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公开(公告)号：US10793486B2
公开(公告)日：2020-10-06
申请号：US16117408
申请日：2018-08-30
Applicant: Goodrich Corporation
Inventor： Jerry A. Lambert , Luis G. Interiano
Abstract: Methods and systems for an explosive cord are disclosed. An explosive cord may comprise a tubing comprising an inner surface and an outer surface, a reactive material comprising hexanitrostilbene and/or boron potassium nitrate coupled to the inner surface of the tubing, and a hollow or solid core through the center of the explosive cord.
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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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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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公开(公告)号：US20200088137A1
公开(公告)日：2020-03-19
申请号：US16136125
申请日：2018-09-19
Applicant: GOODRICH CORPORATION
Inventor： Luis G. Interiano
IPC: F02K9/38
Abstract: A thermally initiated variable venting system may comprise a first linear shape charge (LSC) coupled to a first sensor and a second LSC coupled to a second sensor. An upper apex of the second LSC may be disposed within a lower apex of the first LSC. The output of the system may vary depending on whether the event is fast cook-off (FCO) or slow cook-off (SCO).
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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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Patent Agency Ranking
公开(公告)号：US20230250038A1
公开(公告)日：2023-08-10
申请号：US17666837
申请日：2022-02-08
Applicant: Goodrich Corporation , Raytheon Company
Inventor： Thomas Michael Deppert , Luis G. Interiano , Jerry A. Lambert , Carl Shanholtz
IPC: C06B21/00
CPC classification number: C06B21/0091
Abstract: A method for removing a gas from a propellant composition includes providing an uncured propellant composition comprising a bonding agent, energetic particles, and a polymeric binder, and flowing an inert gas through the uncured propellant composition to remove an evolved gas from the uncured propellant composition.
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公开(公告)号：US20220307449A1
公开(公告)日：2022-09-29
申请号：US17213081
申请日：2021-03-25
Applicant: Goodrich Corporation
Inventor： Matthew D. Salois , Luis G. Interiano
Abstract: A method for generating electric power for a rocket system includes burning a primary solid propellant grain to create a primary high pressure gas for providing thrust to the rocket, opening a first valve to divert a portion of the high pressure gas to an auxiliary solid propellant grain for igniting the auxiliary solid propellant grain, wherein the auxiliary solid propellant grain is disposed in a housing separate from the primary solid propellant grain, and burning the auxiliary solid propellant grain to create an auxiliary high pressure gas for turning a turbine. The method further includes driving a generator with the turbine and generating an electric power with the generator.
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公开(公告)号：US20200024212A1
公开(公告)日：2020-01-23
申请号：US16117408
申请日：2018-08-30
Applicant: Goodrich Corporation
Inventor： Jerry A. Lambert , Luis G. Interiano
Abstract: Methods and systems for an explosive cord are disclosed. An explosive cord may comprise a tubing comprising an inner surface and an outer surface, a reactive material comprising hexanitrostilbene and/or boron potassium nitrate coupled to the inner surface of the tubing, and a hollow or solid core through the center of the explosive cord.
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公开(公告)号：US10087119B2
公开(公告)日：2018-10-02
申请号：US15652647
申请日：2017-07-18
Applicant: Goodrich Corporation
Inventor： Jerry A. Lambert , Luis G. Interiano
Abstract: Methods and systems for an explosive cord are disclosed. An explosive cord may comprise a tubing comprising an inner surface and an outer surface, a reactive material comprising hexanitrostilbene and/or boron potassium nitrate coupled to the inner surface of the tubing, and a hollow or solid core through the center of the explosive cord.
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公开(公告)号：US11598618B1
公开(公告)日：2023-03-07
申请号：US17496490
申请日：2021-10-07
Applicant: GOODRICH CORPORATION
Inventor： Leo P. Leighton , Matthew Salois , Luis G. Interiano , Kevin Mueller
IPC: F42C15/184 , F42C9/10 , F42C15/31
Abstract: A damper system for a pyrotechnic time delay may comprise: a firing pin; a moveable housing defining a chamber therein; a fixed piston comprising a piston head disposed in the chamber, a first rod extending from the piston head axially outward of the moveable housing, and a second rod configured to fixedly couple to a housing; a first spring extending axially from the moveable housing to the firing pin; and a second spring extending axially from the moveable housing to the firing pin.
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