A framework for supporting one or more repair processes of one or more aircraft. The repair processes are based on repair information or repair solution corresponding to the damages to one or more structural components of the aircraft. The framework includes a knowledge engine, and a deployment engi
A framework for supporting one or more repair processes of one or more aircraft. The repair processes are based on repair information or repair solution corresponding to the damages to one or more structural components of the aircraft. The framework includes a knowledge engine, and a deployment engine. The knowledge engine automatically generates one or more knowledge interpretation systems based on the user inputs. The knowledge interpretation systems provide the repair information corresponding to the various structural components of the aircraft based on the user inputs. The deployment engine fulfills the deployment requirements corresponding to the one or more knowledge interpretation systems.
대표청구항▼
1. A framework for supporting one or more repair processes of one or more aircrafts, the framework comprising: a. a query system generator in communication with a microcontroller configured to: receive user inputs pertaining to one or more structural components of the one or more aircrafts via a use
1. A framework for supporting one or more repair processes of one or more aircrafts, the framework comprising: a. a query system generator in communication with a microcontroller configured to: receive user inputs pertaining to one or more structural components of the one or more aircrafts via a user interface,auto populate one or more databases with information on damage and repair of the one or more structural components,create and customize one or more schema templates based on the user inputs and the information in the one or more databases, andgenerate one or more query systems using the one or more schema templates; andb. a deployment engine in communication with the microcontroller configured to: receive deployment requirements corresponding to the one or more query systems, wherein the deployment requirements are provided by one or more deployment users, anddeploy the one or more query systems on one or more networks. 2. The framework of claim 1, wherein the one or more query systems are accessed by the users of the query system to generate one or more queries and obtain responses to the one or more queries based on the information in the one or more databases for identifying one or more repair solutions. 3. The framework of claim 2, wherein the one or more queries are generated based on shape and topological features of the one or more structural components of the one or more aircrafts. 4. A method for supporting one or more repair processes of one or more aircraft, the method comprising: receiving user inputs pertaining to one or more structural components of the one or more aircrafts via a user interface by a query system generator in communication with a micro-controller;auto-populating information on damage and repair of the one or more structural components of the one or more aircrafts in one or more databases by the micro-controller;creating and customizing one or more schema templates, based on the user inputs and the information in the one or more databases, and using the one or more schema templates for automatically generating one or more query systems by the query system generator;receiving deployment requirements corresponding to the one or more query systems by a deployment engine in communication with the microcontroller, wherein the deployment requirements are provided by one or more deployment users via the user interface; anddeploying the automatically generated one or more query systems on one or more networks by using the deployment engine. 5. The method of claim 4, wherein the one or more query systems are accessed by the users of the query systems to generate one or more queries and obtain responses to the one or more queries based on the information in the one or more databases for identifying the one or more repair solutions. 6. The method of claim 5, wherein the one or more queries are generated based on shape and topological features of the one or more structural components of the one or more aircrafts. 7. A computer program product for use with a computer, the computer program product comprising a non-transitory computer usable medium having a computer readable program code embodied therein for supporting one or more repair processes of one or more aircraft, the computer readable program code performing: receiving user inputs pertaining to one or more structural components of the one or more aircrafts via a user interface;auto-populating information on damage and repair of the one or more structural components of the one or more aircrafts in one or more databases, the existing information being maintained by the one or more aircrafts in different data formats;converting the information in different data formats into a predefined format before auto populating the information in the one or more databases;creating and customizing one or more schema templates via the user interface based on the user inputs and the information in the one or more databases;using the one or more schema templates for automatically generating one or more query systems;receiving deployment requirements corresponding to the one or more query systems wherein the deployment requirements are provided by one or more deployment users via the user interface; anddeploying the automatically generated one or more query systems on one or more networks. 8. The framework of claim 1, wherein the query system generator is accessed by the users of the query system generator to modify and create tables in the schema templates to create new schema templates. 9. The framework of claim 1, wherein information on damage and repair exists in different formats with one or more aircrafts. 10. The framework of claim 9, wherein information in different data formats are converted into a predefined format before being auto populated in the one or more databases. 11. The framework of claim 1, wherein the deployment requirements include inputs corresponding to build-time and deployment environment such as operating systems, Lightweight Directory Access Protocol (LDAP) servers for authentication, Simple Mail Transfer Protocol (SMTP) servers for mail configuration, data sources definitions for specifying Open Database Connectivity (ODBC), and Java Database Connectivity (JDBC) servers. 12. The method of claim 4, wherein the query system generator is accessed by one or more users to create and modify tables in the schema templates to create new schema templates. 13. The method of claim 4, wherein information on damage and repair exists in different formats with one or more aircrafts. 14. The method of claim 13, wherein information in different data formats are converted into a predefined format before being auto populated in the one or more databases. 15. The method of claim 4, wherein the deployment requirements include inputs corresponding to build-time and deployment environment such as operating systems, Lightweight Directory Access Protocol (LDAP) servers for authentication, Simple Mail Transfer Protocol (SMTP) servers for mail configuration, data sources definitions for specifying Open Database Connectivity (ODBC), and Java Database Connectivity (JDBC) servers.
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이 특허에 인용된 특허 (22)
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Hogg George W. (Palm Beach Gardens FL) Carron Karen A. (Palm Beach Gardens FL) Wright Brian D. (West Palm Beach FL) Stambaugh ; Sr. Craig T. (Port St. Lucie FL), Engine fault diagnostic system.
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