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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
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.
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公开(公告)号：US11597525B2
公开(公告)日：2023-03-07
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：US11077950B2
公开(公告)日：2021-08-03
申请号：US16422528
申请日：2019-05-24
申请人： AMI Industries, Inc.
发明人： Cyle Teal , Bradley Mastrolia
IPC分类号： B64D25/10
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 latch may be coupled to the primary arm. The latch may comprise a first pair of lugs and may be configured to pivot relative to the primary arm. A primary shear pin may extend between the first pair of lugs. A lanyard may be coupled to the primary shear pin.
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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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5.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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6.发明申请公开(公告)号：US20220024554A1
公开(公告)日：2022-01-27
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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7.发明申请公开(公告)号：US20220033057A1
公开(公告)日：2022-02-03
申请号：US16983828
申请日：2020-08-03
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 mitt extending forward of the sharp breaker and the blunt breaker when in a deployed position, a forward end of the mitt configured to act as a tertiary breaker of the canopy of the aircraft.
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公开(公告)号：US20200369392A1
公开(公告)日：2020-11-26
申请号：US16422528
申请日：2019-05-24
申请人： AMI Industries, Inc.
发明人： Cyle Teal , Bradley Mastrolia
IPC分类号： B64D25/10
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 latch may be coupled to the primary arm. The latch may comprise a first pair of lugs and may be configured to pivot relative to the primary arm. A primary shear pin may extend between the first pair of lugs. A lanyard may be coupled to the primary shear pin.
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公开(公告)号：US11305880B2
公开(公告)日：2022-04-19
申请号：US16707625
申请日：2019-12-09
申请人： AMI Industries, Inc.
发明人： Steve Holstine , Cyle Teal
摘要： An arm restraint assembly for an ejection seat may comprise a primary arm and a primary arm deployment system operationally coupled to the primary arm. The primary arm deployment system may be configured to rotate the primary arm about a primary arm pivot joint. The primary arm deployment system may be configured to attach to the ejection seat such that the primary arm deployment system translates with the ejection seat.
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公开(公告)号：US20220097856A1
公开(公告)日：2022-03-31
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
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.
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