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公开(公告)号：US09897100B2
公开(公告)日：2018-02-20
申请号：US14688484
申请日：2015-04-16
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Daniel J. Laboda , Richard Rateick , Christopher Gedeon , Gary A. Valencourt
CPC classification number: F04D29/2288 , B01D19/0068 , B01D19/0073 , B01D19/0094 , B01D45/12 , B01D45/14 , B04B5/12 , B04B2005/125 , F01M2013/0422 , F04D31/00
Abstract: An in-line continuous flow liquid-gas separator-pump includes a housing, a rotor, a plurality of tubular flow passages, and a plurality of gas flow passages. The rotor includes a rotor first end, a rotor second end, an outer surface, and an inner surface that defines an inner chamber in fluid communication with the purge gas outlet. The tubular flow passages are formed in the rotor and extend between the rotor first end and the rotor second end. Each tubular flow passage includes a fluid inlet that is disposed adjacent the rotor first end and in fluid communication with the liquid/gas inlet, and a fluid outlet that is disposed adjacent the rotor second end and is in fluid communication with the liquid outlet. The gas flow passages are formed in the rotor, and each provides fluid communication between one of the tubular flow passages and the inner chamber.
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公开(公告)号：US20160305440A1
公开(公告)日：2016-10-20
申请号：US14688484
申请日：2015-04-16
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Daniel J. Laboda , Richard Rateick , Christopher Gedeon , Gary A. Valencourt
CPC classification number: F04D29/2288 , B01D19/0068 , B01D19/0073 , B01D19/0094 , B01D45/12 , B01D45/14 , B04B5/12 , B04B2005/125 , F01M2013/0422 , F04D31/00
Abstract: An in-line continuous flow liquid-gas separator-pump includes a housing, a rotor, a plurality of tubular flow passages, and a plurality of gas flow passages. The rotor includes a rotor first end, a rotor second end, an outer surface, and an inner surface that defines an inner chamber in fluid communication with the purge gas outlet. The tubular flow passages are formed in the rotor and extend between the rotor first end and the rotor second end. Each tubular flow passage includes a fluid inlet that is disposed adjacent the rotor first end and in fluid communication with the liquid/gas inlet, and a fluid outlet that is disposed adjacent the rotor second end and is in fluid communication with the liquid outlet. The gas flow passages are formed in the rotor, and each provides fluid communication between one of the tubular flow passages and the inner chamber.
Abstract translation: 在线连续流动液气分离器泵包括壳体，转子，多个管状流动通道和多个气体流动通道。 转子包括转子第一端，转子第二端，外表面和限定与吹扫气体出口流体连通的内室的内表面。 管状流动通道形成在转子中并在转子第一端和转子第二端之间延伸。 每个管状流动通道包括设置在转子第一端附近并与液体/气体入口流体连通的流体入口以及与转子第二端相邻并且与液体出口流体连通的流体出口。 气流通道形成在转子中，并且各自提供一个管状流动通道和内部腔室之间的流体连通。
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Patent Agency Ranking
公开(公告)号：US10197178B2
公开(公告)日：2019-02-05
申请号：US15440460
申请日：2017-02-23
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Richard Rateick , Donna Laboda
Abstract: A vibration-resistant, flexible metallic seal for use in an electrohydraulic servo valve (EHSV), the EHSV comprising an armature, an armature support comprising a base, and a flapper, the seal surrounding a portion of the flapper, the seal having a first end, a second end, a thickness along a length of the seal between the first end and the second end, the thickness being defined between first and second outer surfaces of the seal, and one or a plurality of convolutions between the first end and the second end, the first end disposed between and hermetically connected to the flapper and the armature, the second end disposed within the first opening and hermetically connected to the base, wherein the seal comprises: a non-porous metal that comprises a first fraction of the thickness; a porous metal comprising a plurality of pores that comprises a second fraction of the thickness; and an elastomeric material encompassed by the pores of the second fraction of the thickness, wherein the second fraction comprises one or both of the first and second outer surfaces of the seal.
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公开(公告)号：US09678029B2
公开(公告)日：2017-06-13
申请号：US14466714
申请日：2014-08-22
Applicant: Honeywell International Inc.
Inventor： Richard Rateick
CPC classification number: G01N27/12 , B60T17/18 , B60T17/22 , B64D45/00 , F16D66/00 , G01N27/06 , G01N27/20
Abstract: The exposure of an aircraft component to an oxidation catalyst, such as a deicing solution, may be detected with the aid of an electrical conductivity sensor. In some examples, a system includes an aircraft component, an electrical conductivity sensor mechanically connected to the aircraft component and configured to generate an output, and a processor configured to detect an oxidation catalyst exposure event based on the output generated by the electrical conductivity sensor. The electrical conductivity sensor may be configured and positioned to generate a signal indicative of electrical conductivity of a substance to which the aircraft component is exposed. The processor may be configured to detect an oxidation catalyst exposure event by at least determining whether the electrical conductivity indicated by the signal is greater than or equal to a predetermined conductivity threshold value.
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公开(公告)号：US20170254432A1
公开(公告)日：2017-09-07
申请号：US15440460
申请日：2017-02-23
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Richard Rateick , Donna Laboda
CPC classification number: F16K31/041 , F15B13/0438 , F16J15/52 , F16K31/0682 , H01F7/128 , H01F7/14
Abstract: A vibration-resistant, flexible metallic seal for use in an electrohydraulic servo valve (EHSV), the EHSV comprising an armature, an armature support comprising a base, and a flapper, the seal surrounding a portion of the flapper, the seal having a first end, a second end, a thickness along a length of the seal between the first end and the second end, the thickness being defined between first and second outer surfaces of the seal, and one or a plurality of convolutions between the first end and the second end, the first end disposed between and hermetically connected to the flapper and the armature, the second end disposed within the first opening and hermetically connected to the base, wherein the seal comprises: a non-porous metal that comprises a first fraction of the thickness; a porous metal comprising a plurality of pores that comprises a second fraction of the thickness; and an elastomeric material encompassed by the pores of the second fraction of the thickness, wherein the second fraction comprises one or both of the first and second outer surfaces of the seal.
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公开(公告)号：US20160054249A1
公开(公告)日：2016-02-25
申请号：US14466714
申请日：2014-08-22
Applicant: Honeywell International Inc.
Inventor： Richard Rateick
CPC classification number: G01N27/12 , B60T17/18 , B60T17/22 , B64D45/00 , F16D66/00 , G01N27/06 , G01N27/20
Abstract: The exposure of an aircraft component to an oxidation catalyst, such as a deicing solution, may be detected with the aid of an electrical conductivity sensor. In some examples, a system includes an aircraft component, an electrical conductivity sensor mechanically connected to the aircraft component and configured to generate an output, and a processor configured to detect an oxidation catalyst exposure event based on the output generated by the electrical conductivity sensor. The electrical conductivity sensor may be configured and positioned to generate a signal indicative of electrical conductivity of a substance to which the aircraft component is exposed. The processor may be configured to detect an oxidation catalyst exposure event by at least determining whether the electrical conductivity indicated by the signal is greater than or equal to a predetermined conductivity threshold value.
Abstract translation: 借助于电导率传感器，可以检测飞机部件暴露于氧化催化剂如除冰溶液。 在一些示例中，系统包括飞行器部件，机械地连接到飞行器部件并被配置为产生输出的电导率传感器，以及被配置为基于由电导率传感器产生的输出来检测氧化催化剂暴露事件的处理器。 电导率传感器可以被配置和定位成产生指示飞机部件暴露于的物质的导电性的信号。 处理器可以被配置为通过至少确定由信号指示的电导率是否大于或等于预定电导率阈值来检测氧化催化剂暴露事件。
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7.发明申请公开(公告)号：US20150251960A1
公开(公告)日：2015-09-10
申请号：US14198179
申请日：2014-03-05
Applicant: Honeywell International Inc.
Inventor： Stephen Yates , Mark E. Behnke , Mark L. La Forest , Richard Rateick
CPC classification number: C04B38/0067 , B32B18/00 , B32B2262/106 , B32B2307/72 , C04B35/83 , C04B38/0032 , C04B2111/00362 , C04B2235/48 , C04B2235/5248 , F16D65/12 , F16D65/126 , F16D69/023 , F16D2200/0047 , F16D2200/0091 , Y10T428/30
Abstract: In one example, a method for forming a densified carbon-carbon composite material comprises infiltrating a carbon fiber preform with a monomer mixture for a condensed polynuclear aromatic (COPNA) resin; polymerizing and crosslinking the monomer mixture within the carbon fiber preform to form a crosslinked COPNA by subsequently heating the carbon fiber preform infiltrated with the monomer mixture to a polymerization temperature of the COPNA resin; and carbonizing the crosslinked COPNA resin within the carbon fiber preform by heating the crosslinked COPNA resin to a carbonization temperature to form the densified carbon-carbon composite material, wherein the carbonization temperature is greater than the polymerization temperature.
Abstract translation: 在一个实例中，用于形成致密化的碳 - 碳复合材料的方法包括用缩合多核芳族（COPNA）树脂的单体混合物渗透碳纤维预成型体; 聚合和交联碳纤维预型体内的单体混合物以通过随后将被单体混合物渗透的碳纤维预型体加热到COPNA树脂的聚合温度来形成交联的COPNA; 并且通过将交联的COPNA树脂加热至碳化温度来将交联的COPNA树脂碳化在碳纤维预制件内，以形成致密的碳 - 碳复合材料，其中碳化温度大于聚合温度。
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