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1.发明申请公开(公告)号：US20180065202A1
公开(公告)日：2018-03-08
申请号：US15259921
申请日：2016-09-08
Applicant: Raytheon Company
Inventor： Matthew H. Summers , Jeremy C. Danforth , David G. Garrett , Dmitry V. Knyazev , Stephen M. Baggs , Gaines S. Gibson
CPC classification number: B23K1/0016 , B23K35/0244 , B23K2101/36 , B33Y10/00 , B33Y80/00 , F42B10/661 , H01R4/02 , H01R4/027 , H01R12/51 , H01R12/57 , H01R13/6658 , H01R43/02 , H05K1/0272 , H05K3/3494 , H05K2201/09036 , H05K2203/081
Abstract: A method of making an electrical connection includes soldering using channels in a receptacle to direct hot air (or another hot gas) to effect soldering where the electrical connection is to be made. The connection may be made between device electrical contacts of an electrical device, and other contacts, such as receptacle contacts of the receptacle. The connection may be a blind connection, one in which the connected ends of the contacts are hidden or unable to be directly physically accessed, when the connection is made. The electrical connection may be made between device contacts of an electrical device that is inserted into the receptacle, and receptacle electrical contacts that are part of the receptacle. The channels for directing the hot gas to where the soldering occurs may be parts of the receptacle, for example being produced during additive manufacture of the receptacle.
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公开(公告)号：US20170167833A1
公开(公告)日：2017-06-15
申请号：US14966731
申请日：2015-12-11
Applicant: Raytheon Company
Inventor： Gaston P. Jennett , Kim L. Christianson , Dmitry V. Knyazev , Henri Y. Kim , Robert P. Johnson
CPC classification number: F42B12/32 , F42B1/028 , F42B1/032 , F42B1/036 , F42B12/10 , F42B12/22 , F42B12/76 , F42B33/00
Abstract: A liner includes a plurality of individual projectile cells and a web of joining material holding the plurality of projectile cells in a monolithic and continuous structure. The liner is cylindrical and formed of an additive manufacturing process.
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公开(公告)号：US12281878B2
公开(公告)日：2025-04-22
申请号：US17404747
申请日：2021-08-17
Applicant: Raytheon Company
Inventor： Dmitry V. Knyazev , James P. Henderson , Jeremy J. Radtke
Abstract: A method includes removably coupling a projectile interface of a dongle to a dongle interface of a projectile. The method also includes loading a dongle code from the dongle onto the projectile. The dongle code identifies a pulse repetition frequency (PRF) code to be recognized by the projectile. The dongle code may be unique to an operator of the projectile. The method may further include, prior to loading the dongle code onto the projectile, loading an operator code onto the projectile, where the dongle code is loaded onto the projectile in response to the projectile authorizing the operator code. There may be a limited number of uses of the dongle code with different projectiles, and/or there may be a limited amount of time for using the dongle code. A companion electronic device may be used to authenticate the dongle.
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公开(公告)号：US10578411B2
公开(公告)日：2020-03-03
申请号：US14972211
申请日：2015-12-17
Applicant: Raytheon Company
Inventor： Gaston P. Jennett , Dmitry V. Knyazev , Robert P. Johnson , Morgan J. Bakarich , Michael A. Schurr
Abstract: An explosive device, such as a munition or a part of a munition, has an explosive material surrounded by a casing that has one or more voids within the casing. The one or more voids define sizes and shapes of the fragments that the casing breaks into when the explosive material is detonated. The casing may be made using an additive manufacturing process, with the one or more voids fully between an inner surface of the casing and an outer surface of the casing. The voids may substantially define the size and shape of fragments making up a majority of the volume of the casing, such as 75% or more of the volume of the casing. The voids may change direction within the casing, for example branching and intersecting to define a plurality of rectangular (parallelepiped) or other shaped fragments.
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公开(公告)号：US20180069352A1
公开(公告)日：2018-03-08
申请号：US15259875
申请日：2016-09-08
Applicant: Raytheon Company
Inventor： Matthew H. Summers , Jeremy C. Danforth , David G. Garrett , Dmitry V. Knyazev , Stephen M. Baggs , Gaines S. Gibson
IPC: H01R13/703 , F02K9/38 , H01R43/26
CPC classification number: H01R13/7032 , F02K9/38 , F05D2260/99 , F42B3/182 , F42B10/661 , H01R13/6658 , H01R13/7031 , H01R43/26
Abstract: An electrical device has device electrical contacts that are initially shunted together, to prevent accidental triggering or damage to the device, such as by electrostatic forces. The device is configured to be inserted into a receptacle, with parts of the receptacle disengaging the shunt and making electrical connection within the receptacle, such as with a shunt cutter. The receptacle may also include a pair of receptacle electrical contacts the electrically connect to the device electrical contacts. The configuration, where the shunt is only cut as part of the installation process, enables safer handling of initially-shunted devices, and can also facilitate making blind electrical connections. Making blind connection directly with parts of the receptacle also avoids the need to thread wires through the electrical receptacle and make electrical connections in another way.
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Patent Agency Ranking
公开(公告)号：US10662898B2
公开(公告)日：2020-05-26
申请号：US15259945
申请日：2016-09-08
Applicant: Raytheon Company
Inventor： Matthew H. Summers , Jeremy C. Danforth , David G. Garrett , Dmitry V. Knyazev , Stephen M. Baggs , Gaines S. Gibson
IPC: F02K9/34 , F42B10/66 , F02K9/30 , F02K9/88 , F02K9/97 , F02K9/38 , F02K9/08 , F02K9/36 , F02K9/95
Abstract: A thruster has an additively-manufactured housing that includes an integrally-formed nozzle with a burst disk in it. The housing is part of a casing that surrounds and encloses a propellant that is burned to produce pressurized gases that burst the burst disk and produce thrust. The thruster may be placed in a receptacle that defines a recess for receiving the thruster. The receptacle also may be additively manufactured. The thruster and the recess both may be cylindrical, with the housing being closely fit with the cylindrical walls of the receptacle. This may allow some of the structural loads on the housing, such as loads produced by the combustion of the propellant, to be transferred to the adjoining walls of the receptacle. This enables the housing to have less structural strength than if it were to have to contain the pressure from the propellant all on its own.
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公开(公告)号：US20170175234A1
公开(公告)日：2017-06-22
申请号：US14973788
申请日：2015-12-18
Applicant: Raytheon Company
Inventor： Gaston P. Jennett , Robert P. Johnson , Dmitry V. Knyazev , Richard G. Ames
CPC classification number: C22C30/00 , B22F3/1055 , B22F7/06 , B22F2998/10 , B22F2999/00 , B33Y10/00 , B33Y80/00 , C22C1/045 , Y02P10/295 , B22F1/025 , B22F2202/07 , B22F2003/248
Abstract: A heavy metal part and method of manufacturing includes a dense alloy or a metallic composite consisting of a plurality of dense metal particles formed of a first metal and a melted metal matrix that is a continuous phase of the first metal and a second metal having a lesser density than the first metal. The metal particles are a discrete phase within the continuous phase and the heavy metal part is formed by an additive manufacturing process of a powder feedstock comprising the metal particles coated with the second metal.
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公开(公告)号：US20160178336A1
公开(公告)日：2016-06-23
申请号：US14972211
申请日：2015-12-17
Applicant: Raytheon Company
Inventor： Gaston P. Jennett , Dmitry V. Knyazev , Robert P. Johnson , Morgan J. Bakarich , Michael A. Schurr
CPC classification number: F42B12/24 , F42B12/207 , F42B12/22 , F42B12/32
Abstract: An explosive device, such as a munition or a part of a munition, has an explosive material surrounded by a casing that has one or more voids within the casing. The one or more voids define sizes and shapes of the fragments that the casing breaks into when the explosive material is detonated. The casing may be made using an additive manufacturing process, with the one or more voids fully between an inner surface of the casing and an outer surface of the casing. The voids may substantially define the size and shape of fragments making up a majority of the volume of the casing, such as 75% or more of the volume of the casing. The voids may change direction within the casing, for example branching and intersecting to define a plurality of rectangular (parallelepiped) or other shaped fragments.
Abstract translation: 诸如弹药或弹药的一部分的爆炸装置具有由壳体围绕的爆炸物质，其在壳体内具有一个或多个空隙。 一个或多个空隙定义当爆炸物质被引爆时壳体断裂的碎片的尺寸和形状。 壳体可以使用添加剂制造方法制造，其中一个或多个空隙完全在壳体的内表面和壳体的外表面之间。 空隙可以基本上限定构成壳体体积的大部分的碎片的尺寸和形状，例如壳体体积的75％或更多。 空隙可以改变壳体内的方向，例如分支和相交以限定多个矩形（平行六面体）或其它成形碎片。
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公开(公告)号：US12241718B2
公开(公告)日：2025-03-04
申请号：US17931657
申请日：2022-09-13
Applicant: Raytheon Company
Inventor： Richard O. Beaman , Dmitry V. Knyazev , Peter D. Dunning
IPC: F41F3/055
Abstract: A launcher for launching a flying vehicle, such as a projectile or missile, includes a cutter for cutting a line, such as an umbilical line, that is coupled to the vehicle prior to launch. An example of a line is a tube for providing cooling for onboard components of the vehicle, such as a seeker of the vehicle. The cutter may be part of a mount of the launcher for mounting the line and other components, such as a compressor. The cutter may be configured so that as the vehicle translates relative to the launcher during the initiation of launch, the line moves against the cutter, severing the line. The cutter may retract after severing the line, for example being pulled away from the vehicle (and into the mount) by a spring mechanism.
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公开(公告)号：US20240093964A1
公开(公告)日：2024-03-21
申请号：US17931657
申请日：2022-09-13
Applicant: Raytheon Company
Inventor： Richard O. Beaman , Dmitry V. Knyazev , Peter D. Dunning
IPC: F41F3/055
CPC classification number: F41F3/055
Abstract: A launcher for launching a flying vehicle, such as a projectile or missile, includes a cutter for cutting a line, such as an umbilical line, that is coupled to the vehicle prior to launch. An example of a line is a tube for providing cooling for onboard components of the vehicle, such as a seeker of the vehicle. The cutter may be part of a mount of the launcher for mounting the line and other components, such as a compressor. The cutter may be configured so that as the vehicle translates relative to the launcher during the initiation of launch, the line moves against the cutter, severing the line. The cutter may retract after severing the line, for example being pulled away from the vehicle (and into the mount) by a spring mechanism.
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