公开(公告)号：US11971236B1

公开(公告)日：2024-04-30

申请号：US17929693

申请日：2022-09-03

申请人： Manufacturing Made Simple LLC

发明人： Jerry A. James

IPC分类号： F41A23/00 ,  A47B81/00 ,  F41A23/18

CPC分类号： F41A23/18 ,  A47B81/005 ,  F41A23/00

摘要： A bracket mountable on a door hinge for supporting a gun holder behind an open door. The bracket includes a docking station and an adapter. The docking station mounts to the hinge. The adapter attaches to any gun holder, such as a holster. The gun is stowed in the gun holder on the docking station until needed. When needed, the gun is withdrawn from the mounted holster. Or, the holstered gun with the adapter attached can be lifted out of the docking station to carry or relocate it. Alternately, the gun holder may be a magnet with or without a magnetically transparent holster. The magnet stays attached to the adapter, which is left in the docking station. The gun—holstered or unholstered—adheres magnetically to the bracketed magnet. When needed, the gun is pulled off the magnet and returned to a carry position.

公开(公告)号：US20180266622A1

公开(公告)日：2018-09-20

申请号：US15984549

申请日：2018-05-21

申请人： Suspension Systems Technologies, LLC

发明人： William E. Woodbury, II

IPC分类号： F16M11/24

CPC分类号： F16M11/24 ,  B60G15/12 ,  B60N2/501 ,  B60N2/502 ,  B60N2/505 ,  B60N2/506 ,  B60N2/508 ,  B60N2/522 ,  B60N2/527 ,  B60N2/544 ,  B64D11/06 ,  B64D11/0619 ,  F16F9/06 ,  F16F9/535 ,  F16F13/002 ,  F16F15/002 ,  F16F15/02 ,  F16F15/022 ,  F16F2222/12 ,  F16F2230/0052 ,  F16F2232/08 ,  F41A23/00 ,  F41A23/12

摘要： Various embodiments of the present technology may comprise a method and apparatus for a space-saving suspension system. In various embodiments, the apparatus may comprise a fine suspension device, a coarse suspension device, and a mechanical assembly. In various embodiments, the fine suspension device is arranged at an angle greater than zero degrees from the z-axis. In various embodiments, the mechanical assembly is coupled to the fine suspension device and a payload, such that when a force is exerted on the mechanical assembly by the payload, an applied force is transmitted to the fine suspension device.

公开(公告)号：US20180134414A1

公开(公告)日：2018-05-17

申请号：US15869334

申请日：2018-01-12

申请人： ABBAS ALIKOUHI

发明人： ABBAS ALIKOUHI

IPC分类号： B64G1/00 ,  B64B1/06 ,  B64B1/58 ,  B64B1/70 ,  F41B11/68 ,  F41B11/70

CPC分类号： B64G1/005 ,  B64B1/06 ,  B64B1/50 ,  B64B1/58 ,  B64B1/70 ,  B64B2201/00 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/128 ,  B64C2201/148 ,  B64G1/409 ,  F41A1/00 ,  F41A1/10 ,  F41A21/36 ,  F41A23/00 ,  F41A23/02 ,  F41B11/64 ,  F41B11/68 ,  F41B11/70 ,  F41C9/08 ,  F41F3/06 ,  F42B15/00 ,  F42B15/10

摘要： Disclosed is a high altitude space launcher system for transferring payloads from surface to orbit at a significantly lower cost than conventional rockets. It comprises a aerostat lifted one stage light gas gun operating in stratosphere that shoots rocket assisted projectiles containing payload at near orbital velocities to a low angle trajectory. Alternatively, to launch acceleration sensitive payloads such as astronauts the light gas gun is replaced with a muzzle loaded conventional gun that shoots a single stage rocket at a much lower velocity. The system is mostly static structure, attached to a tether-elevator that moors it to land or a ship and provided it with electricity and lifts the projectiles to the gun.

公开(公告)号：US09688405B2

公开(公告)日：2017-06-27

申请号：US13782621

申请日：2013-03-01

申请人： Cantine Armament, Inc.

发明人： Christopher Cantine ,  John Croghan ,  Andrew Scott

IPC分类号： B64D7/00 ,  B64D9/00 ,  F41A23/00

CPC分类号： B64D7/00 ,  B64D9/00 ,  F41A23/00

摘要： A mounting system is provided including a center platform having a plurality of mounting lugs for mounting the center platform transversely extending at least partially through an aircraft cabin with a first end and second end of the center platform adjacent a respective first and second side opening of the aircraft cabin. A first support pylon may be removably coupleable to the first end of the center platform to extend outwardly from a first side of the aircraft. A second support pylon may be removably coupleable to the second end of the center platform to extend outwardly form a second side of the aircraft. A modular floor component may be removably coupleable relative to a longitudinal side of the center platform to provide a substantially planar load surface including a top portion of the modular floor component and a top surface of the center platform.

公开(公告)号：US20170108305A1

公开(公告)日：2017-04-20

申请号：US15311308

申请日：2014-05-15

申请人： SAAB AB

发明人： Gustav HEURLIN

IPC分类号： F41A23/00

CPC分类号： F41A23/005 ,  F41A23/00 ,  F41G11/001 ,  F41G11/003

摘要： The present invention regards a line-of-sight apparatus locking arrangement for demountable securing a line-of-sight apparatus to said arrangement, comprising a locking device for locking the apparatus to the arrangement comprises a handle member adapted for attachment to a rotation mechanism coupled to a translation mechanism adapted for, during manoeuvre of the locking device, converting rotational motion into translator motion, a pressing portion of the translation mechanism is provided for abutment against an abutment area of the apparatus. The translation mechanism comprises a resilient member provided for urging said pressing portion against the abutment area.

公开(公告)号：US20170089658A1

公开(公告)日：2017-03-30

申请号：US15311286

申请日：2014-05-15

申请人： SAAB AB

发明人： Gustav Heurlin

IPC分类号： F41A23/00

CPC分类号： F41A23/005 ,  F41A23/00 ,  F41A23/18 ,  F41A23/24 ,  F41G11/001

摘要： The present invention regards a line-of-sight apparatus locking arrangement for demountable securing a line-of-sight apparatus to said arrangement. The arrangement comprises a first and second locking device, each of which comprising a handle member adapted for attachment to a rotation mechanism coupled to a translation mechanism adapted for, during manoeuvre of the locking device, converting rotational motion into translator motion, each translation mechanism comprises a pressing portion provided for abutment against an abutment area of the apparatus.

公开(公告)号：US20140263107A1

公开(公告)日：2014-09-18

申请号：US13833642

申请日：2013-03-15

申请人： COVERED 6, LLC

发明人： Robert Arabian ,  Chris L. Dunn

IPC分类号： A47B81/00

CPC分类号： A47B81/005 ,  B60R7/14 ,  E05B1/00 ,  F41A23/00 ,  F41A23/26 ,  F41C33/06 ,  G07C9/00126 ,  G07C9/00912

摘要： In one embodiment there is provided a long gun rack system. The system includes an L-shaped frame; a butt cap secured to the side to accommodate a butt end of the gun; a handcuff ratchet lock mechanism secured to the frame at a position to accommodate the barrel, the lock mechanism configured to unlock in response to the receipt of an electronic code or in response to a key; an electronic security mechanism secured to the frame and is in communication with the lock mechanism; and a side plate having a cut-out region is secured along the frame at a position defined between the lock mechanism and the frame, such that the cut-out region permits the plate to mount in close proximity to the long gun and blocks the removal of the takedown pins and/or the full movement of a charging handle.

摘要翻译： 在一个实施例中，提供了长枪支架系统。 该系统包括L形框架; 一个对接帽固定在一边以容纳枪的对接端; 手套棘轮锁定机构，其在容纳筒的位置处固定到框架，所述锁定机构被配置为响应于接收到电子代码或响应于钥匙来解锁; 电子安全机构，固定在框架上并与锁定机构连通; 并且具有切口区域的侧板沿着框架固定在限定在锁定机构和框架之间的位置处，使得切口区域允许板安装在靠近长枪的位置并阻止移除 的拆卸销和/或充电手柄的全部运动。

公开(公告)号：US20140215889A1

公开(公告)日：2014-08-07

申请号：US14346158

申请日：2012-09-20

申请人： IMPERO ENTERPRISES PTY LTD

发明人： Michael Abdennour ,  Steven Abdennour

IPC分类号： F41A23/02 ,  F41A23/34

CPC分类号： F41A23/34 ,  F41A23/00 ,  F41A23/02 ,  F41A23/04 ,  F41A23/16 ,  F41C27/00

摘要： A portable gun rest made substantially from a block of polymer foam material, featuring magnets attached to at least one surface opposite said groove to enable the gun rest to be removably attached to a metal surface.

摘要翻译： 基本上由聚合物泡沫材料块制成的便携式枪支架，其特征在于，磁体附接到与所述凹槽相对的至少一个表面，以使枪支架可移除地附接到金属表面。

公开(公告)号：US08662064B1

公开(公告)日：2014-03-04

申请号：US13773186

申请日：2013-02-21

申请人： Charles Campbell

发明人： Charles Campbell

IPC分类号： F41B5/20 ,  F41A23/00 ,  F41B5/14

CPC分类号： F41B5/1426 ,  F41A23/00

摘要： The invention disclosed is an apparatus and method for stabilizing an archery bow and reducing recoil during arrow draw and release. The apparatus comprises an adjustable arm clamp assembly; a rod; a support body for attaching the arm clamp assembly to the rod; and a mounting block for attaching the rod to an archery bow. The archery recoil stabilizer is lightweight, adjustable and relies on bracing the arm from the forearm position to restrict translational and rotational movement of the bow as well as minimize recoil impacts. It supports the arm by bracing the forearm relative to the bow, and reduces or eliminates bow hand torque, providing improved stabilization during both arrow draw and release. Additionally, this invention reduces the stress and recoil on the arm of the archer that can cause pain or injury, or can compromise the flight of the arrow and the accuracy of the shot.

摘要翻译： 所公开的发明是用于在箭头拉出和释放期间稳定射箭弓并减少后坐力的装置和方法。 该装置包括一个可调臂臂组件; 一根杆 用于将臂夹具组件附接到杆的支撑体; 以及用于将杆附接到射箭弓的安装块。 射箭反弹稳定器重量轻，可调节，并且依靠从前臂位置支撑臂，以限制弓的平移和旋转运动，并最大限度地减少后坐冲击。 它通过相对于弓弓支撑前臂来支撑臂，并且减少或消除弓形手扭矩，在箭头拉伸和释放期间提供改进的稳定性。 此外，本发明减少了可能引起疼痛或受伤的弓箭手臂上的应力和反冲，或者可能损害箭头的飞行和射击的准确性。

公开(公告)号：US20120049009A1

公开(公告)日：2012-03-01

申请号：US13118509

申请日：2011-05-30

申请人： Waldemar F. Kissel, JR.

发明人： Waldemar F. Kissel, JR.

IPC分类号： B64C39/06

CPC分类号： B64C39/001 ,  B64C29/0025 ,  B64C39/024 ,  B64C39/064 ,  B64C2201/027 ,  B64C2201/108 ,  F41A23/00 ,  F41H5/24 ,  F41H7/00

摘要： Disclosed is a Powered Wing Aircraft. A generalized stabilizer/directional vent is used for providing a standard range of aeronautical control. It controls cross winds, directional velocity, directional control, and torque balancing in one simple easy to control device. It is attached to the axles. These improvements can apply to both military and civilian applications.

摘要翻译： 公开了一种动力翼飞机。 通用的稳定器/定向排气口用于提供标准的航空控制范围。 它在一个简单易于控制的设备中控制交叉风，方向速度，方向控制和扭矩平衡。 它连接到轴。 这些改进可以适用于军事和民用应用。