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11. 发明申请

US20050188876A1 Locking and stabilizing device for grenades 失效
标题翻译：手榴弹锁定稳定装置
公开(公告)号：US20050188876A1
公开(公告)日：2005-09-01
申请号：US10666824
申请日：2003-09-22
申请人： Lamar Auman , Douglas Love , Brad Bachelor
发明人： Lamar Auman , Douglas Love , Brad Bachelor
IPC分类号： F42B10/02 , F42C15/32
CPC分类号： F42B10/02
摘要： The locking and stabilizing device for grenades utilizes a solid nylon ring and multiple nylon ribbons that are attached to the ring at regular intervals around its circumference. During storage, the ring surrounds and locks the slider of the grenade in its storage position. But upon deployment, under aerodynamic forces the ring moves away from the slider, releasing the slider. When the slider is thusly released, it slides out and brings the detonator in place to be impacted upon by the pin when the grenade hits the target, thus detonating the grenade. The multiple ribbons extending from the ring unfurl due to the aerodynamic forces and provide stability to the grenade flight.
摘要翻译：用于手榴弹的锁定和稳定装置使用固体尼龙环和多个尼龙带，其周围以规则的间隔附接到环。在存储期间，环围绕并锁定手榴弹的滑块在其存储位置。但是在展开后，在气动力作用下，环从滑块移开，释放滑块。当滑块因此被释放时，当手榴弹撞击目标时，它滑出并将引爆器引导到被撞击的位置，从而引爆手榴弹。由于空气动力，从环上展开的多个带子将展开，并为手榴弹飞行提供稳定性。

12. 发明授权

US06286789B1 Configurable aerial vehicle aerosurface 失效
标题翻译：可配置的飞行器航空表面
公开(公告)号：US06286789B1
公开(公告)日：2001-09-11
申请号：US09496138
申请日：2000-02-01
申请人： Ralph Shimovetz
发明人： Ralph Shimovetz
IPC分类号： B64C900
CPC分类号： F42B15/01 , B64C3/54 , F42B10/02 , F42B10/64 , Y02T50/14
摘要： A configurable aerial vehicle aerosurface is disclosed, The configurable aerial vehicle aerosurface includes first and second airfoil surfaces in sliding engagement. A plurality of apertures pass transversely through the airfoil surfaces and are disposed in such a relationship so as to define a first position wherein the apertures are in substantial alignment and a second position wherein the apertures are in substantial non-alignment. In this way, the configurable aerial vehicle aerosurface of the present invention can be configured from a first, low drag transport position, to a second, aerodynamic position to provide missile lift and control.
摘要翻译：公开了一种可配置的飞行器气体表面。可配置的飞行器气体表面包括滑动接合的第一和第二翼面。多个孔穿过翼型表面横向通过并且以这样的关系设置，以便限定第一位置，其中孔基本对齐，而第二位置其中孔几乎不对齐。以这种方式，本发明的可配置的飞行器气体表面可以由第一，低阻力输送位置，第二空气动力学位置构成，以提供导弹升降和控制。

13. 发明授权

US5804759A Hunting bullet having a telescoping flechette and comprising a sub-projectile connected to a launcher 失效
标题翻译：狩猎子弹具有伸缩式收音机并且包括连接到发射器的子弹体
公开(公告)号：US5804759A
公开(公告)日：1998-09-08
申请号：US663305
申请日：1996-06-25
申请人： Jean-Claude Sauvestre
发明人： Jean-Claude Sauvestre
IPC分类号： F42B7/10 , F42B10/02 , F42B12/62 , F42B14/06 , F42B5/00 , F42B12/02
CPC分类号： F42B14/061 , F42B10/02 , F42B12/625 , F42B14/064 , F42B7/10
摘要： An ammunition cartridge comprises a full bullet 1 held in a primer socket D containing a propellant charge P. The bullet 1 includes an flechette 2 and a launcher 10 concentrically received on the flechette to allow relative translation. The flechette 1 comprises an flechette body 3 of hard material having a conical head 4, and a stabilizer 6 fixed to a rear of the body 3. The stabilizer 6 has an integral lip 8 which seals the bullet 1 in the barrel to optimize pressure build-up during firing. The launcher translates forward relative to the flechette when released from the primer socket D. The full bullet remains intact in flight. The launcher strikes the target first and transmits high energy to the target. Immediately thereafter, the flechette translates forward to penetrate the target.
摘要翻译： PCT No.PCT / FR95 / 01418 Sec。 371日期1996年6月25日第 102（e）日期1996年6月25日PCT提交1995年10月26日PCT公布。公开号WO96 / 13697 日期1996年5月9日弹药筒包括一个保持在底座插座D中的全弹头1，其中包含推进剂装药P.子弹1包括一个同步接收在收音机上以允许相对平移的收音机2和发射器10。收发器1包括具有锥形头部4的硬质材料的收集器体3和固定在主体3的后部的稳定器6.稳定器6具有一体的唇部8，其将筒体中的子弹1密封以优化压力构造在射击期间。当从底座插座D释放时，发射器相对于收音机转换。飞行中完整的子弹保持完整。发射器首先达到目标，并将高能量传递给目标。此后，收音机向前翻转以穿透目标。

14. 发明授权

US5660356A System for providing power and roll motion stability in a vehicle 失效
标题翻译：用于在车辆中提供动力和侧倾运动稳定性的系统
公开(公告)号：US5660356A
公开(公告)日：1997-08-26
申请号：US351821
申请日：1994-12-08
申请人： Brian J. Selfors , Vijay M. Gondhalekar
发明人： Brian J. Selfors , Vijay M. Gondhalekar
IPC分类号： F42B10/02 , F42B15/00 , H02K7/02 , B64C17/06
CPC分类号： H02K7/025 , F42B10/02 , F42B15/00 , Y02E60/16 , Y10T74/2117
摘要： A dual flywheel assembly for use in an airborne vehicle for storing mechanical energy therein prior to flight and for permitting the extraction of electrical energy therefrom during flight, which assembly includes two flywheels which are linked by a suitable linkage structure such that, if roll motion of the vehicle starts to occur during flight, the flywheels tilt in equal and opposite directions out of their normal planes of rotation, which tilting motions act in a passive manner to stabilize the roll motion of the vehicle.
摘要翻译：一种用于空中飞行器的双飞轮组件，用于在飞行之前在其中存储机械能并且允许在飞行期间从其中提取电能，该组件包括两个由合适的连杆结构连接的飞轮，使得如果滚动运动车辆在飞行中开始发生，飞轮在正常的旋转平面之外以相等和相反的方向倾斜，该倾斜运动以被动方式作用以稳定车辆的滚动运动。

15. 发明授权

US4998994A Aerodynamically compliant projectile nose 失效
标题翻译：空气动力学兼容弹丸鼻
公开(公告)号：US4998994A
公开(公告)日：1991-03-12
申请号：US409900
申请日：1989-09-20
申请人： Edward M. Schmidt , William F. Donovan
发明人： Edward M. Schmidt , William F. Donovan
IPC分类号： F42B10/02
CPC分类号： F42B10/02
摘要： A high velocity aerodynamic projectile having a central body with a forwardnd, a rearward end and a longitudinal axis, the forward end of the body has a pedestal coaxially extending outward from the body. The projectile has aft stabilizing fins or a flare rigidly affixed at its rearward end and a forward stablizing means pivotably attached to the pedestal of the central body. The forward stabilizing means consists of a self-aligning projectile nose having its rearward end separated from the forward end of the projectile's central body so as to allow the self-aligning projectile nose to pivot and align with the oncoming air stream.
摘要翻译：具有具有前端，后端和纵向轴线的中心体的高速气动抛射体，主体的前端具有从主体向外同轴地延伸的基座。抛射体具有后稳定翅片或其后端刚性地固定的火炬，以及可枢转地附接到中心体的基座的向前稳定装置。前向稳定装置包括一个自对准的弹射鼻，其后端与射弹的中心体的前端分开，以便允许自对准的弹射鼻枢转并对准迎面而来的空气流。

16. 发明授权

US4145017A Glide projectile having jettisonable keel fin 失效
标题翻译：滑翔射弹具有可放弃的龙骨鳍
公开(公告)号：US4145017A
公开(公告)日：1979-03-20
申请号：US793508
申请日：1977-05-04
申请人： Lothar Stiklorus
发明人： Lothar Stiklorus
IPC分类号： F42B10/02 , F42B15/36 , F42B15/10 , F42B13/30
CPC分类号： F42B15/36 , F42B10/02
摘要： A non-spinning glide projectile, comprises a body which includes a forward portion having one or more lift-producing devices or outwardly projecting air foil-like surfaces. A keel fin is detachably secured to the body intermediate its length, and means, such as a time fuse device, carried on the body, is employed for detaching the fin and jettisoning it after a predetermined flight path has been completed.
摘要翻译：非旋转的滑行射弹包括主体，其包括具有一个或多个提升产生装置的向前部分或向外突出的空气箔状表面。龙骨鳍可拆卸地固定在身体长度的中间，并且在预定的飞行路径已经完成之后，采用携带在身体上的诸如时间保险丝装置的装置来分离翅片并将其排出。

17. 发明授权

US3782286A Non-lethal projectile and launcher therefor 失效
标题翻译：非标准项目及其发起人
公开(公告)号：US3782286A
公开(公告)日：1974-01-01
申请号：US3782286D
申请日：1972-11-20
申请人： RICHIE E , JONES K , JONES K
发明人： RICHIE E
IPC分类号： F41C27/06 , F42B5/045 , F42B10/02 , F42B12/34 , F42B12/40 , F42B5/14 , F42B5/22
CPC分类号： F42B10/02 , F41C27/06 , F42B5/045 , F42B12/34 , F42B12/40
摘要： A non-lethal projector and launcher therefor for riot control and the like comprising a body formed from a relatively soft, pliant latex material compressed to projectile form and mounted within a restraining cup which in turn is mounted in a firing shell. The body at its rearward end includes retracted guidance structure that extends on the projectile being fired, a chamber at its forward end to receive a marking fluid for marking the target, and internal subdivisions in its mid portion designed to permit the body to expand laterally on impacting into a soft textured mass that flattens on impact to avoid injury to the target. The projectile launcher is in the form of a barrel assembly including a bell shaped muzzle which permits the projectile to be fired without jamming even when held against the target and braking slots for discharging the propelling gases rearwardly of the launcher to reduce recoil.
摘要翻译：一种用于防暴控制的非致命的投影仪及其发射器等包括由相对柔软的柔性胶乳材料形成的主体，其被压缩成射弹形式，并安装在限制杯内，该限制杯又安装在击发壳中。在其后端的主体包括在被射击的射弹上延伸的缩回的引导结构，在其前端处的腔室以接收用于标记目标的标记流体，以及设置成允许身体横向扩张的其中部的内部细分撞击到柔软的纹理质量，在冲击时变平，以避免对目标的伤害。射弹发射器是一个桶组件的形式，包括一个钟形枪口，允许射弹在没有卡住的情况下被发射，即使当它们靠在目标上时，还有制动槽用于将推进气体排放到发射器后面以减少反冲。

18. 发明授权

US2368258A Stabilizing retarder for bombs 失效
标题翻译：炸弹稳定缓凝剂
公开(公告)号：US2368258A
公开(公告)日：1945-01-30
申请号：US42951842
申请日：1942-02-04
申请人： MANSON FRANK G , MASKEY JAMES J
发明人： MANSON FRANK G , MASKEY JAMES J
IPC分类号： F42B10/02 , F42B10/48 , F42B21/00
CPC分类号： F42B21/00 , F42B10/02 , F42B10/48

19. 发明授权

US10871359B2 Single seal projectile 有权
公开(公告)号：US10871359B2
公开(公告)日：2020-12-22
申请号：US16618459
申请日：2018-05-30
申请人： TECHVENTURE INVESTMENTS PTY LTD
发明人： Dale Harrison
IPC分类号： F42B14/02 , F42B10/02 , F42B10/46
CPC分类号： F42B14/02 , F42B10/02 , F42B10/46
摘要： A projectile (10) for firing from a barrel (12) of a firearm has an elongated tubular body (14) with a leading end (16), a trailing end (18) and a passage (100) extending through the body (14) and opening onto the leading end (16). An insert (102) is disposed in the passage (100). A cavity (20) is formed in the body (14) between the insert (102) and the trailing end (18) for holding a volume of propellant. A seal arrangement (22) is formed on the body (14) and located between and in-board of the leading end (16) and the trailing end (18). The seal arrangement (22) extends circumferentially about body to form a substantial seal against an inner circumferential surface of the barrel (12). A driving band (28) is supported on the body (14) between the seal arrangement (22) and the trailing end (18) and arranged to maintain substantial coaxial alignment of the body (14) of the projectile and the barrel (12) of the firearm while the projectile travels along the barrel (12). The driving band (28) has one or more flow paths (38) that enable fluid communication between opposite axial ends of the driving band (28).

20. 发明申请

US20170350680A1 FEATHERS OF AN ARROW 审中-公开
公开(公告)号：US20170350680A1
公开(公告)日：2017-12-07
申请号：US15607428
申请日：2017-05-26
申请人： YEON KIM
发明人： YEON KIM
IPC分类号： F42B6/06 , F42B10/02 , F42B6/02 , F42B6/04
CPC分类号： F42B6/06 , F42B6/02 , F42B6/04 , F42B10/02 , F42B10/08
摘要： The present invention relates to the improved feathers of an arrow, and more particularly, to the improved feathers of an arrow, which prevent instability of flight caused by a vortex generated during the flight of the arrow by forming a plurality of arrow feathers attached to the arrow, which has a cross section which is a curved surface and integrally forming an auxiliary surface having one surface which is the curved surface with the arrow feather to guarantee stable flight.

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