| DEVICE FOR MEASURING AERODYNAMIC PARAMETERS OF AN AIRCRAFT WITH FLAPPING WINGS | |
| 2024-12-16 | |
| 专利权人 | UNIV MISIS NAT SCI & TECHNOLOGY (UMNS-C) |
| 申请日期 | 2024-12-16 |
| 专利号 | RU2837120-C1 |
| 成果简介 | NOVELTY - Invention relates to experimental aerodynamics, in particular to a device for measuring thrust of a flapping wing of an aircraft, and can be used in experimental aviation equipment when designing and investigating aircraft with a flapping wing (ornithopter). Device comprises a lodgement fixed on a plastic adapter fitted on a metal rod placed in a measuring unit mounted on a beam, and a rotating platform fixed on a vertical axis connected to the base. Measuring unit is equipped with a movable carriage on which a metal rod is held. Inside the measuring unit there are horizontal and vertical strain gauges configured to transmit data on lift and angular velocity of the aircraft to a control device mounted on the beam with a step motor configured to control the rotation of the platform and measure the angular velocity of the beam. At the same time on the beam there is additionally a transmitting unit made with possibility of measuring signals transmission for processing. USE - Measuring. ADVANTAGE - Possibility of measurement of aerodynamic characteristics of aircraft, created lift thrust, measurement of flight speed of aircraft without use of wind tunnel, measurement of thrust force depending on change in inclination angle of aircraft with flapping wings. 1 cl, 3 dwg |
| IPC 分类号 | B64C-033/00 ; G01L-005/1627 |
| 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/14046 |
| 专题 | 中国科学院新疆生态与地理研究所 |
| 作者单位 | UNIV MISIS NAT SCI & TECHNOLOGY (UMNS-C) |
| 推荐引用方式 GB/T 7714 | KHABIBULLIN F R,KLIUEV K A,SHCHAPIN V S,et al. DEVICE FOR MEASURING AERODYNAMIC PARAMETERS OF AN AIRCRAFT WITH FLAPPING WINGS. RU2837120-C1[P]. 2024. |
| 条目包含的文件 | 条目无相关文件。 | |||||
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