditions; the maintenance navigation duration (TSLSV) corresponding to the airplane body can be obtained from the airplane navigation data; then, the Half-Life state value may be used to subtract the maintenance voyage duration for that fuselage (i.e., fuselage Half Life — fuselage TSLSV); and then, the result obtained by subtracting the maintenance navigation time of the fuselage from the half-life state value is multiplied by the cost rate of the performance maintenance unit of the fuselage to obtain the MABV of the fuselage.

The specific method for determining the MABV of the landing gear can be as follows: the method can acquire a Half-Life state Adjustment value (Half Life Adjustment) of a main landing gear, a Half-Life state Adjustment value of a left landing gear and a Half-Life state Adjustment value of a right landing gear; subsequently, an average between the half-life state adjustment value for the main landing gear, the half-life state adjustment value for the left landing gear, and the half-life state adjustment value for the right landing gear may be determined; further, a unit cost rate for maintenance of the landing gear for the landing gear may be obtained (e.g., a billing rate for maintenance of the landing gear in one month); the average value and the cost rate of the maintenance unit of the undercarriage can be multiplied to obtain the MABV of the undercarriage. The method for determining the half-life state adjustment value of the main landing gear can be as follows: the maintenance navigation time of the main landing gear can be obtained from the aircraft navigation data; then, a Half-Life state value (Half Life) of the main undercarriage can be inquired from a block chain full database through the part number of the main undercarriage, and the Half-Life state value of the main undercarriage can be used for subtracting the maintenance navigation time of the main undercarriage to obtain the Half-Life state value of the main undercarriage; similarly, the half-life state adjustment values of the left undercarriage and the right undercarriage respectively corresponding to the part numbers of the left undercarriage and the right undercarriage respectively corresponding to the maintenance navigation time length of the right undercarriage can be determined by adopting the mode of the main undercarriage.

Among them, a specific method for determining the MABV of the energy providing device (APU) may be: the half-life state value and the performance maintenance unit cost rate corresponding to the energy supply equipment can be inquired from the block chain full database through the part number corresponding to the energy supply equipment; then, the maintenance navigation Time (TSLSV) corresponding to the energy providing equipment can be obtained, and the maintenance navigation time of the energy providing equipment is subtracted from the Half-Life state value, so that a Half-Life state Adjustment value (Half Life Adjustment) corresponding to the energy providing equipment can be obtained; then, the half-life state adjustment value corresponding to the energy supply device may be multiplied by the performance maintenance unit cost rate to obtain the MABV corresponding to the energy supply device.

Among the specific methods for determining the MABV of the engine may be: according to the type of the engine, the Half-Life virtual asset Value (Half Life Market Value) of the engine can be inquired in a block chain full database; subsequently, a target Maintenance adjustment value (Maintenance Adjustments) for the engine may be obtained, which may refer to an impact value of the repair on the engine virtual asset. And adding the half-life virtual asset value and the target maintenance adjustment value to obtain the maintenance adjustment reference value of the engine. The specific method for determining the target maintenance adjustment value of the engine can be as follows: the method comprises the steps that thrust minus power (Derate percentage) of an engine can be obtained from engine virtual breakage data, and maintenance navigation duration (TSLSV) and maintenance navigation period (CSLSV) of the engine can be obtained from airplane navigation data; then, the ratio between the maintenance navigation duration and the maintenance navigation period can be determined, and the Performance maintenance unit cost rate (EPR rate) matched with the thrust power reduction rate and the ratio can be inquired in a block chain full database through an intelligent contract; the EPR rate may refer to a billing rate for maintenance of the engine per unit time (e.g., a billing rate for maintenance of the engine in one hour). In the block chain full database, the Mean Time Between Repair, MTBR which is matched with the thrust minus power and the ratio can be inquired; subsequently, a passing area corresponding to the maintenance navigation cycle of the engine can be obtained, and an area breakage rate (Operating Region count) corresponding to the passing area can be obtained from the block chain total database, for example, compared with the area B, the Y area has a poorer flying environment and can more affect the performance of the engine, and compared with the area B, the area breakage rate of the Y area is larger; meanwhile, the corresponding navigation breakage rate when the engine is in a non-first navigation state can be obtained from the block chain total database, and the navigation breakage rate can be understood as a non-first navigation breakage rate (Mature Run Discount); then, the average maintenance time, the area breakage rate, and the travel breakage rate may be multiplied, and a result obtained by the multiplication may be divided by 2 to obtain a Half Life state value (Half Life) of the engine. Furthermore, the half-life state value of the engine and the TSLSV of the engine can be subtracted, and the subtracted result and the EPR rate of the engine are multiplied to obtain a performance recovery maintenance Adjustment value (EPR Adjustment) of the engine; further, a time-to-Life component Adjustment value (Life Limited Parts Adjustment, LLP Adjustment) of the engine may be obtained; the recovered performance maintenance Adjustment value (EPR Adjustment) may then be added to the time-to-life component Adjustment value for the engine, and the result may be used as the target maintenance Adjustment value for the engine.

The specific method for obtaining the time-service-life component adjustment value of the engine can be shown as formula (1):

therein, it should be understood that a Life Limited Part (LLP) of an engine may refer to a component of the engine that has a well-defined Life (duration) Limit (Life Limit). The LLP Limit as in equation (1) can be used to characterize the maximum service life (service life Limit) or maximum voyage for each time-life component of the engine; the LLP CSN can be used to characterize the historical voyage period of each time-of-life component of the engine; the LLP Price can be used to characterize the life component virtual asset value of each life component of the engine. It should be understood that, for the method of determining the LLP Limit and the LLP Price, the component number corresponding to each time-life component of the engine can be obtained in the aircraft voyage data through the intelligent contract, and the maximum service life matching with the engine type and the component number of the engine can be obtained in the block chain full database to obtain the time-life component virtual asset value.

Optionally, it is understood that the virtual asset assessment reference value of the airplane may include an airplane contract virtual asset value in addition to the airplane accident breakage rate, the airplane virtual asset breakage rate, the remaining repair time length, and the maintenance adjustment reference value. The contract virtual asset Value may be an airplane leasing Value (Aircraft empty Value, Aircraft LEV).

A particular method for determining the rental value of an aircraft may include the following 4 scenarios:

scheme (1): obtaining a Maintenance Adjustment Benchmark Value (MABV), a net rental virtual asset flow, a net repair preparation virtual asset inflow and a net repair preparation virtual asset outflow of the aircraft via the smart contract; subsequently, the Maintenance Adjustment Benchmark Value (MABV), the net rental virtual asset flow, and the net repair preparation virtual asset inflow may be added, and the result of the addition and the net repair preparation virtual asset outflow may be subtracted, and the result of the subtraction may be used as the contracted virtual asset value of the aircraft. Wherein, the net rental virtual asset flow value may refer to net present values of a series of rental cash flows of the aircraft, the net maintenance preparation virtual asset inflow value may refer to net present values of a series of maintenance preparation cash flow inflows of the aircraft, and the net maintenance preparation virtual asset outflow value may refer to net present values of a series of maintenance preparation cash flow outflows of the aircraft.

For a specific implementation manner of determining the maintenance adjustment reference value, reference may be made to the above description, and details will not be repeated here. And a specific method for determining the net rental virtual asset flow may be as shown in equation (2):

wherein d in the formula (2)_iCan be used to characterize the payment time for the ith rent, which may be, at the earliest, the Lease Start time (Lease Start), d in the temporary use contract (airplane Lease data) for the airplane₁Can be used to characterize the 0 th rental payment time; DR can be used to characterize the rental Discount Rate (Discount Rate), P, of the airplane_iMay be used to characterize the rental payment amount for the ith time.

The specific implementation manner of determining the net value of the repair-preparation virtual asset may also be as shown in the above equation (2). Wherein d in the above formula (2) is d when it is determined that the repair-preparation virtual asset flows into the net value by the formula (2)_iCan be used to characterize the inflow time of the ith repair reserve gold cash flow, d₁Can be used to characterize the inflow time of the 0 th repair preparation gold cash flow; DR can be used to characterize the rental Discount Rate (Discount Rate), P, of the airplane_iCan be used to characterize the amount of the inflow of the ith repair fund cash flow.

The specific implementation manner of determining the net value of the repair-preparation virtual asset outflow may also be as shown in the above formula (2). Wherein d in the above formula (2) is used to determine the net value of the repair-preparation virtual asset when the formula (2) is used to determine the net value of the repair-preparation virtual asset_iCan be used to characterize the flow-out time of the ith repair fund cash flow, d₁Can be used to characterize the 0 th service preparation gold cash flow out time; DR can be used to characterize the rental Discount Rate (Discount Rate), P, of the airplane_iCan be used to characterize the outflow amount of the ith repair fund cash flow.

Scheme (2): the Maintenance Adjustment Benchmark Value (MABV), the rental virtual asset flow net value and the compensation virtual asset net value of the airplane can be obtained through the intelligent contract, and the Maintenance Adjustment Benchmark Value (MABV), the rental virtual asset flow net value and the compensation virtual asset net value are added to be operated, so that the contract virtual asset value can be obtained.

For a specific implementation manner of determining the maintenance adjustment reference value and the net rental virtual asset flow value, reference may be made to the above description, and details will not be described here.

The concrete implementation manner of determining the compensated virtual net worth may also be as shown in the above equation (2). Wherein d in the above formula (2) is used to determine the net value of the compensated virtual asset by the formula (2)_iCan be used to characterize the acquisition time of the ith compensating virtual asset, d₁An acquisition time that can be used to characterize the 0 th compensating virtual asset; DR can be used to characterize the rental Discount Rate (Discount Rate), P, of the airplane_iCan be used to characterize the compensating virtual asset (compensation amount) at the ith time.

Scheme (3): the net rental virtual asset flow, net compensation virtual asset, and net split component virtual asset may be obtained via smart contracts. And adding the net rental virtual asset flow value, the net compensation virtual asset value and the net split component virtual asset value to obtain a contract virtual asset value. The net value of the virtual assets of the split component can refer to the net present value of a series of planned takedown (Part Out) values, and the series of planned takedown values can refer to the value corresponding to the split component of the airplane after the airplane is split within a planned time range.

For specific implementation manners of determining the net rental virtual asset flow and compensating the net rental virtual asset flow, reference may be made to the above description. And for a specific method of determining the net virtual asset value of the split component, the following formula (2) may be used. When the formula (2) is used for determining the virtual net asset value of the split component, d in the formula (2)_iTime available for characterizing the ith planned offer value, d₁Time available to characterize the 0 th planned offer value; DR can be used to characterize the rental Discount Rate (Discount Rate), P, of the airplane_iMay be used to characterize the planned unsell amount for the ith time.

Scheme (4): a net rental virtual asset flow, a net repair-ready virtual asset inflow, a net repair-ready virtual asset outflow, and a net split component virtual asset may be obtained by the smart contract. The rental virtual asset flow net value, the maintenance preparation virtual asset inflow net value and the split component virtual asset net value are added, a subtraction operation processing can be performed on a result obtained by the addition operation processing and the maintenance preparation virtual asset outflow net value, and a result obtained by the subtraction operation processing can be used as a contract virtual asset numerical value. For a specific implementation manner of determining the net rental virtual asset flow, the net maintenance-ready virtual asset inflow, the net maintenance-ready virtual asset outflow, and the net split component virtual asset, reference may be made to the above description, and details will not be described here.

Further, it should be understood that, after generating the virtual asset assessment reference value of the airplane, the blockchain node may transmit the virtual asset assessment reference value to a second device (for example, a device corresponding to a virtual asset provider), and the second device may generate a virtual asset worth value based on the virtual asset assessment reference value, and when the virtual asset worth value is greater than or equal to the application virtual asset value in the weight transfer request, the second device may grant the weight transfer request of the first device for the airplane and transfer virtual asset data corresponding to the application virtual asset value to the first device. The method comprises the steps that a physical right transfer request and a virtual asset assessment reference value can be sent to second equipment, so that the second equipment determines the virtual asset value of the airplane based on the physical right transfer request and the virtual asset assessment reference value, and when the virtual asset value is greater than or equal to an application virtual asset value, a physical right transfer confirmation message is returned according to the application virtual asset value; according to the physical right transfer confirmation message, the equipment account corresponding to the first equipment can be sent to the second equipment, so that the second equipment obtains the virtual asset data corresponding to the application virtual asset numerical value in the equipment account corresponding to the second equipment, and transfers the virtual asset data to the equipment account corresponding to the first equipment.

Optionally, it is understood that, after receiving the weight transfer request for the aircraft sent by the first device, the block link point may determine, based on the relevant data of the aircraft, a virtual asset value corresponding to a component of the aircraft (for example, a virtual asset value corresponding to an undercarriage, a virtual asset value corresponding to a fuselage), a virtual asset value corresponding to an energy supply device of the aircraft, and a virtual asset value corresponding to an engine; the block chain nodes can compare virtual asset values respectively corresponding to the components, the energy supply equipment and the engine with application virtual asset numerical values in the property right transfer request, if any virtual asset value is larger than (or equal to) the application virtual asset numerical value in the virtual asset values respectively corresponding to the components, the energy supply equipment and the engine, the block chain nodes can generate a property right transfer prompt message and send the property right transfer prompt message to the first equipment so as to prompt the first equipment not to transfer the property right of the whole airplane, and only to transfer the property right of the components, the airplane body or the engine, so that the virtual asset data corresponding to the application virtual asset numerical value can be obtained. For example, if the value of the application virtual asset initiated by the first device is 10 ten thousand yuan, the value of the virtual asset corresponding to the energy providing device is 15 ten thousand yuan, the value of the virtual asset corresponding to the landing gear is 11 ten thousand yuan, the value of the virtual asset corresponding to the fuselage is 8 ten thousand yuan, and the value of the virtual asset corresponding to the engine is 12 ten thousand yuan, the block link point can determine that the values of the virtual assets corresponding to the energy providing device, the landing gear, and the engine are all greater than the value of the application virtual asset by 10 ten thousand yuan, the block link node can generate a physical right transfer prompting message to prompt the first device to transfer the physical right of the whole aircraft without transferring the physical right of any one or more of the energy providing device, the landing gear, or the engine, and also can obtain the data of the virtual asset corresponding to the value of the application virtual asset, and the first device can obtain the data of the virtual asset, the energy supply equipment, or the landing gear, or any one or more of the engines or the whole machine can be selected to carry out the weight transfer.

It should be understood that the first device and the second device in this application may both be user terminals, and the first device may be any user terminal in the user terminal cluster in the embodiment corresponding to fig. 1, for example, the user terminal is the user terminal 10 a; the second device may be any user terminal in the user terminal cluster in the embodiment corresponding to fig. 1, for example, the user terminal is the user terminal 10 b.

It should be understood that stable currencies having stable and currency characteristics may be collectively referred to herein as virtual assets, for example, universal currencies having a range of price fluctuations, such as dollars, may be referred to herein as virtual assets; the game virtual currency may also be referred to collectively as a virtual asset, and for example, virtual currency such as game gold, game experience value, game credits, and game diamonds in a game scene may be referred to as a virtual asset.

It should be understood that in a game scenario, a player may initiate a weight transfer (item mortgage authority transfer) request to a game equipment or game item, such as an airplane, to obtain corresponding virtual asset data (virtual asset data corresponding to a virtual asset value applied for) from a provider of virtual assets (virtual currencies, such as game coins, game experience values, game credits, and game diamonds); the user information in the game scene may refer to player information, the player information may include game behavior data (e.g., online duration, speech data, performance data, reported data, complaint data, registration information, a party to which the player belongs, a game system to which the player belongs, etc.) of the player, the blockchain node may acquire the player information of the player after the player initiates the property right transfer request, the blockchain node may calculate a confidence level evaluation value of the player based on the player information, the blockchain node may acquire the registration information (e.g., age, sex, etc.) of the player after the confidence level evaluation value reaches a confidence level threshold, and the blockchain node may acquire virtual asset related data of the airplane when the registration information satisfies a confidence condition (e.g., the age exceeds 16 years), the virtual asset related data may refer to flight data, a sex, and the like of the airplane performing virtual flight in the game, Virtual asset damage data (such as the damage rate after being attacked) of the components of the airplane, the energy supply equipment and the engine in the game, historical maintenance data of the components of the airplane, the energy supply equipment and the engine in the game for maintenance; determining a virtual asset valuation reference value for the aircraft based on the asset correlation data; the blockchain node may transmit the virtual asset assessment reference value to a virtual asset provider, which may determine a virtual asset value (e.g., 60 tokens) for the aircraft based on the virtual asset assessment reference value; if the applied virtual asset value requested by the player is 50 tokens, the virtual asset provider may determine that the virtual asset value (60 tokens) is greater than the applied virtual asset value, and the virtual asset provider may generate a weight transfer confirmation message based on the applied virtual asset value (50 tokens) and transmit the weight transfer message to the blockchain node. The blockchain node may then send the player's gaming virtual account to the virtual asset provider, and the virtual asset provider may retrieve the 50 game chips from the virtual asset provider's virtual account and transfer the 50 game chips to the player's gaming virtual account.

For further understanding of the process of generating the virtual asset assessment reference value of the aircraft, please refer to fig. 4 together, and fig. 4 is a block diagram of generating the virtual asset assessment reference value of the aircraft according to an embodiment of the present disclosure. As shown in fig. 4, the virtual asset assessment reference value of the airplane may include a virtual asset breakage rate, an accident breakage rate, a maintenance adjustment benchmark value, a contract virtual asset value, and a maintenance remaining time length of the airplane. For the virtual asset breakage rate of the aircraft, the virtual asset breakage rate of the engine, the virtual asset breakage rate of the energy supply device, the virtual asset breakage rate of the fuselage, and the virtual asset breakage rate of the undercarriage can be obtained (for example, the virtual asset breakage rate of the engine, the virtual asset breakage rate of the energy supply device, the virtual asset breakage rate of the fuselage, and the virtual asset breakage rate of the undercarriage can be obtained by adding up operations), and the specific implementation manner may refer to the description of determining the virtual asset breakage rate of the aircraft in the embodiment corresponding to fig. 3, which will not be described herein again. For the accident breakage rate of the aircraft, the accident breakage rate of the engine, the accident breakage rate of the energy supply device, the accident breakage rate of the fuselage, and the accident breakage rate of the undercarriage can be obtained (for example, the accident breakage rate of the engine, the accident breakage rate of the energy supply device, the accident breakage rate of the fuselage, and the accident breakage rate of the undercarriage can be obtained by adding up), and the specific implementation manner may refer to the description of determining the accident breakage rate of the aircraft in the embodiment corresponding to fig. 3, and will not be described again here. For the maintenance adjustment reference value of the aircraft, the maintenance adjustment reference value of the engine, the maintenance adjustment reference value of the energy providing device, the maintenance adjustment reference value of the fuselage, and the maintenance adjustment reference value of the undercarriage may be calculated first, and the maintenance adjustment reference value of the aircraft may be generated through the maintenance adjustment reference value of the engine, the maintenance adjustment reference value of the energy providing device, the maintenance adjustment reference value of the fuselage, and the maintenance adjustment reference value of the undercarriage, and the specific generation method may refer to the description of generating the maintenance adjustment reference value of the aircraft in the embodiment corresponding to fig. 3, and will not be described again here; the contract virtual asset numerical value of the airplane can be obtained through maintenance adjustment reference value of the airplane and temporary use contract of the airplane; optionally, the contractual virtual asset value of the aircraft may also be obtained through the contractual virtual asset value of the engine, the contractual virtual asset value of the fuselage, the contractual virtual asset value of the undercarriage, and the contractual virtual asset value of the energy providing device, and the specific method for generating the contractual virtual asset value of the aircraft may refer to the description of generating the contractual virtual asset value of the aircraft in the embodiment corresponding to fig. 3, which will not be described herein again. For the method for determining the remaining maintenance time of the aircraft, reference may be made to the description of generating the remaining maintenance time of the aircraft in the embodiment corresponding to fig. 3, which will not be described herein again.

Further, please refer to fig. 5, wherein fig. 5 is a schematic structural diagram of an aircraft-based data processing apparatus according to an embodiment of the present application. The aircraft-based data processing apparatus may be a computer program (comprising program code) running on a computer device, for example the aircraft-based data processing apparatus being an application software; the aircraft-based data processing apparatus may be used to perform the method illustrated in figure 3. As shown in fig. 5, the aircraft-based data processing apparatus 1 may include: a request acquisition module 11, a contract calling module 12, an accident data generation module 13, an asset data generation module 14 and a reference value generation module 15.

A request obtaining module 11, configured to obtain a weight transfer request sent by a first device; the first equipment is corresponding to a user who has ownership for the airplane; the object right transfer request is used for requesting to transfer the object affiliation authority of the airplane to the second equipment, and the first equipment has the object use authority of the airplane after the object affiliation authority is transferred;

the contract calling module 12 is used for calling an intelligent contract;

the accident data generation module 13 is configured to generate accident breakage rates corresponding to the components, the engine, and the energy supply device through virtual asset breakage data corresponding to the components, the engine, and the energy supply device, which are carried in the intelligent contract and the property right transfer request; the components are parts that make up the aircraft; the energy supply equipment supplies energy to the airplane;

the asset data generation module 14 is configured to generate virtual asset loss rates corresponding to the components, the engine, and the energy providing device through historical maintenance data and virtual asset loss data corresponding to the components, the engine, and the energy providing device respectively, which are carried in the intelligent contract and the property right transfer request;

a reference value generation module 15, configured to generate a virtual asset assessment reference value for an aircraft according to the accident damage rate respectively corresponding to the component, the engine, and the energy providing device, the virtual asset damage rate respectively corresponding to the component, the engine, and the energy providing device, and aircraft navigation data carried in the property right transfer request; the virtual asset assessment reference value is used for assessing and referencing the virtual asset value of the airplane and is used for responding to the property right transfer request to provide the first device with virtual asset data which is smaller than or equal to the virtual asset value of the airplane.

For specific implementation manners of the request obtaining module 11, the contract invoking module 12, the accident data generating module 13, the asset data generating module 14, and the reference value generating module 15, reference may be made to the descriptions of step S101 to step S104 in the embodiment corresponding to fig. 3, and details will not be described here.

referring to fig. 5, the aircraft-based data processing apparatus 1 may further include: a credibility generation module 16 and a credibility matching module 17.

The credibility generating module 16 is used for triggering an intelligent contract based on the property right transfer request, and generating a credibility evaluation value aiming at the user information through the intelligent contract and the user information;

and the credibility matching module 17 is configured to match the credibility evaluation value with a credibility threshold, execute calling an intelligent contract when the matching result and the user information meet a credibility condition, and generate accident damage rates corresponding to the component, the engine, and the energy providing device respectively through virtual asset damage data corresponding to the component, the engine, and the energy providing device respectively carried in the intelligent contract and the property right transfer request.

For a specific implementation manner of the reliability generating module 16 and the reliability matching module 17, reference may be made to the description in step S102 in the embodiment corresponding to fig. 3, and details will not be described here.

the accident data generation module 13 is further specifically configured to generate an equipment accident breakage rate through the intelligent contract and the equipment virtual asset breakage data;

the accident data generation module 13 is further specifically configured to generate a component accident breakage rate through the intelligent contract and the component virtual asset breakage data;

the accident data generating module 13 is further specifically configured to generate an engine accident breakage rate through the intelligent contract and the engine virtual asset breakage data.

The accident data generation module 13 is further specifically configured to traverse the equipment virtual asset depreciation data through the intelligent contract;

the accident data generating module 13 is further specifically configured to, if the device virtual asset breakage data includes device accident certification data of the energy providing device, obtain a device type of the energy providing device by intelligently fitting the device accident certification data into the device virtual asset breakage data, obtain a first accident breakage rate matched with the device type in the block chain full database, and use the first accident breakage rate as the device accident breakage rate; the equipment accident certification data refers to the certification data that the equipment has no accident;

the accident data generating module 13 is further specifically configured to, if there is no equipment accident certification data in the equipment virtual asset breakage data, obtain equipment accident occurrence data in the equipment virtual asset breakage data through intelligent closure, obtain a second accident breakage rate at which the equipment type and the equipment accident occurrence data are matched in the block chain full database, and use the second accident breakage rate as the equipment accident breakage rate; the equipment accident occurrence data refers to historical data of accidents of the energy supply equipment;

the accident data generating module 13 is further specifically configured to, if there is no equipment accident proof data and no equipment accident occurrence data in the equipment virtual asset breakage data, obtain a third accident breakage rate matched with the equipment type in the block chain full database through the intelligent contract, and use the third accident breakage rate as the equipment accident breakage rate.

the asset data generation module 14 is further specifically configured to generate an equipment virtual asset breakage rate through the intelligent contract, the equipment virtual asset breakage data, and the equipment historical maintenance data;

the asset data generation module 14 is further specifically configured to generate a component virtual asset breakage rate through the intelligent contract, the component virtual asset breakage data, and the component historical maintenance data;

the asset data generating module 14 is further specifically configured to generate an engine virtual asset breakage rate through the intelligent contract and the engine virtual asset breakage data.

The asset data generation module 14 is further specifically configured to traverse the device virtual asset depreciation data and the device history maintenance data through the intelligent contract;

the asset data generation module 14 is further specifically configured to, if the sailing authority certification data exists in the equipment virtual asset breakage data and the maintenance certification data exists in the equipment historical maintenance data, obtain a certification breakage rate, which is matched with the sailing authority certification data and the maintenance certification data, in the block chain full database through an intelligent contract, and use the certification breakage rate as the equipment virtual asset breakage rate;

the asset data generating module 14 is further specifically configured to, if the navigation authority certification data exists in the virtual asset damage data of the device and the maintenance certification data does not exist in the historical maintenance data of the device, obtain, by using an intelligent contract, a first certification loss breakage rate matched with the maintenance certification data in the block chain full database, and use the first certification loss breakage rate as the virtual asset damage rate of the device;

the asset data generating module 14 is further specifically configured to, if no navigation authority certification data exists in the device virtual asset breakage data and maintenance certification data exists in the device historical maintenance data, obtain, by using an intelligent contract, a second certification loss breakage rate matched with the navigation authority certification data in the block chain full database, and use the second certification loss breakage rate as the device virtual asset breakage rate;

the asset data generating module 14 is further specifically configured to, if no navigation authority certification data exists in the device virtual asset breakage data and no maintenance certification data exists in the device historical maintenance data, obtain, by using an intelligent contract, a third certification loss breakage rate that matches the navigation authority certification data and the maintenance certification data in the block chain full database, and use the third certification loss breakage rate as the device virtual asset breakage rate.

The reference value generation module 15 is further specifically configured to determine an aircraft accident breakage rate according to the component accident breakage rate, the engine accident breakage rate, and the equipment accident breakage rate;

the reference value generation module 15 is further specifically configured to determine an aircraft virtual asset breakage rate according to the component virtual asset breakage rate, the engine virtual asset breakage rate, and the equipment virtual asset breakage rate;

the reference value generation module 15 is further specifically configured to generate a maintenance remaining duration according to the aircraft navigation data;

the reference value generating module 15 is further specifically configured to determine the aircraft accident breakage rate, the aircraft virtual asset breakage rate, and the maintenance remaining duration as a virtual asset evaluation reference value for the aircraft.

The reference value generation module 15 is further specifically configured to obtain an accident assessment matrix associated with the aircraft; elements in the accident assessment matrix are used for representing accident assessment reference proportions corresponding to the component accident breakage rate, the engine accident breakage rate and the equipment accident breakage rate respectively;

the reference value generating module 15 is further specifically configured to multiply the component accident breakage rate by an accident assessment reference proportion corresponding to the component accident breakage rate to obtain a target component accident breakage rate;

the reference value generation module 15 is further specifically configured to multiply the engine accident breakage rate by an accident assessment reference proportion corresponding to the engine accident breakage rate to obtain a target engine accident breakage rate;

the reference value generating module 15 is further specifically configured to multiply the equipment accident breakage rate by the accident assessment reference proportion corresponding to the equipment accident breakage rate to obtain a target equipment accident breakage rate;

the reference value generating module 15 is further specifically configured to add the target component accident breakage rate, the target engine accident breakage rate, and the target device accident breakage rate to obtain an aircraft accident breakage rate.

The reference value generation module 15 is further specifically configured to obtain an asset evaluation matrix associated with the aircraft; elements in the asset assessment matrix are used for representing asset assessment reference proportions corresponding to the assembly virtual asset breakage rate, the engine virtual asset breakage rate and the equipment virtual asset breakage rate respectively;

the reference value generating module 15 is further specifically configured to multiply the component virtual asset breakage rate by an asset assessment reference proportion corresponding to the component virtual asset breakage rate to obtain a target component virtual asset breakage rate;

the reference value generation module 15 is further specifically configured to multiply the engine virtual asset breakage rate by an asset assessment reference proportion corresponding to the engine virtual asset breakage rate to obtain a target engine virtual asset breakage rate;

the reference value generating module 15 is further specifically configured to multiply the equipment virtual asset breakage rate by an asset assessment reference proportion corresponding to the equipment virtual asset breakage rate to obtain a target equipment virtual asset breakage rate;

the reference value generating module 15 is further specifically configured to add the target component virtual asset breakage rate, the target engine virtual asset breakage rate, and the target device virtual asset breakage rate to obtain an aircraft virtual asset breakage rate.

Referring to fig. 5, the aircraft-based data processing apparatus may further include: a matrix obtaining module 18, a breakage rate obtaining module 19, a prediction data generating module 20 and a matrix adjusting module 21.

A matrix obtaining module 18, configured to obtain an initial accident assessment matrix and an initial asset assessment matrix;

the breakage rate obtaining module 19 is used for obtaining the sample assembly accident breakage rate, the sample engine accident breakage rate and the sample equipment accident breakage rate of the sample airplane;

the prediction data generation module 20 is used for generating a predicted accident breakage rate of the airplane through the initial accident assessment matrix, the sample assembly accident breakage rate, the sample engine accident breakage rate and the sample equipment accident breakage rate;

the prediction data generation module 20 is further configured to generate a virtual asset prediction rate of the aircraft according to the initial asset evaluation matrix, the sample assembly accident breakage rate, the sample engine accident breakage rate, and the sample equipment accident breakage rate;

the matrix adjusting module 21 is configured to obtain a tag accident breakage rate of the airplane and a tag virtual asset breakage rate of the airplane, and adjust the initial accident assessment matrix by predicting the accident breakage rate and the tag accident breakage rate to obtain an accident assessment matrix;

the matrix adjusting module 21 is further configured to adjust the initial asset evaluation matrix by predicting the virtual asset breakage rate and the tag virtual asset breakage rate, so as to obtain an asset evaluation matrix.

For a specific implementation manner of the matrix obtaining module 18, the breakage rate obtaining module 19, the prediction data generating module 20, and the matrix adjusting module 21, reference may be made to the description in step S104 in the embodiment corresponding to fig. 3, and details will not be described here.

The reference value generation module 15 is further specifically configured to obtain, in the aircraft navigation data, an aircraft historical navigation cycle corresponding to the aircraft, a maintenance navigation duration corresponding to the aircraft, and an aircraft type corresponding to the aircraft through an intelligent contract; the historical navigation period of the airplane is the total period of navigation by using the airplane; the maintenance navigation cycle refers to a cycle of navigating by using the airplane after the performance of the airplane is recovered and maintained; the maintenance navigation time is the time for navigating by using the airplane after the performance of the airplane is recovered and maintained;

the reference value generation module 15 is further specifically configured to obtain a maintenance remaining duration set; the maintenance remaining duration set comprises a mapping relation between the configuration data group and the configuration maintenance remaining duration; the configuration data set is a data set consisting of configuration of airplane type, configuration of maintenance navigation duration, configuration of maintenance navigation period and configuration of historical navigation period;

the reference value generation module 15 is further specifically configured to match a target data group composed of the aircraft type, the maintenance voyage duration, the maintenance voyage period, and the aircraft historical voyage period with the maintenance remaining duration set through an intelligent contract, and acquire a configuration data group matched with the target data group in the maintenance remaining duration set as a target configuration data group;

the reference value generating module 15 is further specifically configured to use the configured remaining repair duration having the mapping relationship with the target configuration data set as the remaining repair duration of the aircraft.

referring to fig. 5, the aircraft-based data processing apparatus may further include: a data transmission module 22 and an account transmission module 23.

The data sending module 22 is configured to send the property right transfer request and the virtual asset assessment reference value to the second device, so that the second device determines the virtual asset value of the aircraft based on the property right transfer request and the virtual asset assessment reference value, and returns a property right transfer confirmation message according to the application virtual asset value when the virtual asset value is greater than or equal to the application virtual asset value;

the account sending module 23 is configured to send the device account corresponding to the first device to the second device according to the physical right transfer confirmation message, so that the second device obtains the virtual asset data corresponding to the application virtual asset value from the device account corresponding to the second device, and transfers the virtual asset data to the device account corresponding to the first device.

For specific implementation of the data sending module 22 and the account sending module 23, reference may be made to the description in step S104 in the embodiment corresponding to fig. 3, which will not be described herein again.

Further, please refer to fig. 6, where fig. 6 is a schematic structural diagram of a computer device according to an embodiment of the present application. As shown in fig. 6, the apparatus 1 in the embodiment corresponding to fig. 5 may be applied to the computer device 1000, and the computer device 1000 may include: the processor 1001, the network interface 1004, and the memory 1005, and the computer apparatus 1000 further includes: a user interface 1003, and at least one communication bus 1002. Wherein a communication bus 1002 is used to enable connective communication between these components. The user interface 1003 may include a Display screen (Display) and a Keyboard (Keyboard), and the optional user interface 1003 may also include a standard wired interface and a standard wireless interface. The network interface 1004 may optionally include a standard wired interface, a wireless interface (e.g., WI-FI interface). The memory 1005 may be a high-speed RAM memory or a non-volatile memory (non-volatile memory), such as at least one disk memory. The memory 1005 may optionally be at least one memory device located remotely from the processor 1001. As shown in fig. 6, a memory 1005, which is a kind of computer-readable storage medium, may include therein an operating system, a network communication module, a user interface module, and a device control application program.

In the computer device 1000 shown in fig. 6, the network interface 1004 may provide a network communication function; the user interface 1003 is an interface for providing a user with input; and the processor 1001 may be used to invoke a device control application stored in the memory 1005 to implement:

It should be understood that the computer device 1000 described in this embodiment of the present application may perform the description of the aircraft-based data processing method in the embodiment corresponding to fig. 3, and may also perform the description of the aircraft-based data processing apparatus 1 in the embodiment corresponding to fig. 5, which is not described herein again. In addition, the beneficial effects of the same method are not described in detail.

Further, here, it is to be noted that: an embodiment of the present application further provides a computer-readable storage medium, where a computer program executed by the aforementioned data processing computer device 1000 is stored in the computer-readable storage medium, and the computer program includes program instructions, and when the processor executes the program instructions, the description of the data processing method in the embodiment corresponding to fig. 3 can be executed, so that details are not repeated here. In addition, the beneficial effects of the same method are not described in detail. For technical details not disclosed in embodiments of the computer-readable storage medium referred to in the present application, reference is made to the description of embodiments of the method of the present application.

The computer-readable storage medium may be the data processing apparatus based on the aircraft provided in any of the foregoing embodiments or an internal storage unit of the computer device, such as a hard disk or a memory of the computer device. The computer readable storage medium may also be an external storage device of the computer device, such as a plug-in hard disk, a Smart Memory Card (SMC), a Secure Digital (SD) card, a flash card (flash card), and the like, provided on the computer device. Further, the computer-readable storage medium may also include both an internal storage unit and an external storage device of the computer device. The computer-readable storage medium is used for storing the computer program and other programs and data required by the computer device. The computer readable storage medium may also be used to temporarily store data that has been output or is to be output.

The terms "first," "second," and the like in the description and in the claims and drawings of the embodiments of the present application are used for distinguishing between different objects and not for describing a particular order. Furthermore, the terms "comprises" and any variations thereof, are intended to cover non-exclusive inclusions. For example, a process, method, apparatus, product, or apparatus that comprises a list of steps or elements is not limited to the listed steps or modules, but may alternatively include other steps or modules not listed or inherent to such process, method, apparatus, product, or apparatus.

Those of ordinary skill in the art will appreciate that the elements and algorithm steps of the examples described in connection with the embodiments disclosed herein may be embodied in electronic hardware, computer software, or combinations of both, and that the components and steps of the examples have been described in a functional general in the foregoing description for the purpose of illustrating clearly the interchangeability of hardware and software. Whether such functionality is implemented as hardware or software depends upon the particular application and design constraints imposed on the implementation. Skilled artisans may implement the described functionality in varying ways for each particular application, but such implementation decisions should not be interpreted as causing a departure from the scope of the present application.

The method and the related apparatus provided by the embodiments of the present application are described with reference to the flowchart and/or the structural diagram of the method provided by the embodiments of the present application, and each flow and/or block of the flowchart and/or the structural diagram of the method, and the combination of the flow and/or block in the flowchart and/or the block diagram can be specifically implemented by computer program instructions. These computer program instructions may be provided to a processor of a general purpose computer, special purpose computer, embedded processor, or other programmable data processing apparatus to produce a machine, such that the instructions, which execute via the processor of the computer or other programmable data processing apparatus, create means for implementing the functions specified in the flowchart flow or flows and/or block or blocks of the block diagram. These computer program instructions may also be stored in a computer-readable memory that can direct a computer or other programmable data processing apparatus to function in a particular manner, such that the instructions stored in the computer-readable memory produce an article of manufacture including instruction means which implement the function specified in the flowchart flow or flows and/or block or blocks of the block diagram. These computer program instructions may also be loaded onto a computer or other programmable data processing apparatus to cause a series of operational steps to be performed on the computer or other programmable apparatus to produce a computer implemented process such that the instructions which execute on the computer or other programmable apparatus provide steps for implementing the functions specified in the flowchart flow or flows and/or block or blocks.

The above disclosure is only for the purpose of illustrating the preferred embodiments of the present application and is not to be construed as limiting the scope of the present application, so that the present application is not limited thereto, and all equivalent variations and modifications can be made to the present application.

Claims

1. An aircraft-based data processing method, comprising:

acquiring a property right transfer request sent by first equipment; the first equipment is corresponding to a user who has ownership for the airplane; the property right transfer request is used for requesting to transfer the property affiliation right of the airplane to a second device, and the first device has the property use right of the airplane after the transfer of the property affiliation right;

calling an intelligent contract, and generating accident damage rates corresponding to the component, the engine and the energy supply equipment respectively through virtual asset damage data corresponding to the component, the engine and the energy supply equipment respectively carried in the intelligent contract and the property right transfer request; the components are parts that make up the aircraft; the energy supply device supplies energy to the airplane;

generating virtual asset damage rates corresponding to the component, the engine and the energy providing equipment respectively through historical maintenance data corresponding to the component, the engine and the energy providing equipment respectively and virtual asset damage data corresponding to the component, the engine and the energy providing equipment respectively, which are carried in the intelligent contract and the property right transfer request;

generating a virtual asset assessment reference value aiming at the airplane according to the accident damage rate respectively corresponding to the component, the engine and the energy providing equipment, the virtual asset damage rate respectively corresponding to the component, the engine and the energy providing equipment and airplane navigation data carried by the property right transfer request; the virtual asset assessment reference value is used for assessing and referencing the virtual asset worth value of the airplane and is used for responding to the weight transfer request to provide the first device with virtual asset data which is smaller than or equal to the virtual asset worth value of the airplane.

2. The method of claim 1, wherein the request for transfer of the property right further comprises user information; the user information is information of the user who has ownership for the airplane;

the method further comprises the following steps:

triggering the intelligent contract based on the property right transfer request, and generating a reliability evaluation value aiming at the user information through the intelligent contract and the user information;

and matching the reliability evaluation value with a reliability threshold value, executing the intelligent contract calling when a matching result and the user information meet a reliability condition, and generating accident damage rates corresponding to the component, the engine and the energy supply equipment respectively through virtual asset damage data corresponding to the component, the engine and the energy supply equipment respectively carried in the intelligent contract and the property right transfer request.

3. The method of claim 1, wherein the virtual asset damage data comprises device virtual asset damage data corresponding to the energy providing device, component virtual asset damage data corresponding to the component, and engine virtual asset damage data corresponding to the engine; the accident breakage rate comprises an equipment accident breakage rate corresponding to the energy supply equipment, a component accident breakage rate corresponding to the component and an engine accident breakage rate corresponding to the engine;

generating accident breakage rates respectively corresponding to the component, the engine and the energy supply device through virtual asset breakage data respectively corresponding to the component, the engine and the energy supply device carried in the intelligent contract and the property right transfer request, wherein the accident breakage rates comprise:

generating the equipment accident breakage rate through the intelligent contract and the equipment virtual asset breakage data;

generating the component accident breakage rate through the intelligent contract and the component virtual asset breakage data;

and generating the engine accident breakage rate through the intelligent contract and the engine virtual asset breakage data.

4. The method of claim 3, wherein generating the equipment incident breakage rate from the smart contract and the equipment virtual asset breakage data comprises:

traversing the device virtual asset impairment data through the smart contract;

if the equipment accident certification data of the energy supply equipment exists in the equipment virtual asset breakage data, acquiring the equipment type of the energy supply equipment in the equipment virtual asset breakage data through the intelligent contract, acquiring a first accident breakage rate matched with the equipment type in a block chain full database, and taking the first accident breakage rate as the equipment accident breakage rate; the equipment accident certification data refers to the certification data that the equipment has no accident;

if the equipment accident proof data does not exist in the equipment virtual asset breakage data, acquiring equipment accident occurrence data in the equipment virtual asset breakage data through the intelligent contract, acquiring a second accident breakage rate matched with the equipment type and the equipment accident occurrence data in the block chain full database, and taking the second accident breakage rate as the equipment accident breakage rate; the equipment accident occurrence data refers to historical data of accidents of the energy supply equipment;

and if the equipment accident proof data does not exist in the equipment virtual asset breakage data and the equipment accident occurrence data does not exist, acquiring a third accident breakage rate matched with the equipment type in the block chain full database through the intelligent contract, and taking the third accident breakage rate as the equipment accident breakage rate.

5. The method of claim 3, wherein the historical maintenance data includes device historical maintenance data corresponding to the energy supply device, component virtual asset outage data corresponding to the component, and engine historical maintenance data corresponding to the engine; the virtual asset breakage rate comprises an equipment virtual asset breakage rate corresponding to the energy supply equipment, a component virtual asset breakage rate corresponding to the component and an engine virtual asset breakage rate corresponding to the engine;

the generating of the virtual asset damage rates corresponding to the component, the engine, and the energy supply device respectively through the historical maintenance data corresponding to the component, the engine, and the energy supply device respectively, and the virtual asset damage data corresponding to the component, the engine, and the energy supply device respectively, which are carried in the intelligent contract and the property right transfer request, includes:

generating the equipment virtual asset breakage rate according to the intelligent contract, the equipment virtual asset breakage data and the equipment historical maintenance data;

generating the component virtual asset breakage rate through the intelligent contract, the component virtual asset breakage data and the component historical maintenance data;

and generating the engine virtual asset breakage rate through the intelligent contract and the engine virtual asset breakage data.

6. The method of claim 5, wherein generating the device virtual asset breakage rate from the smart contract, the device virtual asset breakage data, and the device history maintenance data comprises:

traversing the equipment virtual asset depreciation data and the equipment historical maintenance data through the intelligent contract;

if navigation authority certification data exists in the equipment virtual asset breakage data and maintenance certification data exists in the equipment historical maintenance data, obtaining a certification existence breakage rate matched with the navigation authority certification data and the maintenance certification data in a block chain full database through the intelligent contract, and taking the certification existence breakage rate as the equipment virtual asset breakage rate;

if the navigation authority certification data exists in the equipment virtual asset breakage data and the maintenance certification data does not exist in the equipment historical maintenance data, acquiring a first certification loss breakage rate matched with the maintenance certification data in the block chain full-scale database through the intelligent contract, and taking the first certification loss breakage rate as the equipment virtual asset breakage rate;

if the navigation authority certification data does not exist in the equipment virtual asset breakage data and the maintenance certification data exists in the equipment historical maintenance data, acquiring a second certification loss breakage rate matched with the navigation authority certification data in the block chain full-scale database through the intelligent contract, and taking the second certification loss breakage rate as the equipment virtual asset breakage rate;

and if the navigation authority certification data does not exist in the equipment virtual asset breakage data and the maintenance certification data does not exist in the equipment historical maintenance data, acquiring a third certification loss breakage rate matched with the navigation authority certification data and the maintenance certification data in the block chain full-scale database through the intelligent contract, and taking the third certification loss breakage rate as the equipment virtual asset breakage rate.

7. The method according to claim 5, wherein the generating a virtual asset assessment reference value for the aircraft according to the accident damage rate corresponding to the component, the engine and the energy supply device, respectively, the virtual asset damage rate corresponding to the component, the engine and the energy supply device, respectively, and the aircraft flight data carried by the ownership transfer request comprises:

determining the airplane accident breakage rate according to the component accident breakage rate, the engine accident breakage rate and the equipment accident breakage rate;

determining the aircraft virtual asset breakage rate according to the component virtual asset breakage rate, the engine virtual asset breakage rate and the equipment virtual asset breakage rate;

generating the maintenance remaining time length according to the aircraft navigation data;

and determining the aircraft accident breakage rate, the aircraft virtual asset breakage rate and the maintenance remaining time as virtual asset evaluation reference values aiming at the aircraft.

8. The method of claim 7, wherein determining the aircraft accident breakage rate from the component accident breakage rate, the engine accident breakage rate, and the equipment accident breakage rate comprises:

obtaining an incident assessment matrix associated with the aircraft; elements in the accident assessment matrix are used for representing accident assessment reference proportions corresponding to the component accident breakage rate, the engine accident breakage rate and the equipment accident breakage rate respectively;

multiplying the accident breakage rate of the component by the accident assessment reference proportion corresponding to the accident breakage rate of the component to obtain the accident breakage rate of the target component;

multiplying the engine accident breakage rate by an accident assessment reference proportion corresponding to the engine accident breakage rate to obtain a target engine accident breakage rate;

multiplying the equipment accident breakage rate by the accident assessment reference proportion corresponding to the equipment accident breakage rate to obtain a target equipment accident breakage rate;

and adding the target assembly accident breakage rate, the target engine accident breakage rate and the target equipment accident breakage rate to obtain the airplane accident breakage rate.

9. The method of claim 8, wherein determining the aircraft virtual asset breakage rate from the component virtual asset breakage rate, the engine virtual asset breakage rate, and the equipment virtual asset breakage rate comprises:

obtaining an asset assessment matrix associated with the aircraft; elements in the asset assessment matrix are used for representing asset assessment reference proportions corresponding to the component virtual asset breakage rate, the engine virtual asset breakage rate and the equipment virtual asset breakage rate respectively;

multiplying the component virtual asset breakage rate by an asset assessment reference proportion corresponding to the component virtual asset breakage rate to obtain a target component virtual asset breakage rate;

multiplying the engine virtual asset breakage rate by an asset evaluation reference proportion corresponding to the engine virtual asset breakage rate to obtain a target engine virtual asset breakage rate;

multiplying the equipment virtual asset breakage rate by an asset evaluation reference proportion corresponding to the equipment virtual asset breakage rate to obtain a target equipment virtual asset breakage rate;

and adding the target assembly virtual asset breakage rate, the target engine virtual asset breakage rate and the target equipment virtual asset breakage rate to obtain the airplane virtual asset breakage rate.

10. The method of claim 9, further comprising:

acquiring an initial accident assessment matrix and an initial asset assessment matrix;

acquiring the sample assembly accident breakage rate, the sample engine accident breakage rate and the sample equipment accident breakage rate of a sample airplane;

generating a predicted accident breakage rate of the airplane according to the initial accident assessment matrix, the sample assembly accident breakage rate, the sample engine accident breakage rate and the sample equipment accident breakage rate;

generating a predicted virtual asset breakage rate of the aircraft according to the initial asset assessment matrix, the sample assembly accident breakage rate, the sample engine accident breakage rate and the sample equipment accident breakage rate;

acquiring a tag accident breakage rate of the airplane and a tag virtual asset breakage rate of the airplane, and adjusting the initial accident assessment matrix according to the predicted accident breakage rate and the tag accident breakage rate to obtain the accident assessment matrix;

and adjusting the initial asset evaluation matrix according to the predicted virtual asset breakage rate and the tag virtual asset breakage rate to obtain the asset evaluation matrix.

11. The method of claim 7, wherein generating the remaining length of service based on the aircraft voyage data comprises:

acquiring an airplane historical navigation cycle corresponding to the airplane, a maintenance navigation duration corresponding to the airplane and an airplane type corresponding to the airplane in the airplane navigation data through the intelligent contract; the historical navigation period of the airplane is the total period of navigation by using the airplane; the maintenance navigation cycle refers to a cycle of navigating by using the airplane after performance recovery maintenance is carried out on the airplane; the maintenance navigation time is the time for navigating by using the airplane after the performance of the airplane is recovered and maintained;

acquiring a maintenance remaining time set; the maintenance remaining duration set comprises a mapping relation between a configuration data set and configuration maintenance remaining duration; the configuration data set is a data set consisting of configuration airplane type, configuration maintenance navigation time, configuration maintenance navigation period and configuration historical navigation period;

matching a target data group consisting of the type of the airplane, the maintenance navigation time, the maintenance navigation period and the historical navigation period of the airplane with the maintenance residual time set through the intelligent contract, and acquiring a configuration data group matched with the target data group from the maintenance residual time set to serve as a target configuration data group;

and taking the configuration maintenance remaining time length with the mapping relation with the target configuration data set as the maintenance remaining time length of the airplane.

12. The method of claim 1, wherein the rights transfer request further comprises an application for a virtual asset value;

the method further comprises the following steps:

sending the object right transfer request and the virtual asset assessment reference value to second equipment, so that the second equipment determines the virtual asset value of the airplane based on the object right transfer request and the virtual asset assessment reference value, and returning an object right transfer confirmation message according to the application virtual asset value when the virtual asset value is greater than or equal to the application virtual asset value;

and sending the equipment account corresponding to the first equipment to the second equipment according to the property right transfer confirmation message, so that the second equipment obtains the virtual asset data corresponding to the application virtual asset numerical value in the equipment account corresponding to the second equipment, and transfers the virtual asset data to the equipment account corresponding to the first equipment.

13. An aircraft-based data processing apparatus, comprising:

the request acquisition module is used for acquiring a property right transfer request sent by first equipment; the first equipment is corresponding to a user who has ownership for the airplane; the property right transfer request is used for requesting to transfer the property affiliation right of the airplane to a second device, and the first device has the property use right of the airplane after the transfer of the property affiliation right;

the contract calling module is used for calling an intelligent contract;

the accident data generation module is used for generating accident breakage rates corresponding to the components, the engine and the energy supply equipment respectively through virtual asset breakage data corresponding to the components, the engine and the energy supply equipment respectively carried in the intelligent contract and the property right transfer request; the components are parts that make up the aircraft; the energy supply device supplies energy to the airplane;

an asset data generation module, configured to generate virtual asset damage rates corresponding to the component, the engine, and the energy providing device respectively through historical maintenance data corresponding to the component, the engine, and the energy providing device respectively, and virtual asset damage data corresponding to the component, the engine, and the energy providing device respectively, which are carried in the intelligent contract and the property right transfer request;

a reference value generation module, configured to generate a virtual asset assessment reference value for the aircraft according to the accident damage rates respectively corresponding to the component, the engine, and the energy providing device, the virtual asset damage rates respectively corresponding to the component, the engine, and the energy providing device, and aircraft navigation data carried in the property right transfer request; the virtual asset assessment reference value is used for assessing and referencing the virtual asset worth value of the airplane and is used for responding to the weight transfer request to provide the first device with virtual asset data which is smaller than or equal to the virtual asset worth value of the airplane.

14. A computer device, comprising: a processor, a memory, and a network interface;

the processor is coupled to the memory and the network interface, wherein the network interface is configured to provide network communication functionality, the memory is configured to store program code, and the processor is configured to invoke the program code to perform the method of any of claims 1-12.

15. A computer-readable storage medium, in which a computer program is stored which is adapted to be loaded by a processor and to carry out the method of any one of claims 1 to 12.