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公开(公告)号:US12054262B2
公开(公告)日:2024-08-06
申请号:US17332849
申请日:2021-05-27
Applicant: Adient Aerospace, LLC
Inventor: Max Wisniewski
IPC: B64D11/06
CPC classification number: B64D11/0639 , B64D11/0627 , B64D11/0636 , B64D11/0693
Abstract: A seat assembly includes a base structure having at least one of a seat pan shell and a backrest shell, and one or more attachment structures configured to removably couple at least one of the seat pan shell and the backrest shell to a seat surface arrangement or a utility surface arrangement. The base structure is convertible between a passenger seat and a utility element based on the coupling of the seat surface arrangement or the utility surface arrangement, respectively, to the base structure.
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公开(公告)号:US20240239493A1
公开(公告)日:2024-07-18
申请号:US18511395
申请日:2023-11-16
Applicant: HYUNDAI MOBIS CO., LTD.
Inventor: Ik Keun CHOI
IPC: B64D11/06
CPC classification number: B64D11/0639 , B64D11/0619
Abstract: A moving cockpit for a vehicle including a cockpit module provided in an inner front side of the vehicle, a guide rail provided on an inner panel of the vehicle, the guide rail extending in a forward direction and a backward direction relative to the front side of the vehicle, and a cockpit moving unit movably provided on the guide rail, the cockpit configured to move the cockpit module forward and backward in the vehicle.
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公开(公告)号:US11976998B2
公开(公告)日:2024-05-07
申请号:US17339453
申请日:2021-06-04
Applicant: Hyundai Motor Company , Kia Corporation
Inventor: Tae Ho Lee
CPC classification number: G01M1/127 , B64D11/0602 , B64D11/0639 , B64D25/04
Abstract: A device for controlling a balance of an urban air mobility, may include a receiver configured to receive occupant information related to the urban air mobility from a cloud server; and a controller configured to control the balance of the urban air mobility according to the received occupant information.
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公开(公告)号:US20240124141A1
公开(公告)日:2024-04-18
申请号:US17966413
申请日:2022-10-14
Applicant: AMI Industries, Inc.
Inventor: Martin S. Day , Chad Pacheco , Douglas Foisie
IPC: B64D11/06
CPC classification number: B64D11/0619 , B64D11/0639 , B64D11/0698
Abstract: An aircraft seat assembly including stanchions defining elongated guide channels and elongated motion sleds nested in the guide channels and affixed to a seat bucket. An energy absorber implemented as a wire bender assembly is coupled between the stanchions and the motion sled. In use, the elongated guide channels guide motion of the motion sleds and the wire bender assemblies attenuate energy during a dynamic event exceeding a predetermined threshold load value. The elongated interface between the guide channels and motion sleds serve to transfer excessive loading to the seat frame thereby protecting the seat assembly from damage and the occupant from excessive lumbar spinal loads.
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公开(公告)号:US11945591B2
公开(公告)日:2024-04-02
申请号:US17061681
申请日:2020-10-02
Applicant: ZIM Aircraft Seating GmbH
Inventor: Sebastian Lueck , Uwe Salzer
IPC: B64D11/06
CPC classification number: B64D11/0639 , B64D11/0696
Abstract: The invention relates to an aircraft passenger seat, comprising a frame intended to be fastened to a floor of an aircraft passenger cabin, a seat base movably mounted on the frame, and a movably mounted seat back. The aircraft passenger seat is characterized in that at least one rail is fastened to the frame and in that the seat base is slidably arranged on the rail by means of guide elements.
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公开(公告)号:US20240034461A1
公开(公告)日:2024-02-01
申请号:US18344420
申请日:2023-06-29
Applicant: Joby Aero, Inc.
Inventor: Mark Moore , John Conway Badalamenti , Ian Villa , Adam Warmoth , David Josephson
CPC classification number: B64C17/08 , B64C29/0016 , B64D11/0649 , B64D11/0639 , B64D11/003 , B64C17/02 , B64D9/00 , G01G19/07
Abstract: Vertical take-off and landing (VTOL) aircraft can provide opportunities to incorporate aerial transportation into transportation networks for cities and metropolitan areas. However, VTOL aircraft can be sensitive to uneven weight distributions, e.g., the payload of an aircraft is primarily loaded in the front, back, left, or right. When the aircraft is loaded unevenly, the center of mass of the aircraft may shift substantially enough to negatively impact performance of the aircraft. Thus, in turn, there is an opportunity that the VTOL may be loaded unevenly if seating, luggage placement, and/or positions of internal components are not coordinated. Among other advantages, dynamically assigning the payloads and adjusting components of the VTOL aircraft can increase VTOL safety by ensuring the VTOL aircraft is loaded evenly and meets all weight requirements; can increase transportation efficiency by increasing rider throughput; and can increase the availability of the VTOL services to all potential riders.
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公开(公告)号:US11851186B2
公开(公告)日:2023-12-26
申请号:US18102352
申请日:2023-01-27
Applicant: Safran Seats USA LLC , Safran Seats
Inventor: Bastien Bonnefoy , Arthur K. Glain , Victor Carlioz , Matthew Cleary , Eric O. Freienmuth , Patrick Herault , Christopher La Montagna
CPC classification number: B64D11/0606 , B64D11/0023 , B64D11/0639 , B64D2011/0046
Abstract: Passenger seats having improved comfort emergency egress solutions for mini suites or other types of passenger seats that have a privacy screen, wall, or sliding door that divides the passenger seat from the aisle area or other common area. Specific embodiments find particular use on-board passenger transportation vehicles, such as aircraft, where comfort and privacy must be balanced with safety and federal regulations.
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公开(公告)号:US11713123B2
公开(公告)日:2023-08-01
申请号:US17073184
申请日:2020-10-16
Applicant: AMI INDUSTRIES, INC.
Inventor: Ryan Stuart Porter , Keith M. Ferguson , Scott R. Patterson
CPC classification number: B64D11/0639 , B60N2/06 , B60N2/14 , B60N2/146 , B64D11/0648 , A47C3/18 , B63B29/04 , B63B29/06
Abstract: The present disclosure provides a swivel stop comprising a rotating member, a first boss coupled to the rotating member and a second boss coupled to the rotating member, and a second plate having a first interference surface and a second interference surface. An interference between the first boss and the first interference surface and the second boss and the second interference surface tends to limit the rotation of the rotating member with respect to the second plate. The swivel stop may further comprise a rail wherein the second plate is configured to translate along the rail.
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公开(公告)号:US20190233116A1
公开(公告)日:2019-08-01
申请号:US16265706
申请日:2019-02-01
Applicant: OPTIMARES S.P.A.
Inventor: Alessandro BRACA , Alessio MORSICANI , Andrea GIORDANO
IPC: B64D11/06
CPC classification number: B64D11/0601 , B64D11/0604 , B64D11/0639 , B64D11/064
Abstract: An aircraft seat arrangement within an aircraft cabin having a longitudinal axis and two windowed side walls and a central aisle, said arrangement comprising at least two pairs of seats arranged opposite each other along an axis parallel to said longitudinal axis of the cabin, in each pair of seats a window seat being adjacent to a windowed side wall and the other aisle seat being adjacent to said central aisle. Each seat is configured such to perform a reclining movement along a respective reclining axis between a sitting position and an extended position, and vice versa, wherein in said extended position each seat has a maximum extension defined by two points lying on the reclining axis. Each window seat is oriented at a first angle obtained from the intersection of the respective reclining axis with a straight line parallel to the longitudinal axis of the cabin at the first point of maximum extension of the window seat.
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公开(公告)号:US09914541B2
公开(公告)日:2018-03-13
申请号:US15037380
申请日:2014-11-24
Applicant: Zodiac Seats US LLC
Inventor: Udo W. Schultheis , Foek (Phuc) Nguyen Tien Le
CPC classification number: B64D11/0639 , A47C7/029 , A47C7/14 , A47C7/40 , B60N2/02 , B60N2/2881 , B60N2/70 , B60N2/7005 , B60N2/7041 , B60N2/7047 , B64D11/0647
Abstract: Dynamic support systems (10) include a plurality of support members (12), a base material (14), and a support layer (18). Each support member (12) has an upper support surface (20) extending from a first end of a stud (22), and a spherical member (28) extending from a second end of the stud. The base material (14) includes a plurality of receptacles (40) having a socket (42) with a recessed area (52) for positioning a spring (56). The support layer (18) also includes a plurality of apertures (64) that are positioned over the receptacles (40) and allow the studs (22) to extend there through.
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