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公开(公告)号：US20160150627A1
公开(公告)日：2016-05-26
申请号：US15011405
申请日：2016-01-29
Applicant: General Fusion Inc.
Inventor： Stephen James Howard , Michel Georges Laberge , Lon McIlwraith , Douglas Harvey Richardson , James Gregson
Abstract: Embodiments of systems and methods for compressing plasma are disclosed in which plasma can be compressed by impact of a projectile on a magnetized plasma in a liquid metal cavity. The projectile can melt in the liquid metal cavity, and liquid metal may be recycled to form new projectiles.
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公开(公告)号：US09267515B2
公开(公告)日：2016-02-23
申请号：US14385898
申请日：2013-04-04
Applicant: General Fusion, Inc.
Inventor： Victoria Suponitsky , Sandra Justine Barsky , J. Michel G. Laberge , Douglas Harvey Richardson , Peter Leszek Kostka
CPC classification number: B05B1/26 , F15D1/0005 , F15D1/08 , F17D1/00 , G21B3/008 , H05H1/24 , H05H2277/13 , Y10T137/0318 , Y10T137/86163
Abstract: Examples of a jet control device are described. The jet control device can comprise a jet deflecting member that is configured to intercept and/or collide with a high speed jet emerging from a jet formation location. The interaction of the jet deflecting member and the jet can cause the high speed jet to be dispersed into a plurality of jets with a number of flow directions which may be sideways to an initial direction of the high speed jet. In one embodiment the deflecting member can include a liquid guide formed by injecting a fluid out of an outlet nozzle so that the liquid guide extends longitudinally away from the outlet nozzle. In another embodiment the deflecting member can include an array of solid pellets injected through an outlet in a direction of the emerging high speed jet and configured to collide with the emerging jet thereby deflecting its initial direction.
Abstract translation: 描述喷射控制装置的实例。 喷射控制装置可以包括射流偏转构件，其构造成拦截和/或与从喷射形成位置出射的高速喷射器相撞。 喷射偏转构件和射流的相互作用可以使高速射流分散成多个喷射流，其中多个流动方向可以横向到高速射流的初始方向。 在一个实施例中，偏转构件可以包括通过将流体从出口喷嘴喷射而形成的液体引导件，使得液体引导件纵向远离出口喷嘴延伸。 在另一个实施例中，偏转构件可以包括通过出口沿着出现的高速射流的方向注入并配置成与出现的射流碰撞从而偏转其初始方向的固体粒子阵列。
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公开(公告)号：US09463478B2
公开(公告)日：2016-10-11
申请号：US14963868
申请日：2015-12-09
Applicant: General Fusion Inc.
Inventor： Victoria Suponitsky , Sandra Justine Barsky , J. Michel G. Laberge , Douglas Harvey Richardson , Peter Leszek Kostka
CPC classification number: B05B1/26 , F15D1/0005 , F15D1/08 , F17D1/00 , G21B3/008 , H05H1/24 , H05H2277/13 , Y10T137/0318 , Y10T137/86163
Abstract: Examples of a jet control device are described. The jet control device can comprise a jet deflecting member that is configured to intercept and/or collide with a high speed jet emerging from a jet formation location. The interaction of the jet deflecting member and the jet can cause the high speed jet to be dispersed into a plurality of jets with a number of flow directions which may be sideways to an initial direction of the high speed jet. In one embodiment the deflecting member can include a liquid guide formed by injecting a fluid out of an outlet nozzle so that the liquid guide extends longitudinally away from the outlet nozzle. In another embodiment the deflecting member can include an array of solid pellets injected through an outlet in a direction of the emerging high speed jet and configured to collide with the emerging jet thereby deflecting its initial direction.
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公开(公告)号：US20150034164A1
公开(公告)日：2015-02-05
申请号：US14385898
申请日：2013-04-04
Applicant: General Fusion, Inc.
Inventor： Victoria Suponitsky , Sandra Justine Barsky , J. Michel G. Laberge , Douglas Harvey Richardson , Peter Leszek Kostka
CPC classification number: B05B1/26 , F15D1/0005 , F15D1/08 , F17D1/00 , G21B3/008 , H05H1/24 , H05H2277/13 , Y10T137/0318 , Y10T137/86163
Abstract: Examples of a jet control device are described. The jet control device can comprise a jet deflecting member that is configured to intercept and/or collide with a high speed jet emerging from a jet formation location. The interaction of the jet deflecting member and the jet can cause the high speed jet to be dispersed into a plurality of jets with a number of flow directions which may be sideways to an initial direction of the high speed jet. In one embodiment the deflecting member can include a liquid guide formed by injecting a fluid out of an outlet nozzle so that the liquid guide extends longitudinally away from the outlet nozzle. In another embodiment the deflecting member can include an array of solid pellets injected through an outlet in a direction of the emerging high speed jet and configured to collide with the emerging jet thereby deflecting its initial direction.
Abstract translation: 描述喷射控制装置的实例。 喷射控制装置可以包括射流偏转构件，其构造成拦截和/或与从喷射形成位置出射的高速喷射器相撞。 喷射偏转构件和射流的相互作用可以使高速射流分散成多个喷射流，其中多个流动方向可以横向到高速射流的初始方向。 在一个实施例中，偏转构件可以包括通过将流体从出口喷嘴喷射而形成的液体引导件，使得液体引导件纵向远离出口喷嘴延伸。 在另一个实施例中，偏转构件可以包括通过出口沿着出现的高速射流的方向注入并配置成与出现的射流碰撞从而偏转其初始方向的固体粒子阵列。
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公开(公告)号：US20220151054A1
公开(公告)日：2022-05-12
申请号：US17607169
申请日：2020-05-28
Applicant: GENERAL FUSION INC.
Inventor： Stephen James Howard , Douglas Harvey Richardson , Michel Georges Laberge , Merritt Wayne Reynolds , Aaron Matthew Froese , Kelly Bernard Epp , Martin Clifford Wight , Yakov Gofman
Abstract: A method and system for stably generating and accelerating magnetized plasma comprises ionizing an injected gas in plasma generator and generating a formation magnetic field to form a magnetized plasma with a closed poloidal field, generating a reverse poloidal field behind the magnetized plasma and having a same field direction as a back edge of the closed poloidal field and having an opposite field direction of the formation magnetic field, and generating a pushing toroidal field that pushes the reverse poloidal field against the closed poloidal field, thereby accelerating the magnetized plasma through a plasma accelerator downstream from the plasma generator. The reverse poloidal field serves to prevent the reconnection of the formation magnetic field and closed poloidal field after the magnetized plasma is formed, which would allow the pushing toroidal field to mix with the closed poloidal field and cause instability and reduced plasma confinement.
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Patent Agency Ranking
公开(公告)号：US20160361729A1
公开(公告)日：2016-12-15
申请号：US15247740
申请日：2016-08-25
Applicant: General Fusion Inc.
Inventor： Victoria Suponitsky , Sandra Justine Barsky , J. Michel G. Laberge , Douglas Harvey Richardson , Peter Leszek Kostka
CPC classification number: B05B1/26 , F15D1/0005 , F15D1/08 , F17D1/00 , G21B3/008 , H05H1/24 , H05H2277/13 , Y10T137/0318 , Y10T137/86163
Abstract: Examples of a jet control device are described. The jet control device can comprise a jet deflecting member that is configured to intercept and/or collide with a high speed jet emerging from a jet formation location. The interaction of the jet deflecting member and the jet can cause the high speed jet to be dispersed into a plurality of jets with a number of flow directions which may be sideways to an initial direction of the high speed jet. In one embodiment the deflecting member can include a liquid guide formed by injecting a fluid out of an outlet nozzle so that the liquid guide extends longitudinally away from the outlet nozzle. In another embodiment the deflecting member can include an array of solid pellets injected through an outlet in a direction of the emerging high speed jet and configured to collide with the emerging jet thereby deflecting its initial direction.
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公开(公告)号：US10092914B2
公开(公告)日：2018-10-09
申请号：US15247740
申请日：2016-08-25
Applicant: General Fusion Inc.
Inventor： Victoria Suponitsky , Sandra Justine Barsky , J. Michel G. Laberge , Douglas Harvey Richardson , Peter Leszek Kostka
Abstract: Examples of a jet control device are described. The jet control device can comprise a jet deflecting member that is configured to intercept and/or collide with a high speed jet emerging from a jet formation location. The interaction of the jet deflecting member and the jet can cause the high speed jet to be dispersed into a plurality of jets with a number of flow directions which may be sideways to an initial direction of the high speed jet. In one embodiment the deflecting member can include a liquid guide formed by injecting a fluid out of an outlet nozzle so that the liquid guide extends longitudinally away from the outlet nozzle. In another embodiment the deflecting member can include an array of solid pellets injected through an outlet in a direction of the emerging high speed jet and configured to collide with the emerging jet thereby deflecting its initial direction.
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公开(公告)号：US20160107176A1
公开(公告)日：2016-04-21
申请号：US14963868
申请日：2015-12-09
Applicant: General Fusion Inc.
Inventor： Victoria Suponitsky , Sandra Justine Barsky , J. Michel G. Laberge , Douglas Harvey Richardson , Peter Leszek Kostka
CPC classification number: B05B1/26 , F15D1/0005 , F15D1/08 , F17D1/00 , G21B3/008 , H05H1/24 , H05H2277/13 , Y10T137/0318 , Y10T137/86163
Abstract: Examples of a jet control device are described. The jet control device can comprise a jet deflecting member that is configured to intercept and/or collide with a high speed jet emerging from a jet formation location. The interaction of the jet deflecting member and the jet can cause the high speed jet to be dispersed into a plurality of jets with a number of flow directions which may be sideways to an initial direction of the high speed jet. In one embodiment the deflecting member can include a liquid guide formed by injecting a fluid out of an outlet nozzle so that the liquid guide extends longitudinally away from the outlet nozzle. In another embodiment the deflecting member can include an array of solid pellets injected through an outlet in a direction of the emerging high speed jet and configured to collide with the emerging jet thereby deflecting its initial direction.
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9.发明授权公开(公告)号：US09271383B2
公开(公告)日：2016-02-23
申请号：US14518965
申请日：2014-10-20
Applicant: General Fusion, Inc.
Inventor： Stephen James Howard , Michel Georges Laberge , Lon McIlwraith , Douglas Harvey Richardson , James Gregson
Abstract: Embodiments of systems and methods for compressing plasma are disclosed in which plasma can be compressed by impact of a projectile on a magnetized plasma in a liquid metal cavity. The projectile can melt in the liquid metal cavity, and liquid metal may be recycled to form new projectiles.
Abstract translation: 公开了用于压缩等离子体的系统和方法的实施例，其中可以通过射弹对液态金属腔中的磁化等离子体的冲击来压缩等离子体。 抛射体可以在液态金属腔中熔化，并且液态金属可以被再循环以形成新的射弹。
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10.发明申请公开(公告)号：US20150036777A1
公开(公告)日：2015-02-05
申请号：US14518965
申请日：2014-10-20
Applicant: General Fusion, Inc.
Inventor： Stephen James Howard , Michel Georges Laberge , Lon McIlwraith , Douglas Harvey Richardson , James Gregson
Abstract: Embodiments of systems and methods for compressing plasma are disclosed in which plasma can be compressed by impact of a projectile on a magnetized plasma in a liquid metal cavity. The projectile can melt in the liquid metal cavity, and liquid metal may be recycled to form new projectiles.
Abstract translation: 公开了用于压缩等离子体的系统和方法的实施例，其中可以通过射弹对液态金属腔中的磁化等离子体的冲击来压缩等离子体。 抛射体可以在液态金属腔中熔化，并且液态金属可以被再循环以形成新的射弹。
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