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公开(公告)号：US20170240266A1
公开(公告)日：2017-08-24
申请号：US15590693
申请日：2017-05-09
申请人： The Boeing Company
CPC分类号： B64C1/40 , B64C1/38 , B64C30/00 , H01F7/0236
摘要： A thermal insulation system for an aircraft is provided. The thermal insulation system includes a carrier and a container. The carrier has an interior surface including a first plurality of magnets that generate a first magnetic field, and an exterior surface that is thermally coupled to at least one high temperature component. The container is surrounded by the interior surface of the carrier, has an exterior surface including a second plurality of magnets that generate a second magnetic field oriented opposite the first magnetic field, and has an interior surface that is thermally coupled to at least one temperature sensitive component. The first magnetic field and the second magnetic field generate a gap between the carrier and the container to reduce a heat transfer from the at least one high temperature component to the at least one temperature sensitive component during operation of the aircraft.
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公开(公告)号：US20170101170A1
公开(公告)日：2017-04-13
申请号：US14881337
申请日：2015-10-13
申请人： The Boeing Company
CPC分类号： B64C1/38 , B64C30/00 , F41H3/00 , H01F7/0236 , H01F7/0273 , H01F7/064 , H02N15/00
摘要： A thermal insulation system for an aircraft that includes leading surfaces is provided. The thermal insulation system includes a carrier and a container. The carrier has an interior surface that includes a first plurality of magnets that generate a first magnetic field, and an exterior surface that is thermally coupled to the leading surfaces of the aircraft. The container is surrounded by the interior surface of the carrier, has an exterior surface including a second plurality of magnets that generate a second magnetic field oriented opposite the first magnetic field, and has an interior that includes electronics. The first magnetic field and the second magnetic field generate a gap between the carrier and the container to reduce a heat transfer from the leading surfaces to the electronics during operation of the aircraft.
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公开(公告)号：US10124901B2
公开(公告)日：2018-11-13
申请号：US15155079
申请日：2016-05-16
申请人： The Boeing Company
发明人： Mark Joseph Clemen, Jr. , Jerry Lee Wert , George Albert Perry , Scott Hutchinson Gardner , Erik Marc Langhofer , Charles Steven Meis
摘要： 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.
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公开(公告)号：US20160257414A1
公开(公告)日：2016-09-08
申请号：US15155079
申请日：2016-05-16
申请人： The Boeing Company
发明人： Mark Joseph Clemen, JR. , Jerry Lee Wert , George Albert Perry , Scott Hutchinson Gardner , Erik Marc Langhofer , Charles Steven Meis
摘要： 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.
摘要翻译： 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。
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公开(公告)号：US09758235B2
公开(公告)日：2017-09-12
申请号：US14881337
申请日：2015-10-13
申请人： The Boeing Company
CPC分类号： B64C1/38 , B64C30/00 , F41H3/00 , H01F7/0236 , H01F7/0273 , H01F7/064 , H02N15/00
摘要： A thermal insulation system for an aircraft that includes leading surfaces is provided. The thermal insulation system includes a carrier and a container. The carrier has an interior surface that includes a first plurality of magnets that generate a first magnetic field, and an exterior surface that is thermally coupled to the leading surfaces of the aircraft. The container is surrounded by the interior surface of the carrier, has an exterior surface including a second plurality of magnets that generate a second magnetic field oriented opposite the first magnetic field, and has an interior that includes electronics. The first magnetic field and the second magnetic field generate a gap between the carrier and the container to reduce a heat transfer from the leading surfaces to the electronics during operation of the aircraft.
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