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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Figure 000001_ABST
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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