Lower milled inlet for turbojet high-speed target drone
CN310295279SActive Publication Date: 2026-11-03奥瑞思智能科技(阜新)有限公司 +1
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Patent Information
- Application Number
- CN202630102470.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Designs(China)
- Current Assignee / Owner
- Filing Date
- 2026-03-09
- Publication Date
- 2026-11-03
- Estimated Expiration
- 2041-03-09
Smart Images
Figure 000007_ABST
Abstract
1.The name of the design product: lower milling inlet channel for turbojet high-speed target drone. 2.The use of the design product: for unmanned aerial vehicle. 3.The design points of the design product: the combination of shape, pattern and color. 4.The picture or photo that best shows the design points: perspective view 1. 5.The design claimed contains color.
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