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公开(公告)号：US12043390B2
公开(公告)日：2024-07-23
申请号：US17379515
申请日：2021-07-19
申请人： AMI Industries, Inc.
发明人： Kyler J. Marutzky
CPC分类号： B64D11/0643 , B64D11/064 , B64D11/0691
摘要： A leg rest assembly is disclosed. The assembly may include a support sub-assembly configured to provide at least one of leg support or foot support. The support sub-assembly may include a panel and a support cushion. The support cushion may include a cavity defined by one or more surfaces of the support cushion. The assembly may include a translation sub-assembly configured to translate the support sub-assembly. The translation sub-assembly may include one or more translation arms. The translation sub-assembly may include one or more guide rails. The translation sub-assembly may include one or more linear bearings configured to engage with the one or more guide rails, the one or more linear bears slideable along a length of the one or more guide rails. The translation sub-assembly may include one or more translation devices configured to translate the support sub-assembly between a first position and one or more additional positions.
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公开(公告)号：US11993386B2
公开(公告)日：2024-05-28
申请号：US17497624
申请日：2021-10-08
申请人： AMI INDUSTRIES, INC.
CPC分类号： B64D25/10 , A61B5/18 , B64D47/02 , B64D2045/0085
摘要： An ejection system may comprise an ejection seat and a smart deployment system configured to initiate a deployment of the ejection seat. The smart deployment system may comprise a pilot health monitoring system including a plurality of sensors configured to detect a plurality of physiological conditions, and a controller configured to make ejection system decisions based on a pilot health signal received from the pilot health monitoring system and an aircraft health signal output from an aircraft health monitoring system.
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公开(公告)号：US20240124142A1
公开(公告)日：2024-04-18
申请号：US17966283
申请日：2022-10-14
申请人： AMI Industries, Inc.
发明人： Martin S. Day , Chad Pacheco , Douglas Foisie
IPC分类号： B64D11/06
CPC分类号： B64D11/064 , B64D11/062
摘要： An aircraft seat assembly including first and second stanchions forming interior spaces open through forward slots. A seat pan is pivotally attached to the stanchions and includes rearward extensions that extend through the forward slots and are received in the interior spaces. First and second spring mechanisms reside in the respective first and second interior spaces and are attached at opposing ends to their respective stanchion and to the seat pan. In use, rotating the seat pan toward a deployed position elongates the first and second elongation springs thereby energizing a return force of the spring mechanisms.
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公开(公告)号：US20240083582A1
公开(公告)日：2024-03-14
申请号：US17940873
申请日：2022-09-08
申请人： AMI Industries, Inc.
发明人： Chad R. Pacheco
CPC分类号： B64D25/04 , B64D11/0619 , B64D11/0639
摘要： A seat base assembly for an aircraft seat includes parallel rails attached to an aircraft bulkhead, each rail including a slot extending vertically within the rail. The seat (e.g., seatback and seat frame) is attached to a sled capable of vertical translation relative to the bulkhead via slidable members that translate along the slots. The sled includes a hole for accommodating a locking pin controllable by the seat occupant. A metering plate attached to the seat base behind the sled is folded over a lateral axis into a forward and rear layer, the forward layer including holes for the locking pin wherein each hole corresponds to a desired seat height to which the seat may be adjusted by securing the locking pin through the sled hole and metering hole. In response to an impact event, the metering plate deforms to absorb impact energy and control downward deceleration of the seat.
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公开(公告)号：US11845561B2
公开(公告)日：2023-12-19
申请号：US17206551
申请日：2021-03-19
申请人： AMI Industries, Inc.
IPC分类号： B64D25/10
CPC分类号： B64D25/10
摘要： A stabilizer system for an ejection seat may comprise a collapsible support structure configured to be coupled to a seat back or a seat bucket of the ejection seat, an airfoil coupled to the collapsible support structure, and a deployment system operatively coupled to the collapsible support structure and configured to expand the collapsible support structure.
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公开(公告)号：US11767905B2
公开(公告)日：2023-09-26
申请号：US16988392
申请日：2020-08-07
申请人： AMI Industries, Inc.
CPC分类号： F16H55/26 , B23F17/006 , B32B3/02 , B32B3/266 , B32B15/012 , B64D11/0639 , B64D11/0648 , B64D11/0649 , F16H19/04 , B32B2605/18 , F16H2712/06
摘要： A rack is made from a plurality of laminated layers. Each layer defines an alignment feature that allows all of the layers to be affixed to a base plate of an aircraft seat assembly and align the teeth of the rack to within five ten-thousandths of an inch. The rack includes a straight portion and a curved portion such that a pinion gear on the aircraft seat assembly can move the aircraft seat assembly along tracks with straight and curved portions.
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公开(公告)号：US11713127B2
公开(公告)日：2023-08-01
申请号：US17549634
申请日：2021-12-13
申请人： AMI Industries, Inc.
IPC分类号： B64D25/10
CPC分类号： B64D25/10
摘要： An article of manufacture may include a tangible, non-transitory computer-readable storage medium having instructions stored thereon for controlling deployment of aircraft escape and ejection seat subsystems. The instructions, in response to execution by a first sequencer, cause the first sequencer to perform operations which may comprise receiving a power input, determining a seat location and a seat identity of a first ejection seat in which the first sequencer is installed, determining an ejection mode, sending a first deploy command to an escape path clearance subsystem, determining a deployment sequence for a seat rocket catapult subsystem and a plurality of ejection seat subsystems of the first ejection seat based on the seat location, the seat identity, and the ejection mode, sending a second deploy command to the seat rocket catapult subsystem, and sending a series of third deploy commands to the plurality of ejection seat subsystems.
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公开(公告)号：US20230202662A1
公开(公告)日：2023-06-29
申请号：US18176060
申请日：2023-02-28
申请人： AMI Industries, Inc.
发明人： Jaro S. Volny , Kassidy L. Carson
摘要： A life preserver head restraint may be configured to inflate in response to deployment of a parachute assembly. The life preserver head restraint may comprise an inflatable volume and a charge tank fluidly coupled to the inflatable volume. In an inflated state, the life preserver head restraint may restrict head movement during line stretch of the parachute assembly.
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公开(公告)号：US20230088613A1
公开(公告)日：2023-03-23
申请号：US17478432
申请日：2021-09-17
申请人： AMI INDUSTRIES, INC.
发明人： Bang H. Vo , Steve Holstine
摘要： A drogue bridle separation assembly may comprise a housing and a pyrotechnic fastener. The housing may define a riser channel and a fastener opening. The pyrotechnic fastener may be configured to extend through the fastener opening and the riser channel. The pyrotechnic fastener includes a charge configured to undergo an exothermic reaction in response to an electrical signal.
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公开(公告)号：US11560232B2
公开(公告)日：2023-01-24
申请号：US17104930
申请日：2020-11-25
申请人： AMI Industries, Inc.
发明人： Steven Holstine , Tristan Likes , John Hampton
IPC分类号： B64D25/10
摘要： A system for ejection mode verification may comprise: a first ejection seat; a second ejection seat; an ejection mode selector; and a controller configured to: compare a desired ejection mode with a selected ejection mode; and command an indicator to turn “ON” or “OFF” in response to comparing the desired ejection mode with the selected ejection mode.
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