公开(公告)号：US11618577B2

公开(公告)日：2023-04-04

申请号：US17032464

申请日：2020-09-25

申请人： AMI Industries, Inc.

发明人： Dustin J. Wimmer ,  Glen Shaw

IPC分类号： B64D25/10 ,  B64D17/72

摘要： A drogue bridle attachment assembly may comprise a housing, a lock pin, jackscrew gear pin, and a drive gear pin. The housing may define a bridle opening. The lock pin may be configured to translate into the bridle opening. The jackscrew gear pin may include a threaded portion and a gear portion. The threaded portion may engage a threaded opening in the lock pin. The drive gear pin may include a drive gear portion intermeshed with the gear portion of the jackscrew gear pin.

公开(公告)号：US11571938B2

公开(公告)日：2023-02-07

申请号：US15721934

申请日：2017-10-01

申请人： Andrew H B Zhou ,  Tiger T G Zhou ,  Dylan T X Zhou

发明人： Andrew H B Zhou ,  Tiger T G Zhou ,  Dylan T X Zhou

IPC分类号： B60F5/02 ,  B64C37/00 ,  B64C29/00 ,  B64C3/56 ,  B64C13/18 ,  B64C7/00 ,  B64D25/10 ,  B64D27/20 ,  B60J5/04 ,  B64C5/10 ,  B64D17/80

摘要： A hybrid VTOL jet car comprising a light weight floatable chassis adapted for carrying a payload, a retractable tail section attached to a light weight floatable chassis at the rear end adapted for stabilizing the hybrid VTOL jet car, a plurality of wheels at the bottom of the hybrid VTOL jet car, a plurality of retractable wings on the sides of light weight floatable chassis, adapted for maneuvering the hybrid VTOL jet car. Further features may include a plurality of thrust-producing engines adapted for generating the thrust required for driving the hybrid VTOL jet car on a surface as well as in the air and a plurality of parachutes attached to the hybrid VTOL jet car to safely land the hybrid VTOL jet car under emergency.

公开(公告)号：US11548649B2

公开(公告)日：2023-01-10

申请号：US17125494

申请日：2020-12-17

申请人： AMI Industries, Inc.

发明人： John Hampton

IPC分类号： B64D25/10 ,  B64C1/32

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 sequencer, cause the sequencer to perform operations, which may comprise receiving, by the sequencer, a power input; sending, by the sequencer, a first deploy signal to a first aircraft escape subsystem; and sending, by the sequencer, a second deploy signal to a first ejection seat subsystem.

公开(公告)号：US11505326B2

公开(公告)日：2022-11-22

申请号：US17104623

申请日：2020-11-25

申请人： AMI Industries, Inc.

发明人： Steven Holstine ,  Tristan Likes

IPC分类号： B64D25/10

摘要： A system for automatic ejection mode selection may comprise: a first ejection seat configured to receive a first pilot; a second ejection seat configured to receive a second pilot or a non-pilot; a user detection system configured to determine whether the second ejection seat has the second pilot, the non-pilot, or is empty; and a controller configured to adjust an ejection system in response to determining whether the second ejection seat has the second pilot, the non-pilot, or is empty.

公开(公告)号：US11465762B2

公开(公告)日：2022-10-11

申请号：US16983622

申请日：2020-08-03

申请人： AMI Industries, Inc.

发明人： Steve Holstine ,  Kassidy L. Carson ,  Casey Andrew Stribrny ,  Nicholas K. Bharucha

IPC分类号： B64D25/10

摘要： An ejection seat for an aircraft is disclosed. In various embodiments, the ejection seat includes a base, a divergence rocket attached to the base, and a compensation rocket attached to the base.

公开(公告)号：US20220306303A1

公开(公告)日：2022-09-29

申请号：US17214706

申请日：2021-03-26

申请人： AMI Industries, Inc.

发明人： Steve Holstine ,  John Hampton

IPC分类号： B64D25/10 ,  B64D17/44

摘要： A recovery parachute assembly may comprise a container comprising an open base end, a parachute packed within the container, a plurality of riser lines and suspension lines packed within the container and proximate the open base end, a tray including a lip configured to receive the open base end of the parachute container, and a first standoff block coupled to the tray, wherein the first standoff block compresses at least one of the riser lines or suspension lines into the base end of the container and away from the tray, wherein the first standoff block defines a channel between the lip of the tray and the first standoff block, wherein the channel includes a plurality of drain holes formed along a distal edge of the tray.

公开(公告)号：US11427339B2

公开(公告)日：2022-08-30

申请号：US16220828

申请日：2018-12-14

申请人： GOODRICH CORPORATION

发明人： Matthew D Salois ,  Jeff Benjamin

IPC分类号： B64D25/10 ,  B64D25/04 ,  B64D11/06 ,  B64C1/14

摘要： An ejection seat for an aircraft is disclosed. In various embodiments, the ejection seat includes a seat frame; and a moveable headrest attached to the seat frame, the moveable headrest including a first piercer assembly configured for fracturing a canopy.

公开(公告)号：US20220227496A1

公开(公告)日：2022-07-21

申请号：US17152434

申请日：2021-01-19

申请人： AMI INDUSTRIES, INC.

发明人： Steve Holstine ,  Mayur Kali Vadhwana

IPC分类号： B64D25/10 ,  B60N2/427

摘要： A dual switch arm and mode select system for monitoring an ejection mode selection of an ejection system may include a controller. An ejection mode selector, a first arm switch assembly, a second arm switch assembly, and a display may be in communication with the controller. The controller may determine an ejection mode of the ejection system based on a signal received from the ejection mode selector. The controller may determine a position of the first arm switch assembly and a position of the second arm switch assembly. The controller may command the display to output at least one of a fault-free signal, a fault signal, or a warning signal based on the ejection mode and the positions of the first arm switch assembly and the second arm switch assembly.

公开(公告)号：US11370553B2

公开(公告)日：2022-06-28

申请号：US17035422

申请日：2020-09-28

申请人： AMI Industries, Inc.

发明人： Bradley Mastrolia ,  Kassidy L. Carson ,  Cyle Teal

IPC分类号： B64D25/10 ,  B64D11/06

摘要： A fitting for use with an ejection seat system of an aircraft includes a fitting bar configured to extend across a top of a catapult of the ejection seat system and defining an angled slot configured to receive a portion of a gas port of the ejection seat system. The fitting further includes a first leg and a second leg coupled to and extending away from the fitting bar and configured to be pivotally coupled to a smokestack structure of the ejection seat system.

公开(公告)号：US11370552B2

公开(公告)日：2022-06-28

申请号：US16707993

申请日：2019-12-09

申请人： GOODRICH CORPORATION

发明人： Joshua David Carter ,  Jean C. Rodriguez

IPC分类号： B64D25/10 ,  H02K33/16

摘要： A transducer assembly configured to convert a pyrotechnic initiation to an electrical signal may comprise a magnet, a hollow tube, and a conductive element. The hollow tube may be wrapped around the magnet in the shape of a coil. The hollow tube may be at least partially filled with a thermite. The conductive element may be coupled to an outlet of the hollow tube. The conductive element may seal the outlet of the hollow tube.