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公开(公告)号:US20250066022A1
公开(公告)日:2025-02-27
申请号:US18511048
申请日:2023-11-16
Applicant: B/E Aerospace, Inc.
Inventor: Sreekanth Rao , Pradeep Acharya , Mark B. Dowty
IPC: B64D11/06
Abstract: A seat pan includes a break over function. The break over enables downward motion of a portion of the seat pan. The downward motion of the portion of the seat pan allows a distance between passenger seats to be reduced while maintaining a minimum required egress distance between the passenger seats. The breakover seat pan assists in egress. The portion of the seat pan may be actuated upwards to increase the length of the seat pan while a passenger is seated. The seat pan thus creates a supported seat surface when an occupant sits on the seat while presenting with a reduced surface when not occupied.
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公开(公告)号:US20250051014A1
公开(公告)日:2025-02-13
申请号:US18379531
申请日:2023-10-12
Applicant: B/E Aerospace, Inc.
IPC: B64D11/06
Abstract: A row of passenger seats convertible to a bed. The row includes a frame assembly supporting a plurality of laterally adjacent passenger seats. In embodiments, each seat includes a backrest having a first portion and a second portion movable relative to the first portion, a seat pan movable between a first position for seating and a second position for sleeping, and at least one link connecting the second portion of the backrest to the seat pan such that the second portion of the backrest tracks with the seat pan. In use, the second portion of the backrest resides in a plane of the backrest when the seat pan is in the first position, and resides in a plane of the seat pan when the seat pan is in the second position. In embodiments, the row provides a provision for sleeping in an economy class cabin of an airliner when occupancy permits seat row conversion.
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公开(公告)号:US20250038805A1
公开(公告)日:2025-01-30
申请号:US18361389
申请日:2023-07-28
Applicant: B/E Aerospace, Inc.
Inventor: Vivek T. Rathod , ADWAIT A. TRIKANAD , SANJAY G. BAJEKAL
Abstract: A system for an aircraft application using channel state information (CSI) is disclosed. The system includes a CSI generation device, a controllable device, and a controller. The controller is configured to receive CSI data from the CSI generation device, identify one or more classification states from the CSI data associated with one or more of a human presence, a posture, or a gesture, identify an operation to be executed based on the classification state, and, responsive to identifying the operation, send a first command to the controllable device to perform the operation.
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公开(公告)号:US12179925B2
公开(公告)日:2024-12-31
申请号:US18215349
申请日:2023-06-28
Applicant: B/E Aerospace, Inc.
Inventor: Raghavendra Kottem , Arjun Koustubhan
Abstract: A quick release system for an interior apparatus is disclosed. The system may include a release assembly including a release handle and release cables. The release handle may pull the release cables when a force is applied. The system may include a latch assembly including latches coupled to the release cables. The latches may include a latch hook positioned in an open position or a closed position. Upon applying the force to the release handle, the latch hook may release the apparatus to cause the apparatus to rotate about an axis. The system may include a locking assembly including a lever and a lock plate. Upon applying the force to the release handle, the lock plate may translate between the locked position and the unlocked position to disengage the lock plate from the tracks to cause the apparatus to translate along the tracks.
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公开(公告)号:US20240425182A1
公开(公告)日:2024-12-26
申请号:US18615117
申请日:2024-03-25
Applicant: B/E Aerospace, Inc.
Inventor: Sambasiva Rao Kodati , Chandra Sekhar Gudla , Guruswamy Prasad Gundra
IPC: B64D11/06
Abstract: An integrated seat assembly including a fixed subassembly attachable to a seat backrest, a headrest subassembly configured to translate along a rail of the fixed subassembly, and a neck support subassembly also configured to translate along the rail, independently of the translation of the headrest subassembly. Each of the headrest subassembly and the neck support subassembly include articulating supports configured to enhance support of comfort of the respective subassemblies. Each of the headrest subassembly and the neck support subassembly may include a cushion for further comfort.
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公开(公告)号:US12172754B2
公开(公告)日:2024-12-24
申请号:US17953583
申请日:2022-09-27
Applicant: B/E Aerospace, Inc.
Inventor: Oscar Ruiz Lara , Travis John Vaninetti , Brent Ellis , Charles F. Forster
Abstract: A locking assembly of a lavatory door in an aircraft, comprising: a locking mechanism; and an occupancy indicator. The occupancy indicator is configured with a display that enables viewing of a status of the lavatory of availability or is occupancy. The position of the locking mechanism and occupancy indicator has been changed from a higher location on the lavatory door that approximates a line-of-sight from a standing position at the lavatory door to a lower location that approximates the line-of-sight from a seated position at the lavatory door. The display of the occupancy indicator is configured with a plurality of display angles to display the status comprising at least a first display angle to allow viewing from the line-of-sight in the standing position and at a second display angle to allow viewing from the line-of-sight in a seated lower position at the lavatory door.
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公开(公告)号:US12168516B2
公开(公告)日:2024-12-17
申请号:US17988534
申请日:2022-11-16
Applicant: B/E AEROSPACE, INC.
Inventor: Oscar Ruiz Lara , Travis John Vaninetti , Brent Ellis , Scott Marley , Alexander Lei Velet
Abstract: An aircraft lavatory monument is provided that includes a first lavatory including a first door providing access to the first lavatory from an aisle of an aircraft; a second lavatory proximate the first lavatory, the second lavatory including a second door providing access to the second lavatory from the aisle of the aircraft; and a movable wall disposed between the first lavatory and the second lavatory, the movable wall including a latching mechanism positioned on an exterior edge of the movable wall and accessible from the aisle of the aircraft, where the latching mechanism, responsive to being in a locked position, causes the movable wall to be positioned at a first position separating the first lavatory from the second lavatory and providing privacy therebetween, and where the latching mechanism, responsive to being in an unlocked position, allows the movable wall to collapse thereby forming an enlarged bathroom space.
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公开(公告)号:US20240409218A1
公开(公告)日:2024-12-12
申请号:US18734130
申请日:2024-06-05
Applicant: B/E Aerospace, Inc.
Inventor: Michael Princip , Alexander Velet , Charles Martin Hansson , Travis Vaninetti , Daniel Mills , James Kash , Ferhad Tabakovic , Travis Finlay , Brian Green
IPC: B64D11/06
Abstract: A passenger seat assembly includes a first seat, a second seat, and a center console. In embodiments, a privacy divider is positioned atop the center console and serves as a mounting location for amenities for serving the first and second passenger seats. The center console is configurable to include various privacy, comfort, and utility features depending on the intended seating class for the passenger seat assembly. In embodiments, the first and second passenger seats include headrests and privacy assemblies associated with the headrests for enhancing privacy between the seats and/or relative to adjacent aisles.
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公开(公告)号:US20240400206A1
公开(公告)日:2024-12-05
申请号:US18204648
申请日:2023-06-01
Applicant: B/E Aerospace, Inc.
Inventor: Michael M. Princip , Alexander L. Velet , Charles Martin Hansson , Travis J. Vaninetti , Brian D. Green , Karen J. Nanney , Joshua Wilson
IPC: B64D11/06
Abstract: A seat console including an upper console portion defining an interior space, a lower console portion positioned below the upper console portion, and at least one cable-actuated passenger control unit (PCU) positioned in the interior space in the upper console portion, the cable-actuated PCU including at least one pushbutton subassembly including a pushbutton presented through one of a first lateral side and a second lateral side of the upper console portion. The seat console may be implemented as a single seat console, or a center console configured to be positioned between two seats.
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公开(公告)号:US20240391593A1
公开(公告)日:2024-11-28
申请号:US18661375
申请日:2024-05-10
Applicant: B/E Aerospace, Inc.
Inventor: Frederik Adrian Stephan Panjer
Abstract: An air filter assembly for use in an aircraft galley insert, the assembly comprising a cavity for receiving an air filter cassette in use, and a door for providing or blocking access to said cavity, wherein said door is hinged and comprises a front grill configured for intaking air.
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