161 |
Hand grenade |
US13565912 |
2012-08-03 |
US09121681B2 |
2015-09-01 |
Gregory K. Wierenga |
A hand-throwable grenade including a detonator initiating mechanism, a detonator and a locking key. The detonator initiating mechanism is activatable by an operator before the grenade is thrown. The detonator is associated with the detonator initiating mechanism. The locking key interacts with the detonator initiating mechanism to preclude an arming of the detonator until the locking key is removed from the detonator initiating mechanism. The locking key has at least one notch therein. |
162 |
Fuze pull pin detent device |
US14037920 |
2013-09-26 |
US09010250B1 |
2015-04-21 |
Matthew P. Evangelisti; Steve Kotefski; Lidija Kotevska |
A grenade fuze assembly includes a fuze body and a striker lever fixed to the fuze body with a pull pin. A circular pull ring is attached to the pull pin. A detent device is disposed on a top portion of the fuze body and a top portion of the striker lever. The detent device includes four sides with a boss formed on an exterior of one of the four sides. The boss includes a curved slot for receiving and holding the pull ring. A pair of opposed locking tabs on opposite interior sides of the detent device engage the top portion of the fuze body. The detent device secures the pull ring to prevent accidental removal of the pull pin when the grenade is dropped and to prevent undesired noise cause by movement of the pull pin and pull ring. |
163 |
Electro-mechanical fuze for hand grenades |
US13608494 |
2012-09-10 |
US08887640B1 |
2014-11-18 |
Ryan R. Knight; Oliver M. Barham; Thinh Q. Hoang; Robert H. Wood |
A safety fuze includes a magneto striker generator (MSG) as its a power generation source. The MSG provides energy to energize an electronic unit and a safety and arming device. The safety fuze allows safety and arming of military hand grenades, with a fully out-of-line explosive initiator and an integrated power generation means, for improving safety and performance. The MSG includes a striker and a receiving bobbin that houses a conductive coil. The striker comprises a permanent magnet that is mounted on a pivot mechanism for allowing a rotational displacement of the permanent magnet, into the bobbin, in order to generate an electrical current. As the permanent magnet is being inserted inside the bobbin, the magnetic flux change induces an electric current in the coil, creating the necessary energy for the fuze operation. |
164 |
Compact and mechanical inertial igniters for thermal batteries and the like for munitions with short duration firing setback shock |
US13784737 |
2013-03-04 |
US08841567B1 |
2014-09-23 |
Jacques Fischer; Jahangir S Rastegar |
An inertial igniter including: a body having a base; a striker release element rotatably disposed on the body, the striker release element having a first surface; a first biasing element for biasing the striker release element away from the base; a striker mass rotatably disposed on the base along a second axis, the striker mass having a second surface corresponding to the first surface of the striker release element, the first surface obstructing rotation of the striker mass; and a second biasing element for biasing the striker mass such that the second surface is biased towards the first surface; wherein when the body experiences an acceleration profile of a predetermined magnitude and duration, the striker release element rotates towards the base to release an engagement between the first and second surfaces and allow the striker mass to rotate under a biasing force of the second biasing element. |
165 |
Compact and Mechanical Inertial Igniters For Thermal Batteries and the like for Munitions With Short Duration Firing Setback Shock |
US13784737 |
2013-03-04 |
US20140248522A1 |
2014-09-04 |
Jacques Fischer; Jahangir S. Rastegar |
An inertial igniter including: a body having a base; a striker release element rotatably disposed on the body, the striker release element having a first surface; a first biasing element for biasing the striker release element away from the base; a striker mass rotatably disposed on the base along a second axis, the striker mass having a second surface corresponding to the first surface of the striker release element, the first surface obstructing rotation of the striker mass; and a second biasing element for biasing the striker mass such that the second surface is biased towards the first surface; wherein when the body experiences an acceleration profile of a predetermined magnitude and duration, the striker release element rotates towards the base to release an engagement between the first and second surfaces and allow the striker mass to rotate under a biasing force of the second biasing element. |
166 |
SMALL SMART WEAPON AND WEAPON SYSTEM EMPLOYING THE SAME |
US14030254 |
2013-09-18 |
US20140131508A1 |
2014-05-15 |
Steven D. Roemerman |
A weapon and weapon system, and methods of manufacturing and operating the same. In one embodiment, the weapon includes a warhead including destructive elements and a guidance section with a seeker configured to guide the weapon to a target. The seeker includes a detector configured to receive a distorted signal impinging on an objective lens from the target, memory configured to store target criteria and a correction map, and a processor configured to provide a correction signal based on the distorted signal, the target criteria and the correction map to guide the weapon to the target. |
167 |
Miniature safe and arm (S and A) mechanisms for fuzing of gravity dropped small weapons |
US13871241 |
2013-04-26 |
US08701558B2 |
2014-04-22 |
Jahangir S. Rastegar; Richard T. Murray |
A device for enabling safe/arm functionality in a gravity dropped weapon detachably connected to an airframe. The device including: an elastic element disposed in a shell of the weapon; a releasable connection between the weapon and the airframe to release a stored and/or generated energy in the elastic element; and a piezoelectric member connected to one end of the elastic member for converting the one or more of the stored and generated energy to an electrical energy. Wherein the releasable connection includes: a link having a movable connection for movement of the link relative to the shell between a first position constraining the elastic element from movement and a second position releasing the elastic member to generate the electrical energy; and a lanyard for tethering the link to the airframe such that the link is moved to the second position upon the weapon being released from the airframe. |
168 |
Rotating thumb safety fuze for a hand grenade and related methods of operation and assembly |
US13339473 |
2011-12-29 |
US08561540B1 |
2013-10-22 |
Richard Lauch |
A safety fuze for use with a canister, includes a body, a lever that is rotatably secured to one end of the body, a striker assembly that is rotatably secured to another end of the body, and a thumb switch assembly that includes a target and that is rotatably secured to the body. The safety fuze is selectively armed and disarmed. It is settable in one or four states: a safe-locked state; a safe-unlocked state; an armed state; and an initiation state. |
169 |
Small smart weapon and weapon system employing the same |
US12850421 |
2010-08-04 |
US08541724B2 |
2013-09-24 |
Steven D. Roemerman |
A weapon and weapon system, and methods of manufacturing and operating the same. In one embodiment, the weapon includes a warhead including destructive elements and a guidance section with a seeker configured to guide the weapon to a target. The seeker includes a detector configured to receive a distorted signal impinging on an objective lens from the target, memory configured to store target criteria and a correction map, and a processor configured to provide a correction signal based on the distorted signal, the target criteria and the correction map to guide the weapon to the target. |
170 |
Small smart weapon and weapon system employing the same |
US13034333 |
2011-02-24 |
US08443727B2 |
2013-05-21 |
Steven D. Roemerman; Joseph Edward Tepera |
A weapon and weapon system, and methods of manufacturing and operating the same. In one embodiment, the weapon includes a warhead including destructive elements and a guidance section with a target sensor configured to guide the weapon to a target. The target sensor includes a front lens configured to provide a cover to protect the target sensor from an environment and a fast fresnel lens behind the front lens to provide a multi-lens focusing system for the target sensor. In a related embodiment, the weapon includes an aft section including a tail fin having a modifiable control surface area thereby changing an aspect ratio thereof. |
171 |
Miniature safe and arm (S and A) mechanisms for fuzing of gravity dropped small weapons |
US12983301 |
2011-01-01 |
US08443726B2 |
2013-05-21 |
Jahangir S. Rastegar; Richard T. Murray |
A device for enabling safe/arm functionality in a gravity dropped weapon detachably connected to an airframe where the device includes: an elastic element disposed in a shell of the weapon; a releasable connection between the weapon and the airframe to release one or more of a stored and generated energy in the elastic element; and a piezoelectric member connected to one end of the elastic member for converting the one or more of the stored and generated energy to an electrical energy. The releasable connection can include: a link having a movable connection for movement of the link relative to the shell between a first position constraining the elastic element from movement and a second position releasing the elastic member to generate the electrical energy; and a lanyard for tethering the link to the airframe such that the link is moved to the second position upon the weapon being released from the airframe. |
172 |
Miniature Safe and Arm Mechanisms For Fuzing of Gravity Dropped Small Weapons |
US13297234 |
2011-11-15 |
US20120291613A1 |
2012-11-22 |
Jahangir S. Rastegar |
Methods and devices for differentiating an actual air drop of a gravity dropped weapon from an accidental drop of the weapon onto a surface. The method including: connecting a first end of at least one lanyard to an airframe; releasably connecting a second end of the at least one lanyard to a power generation device such that release of the second end with the power generation device initiates power generation by the power generation device; and releasably connecting a third end of the at least one lanyard to at least a portion of an air velocity sensor such that release of the third end one of activates or exposes the air velocity sensor to an air stream; and differentiating the actual air drop from the accidental drop based at least on a detection of an air velocity by the air velocity sensor. |
173 |
RE-LOCKING DEVICE FOR A ROCKER ARM DETONATOR |
US13117456 |
2011-05-27 |
US20110290144A1 |
2011-12-01 |
Christian Johann MULLER; Klaus BASSE; Ilka BOSSE; Wolfgang SCHUTZENDUBEL; Gabriele WETZEL |
A re-locking device for a rocker arm detonator (1) of an armament, such as a hand grenade, irritation body etc., is formed by a security mechanism (3), which facilitates a repeat locking after activation of the armament. The re-locking device includes at least one profile part (4, 4′), which is pivotably arranged and able to engage with the armament by means of an expedient (9), especially with the ignition head (5, 5′) and the rocker arm (2). |
174 |
PROGRAMMABLE INERTIAL IGNITERS FOR GUN-FIRED MUNITIONS, THERMAL BATTERIES AND THE LIKE |
US12079164 |
2008-03-25 |
US20110252994A1 |
2011-10-20 |
Richard T. Murray; Jahangir S. Rastegar; Thomas Spinelli |
An inertial igniter including: a housing; a striker mass movable relative to the housing; a biasing element for biasing the striker mass towards a percussion primer; one or more movable members each having one or more stops, the one or more stops having a first position for preventing a portion of the striker mass from striking the percussion primer and a second position allowing the portion of the striker mass to strike the percussion primer; wherein the movable members move the one or more stops to the second position when subjected to a predetermined acceleration profile. |
175 |
Small smart weapon and weapon system employing the same |
US12754345 |
2010-04-05 |
US07958810B2 |
2011-06-14 |
Steven D. Roemerman; John P. Volpi |
A weapon and weapon system, and methods of manufacturing and operating the same. In one embodiment, the weapon includes a warhead having destructive elements. The weapon also includes a folding lug switch assembly that provides a mechanism to attach the weapon to a delivery vehicle and is configured to close after launching from the delivery vehicle, thereby satisfying a criterion to arm the warhead. The weapon still further includes a guidance section including an antenna configured to receive mission data before launching from the delivery vehicle and further configured to receive instructions after launching from the delivery vehicle to guide the weapon to a target. |
176 |
Small smart weapon and weapon system employing the same |
US11706489 |
2007-02-15 |
US07895946B2 |
2011-03-01 |
Steven D. Roemerman; Joseph Edward Tepera |
A weapon and weapon system, and methods of manufacturing and operating the same. In one embodiment, the weapon includes a warhead including destructive elements and a guidance section with a target sensor configured to guide the weapon to a target. The target sensor includes a front lens configured to provide a cover to protect the target sensor from an environment and a fast fresnel lens behind the front lens to provide a multi-lens focusing system for the target sensor. In a related embodiment, the weapon includes an aft section including a tail fin having a modifiable control surface area thereby changing an aspect ratio thereof. |
177 |
Variable distance detonation mechanism |
US12155168 |
2008-05-30 |
US07861656B2 |
2011-01-04 |
Robert S. Thomas, III; Edward C. Waters, III |
A grenade includes an explosion chamber having an explosive charge to which an ignition charge is connected. The grenade also includes a primer and trigger coupled to the ignition charge for detonation of the explosive charge held within the explosion chamber. A variable distance detonation mechanism is coupled to the trigger and primer for allowing controlled detonation of the grenade a specific distance from the launch point thereof. |
178 |
VARIABLE DISTANCE DETONATION MECHANISM |
US12155168 |
2008-05-30 |
US20100307366A1 |
2010-12-09 |
Robert S. Thomas, III; Edward C. Waters, III |
A grenade includes an explosion chamber having an explosive charge to which an ignition charge is connected. The grenade also includes a primer and trigger coupled to the ignition charge for detonation of the explosive charge held within the explosion chamber. A variable distance detonation mechanism is coupled to the trigger and primer for allowing controlled detonation of the grenade a specific distance from the launch point thereof. |
179 |
Small smart weapon and weapon system employing the same |
US11541207 |
2006-09-29 |
US07690304B2 |
2010-04-06 |
Steven D. Roemerman; John P. Volpi |
A weapon and weapon system, and methods of manufacturing and operating the same. In one embodiment, the weapon includes a warhead having destructive elements. The weapon also includes a folding lug switch assembly that provides a mechanism to attach the weapon to a delivery vehicle and is configured to close after launching from the delivery vehicle, thereby satisfying a criterion to arm the warhead. The weapon still further includes a guidance section including an antenna configured to receive mission data before launching from the delivery vehicle and further configured to receive instructions after launching from the delivery vehicle to guide the weapon to a target. |
180 |
Axially compact mechanical igniter for thermal batteries and the like |
US11599878 |
2006-11-15 |
US07437995B2 |
2008-10-21 |
Jahangir S. Rastegar; Richard Murray; Gary Chen; Raymond Michael Hartley |
An inertial igniter including: a first member having a wall and internal cavity; a second member slidable in the internal cavity, a striker disposed thereon and a first concave portion; a third member slidable on an exterior surface of the wall, a second concave portion; biasing springs for biasing the first and second members in a direction opposite an acceleration; locking balls in the first and second concave portions for preventing movement of the second and third members when the acceleration time profile is below a predetermined threshold; and a percussion cap primer on the first member; wherein when the acceleration time profile is greater than the predetermined threshold the locking balls are released from the concave portions to first permit relative movement of the third member with the first member and after a time delay to permit relative movement of the second member with the first member. |