-
公开(公告)号：US20160167792A1
公开(公告)日：2016-06-16
申请号：US14958994
申请日：2015-12-04
Applicant: United Technologies Corporation
Inventor： Michael D. Greenberg , Zhijun Zheng , David Baszak , Scott W. Simpson
Abstract: An anti-icing system for an aircraft structure includes a cavity that has an exterior surface subject to ice accretion and a bleed source that is configured to provide a fluid to the cavity via a duct. The system includes multiple temperature sensors, disposed at the aircraft structure, with each temperature sensor configured to detect a temperature associated with an aircraft structure location. A controller is in communication with the temperature sensors. The controller is programmed to compare outputs of the temperature sensors and to determine a temperature sensor fault condition.
Abstract translation: 用于飞行器结构的防冰系统包括具有经受积冰的外表面的空腔和被配置为经由导管向腔体提供流体的排泄源。 该系统包括设置在飞机结构处的多个温度传感器，每个温度传感器被配置成检测与飞行器结构位置相关联的温度。 控制器与温度传感器通信。 控制器被编程为比较温度传感器的输出并确定温度传感器故障状况。
-
公开(公告)号：US10421551B2
公开(公告)日：2019-09-24
申请号：US14958994
申请日：2015-12-04
Applicant: United Technologies Corporation
Inventor： Michael D. Greenberg , Zhijun Zheng , David Baszak , Scott W. Simpson
Abstract: An anti-icing system for an aircraft structure includes a cavity that has an exterior surface subject to ice accretion and a bleed source that is configured to provide a fluid to the cavity via a duct. The system includes multiple temperature sensors, disposed at the aircraft structure, with each temperature sensor configured to detect a temperature associated with an aircraft structure location. A controller is in communication with the temperature sensors. The controller is programmed to compare outputs of the temperature sensors and to determine a temperature sensor fault condition.
-
Search Results
2
records
(took 0.009 seconds)
