| Correction clutch for aircraft collective pitch control handle, has bearings mounted on correction coupling housing on which rotary portion is mounted, and shaft attached to rotary portion | |
| 2024-12-18 | |
| 专利权人 | INNOVATIVE AVIATION SYSTEMS LLC (INNO-Non-standard) |
| 申请日期 | 2024-12-18 |
| 专利号 | RU231615-U1 |
| 成果简介 | NOVELTY - The clutch (1) has a correction coupling housing to which a flange portion of the coupling is attached, where bearings are mounted on the correction coupling housing on which a rotary portion is mounted, and a shaft is attached to the rotary portion. A movable lock is mounted on the correction coupling housing. The flange portion of the clutch is attached to a body of the clutch using screws, where the shaft is attached to the rotary portion using screws. USE - Correction clutch for a collective pitch control handle of an aircraft. ADVANTAGE - The clutch lock eliminates arbitrary activation of the correction clutch during flight, thus increasing safety of aircraft operation. DESCRIPTION OF DRAWING(S) - The drawing shows a perspective view of an aircraft collective pitch control handle with a correction clutch. 1Correction coupling 2Collective pitch control handle |
| IPC 分类号 | G05G-001/06 |
| 国家 | 俄罗斯 |
| 专业领域 | 信息技术 |
| 语种 | 英语 |
| 成果类型 | 专利 |
| 文献类型 | 科技成果 |
| 条目标识符 | http://119.78.100.226:8889/handle/3KE4DYBR/13995 |
| 专题 | 中国科学院新疆生态与地理研究所 |
| 作者单位 | INNOVATIVE AVIATION SYSTEMS LLC (INNO-Non-standard) |
| 推荐引用方式 GB/T 7714 | BENDUS A M,BENDUS A V,PAVLOV A V,et al. Correction clutch for aircraft collective pitch control handle, has bearings mounted on correction coupling housing on which rotary portion is mounted, and shaft attached to rotary portion. RU231615-U1[P]. 2024. |
| 条目包含的文件 | 条目无相关文件。 | |||||
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