公开(公告)号：US2764093A

公开(公告)日：1956-09-25

申请号：US36040953

申请日：1953-06-09

申请人： MCCUISTION TOMMY J

发明人： MCCUISTION TOMMY J

IPC分类号： F42C15/21

CPC分类号： F42C15/21

公开(公告)号：US1364008A

公开(公告)日：1920-12-28

申请号：US25516318

申请日：1918-09-21

申请人： STUART THOMSON ,  BOARDMAN HENRY B

发明人： STUART THOMSON ,  BOARDMAN HENRY B

IPC分类号： F42C15/20 ,  F42C15/21

CPC分类号： F42C15/20 ,  F42C15/21

公开(公告)号：US11460280B2

公开(公告)日：2022-10-04

申请号：US17114099

申请日：2020-12-07

申请人： Alliance Development Group Ltd

发明人： Duncan Thomas

IPC分类号： F42C1/04 ,  F42B27/00 ,  F42C14/02 ,  F42C15/21 ,  F41H13/00

摘要： A grenade firing mechanism 12 has a body 18 defining an internal chamber 32 in which a firing pin structure 40 is located. The firing pin structure is actuated by an inertia toggle 64 having a first end contained within the chamber and a second end region 72 which projects from the body. A safety lever 16 is releasably mounted to the second end region 72 of the inertia toggle in an operative position to prevent the inertia toggle moving to actuate the firing pin structure. A lever spring 104 is operative to eject the lever from the inertia toggle allow the firing pin structure to be actuated when the grenade is deployed. The lever 16 carries an abutment pin 120 which extends through the body to engage the firing pin structure 40 to inhibit the firing pin structure moving in a firing direction when the lever is in its operative position. The inertia toggle may have a convex abutment surface which engages the firing pin structure. The firing mechanism is particularly suited to a sound flash distraction grenade.

公开(公告)号：US10605561B2

公开(公告)日：2020-03-31

申请号：US16242908

申请日：2019-01-08

申请人： Fruity Chutes Inc

发明人： Eugene Engelgau ,  Christopher John Attebery

IPC分类号： B64D17/00 ,  F41B7/00 ,  B64D17/70 ,  F42C15/40 ,  F42C15/21

摘要： An ejection launcher is an apparatus that effectively ejects a payload while maintaining a compact structure. The apparatus includes an elongated enclosure, a cover, a trigger mechanism, a spring-loaded piston, and a payload. The elongated enclosure positions and connects the trigger mechanism with the spring-loaded piston. The elongated enclosure also houses the spring-loaded piston and the payload. The trigger mechanism releases the spring-loaded piston which forces the payload from within the elongated enclosure. The payload is a desired delivered item and is preferably a parachute. The trigger mechanism and the spring-loaded piston translates horizontal force into vertical force which releases the payload and reduces the release resistance. The trigger mechanism preferably utilizes and includes a servo motor with a output arm. The output arm pushes against a catch plate of the trigger mechanism and releases a catch pin of the spring-loaded piston.

公开(公告)号：US5889227A

公开(公告)日：1999-03-30

申请号：US989776

申请日：1997-12-12

申请人： Norbert Wardecki

发明人： Norbert Wardecki

IPC分类号： F42C15/21 ,  F42C15/24 ,  F42C15/16

CPC分类号： F42C15/21 ,  F42C15/24

摘要： An explosive projectile carrying an active charge is to be launched from a barrel. Detonation of the charge requires that a firing pin be driven to a firing position where it impacts a percussion cap. The firing pin is held in a safety position by a barrel probe which is movable to an armed position in a direction perpendicularly to the launch direction. Prior to launching, the barrel probe is held immovable by engagement with both the launch barrel and an acceleration sensor. When the projectile leaves the barrel and acceleration displaces the acceleration sensor, the barrel probe is free to move to its armed position. Also provided are a pretensioned spring, and a pyrotechnical delay element for generating propulsion gas. Either the spring or the delay element functions to move the firing pin to its firing position, and the other of the spring and delay element moves the barrel probe to its armed position.

摘要翻译： 一个装有主动装置的爆炸弹将从一个炮弹发射出来。 电荷的爆震需要将击发销驱动到撞击打击乐帽的发射位置。 撞针通过枪管探头保持在安全位置，枪管探针可沿垂直于发射方向的方向移动到武装位置。 在发射之前，通过与发射筒和加速度传感器接合来保持枪管探头不可移动。 当弹丸离开枪管并加速移位加速度传感器时，枪管探头可自由移动到其武装位置。 还提供了预张紧的弹簧和用于产生推进气体的烟火延迟元件。 弹簧或延迟元件用于将击发销移动到其击发位置，弹簧和延迟元件中的另一个将枪管探针移动到其装备位置。

公开(公告)号：US5373790A

公开(公告)日：1994-12-20

申请号：US070220

申请日：1993-06-02

申请人： Patrice H. Chemiere ,  Jean-Paul A. Dupuy ,  Bernard F. Bayard ,  Jean-Pierre Ruet

发明人： Patrice H. Chemiere ,  Jean-Paul A. Dupuy ,  Bernard F. Bayard ,  Jean-Pierre Ruet

IPC分类号： F42B12/58 ,  F42C9/14 ,  F42C15/184 ,  F42C15/21 ,  F42C15/38 ,  F42C15/44 ,  F42C9/08 ,  F42C9/16

CPC分类号： F42C15/21 ,  F42B12/58 ,  F42C15/184 ,  F42C15/38 ,  F42C15/44 ,  F42C9/145

摘要： A mechanical system for self-destruction of a munition, in particular a carrier shell submunition, is provided in a munition having a warhead initiated by a pyrotechnic sequence, a main striker and a priming device composed of a slide movable between a safety position and an armed position and which has a device for priming the charge. The self destruction system includes a secondary striker mounted inside a receptacle of a slide and a control device to release the secondary striker after a preset delay. Secondary striker is integral with a holding element and held abutting a seat by the urging of an arming spring. The control device of the secondary striker has a corrosive agent designed to chemically attack the holding element to release it from its seat. When the holding element is released, secondary striker is translationally moved to contact the detonator to destroy the munition.

摘要翻译： 在具有由烟火序列发起的弹头的弹药，主要撞击器和起动装置的弹药中提供了用于自毁销毁弹药的机械系统，特别是载体壳子弹药，弹药由可在安全位置和 并且具有用于启动费用的装置。 自毁系统包括安装在滑块的容器内的辅助撞针和控制装置，以在预设的延迟之后释放次冲击器。 次级撞击器与保持元件成一体，并通过布置弹簧的推动而保持抵靠座位。 次级撞击器的控制装置具有腐蚀剂，其被设计成化学地攻击保持元件以将其从其座部释放。 当保持元件被释放时，辅助撞针被平移地移动以接触雷管以摧毁弹药。

公开(公告)号：US4729316A

公开(公告)日：1988-03-08

申请号：US947378

申请日：1986-12-29

申请人： Daniel R. J. Evrard ,  Hubert Calmettes ,  Noel Robert

发明人： Daniel R. J. Evrard ,  Hubert Calmettes ,  Noel Robert

IPC分类号： F42C15/192 ,  F42C15/21 ,  F42B4/26 ,  F42C15/34

CPC分类号： F42C15/21 ,  F42C15/192

摘要： A projectile comprises a pyrotechnic charge and a mobile member inside the projectile which rotates between a safe position and an armed position. At least part of a pyrotechnic delay device is accommodated in a passage in this mobile member. The pyrotechnic charge is initiated via this pyrotechnic delay device. The passage is oriented so as to isolate functionally the pyrotechic delay device from the pyrotechnic charge when the mobile member is in the safe position. It functionally couples the pyrotechnic delay device to the pyrotechnic charge when the mobile member is in the armed position. The projectile further comprises an arrangement on the mobile member and on the projectile to guide relative rotation between them about an axis fixed relative to the mobile member and relative to the projectile. A mechanical arming device retains the mobile member in the safe position and against rotation about the aforementioned axis relative to the projectile at least until the projectile is fired. It obliges the mobile member to move to the armed position when the projectile is fired by rotating about the axis relative to the projectile.

摘要翻译： 射弹包括一个烟火炸药和一个在安全位置和武装位置之间旋转的射弹内的移动部件。 烟火延迟装置的至少一部分容纳在该移动构件的通道中。 烟火装置通过烟火延迟装置启动。 通道被定向成在移动构件处于安全位置时将烟火延迟装置与烟火装置隔离开来。 当移动构件处于布防位置时，它将烟火延迟装置功能地耦合到烟火充电。 抛射体还包括在移动构件和射弹上的布置，以引导它们之间围绕相对于移动构件固定的轴线和相对于射弹的相对旋转。 机械布防装置将移动构件保持在安全位置并且相对于射弹围绕上述轴线保持旋转，至少直到射弹被射击。 当弹射器相对于射弹围绕轴旋转时，它迫使移动构件移动到武装位置。

公开(公告)号：US4632010A

公开(公告)日：1986-12-30

申请号：US718399

申请日：1985-04-01

申请人： Waymon Humphries ,  John Bryant ,  Richard C. Eklund ,  Donald C. Hayes ,  Peter Ferko

发明人： Waymon Humphries ,  John Bryant ,  Richard C. Eklund ,  Donald C. Hayes ,  Peter Ferko

IPC分类号： F42B10/56 ,  F42B12/70 ,  F42C15/184 ,  F42C15/21 ,  F42B13/04 ,  F42B25/02

CPC分类号： F42B10/56 ,  F42B12/70 ,  F42C15/184 ,  F42C15/21

摘要： An AIRBOC chaff deployment apparatus comprising a canister with a wind flapttached externally to the canister and connected to a drogue chute that is housed inside the canister. The drogue chute is situated atop a main chute that is atop a release mechanism, which is atop a fuze and that is atop a chaft payload, all of which is housed inside the canister. When the AIRBOC is dropped from a plane, the wind flap extends, pulling out the drogue chute. The drogue chute in turn activates the release mechanism which frees the drogue chute to pull out the main chute to which the drogue chute is connected. The deployment of the main chute causes a force greater than 40 lbs to be applied to the release mechanism, resulting in the chaff payload being released from the canister and the fuze being activated, consequently detonating the released chaff payload.

摘要翻译： 一种AIRBOC谷壳部署装置，其包括具有附接到罐的外部并连接到容纳在罐内的锥形滑槽的风瓣的罐。 锥形滑槽位于主滑槽顶部，位于引擎顶部，位于一个引信顶部，位于一个有效载荷的顶部，所有这些都位于罐内。 当空中客车从飞机上掉下来时，风翼延伸，拉出冷气滑道。 锥形滑道又激活释放机构，释放滑梯滑槽以拉出与滑道滑槽连接的主滑槽。 主滑槽的部署导致大于40磅的力施加到释放机构，导致谷壳有效载荷从罐中释放并且引信被激活，从而引爆释放的谷壳有效载荷。

公开(公告)号：US4458597A

公开(公告)日：1984-07-10

申请号：US354490

申请日：1982-03-03

申请人： Jean-Pierre Reynes

发明人： Jean-Pierre Reynes

IPC分类号： F42B10/02 ,  F42C1/04 ,  F42C15/184 ,  F42C15/21 ,  F42B4/26

CPC分类号： F42B10/02 ,  F42C1/04 ,  F42C15/184 ,  F42C15/21

摘要： A cartridge with firing actuation of the payload comprises a case solid with a case bottom which houses a threaded member constituting an ejection nozzle, and in front of the latter a missile provided with a delay ignition chain interrupted at the level of a transversally movable slide which comes into fire transmission position only after a predetermined delay. The cartridge has in addition a striker device actuated on impact so as to ignite the delay firing chain on impact, and a stabilizer device ensuring an axial deceleration permitting the satisfactory operation of the striker on impact.

摘要翻译： 具有有效载荷的发射致动的盒包括具有壳体底部的壳体固体，壳体底部容纳构成喷射嘴的螺纹构件，并且在其前面具有设置在横向可移动滑块的水平面上的延迟点火链的导弹， 仅在预定的延迟之后才进入火力传播位置。 另外，该弹药筒还具有冲击作用的撞击装置，以便在撞击时点燃延迟击发链;以及稳定装置，确保轴向减速，从而允许冲击器的令人满意的操作。

公开(公告)号：US3894491A

公开(公告)日：1975-07-15

申请号：US45093974

申请日：1974-03-13

申请人： US NAVY

发明人： TIEMANN RALPH A

IPC分类号： F42B4/26 ,  F42C15/21 ,  F42C15/00

CPC分类号： F42B4/26 ,  F42C15/21

摘要： An automatic porting mechanism on a launchable device for latching a bore rider when said device is moved in one direction and for unlatching a bore rider when said device is moved in an opposite direction. The bore rider is pivotally attached to a slidable plug which closes an orifice in the launchable device. A lip on the bore rider is engageable with a shoulder adjacent the orifice to prevent ejection of the bore rider until forward movement of the device relative to a launcher unlatches the bore rider.

摘要翻译： 一种可启动装置上的自动移动机构，用于当所述装置沿一个方向移动时锁定钻孔机，并且当所述装置沿相反方向移动时，用于解除钻孔骑手。 钻孔机可枢转地附接到可关闭可启动装置中的孔口的可滑动塞子。 钻孔骑手上的唇缘可与邻近孔口的肩部接合，以防止钻孔机的弹出，直到装置相对于发射器的向前运动解除钻孔骑手。