专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明授权

US10670321B1 Ice chute 有权
公开(公告)号：US10670321B1
公开(公告)日：2020-06-02
申请号：US16748066
申请日：2020-01-21
申请人： Anthony Vella
发明人： Anthony Vella
IPC分类号： F25C5/20 , A47J31/40
摘要： An ice chute for an ice bin that includes a front uncovered portion having an opening through which ice is deposited into the ice bin. The frame may be removably inserted into the ice bin via the opening. Once inserted, a rear portion of the frame is located below a rear covered portion of the ice bin and a front portion of the frame is located at the opening. An inclined ramp extends upward around the front portion of the frame. When the frame is inserted into the ice bin, a top end of the ramp is positioned vertically above the opening. An area defined by the top end of the ramp is larger than an area of the opening. The ramp is sized and configured such that ice on the ramp slides downwards along the ramp and into the opening of the ice bin.

2. 发明授权

US07878120B1 Ammunition data link 有权
标题翻译：弹药数据链接
公开(公告)号：US07878120B1
公开(公告)日：2011-02-01
申请号：US12006752
申请日：2007-12-20
申请人： Robert Nodarse , Anthony Vella , Thomas V. Louzeiro , David P. Fairman, Jr. , Steven Pigliavento , Jessica M. Monahan , Amy Lynn Mera
发明人： Robert Nodarse , Anthony Vella , Thomas V. Louzeiro , David P. Fairman, Jr. , Steven Pigliavento , Jessica M. Monahan , Amy Lynn Mera
IPC分类号： F42B5/08
CPC分类号： F42B5/285 , F42C11/002 , F42C17/04 , F42C19/06
摘要： A cartridge includes a cartridge case base having a bottom surface, a primer and an annular recess formed in the bottom surface, the annular recess being concentric with the primer; first and second concentric conductive rings disposed in the annular recess, the first and second rings being radially spaced apart and substantially flush with the bottom surface of the cartridge case base, the first and second rings being electrically insulated from the cartridge case base and the primer; a first data pin electrically connected to the first conductive ring and extending into an interior of the cartridge case base; and a second data pin electrically connected to the second conductive ring and extending into the interior of the cartridge case base, the first and second data pins being electrically insulated from the cartridge case base.
摘要翻译：盒包括具有底表面的底盒，底座和形成在底表面中的环形凹槽，所述环形凹槽与底漆同心; 设置在环形凹部中的第一和第二同心导电环，第一和第二环径向间隔开并且基本上与盒壳体底部的底表面齐平，第一和第二环与盒壳体基底和引物电绝缘 ; 第一数据引脚，电连接到第一导电环并延伸到盒壳体的内部; 以及第二数据引脚，电连接到所述第二导电环并延伸到所述盒壳体的内部，所述第一和第二数据引脚与所述盒壳体基座电绝缘。

3. 发明授权

US06978967B1 Space saving fin deployment system for munitions and missiles 失效
标题翻译：用于弹药和导弹的节省空间的部署系统
公开(公告)号：US06978967B1
公开(公告)日：2005-12-27
申请号：US10709180
申请日：2004-04-20
申请人： Eric Scheper , Anthony Vella , Dave Maurizi , Andrew Molina
发明人： Eric Scheper , Anthony Vella , Dave Maurizi , Andrew Molina
IPC分类号： F42B10/00 , F42B10/16
CPC分类号： F42B10/16
摘要： A fin deployment system for missiles and munitions that deploys and activates straight flat fins for roll control authority. The fin deployment system employs numerous design features, among which are the following: A wrap-around fin concept generates space-savings within a projectile body whereby the fins are arranged in a wrapped configuration around a boomtail structure. The fins may be constructed of a super-elastic material; the system eliminates mechanical means of deploying the wrapped fins, eliminating the need for springs to deploy the fins. The fin deployment achieves substantial space savings for increasing the onboard towing capacity of electronic packaging or lethality in the missiles and munitions systems, while at the same time providing a good roll control authority during flight by enabling a straight fin deployment resulting from the use of super-elastic materials.
摘要翻译：用于导弹和弹药的翅片部署系统，用于部署并激活用于滚转控制权限的直扁平翅片。散热器部署系统采用众多的设计特征，其中包括以下内容：绕线散热器概念在射弹体内产生节省空间，由此散热片以围绕吊杆结构的缠绕结构布置。翅片可以由超弹性材料构成; 该系统消除了部署包裹翅片的机械手段，消除了弹簧部署翅片的需要。翅片部署实现了大量的空间节省，以增加导弹和弹药系统中电子包装或杀伤力的板载牵引能力，同时在飞行过程中提供良好的滚转控制权限，通过使用超级弹性材料。

4. 发明授权

US5841062A Tank cartridge 失效
标题翻译：罐筒
公开(公告)号：US5841062A
公开(公告)日：1998-11-24
申请号：US958640
申请日：1997-10-27
申请人： Leon Manole , Stewart Gilman , James Lee , Manuel Munoz , Peter Ngai , Anthony Vella , William Rice , Nick Zuback
发明人： Leon Manole , Stewart Gilman , James Lee , Manuel Munoz , Peter Ngai , Anthony Vella , William Rice , Nick Zuback
IPC分类号： F42B5/18
CPC分类号： F42B5/181 , F42B5/18 , Y10S102/70
摘要： A tank cartridge is described which is capable of withstanding rough handg during loading and unloading operations.
摘要翻译：描述了在装载和卸载操作期间能够承受粗略处理的储罐。

5. 发明授权

US09329008B1 Low collateral damage kinetic energy projectile 有权
标题翻译：低附带损伤动能射弹
公开(公告)号：US09329008B1
公开(公告)日：2016-05-03
申请号：US14444301
申请日：2014-07-28
申请人： Steven Gilbert , Ahmed Hassan , Yin Chen , Anthony Vella
发明人： Steven Gilbert , Ahmed Hassan , Yin Chen , Anthony Vella
IPC分类号： F42B12/02 , F42B12/74 , F42B14/06
CPC分类号： F42B12/02 , F42B10/48 , F42B12/06 , F42B12/74 , F42B14/06
摘要： A low collateral damage, kinetic energy penetrator has multiple segments that are mechanically locked together by centrifugal force generated by penetrator spin. When the penetrator spin decreases below a minimum value, the segments separate and fall to the ground with non-lethal kinetic energy.
摘要翻译：低附加损伤，动能穿透器具有通过穿透器旋转产生的离心力机械地锁定在一起的多个段。当穿透器旋转减小到最小值以下时，分段以非致死动能分离并落到地面。

6. 发明授权

US06983700B1 Variable drag projectile stabilizer for limiting the flight range of a training projectile 失效
标题翻译：用于限制训练射弹的飞行范围的可变阻力弹丸稳定器
公开(公告)号：US06983700B1
公开(公告)日：2006-01-10
申请号：US10709401
申请日：2004-05-03
申请人： Gregory Malejko , Anthony Vella , Eric P. Scheper , Philip M. Donadio
发明人： Gregory Malejko , Anthony Vella , Eric P. Scheper , Philip M. Donadio
IPC分类号： F42B8/00
CPC分类号： F42B10/48 , F42B10/02
摘要： A variable drag projectile stabilizer is utilized by a training projectile to match the trajectory of a tactical projectile for up to 3 km while having a range limitation of 8 km. The stabilizer applies supersonic flow phenomena to alter the aerodynamic characteristics of a training projectile while in free flight to fulfill this requirement. The stabilizer uses a cowling supported by struts to provide tail lift and ensure a stable flight path. Supersonic flow is established through ducts formed by the cowling and struts when launched from a weapon. The flow remains supersonic until the projectile reaches the desired range but then quickly becomes subsonic (choked) due to shock waves emanating from interior angles in the ducts. The geometry of the ducts can be designed to create different shock wave patterns within the ducts. The variance of leading edge location, leading edge angle, cowling intake angle, and flight Mach number influences the shock patterns within the ducts and consequently, the range of the projectile.
摘要翻译：训练射弹使用可变拖弹弹稳定器，将战术射弹的轨迹与距离限制为8公里相距3公里。稳定器采用超音速流动现象来改变训练射弹的空气动力特性，同时在自由飞行中满足这一要求。稳定器使用由支柱支撑的整流罩来提供尾部提升，并确保稳定的飞行路径。超音速流动通过从武器发射时由罩和支柱形成的管道建立。流体保持超音速，直到弹丸达到所需的范围，然后由于管道内角发出的冲击波，迅速变为亚音速（窒息）。管道的几何形状可以设计成在管道内产生不同的冲击波形图案。前缘位置，前缘角，整流罩角度和飞行马赫数的变化影响管道内的冲击模式，从而影响射弹的射程。

7. 发明授权

US08640624B1 Low collateral damage air defense projectile 有权
标题翻译：低附带损害防空弹
公开(公告)号：US08640624B1
公开(公告)日：2014-02-04
申请号：US13332772
申请日：2011-12-21
申请人： Ahmed Hassan , Marco Duca , Mohan Palathingal , Daniel Vo , Anthony Vella
发明人： Ahmed Hassan , Marco Duca , Mohan Palathingal , Daniel Vo , Anthony Vella
IPC分类号： F42B12/02 , F42B30/02
CPC分类号： F42B12/06 , F42B5/025 , F42B5/03 , F42B8/14 , F42B12/62
摘要： A kinetic energy penetrator with a longitudinal axis may include a forward segment having a lateral surface, a rear surface, and at least one air bleed channel extending from the lateral surface to the rear surface. A second segment may be disposed aft of and torsionally engaged with the forward segment. The second segment may include a front surface adjacent the rear surface of the forward segment. The forward and second segments may each be asymmetric about the longitudinal axis of the penetrator. When the penetrator is in flight, bleed air through the bleed channels may impinge on the front surface of the second segment. The second segment may separate from the front segment. Kinetic energies of each of the forward and second segments may be less than about 75 joules upon impact with a ground surface.
摘要翻译：具有纵向轴线的动能穿透器可以包括具有侧表面，后表面和从侧表面延伸到后表面的至少一个排气通道的前段。第二段可以被布置在前部的后部并与前部段扭转接合。第二段可以包括邻近前段的后表面的前表面。前进和第二段可以各自围绕穿透器的纵向轴线是不对称的。当穿透器处于飞行状态时，通过排放通道排出空气可能会撞击到第二段的前表面。第二段可能与前段分离。每个前段和第二段的动能在与地面碰撞时可能小于约75焦耳。

8. 发明授权

US5388314A Pool cover fastener 失效
标题翻译：池盖紧固件
公开(公告)号：US5388314A
公开(公告)日：1995-02-14
申请号：US973420
申请日：1992-11-09
申请人： Anthony Vella
发明人： Anthony Vella
IPC分类号： E04H4/10 , B42F1/02
CPC分类号： E04H4/10 , Y10T24/4406 , Y10T24/44855 , Y10T24/44923
摘要： An integral fastener for securing a pool cover to the top rail of an above-ground pool is disclosed. The fastener is comprised of a first leg, a second leg, a first downwardly-extending, diverging lip connected to said first leg, and a second downwardly-extending diverging lip connected to said second leg.The first leg and the second leg are partially contiguous with each other and form a closed cavity which is defined by a continuous surface consisting of a first substantially linear wall, a substantially concave inner wall, a substantially convex wall, and a second substantially linear wall.
摘要翻译：公开了一种用于将游泳池盖固定到地上池的顶部轨道的整体紧固件。紧固件包括第一腿，第二腿，连接到所述第一腿的第一向下延伸的发散唇缘，以及连接到所述第二腿的第二向下延伸的发散唇。第一腿部和第二腿部彼此部分邻接并形成封闭的腔体，该腔体由连续表面限定，该连续表面由第一基本上直线的壁，基本上凹的内壁，基本上凸的壁和第二基本上直的壁。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式