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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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公开(公告)号:US11739973B2
公开(公告)日:2023-08-29
申请号:US16105864
申请日:2018-08-20
Applicant: THE BOEING COMPANY
Inventor: Bryce A. Vandyke , John Erik West , Douglas D. Maben , Andrew K. Fung , David R. C. Cannal
CPC classification number: F24F13/0263 , B64D2013/0603 , F24F13/0245 , F24F13/0281 , F24F2013/242
Abstract: A duct includes a rigid air-permeable tube of composite material. The duct also includes a layer of insulation coupled to an exterior surface of the rigid air-permeable tube. The duct further includes a non-rigid insulation layer in contact with the layer of insulation. The non-rigid insulation layer forms an air-impermeable duct wall.
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公开(公告)号:US11712872B2
公开(公告)日:2023-08-01
申请号:US16105837
申请日:2018-08-20
Applicant: THE BOEING COMPANY
Inventor: Douglas D. Maben , Bryce A. Vandyke , Mark M. Gmerek , David R. C. Cannal
IPC: F16L9/21 , B29C44/18 , B32B5/18 , B29C70/30 , B29C70/54 , B29D23/00 , B64D13/06 , G10K11/168 , B29K105/04
CPC classification number: B32B5/18 , B29C44/18 , B29C70/30 , B29C70/545 , B29D23/001 , B64D13/06 , F16L9/21 , G10K11/168 , B29K2105/04 , B29K2995/0002 , B64D2013/0625
Abstract: A duct includes a foam-filled honeycomb core structure having a tubular shape. The duct further includes an air-impermeable duct wall coupled to an exterior surface of the foam-filled honeycomb core structure.
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14.
公开(公告)号:US20230010222A1
公开(公告)日:2023-01-12
申请号:US17373453
申请日:2021-07-12
Applicant: The Boeing Company
Inventor: Bryce A. Vandyke , Douglas D. Maben , Dale Hastings , Mark M. Gmerek , Xin Han
IPC: F16L55/033 , F16L55/035 , B64D13/06
Abstract: Described herein are noise attenuating ducts and vehicles using these ducts for environmental control systems. A duct comprises an exoskeleton structure and a sound-absorbing structure, disposed within and conforming to the exoskeleton structure. The exoskeleton structure provides external mechanical support to the sound-absorbing structure thereby helping to maintain the tubular shape of the sound-absorbing structure. This external support does not interfere with the airflow inside the sound-absorbing structure. Furthermore, the external positioning of the exoskeleton structure allows the integration of various support mounting features for the installation of the duct in a vehicle. In some examples, the exoskeleton structure comprises a plurality of enclosed openings to reduce the weight of the exoskeleton structure and provide additional flexibility. Furthermore, additive manufacturing of the exoskeleton structure allows achieving a monolithic structure with various features and characteristics described above.
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公开(公告)号:US11112808B2
公开(公告)日:2021-09-07
申请号:US16456898
申请日:2019-06-28
Applicant: The Boeing Company
Inventor: Tuan Q. Vu , Chao-Hsin Lin , Taylor Goodwin , Douglas D. Maben , Gary A. Pearson
IPC: F16L55/027 , G05D7/01 , F16L55/07
Abstract: A fluid flow restrictor device for controlling fluid flow at a connection between ducts may include a restrictor device body that is partially or fully inserted into and disposed within one of the ducts and an outboard restrictor device flange extending radially outward at an outboard end of the restrictor device body and having an outboard flange outer diameter that is greater than an inner diameter of the ducts so that the restrictor device body or the outboard restrictor device flange is engaged by an open end surface of the duct to prevent full insertion of the fluid flow restrictor device into the duct. A body inner surface defines a restrictor opening through the restrictor device body that can be varied to achieve desired fluid flow characteristics at the connection.
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公开(公告)号:US20230358433A1
公开(公告)日:2023-11-09
申请号:US18346447
申请日:2023-07-03
Applicant: The Boeing Company
Inventor: Bryce A. Vandyke , John Erik West , Douglas D. Maben , Andrew K. Fung , David R.C. Cannal
IPC: F24F13/02
CPC classification number: F24F13/0263 , F24F2013/242
Abstract: A duct includes a rigid air-permeable tube of composite material. The duct also includes a layer of insulation coupled to an exterior surface of the rigid air-permeable tube. The duct further includes a non-rigid insulation layer in contact with the layer of insulation. The non-rigid insulation layer forms an air-impermeable duct wall.
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公开(公告)号:US11378216B2
公开(公告)日:2022-07-05
申请号:US16599419
申请日:2019-10-11
Applicant: The Boeing Company
Inventor: Bryce A. Vandyke , Douglas D. Maben , Luis J. Sanchez , Timothy Chiu
IPC: F16L57/00 , F16L55/115 , B65D59/06
Abstract: A cap for closing an open end of a duct tube has a cylindrical side wall having a length between a closed end and an open end of the side wall. An end wall extends across the closed end of the side wall. A conical section of the side wall extends outwardly from the open end of the side wall and has an interior surface configured to guide an end of a duct tube into a hollow interior volume of the side wall. A groove in an interior surface of the side wall is configured to receive a bead around an end of a duct tube inserted through the conical section and into the hollow interior of the side wall. A plurality of pull tabs extend outwardly from the conical section and are configured to be manually pulled, pulling the cap over the end of the duct tube.
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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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19.
公开(公告)号:US20200056727A1
公开(公告)日:2020-02-20
申请号:US16105837
申请日:2018-08-20
Applicant: THE BOEING COMPANY
Inventor: Douglas D. Maben , Bryce A. Vandyke , Mark M. Gmerek , David R. C. Cannal
Abstract: A duct includes a foam-filled honeycomb core structure having a tubular shape. The duct further includes an air-impermeable duct wall coupled to an exterior surface of the foam-filled honeycomb core structure.
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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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