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公开(公告)号：US10760887B2
公开(公告)日：2020-09-01
申请号：US15153257
申请日：2016-05-12
Applicant: Goodrich Corporation
Inventor： Matthew Campbell , Luis G. Interiano
Abstract: A detonation transfer assembly is disclosed. A detonation transfer assembly may comprise an external casing comprising an input end and an output end axially opposite the input end, an explosive column spanning axially inside the external casing, a primary explosive disposed within the explosive column, and a secondary explosive disposed within the explosive column axially between the primary explosive and the output end. The primary explosive and/or the secondary explosive may comprise a thermally insensitive initiation material that resists at least one of detonation or thermal degradation in response to temperature increase rate of 3.3° C. per hour over at least twenty hours.
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Patent Agency Ranking
公开(公告)号：US20170297725A1
公开(公告)日：2017-10-19
申请号：US15131677
申请日：2016-04-18
Applicant: GOODRICH CORPORATION
Inventor： Matthew Campbell , Luis G. Interiano , James Tulloch , John Hampton
IPC: B64D25/10
CPC classification number: B64D25/10
Abstract: A system for selecting an ejection mode on an aircraft may include an egress actuator, a ballistic signal system operatively connected to the egress actuator, and a processor operatively connected to the ballistic signal system and the egress actuator. The processor may be configured to receive, from an aircraft controller, a flight characteristic, and select, based on the flight characteristic, an ejection mode from two ejection modes. The processor may be further configured to receive a pilot egress command from the ballistic signal system, and transmit, to the egress actuator, a signal to actuate the ejection mode from the two ejection modes.
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公开(公告)号：US10253892B2
公开(公告)日：2019-04-09
申请号：US15428777
申请日：2017-02-09
Applicant: Goodrich Corporation
Inventor： Matthew Salois , Matthew Campbell
IPC: F16K11/065 , F16K11/22 , B64D25/00 , F16K31/122 , F15B13/02 , F15B13/04 , F16K17/00 , F16K17/34
Abstract: An energetic one way sequence termination arrangement may comprise a housing, a first inlet in operable communication with the housing, a second inlet in operable communication with the housing, and an outlet in operable communication with the housing. The energetic one way sequence termination arrangement is configured such that the second inlet is blocked from fluidic communication with the outlet in response to a first signal being received at the first inlet before a second signal is received at the second inlet, and the first inlet establishes fluidic communication with the outlet in response to the second signal being received at the second inlet before the first signal is received at the first inlet.
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公开(公告)号：US20180224007A1
公开(公告)日：2018-08-09
申请号：US15428777
申请日：2017-02-09
Applicant: Goodrich Corporation
Inventor： Matthew Salois , Matthew Campbell
IPC: F16K11/22
CPC classification number: F16K11/22 , B64D25/00 , F15B13/028 , F15B13/0402 , F15B2211/3052 , F16K11/0655 , F16K17/00 , F16K17/003 , F16K17/34 , F16K31/122 , F16K31/1223
Abstract: An energetic one way sequence termination arrangement may comprise a housing, a first inlet in operable communication with the housing, a second inlet in operable communication with the housing, and an outlet in operable communication with the housing. The energetic one way sequence termination arrangement is configured such that the second inlet is blocked from fluidic communication with the outlet in response to a first signal being received at the first inlet before a second signal is received at the second inlet, and the first inlet establishes fluidic communication with the outlet in response to the second signal being received at the second inlet before the first signal is received at the first inlet.
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公开(公告)号：US20170350681A1
公开(公告)日：2017-12-07
申请号：US15153257
申请日：2016-05-12
Applicant: Goodrich Corporation
Inventor： Matthew Campbell , Luis G. Interiano
Abstract: A detonation transfer assembly is disclosed. A detonation transfer assembly may comprise an external casing comprising an input end and an output end axially opposite the input end, an explosive column spanning axially inside the external casing, a primary explosive disposed within the explosive column, and a secondary explosive disposed within the explosive column axially between the primary explosive and the output end. The primary explosive and/or the secondary explosive may comprise a thermally insensitive initiation material that resists at least one of detonation or thermal degradation in response to temperature increase rate of 3.3° C. per hour over at least twenty hours.
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公开(公告)号：US10384788B2
公开(公告)日：2019-08-20
申请号：US15131677
申请日：2016-04-18
Applicant: GOODRICH CORPORATION
Inventor： Matthew Campbell , Luis G. Interiano , James Tulloch , John Hampton
IPC: B64D25/10
Abstract: A system for selecting an ejection mode on an aircraft may include an egress actuator, a ballistic signal system operatively connected to the egress actuator, and a processor operatively connected to the ballistic signal system and the egress actuator. The processor may be configured to receive, from an aircraft controller, a flight characteristic, and select, based on the flight characteristic, an ejection mode from two ejection modes. The processor may be further configured to receive a pilot egress command from the ballistic signal system, and transmit, to the egress actuator, a signal to actuate the ejection mode from the two ejection modes.
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