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公开(公告)号：US11518527B2
公开(公告)日：2022-12-06
申请号：US17036229
申请日：2020-09-29
申请人： AMI Industries, Inc.
发明人： Ronald John McCumber , Casey Andrew Stribrny , Nicholas K. Bharucha , John Hampton , Kassidy L. Carson , Bradley Mastrolia , Steve Holstine
摘要： A system for automatic optimization of an ejection system for an aircraft includes the ejection system having a plurality of adjustable settings. The system further includes a sensor configured to detect weight data corresponding to a weight of a user of the ejection system. The system further includes a controller coupled to the ejection system and to the sensor and configured to adjust at least one of the plurality of the adjustable settings of the ejection system based on the weight data.
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公开(公告)号：US11498685B2
公开(公告)日：2022-11-15
申请号：US17186128
申请日：2021-02-26
申请人： AMI Industries, Inc.
IPC分类号： B64D11/06
摘要： An armrest is disclosed that includes an armrest subframe configured to couple to an arm of the seat that includes a slot within a face of the armrest subframe configured to receive a stop pin. The armrest further includes an arm pad translatably coupled to the armrest subframe and includes a plurality of grooves formed on one edge of the armrest subframe. The arm pad further includes the stop pin that restricts the translation of the arm pad and a spring anchor. The armrest further includes a lever rotationally coupled to the armrest that includes a locking pin configured to engage one or more grooves of the plurality of grooves, and an actuating end, wherein a movement of the actuating end at least one of engages or disengages the locking pin from the one or more grooves of the plurality of grooves. The armrest further includes a biasing spring.
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公开(公告)号：US20220332407A1
公开(公告)日：2022-10-20
申请号：US17231798
申请日：2021-04-15
申请人： AMI Industries, Inc.
摘要： A method for sensor-based ejection of an aircraft occupant from an aircraft may comprise: receiving, via a processor and through a sensor, an ejection command from the aircraft occupant; comparing, via the processor, the ejection command to a predetermined ejection command; determine, via the processor, whether the ejection command matches the predetermined ejection command; and commanding, via the processor, initiation of an ejection event in response to the ejection command matching the predetermined ejection command.
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公开(公告)号：US11465751B2
公开(公告)日：2022-10-11
申请号：US17135633
申请日：2020-12-28
申请人： AMI Industries, Inc.
发明人： Douglas E. Hoover , David A. Ross
IPC分类号： B64D11/06
摘要： Disclosed is an armrest assembly for a vehicle seat such as a pilot seat positioned in an aircraft cockpit. The armrest assembly generally includes a pivoting armrest and an arm pad repositionable relative to the armrest to change the arm pad width. The arm pad includes two functional sides each having a different width dimension. The arm pad is coupled to the armrest such that sequential translational and rotational motion of the arm pad moves one of the first and second sides into a use position atop the armrest and the other of the first and second sides into an out of use position alongside the armrest. The armrest assembly according to the present disclosure is ideal for use in tight quarters within the flight deck, among other installation environments requiring a functional armrest.
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公开(公告)号：US20220315229A1
公开(公告)日：2022-10-06
申请号：US17217109
申请日：2021-03-30
申请人： AMI Industries, Inc.
发明人： Cyle Teal , Neil Cross
摘要： An arm restraint assembly for an ejection seat may comprise a primary arm configured to pivot about a primary arm pivot joint, a first cable portion coupled to the primary arm, and an attenuator coupled to the first cable portion. The first cable portion may be configured to pivot the primary arm about the primary arm pivot joint. The attenuator may include a housing and a plunger having a head located in the housing. The head of the plunger may be biased toward a first end of the housing.
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公开(公告)号：US11434012B2
公开(公告)日：2022-09-06
申请号：US16680313
申请日：2019-11-11
申请人： AMI Industries, Inc.
发明人： Jeff Benjamin , Matthew D Salois
IPC分类号： B64D25/10 , G01G19/52 , G01G19/414 , G01G19/44 , B64D41/00
摘要： A rocket catapult assembly for an ejection seat may comprise a motor assembly including a proximal end and a distal end, a first cartridge, and a second cartridge. The first cartridge and the second cartridge may be configured to provide a variable thrust based on an occupant's weight. The first cartridge may provide a thrust corresponding to a relatively light weight occupant, the second cartridge may provide a thrust corresponding to a relatively average weight occupant, and the first cartridge and second cartridge may provide a combined thrust corresponding to a relatively heavy weight occupant.
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公开(公告)号：US11414197B2
公开(公告)日：2022-08-16
申请号：US17162841
申请日：2021-01-29
申请人： AMI INDUSTRIES, INC.
摘要： An arm restraint assembly for an ejection seat may comprise a primary arm configured to pivot about a primary arm pivot joint, and a secondary arm configured to pivot about a secondary arm pivot joint. A primary airfoil structure may be coupled to the primary arm assembly. The primary airfoil structure may include an airfoil body.
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18.发明授权公开(公告)号：US11345458B2
公开(公告)日：2022-05-31
申请号：US16938780
申请日：2020-07-24
申请人： AMI INDUSTRIES, INC.
发明人： Steven A Holstine , Nathan Eischeid , Bradley Mastrolia , John Hampton , Neil Cross , Kassidy L. Carson , Ian Walter Haas , Patrick Emmett Hyde , Aaron H. Keene , Cyle Teal , John Wade
摘要： A canopy fragilization system for use in an aircraft ejection system may comprise: a sharp breaker disposed on a first side of an ejection seat, the sharp breaker configured to act as a primary breaker of a canopy of an aircraft; a blunt breaker disposed on a second side of the ejection seat, the blunt breaker configured to act as a secondary breaker of the canopy of the aircraft; and a deployable overhead protection assembly comprising a first tertiary breaker and a second tertiary breaker.
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公开(公告)号：US20220127007A1
公开(公告)日：2022-04-28
申请号：US17079293
申请日：2020-10-23
申请人： AMI INDUSTRIES, INC.
IPC分类号： B64D25/10
摘要： A system for controlling an aircraft in response to deployment of an ejection seat may comprise a seat controller located on the ejection seat and configured to output a signal in response to initiation of an ejection sequence. An aircraft controller may be configured to receive the signal from the seat controller. A tangible, non-transitory memory may be configured to communicate with the aircraft controller. The tangible, non-transitory memory may have instructions stored thereon that, in response to execution by the aircraft controller, cause the aircraft controller to perform operations, which may comprise receiving the signal from the seat controller, receiving data signals from an operational data source, and sending command signals configured to control a component of the aircraft
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公开(公告)号：US20220120327A1
公开(公告)日：2022-04-21
申请号：US17076276
申请日：2020-10-21
申请人： AMI Industries, Inc.
发明人： John Hampton , Kassidy L. Carson , Ryan Roseke
摘要： An anti-recoil assembly may include a housing, a shaft, and an energy attenuator. The housing generally defines a cavity, with the housing having a first end portion and a second end portion, according to various embodiments. The shaft may be at least partially disposed within the cavity, and the shaft may be configured to move within the cavity in a first direction from the first end portion to the second end portion. In various embodiments, the energy attenuator is disposed within the cavity at the second end portion. In response to movement of the shaft in the first direction, the energy attenuator is configured to inhibit the shaft from recoiling in a second direction opposite the first direction, according to various embodiments.
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