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公开(公告)号：US10220579B2
公开(公告)日：2019-03-05
申请号：US15884138
申请日：2018-01-30
Applicant: The Boeing Company
Inventor： Andrew M. Hopkins , Donald J. Sutkus , James M. Kestner , Jennifer S. Noel , Robert J. Miller , Marc R. Matsen , Christopher J. Hottes , Mark E. King , Darren R. Walker
Abstract: A processing apparatus such as a heating and/or debulking apparatus that may be used to debulk a plurality of uncured composite layers to form an article such as an aircraft component may include a plurality of interconnected smart susceptor heater blankets. The plurality of smart susceptor heater blankets may be connected in series or in parallel, and may be controlled to uniformly heat the component during formation.
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公开(公告)号：US09914269B2
公开(公告)日：2018-03-13
申请号：US15056783
申请日：2016-02-29
Applicant: The Boeing Company
Inventor： Andrew M. Hopkins , Donald J. Sutkus , James M. Kestner , Jennifer S. Noel , Robert J. Miller , Marc R. Matsen , Christopher J. Hottes , Mark E. King , Darren R. Walker
CPC classification number: B29C70/342 , B29C2035/0811 , B29C2035/0816 , B29K2105/089 , B29L2031/3076 , H05B3/34 , H05B6/105 , H05B2203/003 , H05B2203/007 , H05B2206/023 , Y02T50/43
Abstract: A processing apparatus such as a heating and/or debulking apparatus that may be used to debulk a plurality of uncured composite layers to form an article such as an aircraft component may include a plurality of interconnected smart susceptor heater blankets. The plurality of smart susceptor heater blankets may be connected in series or in parallel, and may be controlled to uniformly heat the component during formation.
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公开(公告)号：US20170135157A1
公开(公告)日：2017-05-11
申请号：US14937511
申请日：2015-11-10
Applicant: The Boeing Company
Inventor： Robert J. Miller , John F. Spalding, JR. , Diane C. Rawlings , Darrell M. Storvick , Christopher J. Hottes
CPC classification number: H05B3/36 , H05B1/0272 , H05B6/105 , H05B2206/023
Abstract: A heating blanket is disclosed. The heating blanket may include a thermoplastic matrix configured to become conformable at a predetermined temperature, a conductor embedded in the thermoplastic matrix and configured to receive electrical current and generate a magnetic field in response to the electrical current, and a plurality of susceptors embedded in the thermoplastic matrix and composed of a magnetic material having a Curie point.
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公开(公告)号：US20150246730A1
公开(公告)日：2015-09-03
申请号：US14195091
申请日：2014-03-03
Applicant: The Boeing Company
Inventor： Vyacheslav Khozikov , Robert J. Miller , Rangasamy Elangovan , Marc R. Matsen , Stephen R. Amorosi , Robert G. Albers , Michael Strasik , John R. Hull
IPC: B64D15/12
Abstract: A system and method for operating an ice detection and deicing system are provided herein. The ice detection and deicing system may use changing magnetic properties of various components caused by temperature changes to detect conditions conducive to, or indicating, ice formation. The ice detection and deicing system may further use eddy currents induced in one or more layers of the system to increase the temperature of the one or more layers to reduce the amount of ice formation or reduce the probability of ice being formed.
Abstract translation: 本文提供了一种用于操作冰检测和除冰系统的系统和方法。 冰检测和除冰系统可以使用由温度变化引起的各种部件的变化的磁性，以检测有利于或指示冰的形成。 冰检测和除冰系统可以进一步使用在系统的一个或多个层中感应的涡流来增加一个或多个层的温度，以减少冰的形成量或降低形成冰的可能性。
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15.发明申请AIRCRAFT STRUCTURES BONDED WITH ADHESIVE INCLUDING MAGNETOSTRICTIVE MATERIAL 审中-公开与粘合剂结合的飞机结构，包括磁性材料公开(公告)号：US20140023837A1
公开(公告)日：2014-01-23
申请号：US13732270
申请日：2012-12-31
Applicant: THE BOEING COMPANY
Inventor： Robert J. Miller , Diane C. Rawlings , Kenneth A. Krienke , James H. Mabe , Robert T. Ruggeri , Dan J. Clingman
IPC: B64C7/00
CPC classification number: B64C7/00 , B29C65/48 , B29C65/4815 , B29C65/483 , B29C65/4855 , B29C65/4865 , B29C65/4875 , B29C65/8253 , B29C65/8284 , B29C66/721 , B29C70/88 , B29K2101/10 , B29K2101/12 , B29K2105/16 , B29K2503/06 , B29K2705/00 , B29K2705/12 , B29K2995/0003 , B29K2995/0008 , B29L2031/3082 , B29L2031/3085 , B64C1/06 , B64C1/12 , B64D2045/0085 , B64F5/60 , C09J5/00 , C09J9/00 , C09J11/00 , G01L1/12 , G01M5/0016 , G01M5/0041 , G01M5/0091 , G01N29/2412 , Y02T50/43 , Y10T156/10 , Y10T428/24851 , Y10T428/31529 , Y10T442/10
Abstract: First and second aircraft structures are bonded together with an adhesive including strain-sensitive magnetostrictive material. The magnetostrictive material has a magnetomechanical coefficient greater than e−5.
Abstract translation: 第一和第二飞行器结构用包括应变敏感的磁致伸缩材料的粘合剂粘合在一起。 磁致伸缩材料的磁机械系数大于e-5。
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Patent Agency Ranking
公开(公告)号：US11452178B2
公开(公告)日：2022-09-20
申请号：US14937511
申请日：2015-11-10
Applicant: The Boeing Company
Inventor： Robert J. Miller , John F. Spalding, Jr. , Diane C. Rawlings , Darrell M. Storvick , Christopher J. Hottes
Abstract: A heating blanket is disclosed. The heating blanket may include a thermoplastic matrix configured to become conformable at a predetermined temperature, a conductor embedded in the thermoplastic matrix and configured to receive electrical current and generate a magnetic field in response to the electrical current, and a plurality of susceptors embedded in the thermoplastic matrix and composed of a magnetic material having a Curie point.
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公开(公告)号：US20180147794A1
公开(公告)日：2018-05-31
申请号：US15884138
申请日：2018-01-30
Applicant: The Boeing Company
Inventor： Andrew M. Hopkins , Donald J. Sutkus , James M. Kestner , Jennifer S. Noel , Robert J. Miller , Marc R. Matsen , Christopher J. Hottes , Mark E. King , Darren R. Walker
CPC classification number: B29C70/342 , B29C2035/0811 , B29C2035/0816 , B29K2105/089 , B29L2031/3076 , H05B3/34 , H05B6/105 , H05B2203/003 , H05B2203/007 , H05B2206/023 , Y02T50/43
Abstract: A processing apparatus such as a heating and/or debulking apparatus that may be used to debulk a plurality of uncured composite layers to form an article such as an aircraft component may include a plurality of interconnected smart susceptor heater blankets. The plurality of smart susceptor heater blankets may be connected in series or in parallel, and may be controlled to uniformly heat the component during formation.
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公开(公告)号：US20170246817A1
公开(公告)日：2017-08-31
申请号：US15056783
申请日：2016-02-29
Applicant: The Boeing Company
Inventor： Andrew M. Hopkins , Donald J. Sutkus , James M. Kestner , Jennifer S. Noel , Robert J. Miller , Marc R. Matsen , Christopher J. Hottes , Mark E. King , Darren R. Walker
CPC classification number: B29C70/342 , B29C2035/0811 , B29C2035/0816 , B29K2105/089 , B29L2031/3076 , H05B3/34 , H05B6/105 , H05B2203/003 , H05B2203/007 , H05B2206/023 , Y02T50/43
Abstract: A processing apparatus such as a heating and/or debulking apparatus that may be used to debulk a plurality of uncured composite layers to form an article such as an aircraft component may include a plurality of interconnected smart susceptor heater blankets. The plurality of smart susceptor heater blankets may be connected in series or in parallel, and may be controlled to uniformly heat the component during formation.
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公开(公告)号：US20170246815A1
公开(公告)日：2017-08-31
申请号：US15056297
申请日：2016-02-29
Applicant: The Boeing Company
Inventor： James M. Kestner , Marc R. Matsen , Scott D. Billings , John A. Mittleider , Robert J. Miller
CPC classification number: B29C70/342 , B29C35/0805 , B29C73/10 , B29C73/34 , B29C2035/0811 , B29C2035/0816 , B29K2105/089 , B29L2031/3076 , H05B3/34 , H05B2203/003 , H05B2203/007 , H05B2203/014
Abstract: A processing apparatus such as a heating and/or debulking apparatus that may be used to debulk a plurality of uncured composite layers to form an article such as an aircraft component may include a plurality of interconnected smart susceptor heater blankets. The plurality of smart susceptor heater blankets may be connected in series or in parallel, and may be controlled to uniformly heat the component during formation.
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公开(公告)号：US20160122025A1
公开(公告)日：2016-05-05
申请号：US14526972
申请日：2014-10-29
Applicant: The Boeing Company
Inventor： John R. Hull , Vyacheslav Khozikov , Robert J. Miller , Stephen R. Amorosi , Rangasamy Elangovan
CPC classification number: B64D15/12 , H05B6/04 , H05B6/105 , H05B6/36 , H05B6/38 , H05B6/40 , H05B6/44 , H05B2214/02
Abstract: An induction heating system employs a ferromagnetic susceptor mounted proximate an exterior of flight surface of an aircraft. At least one electrically conductive coil is mounted proximate the ferromagnetic susceptor. The at least one electrically conductive coil is powered by a first power source with a first frequency. At least one compensating coil is mounted proximate the ferromagnetic susceptor having a geometry determined to provide substantially net-zero flux with respect to the at least one electrically conductive coil and positioned to induce induction heating where the first plurality of electrically conductive coils lacks induced inductive heating coverage. The at least one compensating coils is powered by a second AC power source with a second frequency.
Abstract translation: 感应加热系统采用安装在飞行器飞行表面外部的铁磁基座。 至少一个导电线圈安装在铁磁基座附近。 至少一个导电线圈由具有第一频率的第一电源供电。 至少一个补偿线圈安装在铁磁基座附近，其几何形状被确定为相对于至少一个导电线圈提供基本上净零的通量并被定位成诱导感应加热，其中第一组多个导电线圈缺少感应感应加热 覆盖面 至少一个补偿线圈由具有第二频率的第二AC电源供电。
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