Flight parameter data quick interpretation analysis interface for electronic device

CN310205751SActive Publication Date: 2026-09-15CHINA AERONAUTICAL CONTROL SYST RES INST
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Patent Information

Application Number
CN202530645290.4
Authority / Receiving Office
CN · China
Patent Type
Designs(China)
Current Assignee / Owner
Filing Date
2025-11-03
Publication Date
2026-09-15
Estimated Expiration
2040-11-03

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Abstract

1. The name of the design product: flight parameter data rapid interpretation analysis interface for electronic equipment. 2. The use of the design product: for rapid interpretation and analysis of flight parameter data. 3. The design points of the design product: the graphical user interface content in the screen. 4. The picture or photo that best indicates the design points: front view. 5. No design points, omit rear view, left view, right view, top view and bottom view. 6. The use of the graphical user interface: the front view is the main page diagram of the flight parameter data rapid interpretation and analysis, and the "fault quick judgment", "parameter analysis", "vibration spectrum" and other buttons can be clicked to rapidly interpret and analyze the flight parameter data.
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