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公开(公告)号:US12050093B2
公开(公告)日:2024-07-30
申请号:US17533658
申请日:2021-11-23
申请人: G9 Holdings, LLC
发明人: Joshua Mahnke
IPC分类号: F42B10/26 , F42B10/22 , F42B10/24 , F42B10/46 , F42B12/02 , F42B12/06 , F42B12/34 , F42B12/74 , F42B30/02
CPC分类号: F42B12/02 , F42B10/22 , F42B10/24 , F42B10/26 , F42B10/46 , F42B12/06 , F42B12/34 , F42B12/74 , F42B30/02
摘要: The present invention provides a projectile device and a method of manufacture of a projectile device and in particular, to a pistol bullet and a rifle bullet and method of manufacture of same. In one embodiment, the projectile apparatus has a cylindrical body portion having a diameter, a front nose section tapering from a most proximal point of the projectile to the cylindrical body portion, and a rear tail section connected to the body portion and extending to the most distal point of the projectile, in which the front nose portion comprises a plurality of twisting depressions forming troughs.
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公开(公告)号:US11808550B2
公开(公告)日:2023-11-07
申请号:US17354347
申请日:2021-06-22
申请人: G9 Holdings, LLC
发明人: Joshua Mahnke
IPC分类号: F42B10/24 , F42B12/34 , F42B12/02 , F42B12/74 , F42B10/22 , F42B10/26 , F42B10/46 , F42B12/06 , F42B30/02
CPC分类号: F42B12/02 , F42B10/22 , F42B10/24 , F42B10/26 , F42B10/46 , F42B12/06 , F42B12/34 , F42B12/74 , F42B30/02
摘要: The present invention provides a projectile device and a method of manufacture of a projectile device and in particular to a pistol bullet and a rifle bullet and method of manufacture of the same. In one embodiment, the projectile apparatus has a cylindrical body portion having a diameter, a front nose section tapering from a most proximal point of the projectile to the cylindrical body portion, and a rear tail section connected to the body portion and extending to the most distal point of the projectile, in which the front nose portion comprises a plurality of twisting depressions forming troughs.
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公开(公告)号:US20230264836A1
公开(公告)日:2023-08-24
申请号:US18140122
申请日:2023-04-27
发明人: Miles R. Palmer
IPC分类号: B64G1/00 , B64G5/00 , F41A1/02 , F41B11/62 , F41B11/68 , F41B11/723 , B64F1/02 , B64F1/04 , F42B12/02
CPC分类号: B64G1/002 , B64F1/025 , B64F1/04 , B64G5/00 , F41A1/02 , F41B11/62 , F41B11/68 , F41B11/723 , F42B12/02
摘要: The present disclosure relates to a launch system and method. The launch system and method can include at least a preliminary accelerator tube system (PAT) that can be combined with a main accelerator tube system (MAT). The PAT alone or combined with the MAT can be used for launch of a vehicle for testing and/or for delivery of a payload.
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公开(公告)号:US20220260351A1
公开(公告)日:2022-08-18
申请号:US17533658
申请日:2021-11-23
申请人: G9 Holdings, LLC
发明人: Joshua Mahnke
IPC分类号: F42B12/02 , F42B12/74 , F42B10/22 , F42B10/24 , F42B10/26 , F42B10/46 , F42B12/06 , F42B30/02
摘要: The present invention provides a projectile device and a method of manufacture of a projectile device and in particular, to a pistol bullet and a rifle bullet and method of manufacture of same. In one embodiment, the projectile apparatus has a cylindrical body portion having a diameter, a front nose section tapering from a most proximal point of the projectile to the cylindrical body portion, and a rear tail section connected to the body portion and extending to the most distal point of the projectile, in which the front nose portion comprises a plurality of twisting depressions forming troughs.
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公开(公告)号:US11067374B2
公开(公告)日:2021-07-20
申请号:US16153696
申请日:2018-10-05
发明人: Jeffrey Hill
IPC分类号: F42B15/01 , G05D1/00 , F42B10/38 , G06K9/00 , F42C13/04 , F42B12/02 , F42B15/10 , H04N7/18 , F42C1/00
摘要: An ordnance for air-borne delivery to a target under remotely controlled in-flight navigation. In one embodiment, self-powered aerial ordnance includes upper and lower cases. A plurality of co-axial, deployable blades is powered by a motor positioned in the upper case. When deployed, the blades are rotatable about the upper case to impart thrust and bring the vehicle to a first altitude above a target position. An explosive material and a camera are positioned in a lower case which is attached to the upper case. The camera generates a view along the ground plane and above the target when the ordinance is in flight. When the vehicle is deployed it is remotely controllable to deliver the vehicle to the target to detonate the explosive at the target. The ordnance may drop directly on a target as a bomb does.
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公开(公告)号:US11041703B2
公开(公告)日:2021-06-22
申请号:US16707820
申请日:2019-12-09
申请人: G9 Holdings, LLC
发明人: Joshua Mahnke
IPC分类号: F42B10/24 , F42B12/06 , F42B12/02 , F42B12/74 , F42B10/22 , F42B10/26 , F42B10/46 , F42B30/02
摘要: The present invention provides a projectile device and a method of manufacture of a projectile device and in particular to a pistol bullet and a rifle bullet and method of manufacture of same. In one embodiment, the projectile apparatus has a cylindrical body portion having a diameter, a front nose section tapering from a most proximal point of the projectile to the cylindrical body portion, and a rear tail section connected to the body portion and extending to the most distal point of the projectile, in which the front nose portion comprises a plurality of twisting depressions forming troughs.
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公开(公告)号:US11031885B1
公开(公告)日:2021-06-08
申请号:US15966193
申请日:2018-04-30
申请人: Dmitriy Yavid
发明人: Dmitriy Yavid
摘要: An electric power generator for a projectile moving through the air is based on vibrational, rather than rotational motion. The electric power generator uses an air stream through, which the projectile is traveling typically 100-250 m/s for mortars to up to 1,500 m/s for sabot or even higher electrically fired rounds. A typical 223 rifle round after being fired has energy of over 1700 J, which is equivalent to 1700 W seconds. If a Nano computer was able to extract energy of for example 50 nanowatts during bullet flight which rarely exceeds two seconds the power needed during the flight would be only a few parts per billion of the bullets energy. Even allowing for very inefficient extraction of power, the necessary power to operate on onboard electronic devices such as computers and sensors can be extracted from the airstream through which the projectile travels.
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公开(公告)号:US20200284564A1
公开(公告)日:2020-09-10
申请号:US16724304
申请日:2019-12-22
发明人: David E. Emary
摘要: A bullet with controlled fragmentation has a core in the form of a generally cylindrical body having a forward end and a rear end and intermediate side portions extending there between, the forward end of the core defining a cavity, a jacket encompassing the rear end and at least selected portions of the sides of the core, the jacket having a sidewall having a first drive band portion having a first wall thickness, and a second portion immediately forward of the drive band portion having a second thickness less than the first thickness, the exterior of the jacket defining a cannelure groove encircling the bullet, and the cannelure groove being positioned forward of the first drive band portion. The drive band may have forward edge defining a step. The bullet of the present invention may also be received in the case mouth of a rimless case and be partially protruding therefrom.
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公开(公告)号:US20200064111A1
公开(公告)日:2020-02-27
申请号:US16423747
申请日:2019-05-28
发明人: David B. Fricke
摘要: A projectile has a base, a tip, and a body axis intersecting the base at a trailing axis point and the tip at a leading axis point. The projectile includes a meplat that is substantially orthogonal to the body axis and a plurality of standoffs that extend away from both the trailing axis point and the leading axis point.
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公开(公告)号:US10168131B2
公开(公告)日:2019-01-01
申请号:US14358892
申请日:2012-11-30
申请人: RUAG AMMOTECH GMBH
发明人: Heinz Riess
摘要: The invention relates to a method for producing a core (1) for a projectile (2). So that the dividing behavior of the projectile can be set in a simple manner, wherein the core is lead-free, it is proposed that one or more wires or wire sections composed of a lead-free material are compressed to form a cavity-free core (1), wherein the wires or wire sections have one or more geometrical shapes (3) in the interior or on the outside diameter and/or predetermined braking points (4) obtained during the compression are provided in the core (1).
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