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公开(公告)号：US12110115B2
公开(公告)日：2024-10-08
申请号：US17348429
申请日：2021-06-15
申请人： The Boeing Company
发明人： Douglas D. Maben
CPC分类号： B64D13/06 , B64D11/06 , B64D2013/003 , B64D2013/0651
摘要： Methods and apparatus to direct ventilation of vehicle occupants are disclosed. A disclosed example apparatus includes an air supply duct of a cabin of a vehicle, a manifold fluidly coupled to the air supply duct, the manifold to extend to occupant seats of the cabin, and nozzles fluidly coupled to the manifold, the nozzles to be positioned to face toward a front of a face of an occupant when the occupant occupies one of the occupant seats.
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2.发明公开公开(公告)号：US20240271715A1
公开(公告)日：2024-08-15
申请号：US18211247
申请日：2023-06-17
发明人： Laurent L’EMEILLAT , Eric LAFOND , Raphael VILAMOT
CPC分类号： F16K31/046 , F16K37/0041 , B64D13/00
摘要： The invention relates to a fluid system of an aircraft comprising at least one flow conduit for a fluid, at least one electric valve (30, 40, 50) for regulating the flow of fluid in said fluid conduit by movement of a regulating member in said fluid conduit, a central computer (20) configured to be able to issue control instructions to each electric regulating valve (30, 40, 50) depending on the in-flight conditions of said aircraft, and an electric circuit (60) for powering said computer and each electric regulating valve, characterized in that at least one electric regulating valve, referred to as smart valve, is equipped with an integrated actuator connected to the central computer and/or to another smart valve of the fluid system by at least one multiplexed data communications bus (22, 24, 42, 44).
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公开(公告)号：US12049323B2
公开(公告)日：2024-07-30
申请号：US17368137
申请日：2021-07-06
申请人： The Boeing Company
发明人： Douglas Dean Maben
CPC分类号： B64D13/02 , B64D11/003 , B64D2013/003
摘要： An aircraft including a fuselage having a side wall at least partially defining a passenger cabin and a crown section of the aircraft. The passenger cabin includes an overhead zone, a passenger zone, and a floor zone. An air supply duct is positioned within the crown section, and the air supply duct is configured to pressurize the crown section with air. At least one return air outlet is defined in the floor zone. An interior structure is coupled to the side wall and extends between the passenger cabin and the crown section. The interior structure includes a plurality of nozzles oriented to discharge the pressurized air from the crown section along an airflow path that extends downward through the overhead zone, downward through the passenger zone, and then towards the at least one return air outlet.
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公开(公告)号：US20240246679A1
公开(公告)日：2024-07-25
申请号：US18191713
申请日：2023-03-28
申请人： B/E Aerospace, Inc.
发明人： Sambasiva Rao Kodati
CPC分类号： B64D13/00 , B60H1/00828 , B60H1/00871 , B60H1/3421 , B60H1/345 , B64F5/10 , F24F9/00 , B60H2001/3478 , B64D2013/003 , F24F2009/002
摘要： A gasper module for use in an aircraft. The gasper module including an inlet configured to receive intake air and a first outlet configured to direct a stream of an airflow from the intake air towards a passenger. Also, a second outlet configured to form an air curtain from the intake air between the passenger receiving the direct stream of airflow and an adjacent passenger.
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公开(公告)号：US20240217662A1
公开(公告)日：2024-07-04
申请号：US18532378
申请日：2023-12-07
发明人： Jens LOHMAR
IPC分类号： B64D13/00
CPC分类号： B64D13/00
摘要： A method for using an air distribution system in a fuselage, comprising the following method steps: providing an air distribution system which has an air distribution line, which is formed at least in part from a fluid-tight and flexible material, wherein the air distribution line is configured to switch from a first state in which the flexible material is substantially taut to a second state in which the flexible material is substantially slack, arranging the air distribution line in a place of installation in the fuselage, occupying the first state of the air distribution line in order to operate the air distribution system, or occupying the second state of the air distribution line in order to carry out maintenance in a spatial region near the place of installation.
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公开(公告)号：US11910547B2
公开(公告)日：2024-02-20
申请号：US17421931
申请日：2020-01-14
CPC分类号： H05K5/0213 , B64D13/00
摘要： A protection device for an electrical cabinet is divided into a plurality of compartments, the protection device including a rain guard and an air manifold formed as an integral unit. The rain guard is designed to cover a section of an electrical cabinet and thus prevent water from falling on it. The air manifold includes at least one first pipe fluidically connected to a second pipe. Each first pipe intended to be connected to a corresponding air-circulation opening of a compartment, and the second pipe being intended to be connected to an air-circulation means in order thus to allow air to be circulated in the plurality of compartments. A cabinet is provided with such a protection device.
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公开(公告)号：US11884403B2
公开(公告)日：2024-01-30
申请号：US17361075
申请日：2021-06-28
申请人： The Boeing Company
发明人： Timothy D. Pattee , William C. Haas
CPC分类号： B64D13/00 , B05B1/044 , B64D2013/003
摘要： Air distribution nozzles, aircraft that include air distribution nozzles, and/or methods of utilizing air distribution nozzles are disclosed herein. The air distribution nozzles include an elongate inlet chamber, an elongate outlet chamber, a tapered elongate slot, an inlet port into the elongate inlet chamber, and an elongate outlet port from the elongate outlet chamber. The elongate inlet chamber extends along an inlet chamber length. The elongate outlet chamber extends along the inlet chamber length. The tapered elongate slot extends between, and fluidly interconnects, the elongate inlet chamber and the elongate outlet chamber. The inlet port is configured to receive an inlet fluid flow along an inlet flow axis. The elongate outlet port is configured to discharge an outlet fluid flow along an outlet flow axis that is oriented at a skew angle relative to the inlet flow axis.
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公开(公告)号：US11879787B2
公开(公告)日：2024-01-23
申请号：US17064105
申请日：2020-10-06
发明人： James Allen Varnell
IPC分类号： H01B13/00 , H01B13/004 , H01B13/016 , H01B13/22 , G01K11/06 , B64D13/00 , G01K3/00
CPC分类号： G01K11/06 , B64D13/00 , G01K3/005 , H01B13/00 , H01B13/004 , H01B13/016 , H01B13/22
摘要： Disclosed is a heat sensor cable having: a conductor defining a conductor first end and a conductor body extending by a first longitudinal span from the conductor first end to a conductor second end; a coil that is non-conductive and includes a coil first end and a coil body extending by a second longitudinal span from the coil first end to a coil second end, wherein the coil surrounds the conductor from the conductor first end to the conductor second end; an outer sheath that is conductive and includes an outer sheath first end and an outer sheath body extending by a third longitudinal span from the outer sheath first end to an outer sheath second end, wherein the outer sheath surrounds the coil from the conductor first end to the conductor second end; and an eutectic salt that is disbursed between the conductor and the outer sheath.
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公开(公告)号：US11851207B2
公开(公告)日：2023-12-26
申请号：US18194769
申请日：2023-04-03
CPC分类号： B64D47/02 , B64D11/00 , B64D13/00 , B60Q3/54 , B64D2011/0053 , B64D2013/003
摘要： A fixture configured to secure a component in a vehicle includes a panel separating an internal cabin from an external compartment. The panel has a first side facing the internal cabin and a second side facing the external compartment. A hole is disposed within the panel. The component is configured for mounting to the panel via the hole. The component includes a flange configured for abutting the first side of the panel and a coupling feature configured to extend through the hole into the external compartment. A fastener is configured to removably couple with the coupling feature and abut the second side of the panel for fastening the component to the panel.
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公开(公告)号：US11820518B2
公开(公告)日：2023-11-21
申请号：US16842519
申请日：2020-04-07
申请人： Clark C. Hampe, Jr.
发明人： Clark C. Hampe, Jr.
IPC分类号： B64D13/00 , B64D13/06 , F24F13/065
CPC分类号： B64D13/06 , F24F13/065 , B64D2013/003
摘要： Disclosed is a stowable airflow diverter for removable attachment to a floor vent of a turbine aircraft. The air diverter comprises vertical ducting extending from a base. A flexible gasket and magnets are attached to the base for engagement with the floor vent. A nozzle attached to the vertical ducting redirects the airflow emanating from the floor vent from horizontal to vertical in order to direct air conditioned air into the cock pit of the aircraft. In an alternate embodiment, the nozzle is rotatable with respect to the vertical axis of the duct. In another alternate embodiment, the nozzle and vertical duct comprise telescoping segments such that the device can be collapsed into the floor vent.
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