-
公开(公告)号：US10124901B2
公开(公告)日：2018-11-13
申请号：US15155079
申请日：2016-05-16
Applicant: The Boeing Company
Inventor： Mark Joseph Clemen, Jr. , Jerry Lee Wert , George Albert Perry , Scott Hutchinson Gardner , Erik Marc Langhofer , Charles Steven Meis
Abstract: A method for detecting an icing condition using an apparatus comprising a piezoelectric material and a vibration detector. The piezoelectric material has a surface proximate to a surface of a vehicle. The piezoelectric material is configured to vibrate. The vibration detector is configured to detect a change in vibrations in the piezoelectric material that indicates a presence of an icing condition on the surface of the piezoelectric material.
-
Patent Agency Ranking
公开(公告)号：US09227733B2
公开(公告)日：2016-01-05
申请号：US13732707
申请日：2013-01-02
Applicant: The Boeing Company
Inventor： Charles Steven Meis , Erik Marc Langhofer
CPC classification number: B64D15/20 , B64D15/22 , G01N1/2202 , G01N1/2214 , G01N15/0227 , G01N2001/2833 , G08B19/02
Abstract: A method and apparatus for detecting an icing condition. The apparatus comprises a sensor system and an icing condition detector. The sensor system is configured to collect drops of water from air on an exterior of an aircraft and generate a number of images of the drops of water collected. The icing condition detector is configured to detect a presence of a number of types of icing conditions for the aircraft using the number of images from the sensor.
Abstract translation: 一种检测结冰条件的方法和装置。 该装置包括传感器系统和结冰条件检测器。 传感器系统被配置为从飞机外部的空气中收集一滴水，并产生一些收集的水滴的图像。 结冰条件检测器被配置为使用来自传感器的图像的数量来检测飞机的多种类型的结冰条件的存在。
-
公开(公告)号：US20160257414A1
公开(公告)日：2016-09-08
申请号：US15155079
申请日：2016-05-16
Applicant: The Boeing Company
Inventor： Mark Joseph Clemen, JR. , Jerry Lee Wert , George Albert Perry , Scott Hutchinson Gardner , Erik Marc Langhofer , Charles Steven Meis
Abstract: A method for detecting an icing condition using an apparatus comprising a piezoelectric material and a vibration detector. The piezoelectric material has a surface proximate to a surface of a vehicle. The piezoelectric material is configured to vibrate. The vibration detector is configured to detect a change in vibrations in the piezoelectric material that indicates a presence of an icing condition on the surface of the piezoelectric material.
Abstract translation: 一种使用包括压电材料和振动检测器的装置检测结冰条件的方法。 压电材料具有靠近车辆表面的表面。 压电材料构造成振动。 振动检测器被配置为检测表示在压电材料的表面上存在结冰条件的压电材料的振动的变化。
-
公开(公告)号：US11912420B2
公开(公告)日：2024-02-27
申请号：US17717202
申请日：2022-04-11
Applicant: THE BOEING COMPANY
Inventor： Edward Charles Natsui , Melissa Marie Bravin , Erik Marc Langhofer
Abstract: A system and method include a first icing detector configured to detect a first icing condition in relation to one or more portions of an aircraft. The first icing detector is configured to output a first icing signal indicative of the first icing condition. A second icing detector is configured to detect a second icing condition in relation to the one or more portions of the aircraft. The second icing detector is configured to output a second icing signal indicative of the second icing condition. A control unit is in communication with the first icing detector and the second icing detector. The control unit is configured to receive the first icing signal from the first icing detector and the second icing signal from the second icing detector. The control unit is further configured to distinguish between presence of supercooled liquid water and ice crystal icing in response to receiving one or both of the first icing signal or the second icing signal.
-
公开(公告)号：US20230322393A1
公开(公告)日：2023-10-12
申请号：US17717202
申请日：2022-04-11
Applicant: THE BOEING COMPANY
Inventor： Edward Charles Natsui , Melissa Marie Bravin , Erik Marc Langhofer
Abstract: A system and method include a first icing detector configured to detect a first icing condition in relation to one or more portions of an aircraft. The first icing detector is configured to output a first icing signal indicative of the first icing condition. A second icing detector is configured to detect a second icing condition in relation to the one or more portions of the aircraft. The second icing detector is configured to output a second icing signal indicative of the second icing condition. A control unit is in communication with the first icing detector and the second icing detector. The control unit is configured to receive the first icing signal from the first icing detector and the second icing signal from the second icing detector. The control unit is further configured to distinguish between presence of supercooled liquid water and ice crystal icing in response to receiving one or both of the first icing signal or the second icing signal.
-
公开(公告)号：US20140184789A1
公开(公告)日：2014-07-03
申请号：US13732707
申请日：2013-01-02
Applicant: THE BOEING COMPANY
Inventor： Charles Steven Meis , Erik Marc Langhofer
IPC: G01N21/84
CPC classification number: B64D15/20 , B64D15/22 , G01N1/2202 , G01N1/2214 , G01N15/0227 , G01N2001/2833 , G08B19/02
Abstract: A method and apparatus for detecting an icing condition. The apparatus comprises a sensor system and an icing condition detector. The sensor system is configured to collect drops of water from air on an exterior of an aircraft and generate a number of images of the drops of water collected. The icing condition detector is configured to detect a presence of a number of types of icing conditions for the aircraft using the number of images from the sensor.
Abstract translation: 一种检测结冰条件的方法和装置。 该装置包括传感器系统和结冰条件检测器。 传感器系统被配置为从飞机外部的空气中收集一滴水，并产生一些收集的水滴的图像。 结冰条件检测器被配置为使用来自传感器的图像的数量来检测飞机的多种类型的结冰条件的存在。
-
-
-
-
-
Search Results
6
records
(took 0.016 seconds)
