The invention relates to an inertial measurement module, a flight control inertial measurement assembly and an aircraft, and the inertial measurement module comprises an inertial measurement unit which is used for measuring the inertial parameters of a moving object; an electric heating piece, which is arranged side by side with the inertia measurement unit at an interval, and is used for exchanging heat with the inertia measurement unit; a packaging structure which is used for packaging the inertial measurement unit and the electric heating piece inside; and a heat-conducting medium which isfilled in a gap between the inertial measurement unit and the electric heating piece and does not cover the top surface of the inertial measurement unit. The working temperature of the inertial measurement unit in the inertial measurement module can be maintained in an optimal state, and the pressure borne by the inertial measurement unit is small, so that the measurement accuracy and reliabilityof the inertial measurement unit are improved.
本公开涉及一种惯性测量模组、飞控惯性测量组件及飞行器,该惯性测量模组包括:惯性测量单元,用于测量移动物体的惯性参数;电加热件,与所述惯性测量单元并排间隔设置,用于与所述惯性测量单元进行热交换;封装结构,用于将所述惯性测量单元和所述电加热件封装在其内部;导热介质,填充在所述惯性测量单元和所述电加热件之间的间隙中,且未覆盖所述惯性测量单元的顶面。本公开实施例中的惯性测量模组中的惯性测量单元的工作温度能够维持在最佳状态,且所受的压力小,从而提高惯性测量单元的测量精准度和可靠性。
Inertia measurement module, flight control inertia measurement assembly and aircraft
惯性测量模组、飞控惯性测量组件及飞行器
2021-03-02
Patent
Electronic Resource
Chinese
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |