EP2976591A1 - Barrel opening mechanism of grenade launcher - Google Patents

Barrel opening mechanism of grenade launcher

Info

Publication number
EP2976591A1
EP2976591A1 EP14769600.9A EP14769600A EP2976591A1 EP 2976591 A1 EP2976591 A1 EP 2976591A1 EP 14769600 A EP14769600 A EP 14769600A EP 2976591 A1 EP2976591 A1 EP 2976591A1
Authority
EP
European Patent Office
Prior art keywords
barrel
pivot
grenade launcher
pin
latch
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP14769600.9A
Other languages
German (de)
French (fr)
Other versions
EP2976591B1 (en
EP2976591A4 (en
Inventor
Khee Ngee HENG
Weixian Wilson LI
Wei Qiang TANG
Kheng Hong Samuel PANG
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
ST Engineering Advanced Material Engineering Pte Ltd
Original Assignee
Advanced Material Engineering Pte Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Advanced Material Engineering Pte Ltd filed Critical Advanced Material Engineering Pte Ltd
Publication of EP2976591A1 publication Critical patent/EP2976591A1/en
Publication of EP2976591A4 publication Critical patent/EP2976591A4/en
Application granted granted Critical
Publication of EP2976591B1 publication Critical patent/EP2976591B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A9/00Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
    • F41A9/38Loading arrangements, i.e. for bringing the ammunition into the firing position
    • F41A9/45Loading arrangements, i.e. for bringing the ammunition into the firing position the cartridge chamber or the barrel as a whole being tiltable or transversely slidable between a loading and a firing position
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A3/00Breech mechanisms, e.g. locks
    • F41A3/02Block action, i.e. the main breech opening movement being transverse to the barrel axis
    • F41A3/04Block action, i.e. the main breech opening movement being transverse to the barrel axis with pivoting breech-block
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A3/00Breech mechanisms, e.g. locks
    • F41A3/58Breakdown breech mechanisms, e.g. for shotguns
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A35/00Accessories or details not otherwise provided for
    • F41A35/06Adaptation of guns to both right and left hand use
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41CSMALLARMS, e.g. PISTOLS, RIFLES; ACCESSORIES THEREFOR
    • F41C27/00Accessories; Details or attachments not otherwise provided for
    • F41C27/06Adaptations of smallarms for firing grenades, e.g. rifle grenades, or for firing riot-control ammunition; Barrel attachments therefor

Definitions

  • the present invention relates to a barrel opening mechanism for loading and unloading of cartridges into a barrel of a grenade launcher.
  • a grenade launcher may be a standalone device or detachably mounted below a rifle.
  • the grenade launcher uses a spin-stabilised 40 mm cartridge.
  • a conventional grenade launcher may employ different methods of opening the barrel: longitudinal sliding opening; lateral swinging to the left hand, to the right hand side, downward or upward; and a combination of longitudinal sliding followed by a lateral swing. These methods of opening the barrel involve many components and often only designed for a right- or left- handed operator; in other words, these conventional grenade launchers are often not ambidextrous.
  • US 7,487,612 assigned to FN Herstal S.A., discloses two sliding blocks (13, 14) operable to slide with two longitudinal slides (17) such that the barrel is advanced in a first longitudinal direction and swiveled laterally in the final phase of the longitudinal movement.
  • US 3,641 ,691 assigned to the US Army, discloses a grenade launcher in which the barrel is pivotable downwardly to a 15 degree angle and an ejector rod is used to eject the used cartridge. When the barrel is closed, the firing mechanism is automatically locked in the firing position.
  • the present invention seeks to provide a barrel opening mechanism for a grenade launcher that is ambidextrous in operation yet designed with a minimum number of components.
  • the Picatinny rail on the top portion of the barrel is configured to transfer recoil forces from the grenade launcher to a supporting rifle it is connected to.
  • the present invention provides a a receiver body, which is substantially an inverted L-shaped, with a forward pointing arm and a proximal arm, wherein the proximal ami is configured for housing a trigger mechanism; and a barrel connected below the forward pointing receiver ami by a barrel pivot and a latch mechanism; wherein the latch mechanism comprises a latch disposed in the forward receiver arm and is operable to engage with a catch disposed on a top portion of the barrel so that the latch is engageable with the catch when the barrel is in a closed position and longitudinal X-axes of the barrel and forward receiver arm are substantially parallel, and when the latch is actuated by an appendage of a left or right hand of a user supporting the barrel, the latch becomes released from the catch, thereby allowing the barrel to droop or pivot away from the forward receiver arm about a transverse Y-axis at the ban-el pivot so that the same hand is operable to turn a chamber end of the barrel laterally to the left or
  • the present invention provides a method of opening a barrel release and lock mechanism of a grenade launcher.
  • This method comprises: supporting a barrel of a grenade launcher with a left or right hand of a user; using an appendage of said left or right hand to push a lever portion that protrudes on each of two sides of a receiver arm to release a barrel latch, thereby allowing a chamber end of the barrel to droop about a transverse Y-axis of a pivot disposed near a distal end of the receiver arm; turning said banel with said left or right hand so that the chamber end of the banel is moved laterally to the left or right side of the receiver arm about a vertical Z-axis of the pivot to allow the user to load or unload a cartridge into/from the chamber of the banel; and laterally turning the barrel back to align the barrel with the receiver ami and then pivoting the barrel back to the receiver arm to release a spring-loaded pin so that the barrel latch is engage
  • the barrel pivot comprises a substantially cylindrical pivot pin that is joumaled in the forward receiver ami to pivot about the Z-axis and a clevis pin pivotable about the Y-axis, with the clevis pin passing through a bore on the pivot pin and the clevis pin being supported by a pair of clevises disposed on a top surface of the barrel.
  • the clevis pin allows the barrel to pivot substantially 5 degree angle away from the X-axis whilst the pivot pin allows the barrel to be turned laterally to the left or right hand side of the receiver body by substantially 20 degree.
  • the barrel opening mechanism comprises a barrel pivot direction lockout pin or selector.
  • the barrel opening mechanism has two notches fomied on its cylindrical surface, with the notches being angularly oriented with respect to each other and a paw extending from the pivot pin is restricted to move within a length of the selected notch, so that the direction of swivel of the barrel chamber end is selectable depending on whether the user is right-handed or left- handed.
  • the latch mechanism comprises a spring-loaded release pin, which allows the latch to engage with the catch only when the catch is received in the recess and the spring-loaded release pin is depressed.
  • the latch also comprises a hook configured integrally on a pivoted lever, such that a lever portion projects out on a left hand side of the forward receiver arm and another lever portion projects out on the right hand side of the forward receiver ami and the hook is engageable with a slot fomied on the catch.
  • a closed end of a Picatinny rail fomied along an upper portion of the forward receiver ami is disposed a stopper plate.
  • the stopper plate is located substantially above the barrel pivot and it keeps the pivot pin in position and at the same time transfer recoil forces from the grenade launcher to a supporting rifle mounted at the Picatinny rail.
  • FIG. 1A illustrates a grenade launcher (without a barrel guard) with a barrel latch in the locked position according to an embodiment of the present invention
  • FIG. IB illustrates the grenade launcher with the barrel disposed partially in a barrel sleeve
  • FIG. 1 C illustrates the grenade launcher can be connected to a rifle by means of a Picatinny rail;
  • FIG. 2A illustrates the grenade launcher shown in FIG. 1 A with the barrel latch in the released position such that the chamber side of the barrel droops downward;
  • FIGs. 2B and 2C illustrate the chamber side of the barrel being turned to the left hand side of the launcher; whilst FIG. 2D illustrates the chamber side of the barrel being turned to the right hand side;
  • FIG. 3A illustrates an exploded view of the barrel from the receiver body showing the pivot and latch mechanism of the present invention
  • FIG. 3B illustrates a plan view of the grenade launcher shown in FIG. 1A;
  • FIG. 3C illustrates a cut-out view showing the latch mechanism
  • FIG. 3D illustrates a sectional view showing the latch mechanism and barrel pivot
  • FIG. 4A illustrates a sectional view of the grenade launcher shown in FIG. 2A, whilst FIGs. 4B and 4C illustrate the barrel being turned respectively to the right hand and left hand sides; and
  • FIGs. 5 A and 5B illustrate perspective and exploded views of the grenade launcher incorporating a barrel pivot direction lockout pin or selector, whilst FIGs. 5C and 5D illustrate the chamber end of the barrel being restricted selectively to turn respectively to the right hand and left hand sides.
  • FIGs. 1A and IB show a grenade launcher 100 employing a barrel opening mechanism 105 according to the present invention.
  • the barrel opening mechanism 105 includes a barrel pivot 150 and a barrel latch mechanism 170.
  • the barrel opening mechanism 105 can be used in any single-shot gun, as exemplified by a grenade launcher.
  • the grenade launcher 100 includes a receiver body 1 10, a barrel 130 being connected to the receiver body 1 10 by the barrel pivot 150 and latch mechanism 170, a barrel sleeve 140 and a lock sleeve 132 to lock the barrel sleeve 140 to the barrel 130.
  • the receiver body 1 10 is substantially inverted L-shaped, with a forward pointing ann 1 10a provided to support the barrel 130, and the other proximal ann 1 10b for housing a trigger mechanism, with a portion being shaped for handgrip or as a butt stock.
  • the barrel pivot 150 is pivotable about two orthogonal axes, that is, a Y-axis transverse to the receiver arm 1 10a and a Z-axis perpendicular to the receiver arm 1 10a, with a longitudinal X-axis along a length of the receiver arm.
  • the latch mechanism 170 includes a pivoted lever 172 mounted inside the receiver arm 1 10a and a catch 180 disposed on a top surface of the barrel.
  • the lever 172 engages with the catch 180.
  • the lever 172 extends on both sides of the receiver arm 1 10a (as seen more clearly in FIG. 3B) so that it can be actuated with a thumb or finger of one's hand supporting the barrel 130.
  • a chamber end 134 of the barrel into which a projectile is inserted
  • the barrel 130 is supported only at the barrel pivot 150, as seen more clearly in FIG. 2A.
  • the drooped barrel is no longer in contact with any part of the receiver body 1 10 and is free to be turned laterally to the left or right hand side of the receiver body 1 10 about the Z-axis at the pivot 150.
  • the barrel 130 is operable to be turned laterally to the left or right side of the receiver body 1 10 by substantially 20 degree about the pivot 150 such that the projectile can be loaded or unloaded at the chamber end 134 of the barrel 130 without obstruction by the receiver arm 1 10b, as seen more clearly in FIGs. 2B, 2C, 2D, 4B and 4C.
  • FIG. 3A shows an exploded view of the barrel opening mechanism 105.
  • the pivot 150 is made up of a pivot pin 152, a pair of clevises 156 and a clevis pin 157.
  • the pivot pin 152 is substantially cylindrical in shape along the Z-axis but has two parallel flat surfaces 153 to cooperate with the pair of clevises 156.
  • a top part of the pivot pin 152 has a lateral projection 154 so that the lateral projection 154 is received in the receiver arm 1 10a for pivotal movement about the Z-axis.
  • a stopper plate 122 mounted at the end of a Picatinny rail 120 formed on an upper surface of the receive arm 1 10a, keeps the pivot pin 152 pivotable in the receiver arm 1 10a.
  • the clevis pin 157 goes through a bore on the clevises 156 and another bore through the pivot pin 152 to allow the barrel to pivot about the Y-axis.
  • the pivot 150 allows the barrel 130 to tilt or droop substantially 5 degree from the X-axis and at the same time be pivotable laterally to the left- or right-hand side of the receiver body 1 10 by substantially 20 degree.
  • An advantage of the present invention is that when the barrel 130 is in the open position, the chamber end 134 is unobstructed for loading and unloading of a projectile; this means that the barrel chamber is suitable to receive projectiles of a predetermined design but of varied lengths, thus ensuring the grenade launcher 100 incorporating the barrel opening mechanism 105 is usable with future projectiles that may be longer in lengths.
  • the other advantage of the present invention is that the barrel 130 is pivotable to the left- or right- hand side of the receiver body 1 10, thus making the grenade launcher ambidexterous.
  • the barrel sleeve 140 has an open channel 142 formed on the top, longitudinal portion as seen in the figures.
  • the open channel 142 is as wide as the distance between the outside faces of the clevises 156 or length of the clevis pin 157.
  • the width of the open channel 142 is substantially wider that the distance between the clevises or length of the clevis pin 157 but the edges of the open channel 142 are provided with a pair of projections 144, which are spaced apart to accommodate the distance between the clevises 156 or length of the clevis pin 157.
  • tolerance of the width between the pair of projections 144 need only to be controlled instead of along the entire length of the open channel 142.
  • the pair of projections 144 locate the clevis pin 157 in the clevises 156; with this arrangement, there is no need to provide any locking mechanism for the clevis pin 157, thus allowing the number of components of the barrel opening mechanism 105 to be reduced and further simplifying this mechanism.
  • the latch mechanism 170 includes the lever 172 and the cooperating catch 180 disposed on the top surface of the barrel 130 along the longitudinal X-axis.
  • FIG. 3C shows a cut-out portion of the latch mechanism 170 and shows the lever 172 has a portion being formed with a hook 174 to engage with a slot 182 formed on the catch 180.
  • the lever 172 is biased in the normal, engaged position by a spring 176.
  • the catch 180 extends out of the top surface of the barrel 130 but when the barrel is in the closed position, the catch 180 is received into the receiver arm 1 10a within a cavity located below the lever 172, as seen more clearly in FIG.
  • a spring-loaded pin 178 (not shown in the figures) is extended to prevent the lever 172 from returning to its original position after the latch mechanism 170 is activated and the barrel 130 is released from its connection at the catch 180 with the receiver arm 1 10a; in other words, the spring- loaded pin 178 is provided to prevent the hook 174 from re-engaging with the slot 182 until the barrel 130 is returned to its closed position, the catch 180 is fully received into its cavity below the receiver arm 1 10a and the spring loaded pin 1 78 is depressed.
  • the spring-loaded pin 178 serves as a very important safety lock to ensure that the barrel130 is connected to the receiver ami 1 10a by the latch mechanism 170 before the grenade launcher 100 is deployed.
  • the latch mechanism 170 is spaced apart from the pivot 150.
  • the latch mechanism 170 such as the parts of the lever 172 that projects out of the receiver arm 110a are located substantially forward with respect to the trigger guard 136. This allows a user to support the grenade launcher 100 with one hand at a position forward of the trigger guard 136 yet allowing a finger or thumb of the same hand to actuate the latch lever 172, with the other hand on the handgrip and its finger to activate the trigger.
  • a transverse lock pin 210 is disposed across the Picatinny rail 120 to lock a matching male component of the Picatinny rail disposed on a rifle 200 (as seen in FIG. 1 C) to which the grenade launcher 100 is to be mounted to.
  • the free end of the male component of the rifle's Picatinny rail is in butt contact with a thickness edge of the stopper plate 122 such that locking of the two Picatinny rail components at the lock pin 210 has a clearance fit.
  • the lock pin 210 is used to lock together the two components of the Picatinny rail when the grenade launcher 100 is mounted below the rifle 200 but does not take up any recoil forces during deployment. For this reason, the lock pin 210 is relatively small in size of substantially 2 to 3 mm square in cross-section.
  • FIGs. 5 A and 5B show exploded views of the above grenade launcher 100 incorporating a barrel pivot direction lockout pin or selector 160.
  • the pivot direction lockout pin or selector 160 is disposed on the receiver arm 1 10a parallel to and at a distance aft of the clevis pin 157. As shown in FIGs.
  • the direction lockout pin 160 has two notches 162a, 162b formed on the cylindrical surface, with the notches 162a, 162b being angularly oriented with each other; preferably, the notches 162a, 162b are substantially 90 degrees oriented to each other.
  • one of the notch 162a or 162b engages with a paw 158 extending laterally from a pivot pin 152a (which is a variation of the above pivot pin 152).
  • the direction lockout pin 160 extends out of the width of the receiver arm 110 and each end terminates with a knurled knob 164. Each knurled knob 164 may be located on the direction lockout pin 160 by means of a locking pin 166.
  • a user By turning the knurled knob 164, a user sets the rotational orientation of the direction lockout pin or selector 160 so that the paw 158 engages with the notch 162a or 162b; in effect, the direction of barrel swivel to the left- or right-hand side of the receiver arm 110a is restricted by the paw 158 moving within a length of the notch 162a or 162b.
  • the user selectively determines the direction of swivel of the barrel 130 to the left- or right-hand side of the receiver arm 110a by setting the direction lockout pin or selector 160 in a clockwise or anti-clockwise position depending on whether the user is right-handed or left-handed. For illustration, FIG.
  • FIG. 5C shows a left-handed user (ie. left hand on the hand-grip or butt 1 10b) and the position lockout pin 160 being set so that the paw 158 engages with the notch 162a and the chamber end 134 of the barrel 130 is to the right side of the receiver arm 110a.
  • FIG. 5D shows a right-handed user having set the position lockout pin 160 so that the paw 158 engages with the notch 162b and the chamber end 134 of the barrel 130 is swiveled to the left side of the receiver ami 1 10a.
  • the barrel opening mechanism of the present invention is advantageously ambidextrous.
  • the grenade launcher incorporating the barrel mechanism has relatively few additional parts, so making the grenade launcher still relatively light.
  • Another advantage of the present invention is that no tools are required to dismantle the barrel opening mechanism 105 or the entire barrel 130, for example, for cleaning. For example, by unscrewing the lock sleeve 132 from the ban-el 130, the barrel sleeve 140 can be removed from the barrel 130, thereby allowing the clevis pin 157 to be removed and the entire barrel 130 to be dismantled from the receiver body 110. In the same manner, no tools are required to reassemble the barrel opening mechanism or barrel onto the receiver body.
  • the above barrel opening mechanism 105 can be used on any single-shot gun, such as, a shotgun, irrespective of it being single- or double-barrel and its barrel size.
  • the spring-loaded pin 178 may be configured as a detent ball.

Abstract

The present invention provides a grenade launcher (100) in which a barrel (130) is connected to a receiver arm (110a) by a barrel pivot (150) and a releasable latch mechanism (170). When the barrel (130) is released from the receiver arm (110a) by the latch mechanism (170), the barrel pivot (150) allows the barrel to droop about 5 degree about a transverse Y-axis at the barrel pivot (150) and at the same time allowing the barrel to be turned laterally about a vertical Z-axis to the left or right hand side of the receiver arm. A top surface of the receiver arm has a Picatinny rail (120), a forward end of which is disposed a stopper plate (122) to secure a pivot pin (152) within the receiver arm (110a). The stopper plate (122) is provided to transmit recoil forces to an external device connected at the Picatinny rail (120).

Description

Barrel Opening Mechanism of Grenade Launcher
Field of Invention
[001] The present invention relates to a barrel opening mechanism for loading and unloading of cartridges into a barrel of a grenade launcher.
Background
[002] A grenade launcher may be a standalone device or detachably mounted below a rifle. For example, the grenade launcher uses a spin-stabilised 40 mm cartridge. A conventional grenade launcher may employ different methods of opening the barrel: longitudinal sliding opening; lateral swinging to the left hand, to the right hand side, downward or upward; and a combination of longitudinal sliding followed by a lateral swing. These methods of opening the barrel involve many components and often only designed for a right- or left- handed operator; in other words, these conventional grenade launchers are often not ambidextrous. For example, US 7,487,612, assigned to FN Herstal S.A., discloses two sliding blocks (13, 14) operable to slide with two longitudinal slides (17) such that the barrel is advanced in a first longitudinal direction and swiveled laterally in the final phase of the longitudinal movement.
[003] In another example, US 3,641 ,691 , assigned to the US Army, discloses a grenade launcher in which the barrel is pivotable downwardly to a 15 degree angle and an ejector rod is used to eject the used cartridge. When the barrel is closed, the firing mechanism is automatically locked in the firing position.
[004] Despite development of known grenade launchers, there exists a need for another type of barrel opening mechanism that is ambidextrous yet not complex or heavy in design.
Summary
[005] The following presents a simplified summary to provide a basic understanding of the present invention. This summary is not an extensive overview of the invention, and is not intended to identify key features of the invention. Rather, it is to present some of the inventive concepts of this invention in a generalised form as a prelude to the detailed description that is to follow. [006] The present invention seeks to provide a barrel opening mechanism for a grenade launcher that is ambidextrous in operation yet designed with a minimum number of components. In addition, the Picatinny rail on the top portion of the barrel is configured to transfer recoil forces from the grenade launcher to a supporting rifle it is connected to. [007] In one embodiment, the present invention provides a a receiver body, which is substantially an inverted L-shaped, with a forward pointing arm and a proximal arm, wherein the proximal ami is configured for housing a trigger mechanism; and a barrel connected below the forward pointing receiver ami by a barrel pivot and a latch mechanism; wherein the latch mechanism comprises a latch disposed in the forward receiver arm and is operable to engage with a catch disposed on a top portion of the barrel so that the latch is engageable with the catch when the barrel is in a closed position and longitudinal X-axes of the barrel and forward receiver arm are substantially parallel, and when the latch is actuated by an appendage of a left or right hand of a user supporting the barrel, the latch becomes released from the catch, thereby allowing the barrel to droop or pivot away from the forward receiver arm about a transverse Y-axis at the ban-el pivot so that the same hand is operable to turn a chamber end of the barrel laterally to the left or right hand side about a vertical Z-axis at the ban-el pivot for loading or unloading a cartridge into the barrel. [008] In another embodiment, the present invention provides a method of opening a barrel release and lock mechanism of a grenade launcher. This method comprises: supporting a barrel of a grenade launcher with a left or right hand of a user; using an appendage of said left or right hand to push a lever portion that protrudes on each of two sides of a receiver arm to release a barrel latch, thereby allowing a chamber end of the barrel to droop about a transverse Y-axis of a pivot disposed near a distal end of the receiver arm; turning said banel with said left or right hand so that the chamber end of the banel is moved laterally to the left or right side of the receiver arm about a vertical Z-axis of the pivot to allow the user to load or unload a cartridge into/from the chamber of the banel; and laterally turning the barrel back to align the barrel with the receiver ami and then pivoting the barrel back to the receiver arm to release a spring-loaded pin so that the barrel latch is engageable with a cooperating catch and the barrel is re-connected to the receiver arm at the latch. [009] Preferably, the barrel pivot comprises a substantially cylindrical pivot pin that is joumaled in the forward receiver ami to pivot about the Z-axis and a clevis pin pivotable about the Y-axis, with the clevis pin passing through a bore on the pivot pin and the clevis pin being supported by a pair of clevises disposed on a top surface of the barrel. [0010] Preferably, the clevis pin allows the barrel to pivot substantially 5 degree angle away from the X-axis whilst the pivot pin allows the barrel to be turned laterally to the left or right hand side of the receiver body by substantially 20 degree. Preferably, the barrel opening mechanism comprises a barrel pivot direction lockout pin or selector. The barrel opening mechanism has two notches fomied on its cylindrical surface, with the notches being angularly oriented with respect to each other and a paw extending from the pivot pin is restricted to move within a length of the selected notch, so that the direction of swivel of the barrel chamber end is selectable depending on whether the user is right-handed or left- handed. [0011] Preferably, the latch mechanism comprises a spring-loaded release pin, which allows the latch to engage with the catch only when the catch is received in the recess and the spring-loaded release pin is depressed. The latch also comprises a hook configured integrally on a pivoted lever, such that a lever portion projects out on a left hand side of the forward receiver arm and another lever portion projects out on the right hand side of the forward receiver ami and the hook is engageable with a slot fomied on the catch.
[0012] Preferably, a closed end of a Picatinny rail fomied along an upper portion of the forward receiver ami is disposed a stopper plate. The stopper plate is located substantially above the barrel pivot and it keeps the pivot pin in position and at the same time transfer recoil forces from the grenade launcher to a supporting rifle mounted at the Picatinny rail. Brief Description of the Drawings
[0013] This invention will be described by way of non-limiting embodiments of the present invention, with reference to the accompanying drawings, in which: [0014] FIG. 1A illustrates a grenade launcher (without a barrel guard) with a barrel latch in the locked position according to an embodiment of the present invention, whilst FIG. IB illustrates the grenade launcher with the barrel disposed partially in a barrel sleeve;
FIG. 1 C illustrates the grenade launcher can be connected to a rifle by means of a Picatinny rail;
[0015] FIG. 2A illustrates the grenade launcher shown in FIG. 1 A with the barrel latch in the released position such that the chamber side of the barrel droops downward;
FIGs. 2B and 2C illustrate the chamber side of the barrel being turned to the left hand side of the launcher; whilst FIG. 2D illustrates the chamber side of the barrel being turned to the right hand side;
[0016] FIG. 3A illustrates an exploded view of the barrel from the receiver body showing the pivot and latch mechanism of the present invention;
FIG. 3B illustrates a plan view of the grenade launcher shown in FIG. 1A;
FIG. 3C illustrates a cut-out view showing the latch mechanism, whilst FIG. 3D illustrates a sectional view showing the latch mechanism and barrel pivot;
[0017] FIG. 4A illustrates a sectional view of the grenade launcher shown in FIG. 2A, whilst FIGs. 4B and 4C illustrate the barrel being turned respectively to the right hand and left hand sides; and
[0018] FIGs. 5 A and 5B illustrate perspective and exploded views of the grenade launcher incorporating a barrel pivot direction lockout pin or selector, whilst FIGs. 5C and 5D illustrate the chamber end of the barrel being restricted selectively to turn respectively to the right hand and left hand sides.
Detailed Description [0019] One or more specific and alternative embodiments of the present invention will now be described with reference to the attached drawings. It shall be apparent to one skilled in the art, however, that this invention may be practised without such specific details. Some of the details may not be described at length so as not to obscure the invention. For ease of reference, common reference numerals or series of numerals will be used throughout the figures when referring to the same or similar features common to the figures.
[0020] FIGs. 1A and IB show a grenade launcher 100 employing a barrel opening mechanism 105 according to the present invention. The barrel opening mechanism 105 includes a barrel pivot 150 and a barrel latch mechanism 170. The barrel opening mechanism 105 can be used in any single-shot gun, as exemplified by a grenade launcher. As shown in FIGs. 1 A and I B, the grenade launcher 100 includes a receiver body 1 10, a barrel 130 being connected to the receiver body 1 10 by the barrel pivot 150 and latch mechanism 170, a barrel sleeve 140 and a lock sleeve 132 to lock the barrel sleeve 140 to the barrel 130. The receiver body 1 10 is substantially inverted L-shaped, with a forward pointing ann 1 10a provided to support the barrel 130, and the other proximal ann 1 10b for housing a trigger mechanism, with a portion being shaped for handgrip or as a butt stock. The barrel pivot 150 is pivotable about two orthogonal axes, that is, a Y-axis transverse to the receiver arm 1 10a and a Z-axis perpendicular to the receiver arm 1 10a, with a longitudinal X-axis along a length of the receiver arm. The latch mechanism 170 includes a pivoted lever 172 mounted inside the receiver arm 1 10a and a catch 180 disposed on a top surface of the barrel. In the normal barrel closed position, the lever 172 engages with the catch 180. The lever 172 extends on both sides of the receiver arm 1 10a (as seen more clearly in FIG. 3B) so that it can be actuated with a thumb or finger of one's hand supporting the barrel 130. When the latch mechanism 170 is released by momentarily pressing on the lever 172 on either side of the receiver arm 1 10a, a chamber end 134 of the barrel (into which a projectile is inserted) is allowed to droop substantially 5 degree from the longitudinal X-axis about the Y-axis at the barrel pivot 150. In this drooped-down or open pivoted position, the barrel 130 is supported only at the barrel pivot 150, as seen more clearly in FIG. 2A. As the pivot 150 is close to the top surface of the barrel 130 and with a relief angle provided at a front tip 1 14 of the receiver arm 1 10a, the drooped barrel is no longer in contact with any part of the receiver body 1 10 and is free to be turned laterally to the left or right hand side of the receiver body 1 10 about the Z-axis at the pivot 150. In one embodiment, the barrel 130 is operable to be turned laterally to the left or right side of the receiver body 1 10 by substantially 20 degree about the pivot 150 such that the projectile can be loaded or unloaded at the chamber end 134 of the barrel 130 without obstruction by the receiver arm 1 10b, as seen more clearly in FIGs. 2B, 2C, 2D, 4B and 4C.
[0021] FIG. 3A shows an exploded view of the barrel opening mechanism 105. As shown in FIG. 3 A, the pivot 150 is made up of a pivot pin 152, a pair of clevises 156 and a clevis pin 157. The pivot pin 152 is substantially cylindrical in shape along the Z-axis but has two parallel flat surfaces 153 to cooperate with the pair of clevises 156. A top part of the pivot pin 152 has a lateral projection 154 so that the lateral projection 154 is received in the receiver arm 1 10a for pivotal movement about the Z-axis. A stopper plate 122, mounted at the end of a Picatinny rail 120 formed on an upper surface of the receive arm 1 10a, keeps the pivot pin 152 pivotable in the receiver arm 1 10a. The clevis pin 157 goes through a bore on the clevises 156 and another bore through the pivot pin 152 to allow the barrel to pivot about the Y-axis. With this pivot design, the pivot 150 allows the barrel 130 to tilt or droop substantially 5 degree from the X-axis and at the same time be pivotable laterally to the left- or right-hand side of the receiver body 1 10 by substantially 20 degree. An advantage of the present invention is that when the barrel 130 is in the open position, the chamber end 134 is unobstructed for loading and unloading of a projectile; this means that the barrel chamber is suitable to receive projectiles of a predetermined design but of varied lengths, thus ensuring the grenade launcher 100 incorporating the barrel opening mechanism 105 is usable with future projectiles that may be longer in lengths. The other advantage of the present invention is that the barrel 130 is pivotable to the left- or right- hand side of the receiver body 1 10, thus making the grenade launcher ambidexterous.
[0022] Referring back to FIGs. IB and 3 A, the barrel sleeve 140 has an open channel 142 formed on the top, longitudinal portion as seen in the figures. The open channel 142 is as wide as the distance between the outside faces of the clevises 156 or length of the clevis pin 157. Preferably, the width of the open channel 142 is substantially wider that the distance between the clevises or length of the clevis pin 157 but the edges of the open channel 142 are provided with a pair of projections 144, which are spaced apart to accommodate the distance between the clevises 156 or length of the clevis pin 157. In the later embodiment, tolerance of the width between the pair of projections 144 need only to be controlled instead of along the entire length of the open channel 142. In use, when the barrel sleeve 140 is in place around the barrel 130, the pair of projections 144 locate the clevis pin 157 in the clevises 156; with this arrangement, there is no need to provide any locking mechanism for the clevis pin 157, thus allowing the number of components of the barrel opening mechanism 105 to be reduced and further simplifying this mechanism.
[0023] As can also be seen in FIG. 3 A, the latch mechanism 170 includes the lever 172 and the cooperating catch 180 disposed on the top surface of the barrel 130 along the longitudinal X-axis. FIG. 3C shows a cut-out portion of the latch mechanism 170 and shows the lever 172 has a portion being formed with a hook 174 to engage with a slot 182 formed on the catch 180. The lever 172 is biased in the normal, engaged position by a spring 176. As seen in FIGs. 2 A, 2B or 3 A, the catch 180 extends out of the top surface of the barrel 130 but when the barrel is in the closed position, the catch 180 is received into the receiver arm 1 10a within a cavity located below the lever 172, as seen more clearly in FIG. 3C, so that the longitudinal axes of the barrel 130 and receiver arm 1 10a are substantially parallel. In order to ensure that the latch mechanism 170 is operable only when the catch 180 is received in the cavity located below the lever 172, a spring-loaded pin 178 (not shown in the figures) is extended to prevent the lever 172 from returning to its original position after the latch mechanism 170 is activated and the barrel 130 is released from its connection at the catch 180 with the receiver arm 1 10a; in other words, the spring- loaded pin 178 is provided to prevent the hook 174 from re-engaging with the slot 182 until the barrel 130 is returned to its closed position, the catch 180 is fully received into its cavity below the receiver arm 1 10a and the spring loaded pin 1 78 is depressed. In this way, the spring-loaded pin 178 serves as a very important safety lock to ensure that the barrel130 is connected to the receiver ami 1 10a by the latch mechanism 170 before the grenade launcher 100 is deployed.
[0024] In the above ban-el opening mechanism 105, the latch mechanism 170 is spaced apart from the pivot 150. Preferably, the latch mechanism 170, such as the parts of the lever 172 that projects out of the receiver arm 110a are located substantially forward with respect to the trigger guard 136. This allows a user to support the grenade launcher 100 with one hand at a position forward of the trigger guard 136 yet allowing a finger or thumb of the same hand to actuate the latch lever 172, with the other hand on the handgrip and its finger to activate the trigger.
[0025] In a further embodiment, a transverse lock pin 210 is disposed across the Picatinny rail 120 to lock a matching male component of the Picatinny rail disposed on a rifle 200 (as seen in FIG. 1 C) to which the grenade launcher 100 is to be mounted to. In use, the free end of the male component of the rifle's Picatinny rail is in butt contact with a thickness edge of the stopper plate 122 such that locking of the two Picatinny rail components at the lock pin 210 has a clearance fit. With clearance fit between the lock pin 210 and the rifle's Picantinny rail component, recoil forces on the receiver body 100 are transferred to the rifle 200 through the stopper plate 122 and Picatinny rail without the lock pin 210 taking up the recoil forces. In other words, in the present invention, the lock pin 210 is used to lock together the two components of the Picatinny rail when the grenade launcher 100 is mounted below the rifle 200 but does not take up any recoil forces during deployment. For this reason, the lock pin 210 is relatively small in size of substantially 2 to 3 mm square in cross-section. By providing the lock pin 210, the grenade launcher 100 according to the present invention can be deployed as a stand-alone equipment or detachably mounted to a rifle. [0026] FIGs. 5 A and 5B show exploded views of the above grenade launcher 100 incorporating a barrel pivot direction lockout pin or selector 160. The pivot direction lockout pin or selector 160 is disposed on the receiver arm 1 10a parallel to and at a distance aft of the clevis pin 157. As shown in FIGs. 5A and 5B, the direction lockout pin 160 has two notches 162a, 162b formed on the cylindrical surface, with the notches 162a, 162b being angularly oriented with each other; preferably, the notches 162a, 162b are substantially 90 degrees oriented to each other. When assembled, one of the notch 162a or 162b engages with a paw 158 extending laterally from a pivot pin 152a (which is a variation of the above pivot pin 152). The direction lockout pin 160 extends out of the width of the receiver arm 110 and each end terminates with a knurled knob 164. Each knurled knob 164 may be located on the direction lockout pin 160 by means of a locking pin 166. By turning the knurled knob 164, a user sets the rotational orientation of the direction lockout pin or selector 160 so that the paw 158 engages with the notch 162a or 162b; in effect, the direction of barrel swivel to the left- or right-hand side of the receiver arm 110a is restricted by the paw 158 moving within a length of the notch 162a or 162b. In this manner, the user selectively determines the direction of swivel of the barrel 130 to the left- or right-hand side of the receiver arm 110a by setting the direction lockout pin or selector 160 in a clockwise or anti-clockwise position depending on whether the user is right-handed or left-handed. For illustration, FIG. 5C shows a left-handed user (ie. left hand on the hand-grip or butt 1 10b) and the position lockout pin 160 being set so that the paw 158 engages with the notch 162a and the chamber end 134 of the barrel 130 is to the right side of the receiver arm 110a. On the other hand, FIG. 5D shows a right-handed user having set the position lockout pin 160 so that the paw 158 engages with the notch 162b and the chamber end 134 of the barrel 130 is swiveled to the left side of the receiver ami 1 10a.
[0027] From the above description, a reader will appreciate that the barrel opening mechanism of the present invention is advantageously ambidextrous. In addition, the grenade launcher incorporating the barrel mechanism has relatively few additional parts, so making the grenade launcher still relatively light. Another advantage of the present invention is that no tools are required to dismantle the barrel opening mechanism 105 or the entire barrel 130, for example, for cleaning. For example, by unscrewing the lock sleeve 132 from the ban-el 130, the barrel sleeve 140 can be removed from the barrel 130, thereby allowing the clevis pin 157 to be removed and the entire barrel 130 to be dismantled from the receiver body 110. In the same manner, no tools are required to reassemble the barrel opening mechanism or barrel onto the receiver body.
[0028] While specific embodiments have been described and illustrated, it is understood that many changes, modifications, variations and combinations thereof could be made to the present invention without departing from the scope of the invention. For example, the above barrel opening mechanism 105 can be used on any single-shot gun, such as, a shotgun, irrespective of it being single- or double-barrel and its barrel size. In a further example, the spring-loaded pin 178 may be configured as a detent ball.

Claims

CLAIMS:
1. A grenade launcher comprising:
a receiver body, which is substantially an inverted L-shaped. with a forward pointing ami and a proximal ami, wherein the proximal ami is configured for housing a trigger mechanism; and
a barrel connected below the forward pointing receiver arm by a barrel pivot and a latch mechanism;
wherein the latch mechanism comprises a latch disposed in the forward receiver arm and is operable to engage with a catch disposed on a top portion of the barrel so that the latch is engageable with the catch when the barrel is in a closed position and longitudinal X-axes of the ban-el and forward receiver arm are substantially parallel, and when the latch is actuated by an appendage of a left or right hand of a user supporting the barrel, the latch becomes released from the catch, thereby allowing the barrel to droop or pivot away from the forward receiver ami about a transverse Y-axis at the barrel pivot so that the same hand is operable to turn a chamber end of the barrel laterally to the left or right hand side about a vertical Z-axis at the barrel pivot for loading or unloading a cartridge into the barrel.
2. A grenade launcher according to claim 1 , wherein said barrel pivot comprises a substantially cylindrical pivot pin that is journaled in the forward receiver ami to pivot about the Z-axis and a clevis pin pivotable about the Y-axis, with the clevis pin passing through a bore on the pivot pin and the clevis pin being supported by a pair of clevises disposed on a top surface of the barrel.
3. A grenade launcher according to claim 2, wherein the clevis pin allows the barrel to pivot substantially 5 degree angle away from the X-axis whilst the pivot pin allows the ban-el to be turned laterally to the left or right hand side of the receiver body by substantially 20 degree.
4. A grenade launcher according to any one of claims 1-3, wherein the catch is a projected element mounted on the top surface portion of the barrel.
5. A grenade launcher according to claim 4, wherein the catch is received in a recess formed in the forward receiver at the position below the latch.
6. A grenade launcher according to claim 5, wherein said latch mechanism further comprises a spring-loaded release pin, which allows the latch to engage with the catch only when the catch is received in the recess and the spring-loaded release pin is depressed.
7. A grenade launcher according to any one of claims 1 -6, wherein the latch comprises a hook configured integrally on a pivoted lever, such that a lever portion projects out on a left hand side of the forward receiver arm and another lever portion projects out on the right hand side of the forward receiver arm and the hook is engageable with a slot fomied on the catch.
8. A grenade launcher according to any one of claims 2-7, further comprising a pivot direction lockout pin disposed on the forward receiver arm in a position parallel to the clevis pin and at a distance to engage with a paw projecting laterally from the pivot pin.
9. A grenade launcher according to claim 8, wherein the pivot direction lockout pin has two notches formed on a cylindrical surface of the direction lockout pin, with the notches being angularly oriented with respect to each other and the paw is restricted to move within a length of the selected notch depending on whether the user is right-handed or left-handed.
10. A grenade launcher according to any one of claims 1-9, further comprising a barrel sleeve to receive the barrel.
1 1. A grenade launcher according to claim 10, wherein the barrel sleeve comprises an open channel, with the width of the open channel being configured to locate the clevis pin.
12. A grenade launcher according to claim 1 1 , wherein the width of the open channel is controlled only at a pair of projections projecting into the open channel.
13. A grenade launcher according to any one of claims 10- 12, wherein the barrel sleeve is locked in position on the barrel by a lock sleeve, and locking and unlocking of the barrel sleeve does not require any tool.
14. A grenade launcher according to any one of claims 1 - 13, wherein an upper portion of the forward receiver arm comprises a female half of a Picatinny rail.
15. A grenade launcher according to claim 14, wherein a closed end of the Picatinny rail is disposed a stopper plate, which is located substantially above the ban-el pivot.
16. A grenade launcher according to claim 15, further comprising a lock pin disposed transversely through' the female half of the Picatinny rail to prevent an external device mounted in the Picatinny rail from dislodgment, wherein the lock pin is disposed a predetermined distance from a contiguous face of the stopper plate so that impulse forces of the grenade launcher are transitted to the external device directly tlirough the contiguous face of the stopper plate.
17. A method of operating a barrel release and lock mechanism, said method comprising:
supporting a barrel of a grenade launcher with a left or right hand of a user;
using an appendage of said left or right hand to push a lever portion that protrudes on each of two sides of a receiver arm to release a barrel latch, thereby allowing a chamber end of the barrel to droop about a transverse Y-axis of a pivot disposed near a distal end of the receiver arm;
turning said barrel with said left or right hand so that the chamber end of the barrel is moved laterally to the left or right side of the receiver arm about a vertical Z-axis of the pivot to allow the user to load or unload a cartridge into/from the chamber of the ban-el; and
laterally turning the barrel back to align the ban-el with the receiver ami and then pivoting the ban-el back to the receiver ami to release a spring-loaded pin so that the barrel latch is engageable with a cooperating catch and the ban-el is re-connected to the receiver aim at the latch.
EP14769600.9A 2013-03-20 2014-03-19 Barrel opening mechanism of grenade launcher Active EP2976591B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SG2013020433A SG2013020433A (en) 2013-03-20 2013-03-20 Barrel opening mechanism of grenade launcher
PCT/SG2014/000136 WO2014149003A1 (en) 2013-03-20 2014-03-19 Barrel opening mechanism of grenade launcher

Publications (3)

Publication Number Publication Date
EP2976591A1 true EP2976591A1 (en) 2016-01-27
EP2976591A4 EP2976591A4 (en) 2016-11-02
EP2976591B1 EP2976591B1 (en) 2018-05-16

Family

ID=55129335

Family Applications (1)

Application Number Title Priority Date Filing Date
EP14769600.9A Active EP2976591B1 (en) 2013-03-20 2014-03-19 Barrel opening mechanism of grenade launcher

Country Status (5)

Country Link
EP (1) EP2976591B1 (en)
BR (1) BR112015024157B1 (en)
SG (2) SG2013020433A (en)
TR (1) TR201811923T4 (en)
WO (1) WO2014149003A1 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10234222B2 (en) * 2016-08-09 2019-03-19 Gonzalo Couce Single 40 mm projectile launcher
WO2020027747A1 (en) * 2018-02-15 2020-02-06 Mertsav Savunma Sistemleri Sanayi Ve Ticaret Limited Sirketi A barrel tilting mechanism
TR201808565A2 (en) 2018-06-18 2018-07-23 Armsan Silah Sanayi Ve Ticaret Anonim Sirketi A Modular Bomb Launcher
RU2694383C1 (en) * 2018-10-05 2019-07-12 Акционерное общество "Концерн "Калашников" Under-barrel grenade launcher to small arms
WO2020236092A1 (en) 2019-05-17 2020-11-26 Ata Silah Sanayi Anonim Sirketi Safety apparatus for grenade launcher assembly

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3332162A (en) * 1965-12-22 1967-07-25 Honeywell Inc Combined rifle and grenade launcher
US3641691A (en) * 1969-05-21 1972-02-15 Us Army Grenade launcher with pivotally mounted barrel
US3967402A (en) * 1975-01-22 1976-07-06 The United States Of America As Represented By The Scretary Of The Army Manually-operated firearm with forward-moving barrel and pivoted breech block
DE3202806C2 (en) * 1982-01-28 1985-05-30 Heckler & Koch Gmbh, 7238 Oberndorf Grenade launcher additional weapon for attachment to automatic fire rifles
DE19925864C1 (en) * 1999-06-07 2000-08-10 Heckler & Koch Gmbh Grenade launcher for fixture to rifle has launching barrel pivotable around static cross axis near to mouth, with base housing supporting trigger mechanism
BE1016610A3 (en) 2005-05-31 2007-02-06 Fn Herstal Sa Grenade launcher improved.
US7360478B2 (en) * 2005-09-30 2008-04-22 Colt Canada Corporation Projectile launcher convertible for left or right hand operation

Also Published As

Publication number Publication date
TR201811923T4 (en) 2018-09-21
WO2014149003A1 (en) 2014-09-25
BR112015024157A2 (en) 2017-07-18
BR112015024157B1 (en) 2022-05-10
EP2976591B1 (en) 2018-05-16
SG11201507699WA (en) 2015-10-29
EP2976591A4 (en) 2016-11-02
SG2013020433A (en) 2014-10-30

Similar Documents

Publication Publication Date Title
EP2976591B1 (en) Barrel opening mechanism of grenade launcher
EP2721364B1 (en) Locking front sight for a firearm and firearm with locking front sight
US7810269B2 (en) Frame-mounted trigger safety and well extension
EP2122291B1 (en) Lockable safety for firearm
US8567301B1 (en) Side offset charging handle
US20060254111A1 (en) Adjustable firearm stock
US9222738B2 (en) Ambidextrous charging handle for firearm
US8307747B2 (en) Self-engaging non-reciprocating charging handle
US8549982B2 (en) Firearm control devices
US10215513B2 (en) AR style receiver compatible with pistol magazines and cartridges
US9500421B1 (en) Firearm charging handle
US20110154709A1 (en) Insertion magazine for a small arm
US8186087B2 (en) Rifle trigger safety block
US9835394B2 (en) Charging handle for a firearm with angled latch
US10041751B2 (en) Rotary lockup action
US6360467B1 (en) Muzzleloading rifle with pivotal bolt action
US6968642B1 (en) Close combat handguard for rifles
EP4022245A1 (en) Folding stock assembly for firearms
US6405470B1 (en) Firearm safety lock
US6817131B1 (en) Safety device for firearms with a firing pin lock

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20151020

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

DAX Request for extension of the european patent (deleted)
A4 Supplementary search report drawn up and despatched

Effective date: 20161006

RIC1 Information provided on ipc code assigned before grant

Ipc: F41A 35/06 20060101ALI20160929BHEP

Ipc: F41A 3/04 20060101ALI20160929BHEP

Ipc: F41A 3/58 20060101ALI20160929BHEP

Ipc: F41C 27/06 20060101ALI20160929BHEP

Ipc: F41A 9/45 20060101AFI20160929BHEP

RIC1 Information provided on ipc code assigned before grant

Ipc: F41C 27/06 20060101ALI20171010BHEP

Ipc: F41A 3/58 20060101ALI20171010BHEP

Ipc: F41A 3/04 20060101ALI20171010BHEP

Ipc: F41A 9/45 20060101AFI20171010BHEP

Ipc: F41A 35/06 20060101ALI20171010BHEP

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

INTG Intention to grant announced

Effective date: 20171120

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

RIN1 Information on inventor provided before grant (corrected)

Inventor name: PANG, KHENG HONG SAMUEL

Inventor name: HENG, KHEE NGEE

Inventor name: TANG, WEI QIANG

Inventor name: LI, WEIXIAN WILSON

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602014025619

Country of ref document: DE

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 999969

Country of ref document: AT

Kind code of ref document: T

Effective date: 20180615

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20180516

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180816

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180816

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180516

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180516

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180516

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180516

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180516

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180516

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180516

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180817

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180516

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 999969

Country of ref document: AT

Kind code of ref document: T

Effective date: 20180516

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180516

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180516

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180516

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180516

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180516

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180516

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180516

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602014025619

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180516

Ref country code: IT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180516

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20190219

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180516

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180516

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20190319

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180516

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190319

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20190331

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190319

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190331

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190319

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190331

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190331

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190331

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190319

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180917

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180516

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180916

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20140319

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180516

REG Reference to a national code

Ref country code: DE

Ref legal event code: R081

Ref document number: 602014025619

Country of ref document: DE

Owner name: ST ENGINEERING ADVANCED MATERIAL ENGINEERING P, SG

Free format text: FORMER OWNER: ADVANCED MATERIAL ENGINEERING PTE. LTD., SINGAPORE, SG

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: TR

Payment date: 20230308

Year of fee payment: 10

Ref country code: DE

Payment date: 20230331

Year of fee payment: 10

P01 Opt-out of the competence of the unified patent court (upc) registered

Effective date: 20230522