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公开(公告)号：US11518522B2
公开(公告)日：2022-12-06
申请号：US16662855
申请日：2019-10-24
Applicant: THE BOEING COMPANY
Inventor： Michael L. Trent , Warren A. Atkey
Abstract: An aircraft includes a fuselage defining a cabin region and a crown region. The aircraft also includes a duct disposed within the fuselage. The duct is coupled to one or more drying air vents disposed in the crown region and coupled to one or more cabin vents disposed with the cabin region. The one or more drying air vents are configured to output drying air, received via the duct, into the crown region, and the one or more cabin vents are configured to output conditioned air, received via the duct, into the cabin region. The aircraft further includes one or more valves coupled to the duct and configured to, in a first valve position, route airflow within the duct to the one or more drying air vents and configured to, in a second valve position, route the airflow within the duct to the one or more cabin vents.
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公开(公告)号：US20210122477A1
公开(公告)日：2021-04-29
申请号：US16662855
申请日：2019-10-24
Applicant: THE BOEING COMPANY
Inventor： Michael L. Trent , Warren A. Atkey
IPC: B64D13/08
Abstract: An aircraft includes a fuselage defining a cabin region and a crown region. The aircraft also includes a duct disposed within the fuselage. The duct is coupled to one or more drying air vents disposed in the crown region and coupled to one or more cabin vents disposed with the cabin region. The one or more drying air vents are configured to output drying air, received via the duct, into the crown region, and the one or more cabin vents are configured to output conditioned air, received via the duct, into the cabin region. The aircraft further includes one or more valves coupled to the duct and configured to, in a first valve position, route airflow within the duct to the one or more drying air vents and configured to, in a second valve position, route the airflow within the duct to the one or more cabin vents.
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公开(公告)号：US20210122476A1
公开(公告)日：2021-04-29
申请号：US16662793
申请日：2019-10-24
Applicant: THE BOEING COMPANY
Inventor： Michael L. Trent , Warren A. Atkey
Abstract: An aircraft includes a fuselage defining a cabin region and a crown region. The aircraft also includes a duct disposed within the fuselage. The duct is coupled to one or more drying air vents disposed in the crown region and coupled to one or more cabin vents disposed with the cabin region. The one or more drying air vents are configured to output drying air, received via the duct, into the crown region, and the one or more cabin vents are configured to output conditioned air, received via the duct, into the cabin region. The aircraft further includes one or more valves coupled to the duct and configured to, in a first valve position, route airflow within the duct to the one or more drying air vents and configured to, in a second valve position, route the airflow within the duct to the one or more cabin vents.
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公开(公告)号：US09663233B2
公开(公告)日：2017-05-30
申请号：US14188603
申请日：2014-02-24
Applicant: The Boeing Company
Inventor： Julie K. Plessner , Douglas D. Maben , Daniel F. Lewinski , George A. McEachen , Mark E. Smith , Michael L. Trent , Richard K. Johnson
CPC classification number: B64D13/00 , B64C1/1453 , B64D41/00 , F16L25/026
Abstract: An aircraft comprises composite skin having an opening, and a ventilation conduit having an end portion that extends to the opening in the composite skin. The conduit is made of metal except for the end portion, which functions as an electrical insulator.
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公开(公告)号：US09508970B2
公开(公告)日：2016-11-29
申请号：US14188685
申请日：2014-02-24
Applicant: The Boeing Company
Inventor： Kelly T. Jones , Al R. Carlo , Alan D. Amort , Daniel F. Lewinski , Daniel J. Murray , Douglas D. Maben , Harry H. Ayubi , Howard E. McKenzie , Julie K. Plessner , Kevin S. Callahan , Michael L. Trent , Mike R. Madden , Mohammad M. Malik , Richard K. Johnson , Royal E. Boggs
CPC classification number: H01M2/1241 , H01M2/1016 , H01M2/1072 , H01M2/1094 , H01M2/12 , H01M2/1252 , H01M2200/20 , H01M2220/20
Abstract: An apparatus comprises a rechargeable battery susceptible to thermal runaway, and a metal enclosure for the battery. The enclosure is configured to mitigate battery failure consequences resulting from thermal runaway.
Abstract translation: 一种装置包括易受热失控的可充电电池和用于电池的金属外壳。 外壳配置为减轻热失控造成的电池故障后果。
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Patent Agency Ranking
公开(公告)号：US11858641B2
公开(公告)日：2024-01-02
申请号：US16662793
申请日：2019-10-24
Applicant: THE BOEING COMPANY
Inventor： Michael L. Trent , Warren A. Atkey
CPC classification number: B64D13/08 , B64D13/06 , B64F5/60 , B64D41/00 , B64D2013/064 , B64D2013/0611 , B64D2013/0618 , B64D2013/0655 , B64D2013/0662 , B64D2013/0688
Abstract: An aircraft includes a fuselage defining a cabin region and a crown region. The aircraft also includes a duct disposed within the fuselage. The duct is coupled to one or more drying air vents disposed in the crown region and coupled to one or more cabin vents disposed with the cabin region. The one or more drying air vents are configured to output drying air, received via the duct, into the crown region, and the one or more cabin vents are configured to output conditioned air, received via the duct, into the cabin region. The aircraft further includes one or more valves coupled to the duct and configured to, in a first valve position, route airflow within the duct to the one or more drying air vents and configured to, in a second valve position, route the airflow within the duct to the one or more cabin vents.
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公开(公告)号：US20210055023A1
公开(公告)日：2021-02-25
申请号：US16547258
申请日：2019-08-21
Applicant: The Boeing Company
Inventor： Michael L. Trent , Zachary G. Brown , Chetan B. Megchiani
Abstract: A filter dryer functions bypass system in a vapor cycle machine includes a refrigerant filter/dryer receiving a flow of liquid refrigerant from an inlet line and expelling the liquid refrigerant to an outlet line. A bypass line interconnects the inlet line and the outlet line and a bypass valve is configured to divert a portion or all of the flow of liquid refrigerant from the inlet line into the bypass line. A condition sensor provides a status signal indicative of refrigerant filter dryer condition and the bypass valve is operable responsive to the status signal.
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公开(公告)号：US10734622B2
公开(公告)日：2020-08-04
申请号：US15495436
申请日：2017-04-24
Applicant: The Boeing Company
Inventor： Julie K. Plessner , Douglas D. Maben , Daniel F. Lewinski , George A. McEachen , Mark E. Smith , Michael L. Trent , Richard K. Johnson
Abstract: According to an embodiment, an aircraft comprises a fuselage including composite skin; an enclosure located inside the fuselage; a rechargeable battery disposed inside the enclosure; and a ventilation conduit extending from the enclosure to an opening in the composite skin, the ventilation conduit including: a first portion having a first end coupled to the enclosure and a second end spaced from the composite skin, and a second portion extending between the composite skin and the second end of the first portion, the second portion comprising an electrically non-conductive material.
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公开(公告)号：US20170259937A1
公开(公告)日：2017-09-14
申请号：US15495436
申请日：2017-04-24
Applicant: The Boeing Company
Inventor： Julie K. Plessner , Douglas D. Maben , Daniel F. Lewinski , George A. McEachen , Mark E. Smith , Michael L. Trent , Richard K. Johnson
Abstract: According to an embodiment, an aircraft comprises a fuselage including composite skin; an enclosure located inside the fuselage; a rechargeable battery disposed inside the enclosure; and a ventilation conduit extending from the enclosure to an opening in the composite skin, the ventilation conduit including: a first portion having a first end coupled to the enclosure and a second end spaced from the composite skin, and a second portion extending between the composite skin and the second end of the first portion, the second portion comprising an electrically non-conductive material.
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公开(公告)号：US09614209B2
公开(公告)日：2017-04-04
申请号：US14188683
申请日：2014-02-24
Applicant: The Boeing Company
Inventor： Kelly T. Jones , Alfred R. Carlo , Alan D. Amort , Daniel F. Lewinski , Daniel J. Murray , Douglas D. Maben , Harry H. Ayubi , Craig G. Robotham , Julie K. Plessner , Kevin S. Callahan , Michael L. Trent , Michael R. Madden , Mohammad M. Malik , Richard K. Johnson , Royal E. Boggs , Mehdy Barekatein , Frederic P. Lacaux , Bruce L. Drolen , James C. Russell , John R. Lowell , Thomas P. Barrera , Timothy R. North , Richard P. Lorenz , Matthew J. O'Brien , Nels A. Olson , David C. Shangraw , Mark E. Smith , Jean-Philippe Belieres , George A. McEachen
IPC: H01M2/12 , H01M2/18 , H01M10/48 , H01M2/10 , H01M2/34 , H01M10/625 , H01M10/658 , H01M10/0525 , H01M10/647
CPC classification number: H01M2/1241 , H01M2/1077 , H01M2/12 , H01M2/1229 , H01M2/1252 , H01M2/18 , H01M2/34 , H01M2/348 , H01M10/0525 , H01M10/48 , H01M10/482 , H01M10/486 , H01M10/625 , H01M10/647 , H01M10/658 , H01M2200/00 , H01M2200/10 , H01M2220/20 , Y02E60/122
Abstract: An aircraft comprises a rechargeable battery including an array of battery cells, and means for mitigating consequences of failure of the rechargeable battery due to aircraft operating cycles.
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