CN-121998577-A - Design and support method of electronic engineering card for test flight preparation

CN121998577ACN 121998577 ACN121998577 ACN 121998577ACN-121998577-A

Abstract

The application provides a test flight preparation-oriented engineering electronic work card design and support method, which comprises the steps of preparing and managing aircraft basic data, preparing and associating test flight task list data, importing or creating test flight task list information based on the preprocessed aircraft basic information, establishing an association mapping relation between the aircraft basic information and the test flight task list, creating multiple types of engineering electronic work cards based on the aircraft basic information and test flight task requirements, configuring basic attributes for various types of engineering electronic work cards, associating and binding the configured electronic work cards with corresponding task lists, structuring the work card tasks, adding specific task items in the created electronic work cards, guaranteeing data consistency and compatibility, establishing a data synchronization mechanism between the aircraft basic data, the test flight task list and the electronic work cards, reducing human error risks, and guaranteeing the standardization and data traceability of test flight preparation work.

Inventors

HUANG ZHUN
YANG CHAODONG
YUAN YE
LIU PAN
CHEN HAIYANG
ZHOU JUN
Wan Yinwei

Assignees

中国飞行试验研究院

Dates

Publication Date: 20260508
Application Date: 20251227

Claims (8)

1. A method for designing and supporting a pilot-flight preparation-oriented engineering electronic work card is characterized by comprising the following steps: The aircraft basic data preparation and management, namely importing from a data source or creating aircraft basic information through user operation; the method comprises the steps of preparing and associating flight test task sheet data, importing or creating flight test task sheet information based on preprocessed aircraft basic information, and establishing an association mapping relation between the aircraft basic information and the flight test task sheet; creating and configuring a plurality of types of electronic engineering cards based on airplane basic information and test flight task requirements, configuring basic attributes for various types of electronic engineering cards, and performing association binding on the configured electronic engineering cards and corresponding task sheets according to the specific content of the test flight task sheets; The construction configuration of the task of the work card comprises the steps of adding specific task items into the created electronic work card, and defining operation guidance, inspection standard, responsible person qualification requirement and required tool equipment list of each task; And the data consistency and compatibility guarantee is that a data synchronization mechanism among the aircraft basic data, the test flight task list and the electronic work card is established, and when the associated basic data is changed, the automatic update prompt of the relevant information of the work card is triggered.
2. The method of claim 1, wherein the aircraft base information includes aircraft model number, aircraft number, system parameters, and configuration information.
3. The method of claim 1, wherein the test flight ticket information includes a task name, a unique task number, a scheduled start time, a scheduled completion time limit, and a task priority identification.
4. The method of claim 1, wherein the multiple types of mechanical electronic work card types include a general inspection work card, an appearance inspection work card, a service preparation work card, a power-on inspection work card, a post-flight inspection work card, a project-on-demand work card, a fly-out validation work card, a missile inspection work card, and a pre-inspection work card.
5. The method of claim 1, wherein the mission electronics work card configuration base attributes include work card number, corresponding aircraft model, applicable mission type, and work card version information.
6. The method of claim 1, wherein the aircraft base data preparation and management further comprises: And managing the full life cycle of the aircraft basic data, performing parameter updating and information deleting operation on the recorded aircraft basic information, and recovering the data after false deletion.
7. The method of claim 1, wherein the test flight ticket data is prepared for association with, further comprising: dynamically managing the test flight task list, editing and deleting the task list information, and backing up and recovering the task list data.
8. The method of claim 1, wherein the work card task structured configuration further comprises: The multimedia description file associated with the task item configuration is added, and the multimedia description file comprises an operation schematic diagram, a standard flow video and a key parameter reference table, so that task executives can be assisted to operate accurately.

Description

Design and support method of electronic engineering card for test flight preparation Technical Field The application belongs to the technical field of aviation engineering, and particularly relates to a method for designing and supporting a test flight preparation-oriented engineering electronic work card. Background In the field of aviation test flight, the efficiency and accuracy of test flight preparation work directly influence the smooth development of test flight tasks, and a machine work card is used as a core operation basis in the test flight preparation stage, so that the design rationality and the management efficiency are important. The traditional engineering work cards mostly adopt paper forms or simple electronic documents, and have the problems that the engineering card creation depends on manual writing, has single type and is difficult to flexibly configure according to the test flight task, the association degree of the engineering card and the airplane basic information is low, the task execution state cannot be tracked in real time, and the like. In the prior art, the electronic work card system often fails to realize the deep association of the aircraft basic data, the test flight task data and the work card data, the work card task allocation lacks a scientific load balancing mechanism, the state feedback in the task execution process is lagged, and the data tracing is difficult, so that the problems of task omission, untimely information transmission, irregular operation and the like easily occur in the test flight preparation work, the time cost and the error risk of the test flight preparation are increased, and the high-efficiency and accurate test flight preparation requirement is difficult to meet. Disclosure of Invention The invention aims to solve the problems, provides a design and support method of the electronic work card for test flight preparation, aims to improve the efficiency and accuracy of test flight preparation work, and solves the technical problems of the electronic work card for test flight in the processes of creating, configuring, tracking and data management. The application provides a method for designing and supporting a duty electronic work card for test flight preparation, which comprises the following steps: The aircraft basic data preparation and management, namely importing from a data source or creating aircraft basic information through user operation; the method comprises the steps of preparing and associating flight test task sheet data, importing or creating flight test task sheet information based on preprocessed aircraft basic information, and establishing an association mapping relation between the aircraft basic information and the flight test task sheet; creating and configuring a plurality of types of electronic engineering cards based on airplane basic information and test flight task requirements, configuring basic attributes for various types of electronic engineering cards, and performing association binding on the configured electronic engineering cards and corresponding task sheets according to the specific content of the test flight task sheets; The construction configuration of the task of the work card comprises the steps of adding specific task items into the created electronic work card, and defining operation guidance, inspection standard, responsible person qualification requirement and required tool equipment list of each task; And the data consistency and compatibility guarantee is that a data synchronization mechanism among the aircraft basic data, the test flight task list and the electronic work card is established, and when the associated basic data is changed, the automatic update prompt of the relevant information of the work card is triggered. Preferably, the aircraft basic information includes an aircraft model number, an aircraft number, system parameters and configuration information. Preferably, the flight test task list information comprises a task name, a unique task number, a planned starting time, a planned completion time limit and a task priority identification. Preferably, the multi-type mechanical electronic work card type comprises a common inspection work card, an appearance inspection work card, a service preparation work card, an electrifying inspection work card, a post-flight inspection work card, a project inspection work card, a flying confirmation work card, a missile inspection work card and a pre-inspection work card. Preferably, the basic attribute of the configuration of the engineering electronic work card comprises a work card number, a corresponding airplane model, an applicable task type and work card version information. Preferably, the aircraft base data preparation and management further comprises: And managing the full life cycle of the aircraft basic data, performing parameter updating and information deleting operation on the recorded aircraft basic information, and recovering the data