Twin-engine aircraft throttle lever
CN309916515SActive Publication Date: 2026-04-14李志阳
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Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Designs(China)
- Current Assignee / Owner
- Filing Date
- 2025-09-11
- Publication Date
- 2026-04-14
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Figure 000007_ABST
Abstract
1. Name of the product in this design: Twin-engine aircraft throttle lever. 2. Purpose of this design: This design is used to adjust the operating force of the aircraft throttle lever. 3. The key design feature of this product is its shape. 4. The image or photograph that best illustrates the design's key points: a 3D model.
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