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发明申请
US20070186672A1 Integrated Sensor For Airfoils of Aircraft, Particularly Of Airplanes and Helicopters, As Well As Rotor Blades and Airplane Airfoil 失效
飞机，特别是飞机和直升机的翼型集成传感器，以及转子叶片和飞机机翼

Integrated Sensor For Airfoils of Aircraft, Particularly Of Airplanes and Helicopters, As Well As Rotor Blades and Airplane Airfoil
摘要：
An integratable sensor for an airfoil of an aircraft such as an airplane and a helicopter comprises a sensor capsule, in whose inner chamber a measuring element for measuring an environmental parameter is situated. A capsule carrier is implemented to accommodate and removably attach the sensor capsule and is integratable in an airfoil of an airplane or a helicopter. Elastic contact elements are used for secure electrical connection of the sensor capsule to the capsule carrier. The sensor capsule is replaceable, while the capsule carrier is permanently integrated in the airfoil, in particular in a rotor blade. The measuring element is, for example, a pressure sensor.
摘要（中）：

用于诸如飞机和直升机的飞机的翼型的可整合传感器包括传感器胶囊，其内室中设置有用于测量环境参数的测量元件。 实施胶囊载体以容纳和可移除地附接传感器囊，并且可与飞机或直升机的翼型集成。 弹性接触元件用于传感器胶囊与胶囊载体的牢固电连接。 传感器胶囊是可替换的，而胶囊载体永久地集成在翼型件中，特别是在转子叶片中。 测量元件例如是压力传感器。

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