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US3745876A - Telescoping ammunition launcher - Google Patents

Telescoping ammunition launcher Download PDF

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Publication number
US3745876A
US3745876A US00082656A US3745876DA US3745876A US 3745876 A US3745876 A US 3745876A US 00082656 A US00082656 A US 00082656A US 3745876D A US3745876D A US 3745876DA US 3745876 A US3745876 A US 3745876A
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Prior art keywords
firearm
deflector
firing tube
button
trigger
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US00082656A
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J Rocha
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US Department of Army
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US Department of Army
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00Rocket or torpedo launchers
    • F41F3/04Rocket or torpedo launchers for rockets
    • F41F3/045Rocket or torpedo launchers for rockets adapted to be carried and used by a person, e.g. bazookas
    • F41F3/0455Bazookas
    • 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
    • F41A1/00Missile propulsion characterised by the use of explosive or combustible propellant charges
    • F41A1/08Recoilless guns, i.e. guns having propulsion means producing no recoil
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00Rocket or torpedo launchers
    • F41F3/04Rocket or torpedo launchers for rockets
    • F41F3/042Rocket or torpedo launchers for rockets the launching apparatus being used also as a transport container for the rocket
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00Rocket or torpedo launchers
    • F41F3/04Rocket or torpedo launchers for rockets
    • F41F3/077Doors or covers for launching tubes

Definitions

  • a telescopic firearm including a firing tube for the [21] Appl. No.: 82,656 discharge of a projectile, a blast deflector, a flash deflector for receiving said firing tube and blast deflector when telescoped thereinto, covers mounted by hinges [52] U.S.
  • This invention relates to recoilless firearms and more particularly to recoilless launchers of shells.
  • FIG. 1 shows the firearm extended and being aimed at a target
  • FIG. 2 is a longitudinally cross-sectioned view of the firearm shown telescoped
  • FIG. 3 is a cross-sectional view of the front cover taken through the mounting hinge
  • FIG. 4 is a cross-sectioned view of the rear cover taken through the mounting hinge
  • FIG. 5 is an exploded perspective view of the firing mechanism
  • FIG. 6 is a longitudinally cross-sectioned view of the firearm shown extended
  • FIG. 7 is a view taken along line 77 of FIG. 6;
  • FIG. 8 is a view taken along line 8-8 of FIG. 6;
  • FIG. 9 is an enlarged cross-sectioned view of the latch for releasably holding the sections of the firearm extended.
  • a firearm 12 which is adapted for firing a 75mm projectile 14 carrying a warhead 15 and which includes in telescopic arrangement a firing tube 16, a flash deflector 18, and a blast deflector 20 composed of three telescopic sections including an inner section 22.
  • firing tube 16 and blast deflector 20 are nested within flash deflector 18 which acts as a casing therefor and the ends of the flash deflector are respectively closed by a front cover 26 and a rear cover 28 which are hingedly mounted on the flash deflector as hereinafter described.
  • Front cover 26 and rear cover 28 are semielliptical in shape for added strength and are fabricated from transparent plastic material for a reason noted hereinafter.
  • firearm has a length of about 30 inches and, when telescoped, is approximately 10% inches long.
  • firing tube 16 is rolled back over the outside thereof, as noted at 30, to form a bearing surface for slidingly supporting flash deflector 18 so as to be extendable forwardly relative to the firing tube.
  • the rear end of flash deflector 18 is :rolled back inwardly, as noted at 32, so as to be receivable by rolled end 30 of firing tube 16 to limit the extension of the flash deflector relative thereto.
  • the sections of blast deflector 20 are corrugated longitudinally along the entire lengths hereof for added structural strength so as to be radially expandable to relieve any excessive gas pressure in event the blast defiector should be plugged by dirt. or other obstruction when firearm 12 is discharged.
  • a ring 34 Provided inside of inner section 22 at the front end thereof is a ring 34 the inside diameter of which is the same as the outside diameter of firing tube 16 so as to have sliding contact therewith, and such ring is contactable with a collar 36 provided on the outside of the rear end of the firing tube 16 to limit the rearward displacement of the inner section relative thereto.
  • An external collar 38 and an internal ring 40 are provided respectively on the rear and front ends of each of the sections of blast deflector 20 to limit the extension of the sections and such sections and flash deflector 18 are releasably held extended by spring latches 41 as best shown in FIG. 9.
  • Firing tube 16 is provided with a combustion chamber 42 in the rear portion and a launching section 44 in the front portion. The rear portion of projectile 14 is received by launching section 44 with warhead 15 extending forwardly therefrom. Flash deflector 18 is sufficiently longer than firing tube 16 to inclose warhead 15 when the flash deflector is telescoped over the firing tube.
  • a rifled rotating band 45 is provided at the front end of launching section 44 to mate with pre-engraved grooves 46 on the rear portion of projectile 14 for spinning the projectile when propelled from the launching section.
  • Four stabilizing fins 48 are hingedly mounted on the rear end of projectile l4 and such fins are folded up to be received by combustion chamber 42.
  • the spin of projectile 14 by rotating band 45 causes fins 48 to open, according to conventional design, as the projectile leaves firing tube 16.
  • Projectile 14 is propelled into flight by a propellant 49 which is packed in combustion chamber 42 around fins 48 at the rear end of the projectile.
  • venturi 50 which permits the rearward escape of a predetermined amount of the exploded gases therethrough, when propellant 49 is ignited, for counteracting the recoil forces produced in firearm 12 by the ignition.
  • the rear end of firing tube 16 is sealed forwardly of venturi 50 by a rupture disc 52 which holds propellant 49 in combustion chamber 42 and aids ignition of the propellant.
  • Rupture disc 52 is preferably fabricated from plastic material which is completely disintegrated when propellant 49 is ignited, to reduce the hazard of the disc becoming a secondary missile.
  • Propellant 49 is ignited by a firing mechanism 54 which includes a housing 56 fixed to the inside of combustion chamber 42.
  • Housing 56 is U-shaped in crosssection with an opening 58 therethrough and is longitudinally disposed so as to be straddled by one pair of the fins 48 and so that the rear end of housing 56 is spaced from rupture disc 52.
  • a primer 60 which, when initiated, ignites propellant 49.
  • Primer 60 is initiated by a firing pin 62 which is slidingly disposed in opening 58 and which is provided with a pair of longitudinally spaced collars 63 which form a channel 64.
  • Firing pin 62 is biased rearwardly for striking primer 60 by a coil spring 65 which is disposed between the rear end of housing 56 and the front one of the collars.
  • Firing pin 62 is releasably held in a cocked position by a scar 66 which is actuatable to release the firing pin by a trigger 68 slidingly received by a radial hole 70 of rectangular cross-section through the wall of firing tube l6.
  • Sear 66 is received between the collars 63 and is provided with alongitudinal recess 71 along the underside to receive the axial section of channel 64. Whereby vertical displacement of sear 66 is permitted between a firing pin holding position wherein the sear is extended upwardly to be partially received by hole 70 and a firing pin release position wherein the sear is entirely received by opening 58.
  • sear 66 Provided along the top of sear 66 is a T-flange 72 which is longitudinally disposed and which is received by a mating T-slot 74 in the bottom of trigger 68 whereby the sear and trigger are locked together to prevent relative vertical displacement yet permit the sear to be displaced rearwardly, relative to the trigger, when actuated to the firing pin release position.
  • the rear end of sear 66 is cut away at the upper portion to form a pair of rearwardly projecting lips 76 which are extendable rearwardly under the wall of firing tube 16 to prevent outer displacement of the sear and, consequently, trigger 68 which is locked thereto. Lips 76 are held under the wall of firing tube 16 through the rearward bias of firing pin 62, which is transferred to sear 66 through the contact of the forward one of the collars 63 therewith.
  • An elongated firing button 78 is rotatably mounted on the external end of trigger 68 and such button is arcuately formed to the same diameter as the outside of firing tube 16.
  • button 78 is longitudinally disposed in a safe position as shown in FIG. 2, the ends thereof contact the outside of firing tube 16 to prevent depression of trigger 68 and, when the button is transversely disposed to a fire position, as shown in FIG. 8, it is spaced throughout from the outside of the firing tube so that, when the button is depressed, the trigger is displaced for actuating sear 66 to the firing pin release position.
  • button 78 is straddled by a pair of the corrugations of inner section 22 when the button is in the safe position and the inner section is telescoped thereover.
  • button 78 is protectingly covered and is held against rotation to the fire position until blast deflector 20 is fully extended to the ready-to-fire position.
  • Front cover 26 and rear cover 28 cooperate to form a sighting device 80 when they are swung open 180 on hinges 82 and 84 provided respectively therefor.
  • Hinges 82 and 84 are provided respectively with cooperating springs 86 and 88 which are disposed so as to hold the covers 26 and 28 in either the closed position, wherein the ends of flash deflector 18 are closed thereby, or the open position wherein the covers are positioned to form sighting device 80.
  • Covers 26 and 28 are mounted on flash deflector 18 so that, when disposed in the sighting position thereof,
  • Sighting device 80 includes a rear sight reference reticle 90 inscribed as a circle on rear cover 28 and a first pair of graduated lines 92 and a second pair of graduated lines 94 inscribed on front cover 26 as hereinafter described.
  • Reference reticle 90 is located in rear cover 28 adjacent the perimeter thereof and in an extension of the longitudinal plane intersecting the centers of rear cover 28 and front cover 26 and the pairs of graduated lines 92 and 94 are symmetrical to such plane as shown in FIG. 7.
  • Firearm 12 is adapted for use against tanks and, therefore, lines 92 are graduated so that, when a tank target is broadside and the front and rear ends of the tank touch both of the lines as shown in phantom in FIG. 7, the firearm is correctly elevated for the range.
  • the lines 94 are graduated for finding the range when the front or rear end of a tank is the target.
  • firearm 12 which when collapsed is only 10% inches long, may be easily carried as a sidearm by in fantry troops and it is easily fired by hand, although carrying an anti-tank projectile of artillery capabilities, because of its recoilless operation.
  • Firearm 12 is quickly readied for firing by opening covers 26 and 28 and extending flash deflector l8 and blast deflector 20.
  • blast deflector 20 When blast deflector 20 is fully extended, button 78 is uncovered and released so that it may be rotated from the safe to the fire position. If firearm 12 is not discharged after extension to the ready-to-fire position, it may be made safe by telescoping inner section 22 over firing tube 16 sufficiently to cover and protect button 78 after the button is rotated to the safe position thereof.
  • button 78 When firearm 12 is fired, button 78 is depressed to move sear 66 to the firing pin release position wherein the sear is completely received by opening 58 and thereby firing pin 62 is freedto strike primer 60 with the sear being carried forwardly by the firing pin in such opening.
  • Firearm 12 is sighted on its target by rotating it until rear sight reticle 90 and the graduated lines 92 and 94 are in vertical relationship, as shown in FIG. 7, and then the elevation of the firearm is varied until the tank target is positioned between either the graduated lines 92, if the tank is broadside, or graduated lines 94, if the target is at the front or rear end of the tank.
  • firearm 12 is correctly elevated to lob projectile 14 onto the target.
  • a telescopic firearm including a firing tube for the discharge of a projectile, a blast deflector, a flash deflector for receiving said firing tube and blast deflector when telescoped thereinto, covers mounted by hinges on said flash deflector for closing the ends thereof, and a sight system incorporated in said covers.
  • said blast deflector is composed of a plurality of telescopic sections which are corrugated longitudinally for added strength and to relieve any excessive gas pressure produced therein.
  • said firing tube is provided with a firing mechanism including a trigger extending radially through said firing tube and said blast deflector is provided with longitudinal corrugations which when said blast deflector is partially telescoped on said firing tube straddles said trigger to prevent actuation thereof.
  • said firing tube is provided with a firing mechanism including a trigger extending radially through said firing tube and an actuating button rotatingly mounted on the outside of said trigger, said button being arcuately formed according to the radius of said firing tube so that when said button is disposed longitudinally, respective to said firing tube, said trigger is held against actuation through the contact of the ends of said button with the outside of said firing tube and when said button is rotated so as to be transversely disposed said trigger is freed for actuation, and wherein said blast deflector is provided with longitudinal corrugations disposed so as to straddle said button when longitudinally disposed and said blast deflector is partially telescoped to prevent rotation thereof from the longitudinal position and to guard said button against accidental actuation.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

1. A telescopic firearm including a firing tube for the discharge of a projectile, a blast deflector, a flash deflector for receiving said firing tube and blast deflector when telescoped thereinto, covers mounted by hinges on said flash deflector for closing the ends thereof, and a sight system incorporated in said covers.

Description

United States Patent [191 Rocha Jul 17 1973 TELESCOPING AMMUNITION LAUNCHER 89/4l.6l, 41.62; 33/48; 42/1, 15 [75] Inventor: John G. Rocha, Westfield, Mass.
Primary ExaminerSamuel W. Engle [73] Asslgnee: The United States of America as Atmmey S. J. Rotondi and Dupom represented by the Secretary of the Army, Washington, D.C. EXEMPLARY CLAIM [22] Filed: 1961 l. A telescopic firearm including a firing tube for the [21] Appl. No.: 82,656 discharge of a projectile, a blast deflector, a flash deflector for receiving said firing tube and blast deflector when telescoped thereinto, covers mounted by hinges [52] U.S. Cl 89/1.7, 89/l.705, 8899//ll.88ll67, on Said flash deflector for Closing the ends thereof, and Int Cl F4" 5 a sight system incorporated in said covers. [58] Field of Search 89/1, 1.3, 1.7, 41.6, 8 Claims, 9 Drawing Figures PATENTED Y 3. 745.876
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Jmhn [lRuchtL TELESCOPING AMMUNITION LAUNCHER The invention described herein may be manufac tured and used by or for the Government for governmental purposes without the payment of any royalty thereon.
This invention relates to recoilless firearms and more particularly to recoilless launchers of shells.
It is one object of this invention to provide for infantry troops a supplemental sidearm having artillery capability at pistol weight.
It is another object of this invention to provide such a firearm which may be hand held when fired by being virtually recoilless.
It is a further object of this invention to provide such a firearm which is compact as to size, so that it may be carried as a sidearm, is inexpensive to manufacture, so as to be expendable, and is simple yet positive in design.
It is a still further object of this invention to provide such a firearm which consists of a firing tube and two or more flash and blast deflector sections which may be telescoped into a small size for carrying with the forward flash deflector acting as a casing for the'weapon when telescoped.
It is still another object of this invention to provide such a firearm wherein the flash deflector is closed at the ends by covers which are hinged thereto and which incorporate the sighting device of the weapon.
It is still another object of this invention to provide such a firearm wherein the trigger mechanism is covered by the blast deflector when telescoped over the firing tube.
The specific nature of the invention as well as other objects and advantages thereof will clearly appear from a description of a preferred embodiment as shown in the accompanying drawings in which:
FIG. 1 shows the firearm extended and being aimed at a target;
FIG. 2 is a longitudinally cross-sectioned view of the firearm shown telescoped;
FIG. 3 is a cross-sectional view of the front cover taken through the mounting hinge;
FIG. 4 is a cross-sectioned view of the rear cover taken through the mounting hinge;
FIG. 5 is an exploded perspective view of the firing mechanism;
FIG. 6 is a longitudinally cross-sectioned view of the firearm shown extended;
FIG. 7 is a view taken along line 77 of FIG. 6;
FIG. 8 is a view taken along line 8-8 of FIG. 6; and
FIG. 9 is an enlarged cross-sectioned view of the latch for releasably holding the sections of the firearm extended.
Shown in the figures is a firearm 12 which is adapted for firing a 75mm projectile 14 carrying a warhead 15 and which includes in telescopic arrangement a firing tube 16, a flash deflector 18, and a blast deflector 20 composed of three telescopic sections including an inner section 22. When firearm 12 is fully telescoped, firing tube 16 and blast deflector 20 are nested within flash deflector 18 which acts as a casing therefor and the ends of the flash deflector are respectively closed by a front cover 26 and a rear cover 28 which are hingedly mounted on the flash deflector as hereinafter described. Front cover 26 and rear cover 28 are semielliptical in shape for added strength and are fabricated from transparent plastic material for a reason noted hereinafter. When extended, firearm has a length of about 30 inches and, when telescoped, is approximately 10% inches long.
The front end of firing tube 16 is rolled back over the outside thereof, as noted at 30, to form a bearing surface for slidingly supporting flash deflector 18 so as to be extendable forwardly relative to the firing tube. The rear end of flash deflector 18 is :rolled back inwardly, as noted at 32, so as to be receivable by rolled end 30 of firing tube 16 to limit the extension of the flash deflector relative thereto.
The sections of blast deflector 20 are corrugated longitudinally along the entire lengths hereof for added structural strength so as to be radially expandable to relieve any excessive gas pressure in event the blast defiector should be plugged by dirt. or other obstruction when firearm 12 is discharged. Provided inside of inner section 22 at the front end thereof is a ring 34 the inside diameter of which is the same as the outside diameter of firing tube 16 so as to have sliding contact therewith, and such ring is contactable with a collar 36 provided on the outside of the rear end of the firing tube 16 to limit the rearward displacement of the inner section relative thereto. An external collar 38 and an internal ring 40 are provided respectively on the rear and front ends of each of the sections of blast deflector 20 to limit the extension of the sections and such sections and flash deflector 18 are releasably held extended by spring latches 41 as best shown in FIG. 9.
Firing tube 16 is provided with a combustion chamber 42 in the rear portion and a launching section 44 in the front portion. The rear portion of projectile 14 is received by launching section 44 with warhead 15 extending forwardly therefrom. Flash deflector 18 is sufficiently longer than firing tube 16 to inclose warhead 15 when the flash deflector is telescoped over the firing tube.
A rifled rotating band 45 is provided at the front end of launching section 44 to mate with pre-engraved grooves 46 on the rear portion of projectile 14 for spinning the projectile when propelled from the launching section. Four stabilizing fins 48 are hingedly mounted on the rear end of projectile l4 and such fins are folded up to be received by combustion chamber 42. The spin of projectile 14 by rotating band 45 causes fins 48 to open, according to conventional design, as the projectile leaves firing tube 16. Projectile 14 is propelled into flight by a propellant 49 which is packed in combustion chamber 42 around fins 48 at the rear end of the projectile. Provided in the rear end of firing tube 16 is a venturi 50 which permits the rearward escape of a predetermined amount of the exploded gases therethrough, when propellant 49 is ignited, for counteracting the recoil forces produced in firearm 12 by the ignition. The rear end of firing tube 16 is sealed forwardly of venturi 50 by a rupture disc 52 which holds propellant 49 in combustion chamber 42 and aids ignition of the propellant. Rupture disc 52 is preferably fabricated from plastic material which is completely disintegrated when propellant 49 is ignited, to reduce the hazard of the disc becoming a secondary missile.
Propellant 49 is ignited by a firing mechanism 54 which includes a housing 56 fixed to the inside of combustion chamber 42. Housing 56 is U-shaped in crosssection with an opening 58 therethrough and is longitudinally disposed so as to be straddled by one pair of the fins 48 and so that the rear end of housing 56 is spaced from rupture disc 52. Provided at the rear end of opening 58 is a primer 60 which, when initiated, ignites propellant 49.
Primer 60 is initiated by a firing pin 62 which is slidingly disposed in opening 58 and which is provided with a pair of longitudinally spaced collars 63 which form a channel 64. Firing pin 62 is biased rearwardly for striking primer 60 by a coil spring 65 which is disposed between the rear end of housing 56 and the front one of the collars. Firing pin 62 is releasably held in a cocked position by a scar 66 which is actuatable to release the firing pin by a trigger 68 slidingly received by a radial hole 70 of rectangular cross-section through the wall of firing tube l6. Sear 66 is received between the collars 63 and is provided with alongitudinal recess 71 along the underside to receive the axial section of channel 64. Whereby vertical displacement of sear 66 is permitted between a firing pin holding position wherein the sear is extended upwardly to be partially received by hole 70 and a firing pin release position wherein the sear is entirely received by opening 58.
Provided along the top of sear 66 is a T-flange 72 which is longitudinally disposed and which is received by a mating T-slot 74 in the bottom of trigger 68 whereby the sear and trigger are locked together to prevent relative vertical displacement yet permit the sear to be displaced rearwardly, relative to the trigger, when actuated to the firing pin release position. The rear end of sear 66 is cut away at the upper portion to form a pair of rearwardly projecting lips 76 which are extendable rearwardly under the wall of firing tube 16 to prevent outer displacement of the sear and, consequently, trigger 68 which is locked thereto. Lips 76 are held under the wall of firing tube 16 through the rearward bias of firing pin 62, which is transferred to sear 66 through the contact of the forward one of the collars 63 therewith.
An elongated firing button 78 is rotatably mounted on the external end of trigger 68 and such button is arcuately formed to the same diameter as the outside of firing tube 16. Whereby, when button 78 is longitudinally disposed in a safe position as shown in FIG. 2, the ends thereof contact the outside of firing tube 16 to prevent depression of trigger 68 and, when the button is transversely disposed to a fire position, as shown in FIG. 8, it is spaced throughout from the outside of the firing tube so that, when the button is depressed, the trigger is displaced for actuating sear 66 to the firing pin release position.
Housing 56 and blast deflector are so related that button 78 is straddled by a pair of the corrugations of inner section 22 when the button is in the safe position and the inner section is telescoped thereover. Thus, button 78 is protectingly covered and is held against rotation to the fire position until blast deflector 20 is fully extended to the ready-to-fire position.
Front cover 26 and rear cover 28 cooperate to form a sighting device 80 when they are swung open 180 on hinges 82 and 84 provided respectively therefor. Hinges 82 and 84 are provided respectively with cooperating springs 86 and 88 which are disposed so as to hold the covers 26 and 28 in either the closed position, wherein the ends of flash deflector 18 are closed thereby, or the open position wherein the covers are positioned to form sighting device 80.
Covers 26 and 28 are mounted on flash deflector 18 so that, when disposed in the sighting position thereof,
a plane coincident with the longitudinal axis of the flash deflector and intersecting the center of front cover 26 is right angular to a plane coincident with the longitudinal axis of the flash deflector and intersecting the center of rear cover 28. Whereby, the sighting plane of sighting device intersecting the centers of both the covers 26 and 28 is unobstructed by flash deflector 18 as is clearly shown in FIG. 7.
Sighting device 80 includes a rear sight reference reticle 90 inscribed as a circle on rear cover 28 and a first pair of graduated lines 92 and a second pair of graduated lines 94 inscribed on front cover 26 as hereinafter described. Reference reticle 90 is located in rear cover 28 adjacent the perimeter thereof and in an extension of the longitudinal plane intersecting the centers of rear cover 28 and front cover 26 and the pairs of graduated lines 92 and 94 are symmetrical to such plane as shown in FIG. 7. Firearm 12 is adapted for use against tanks and, therefore, lines 92 are graduated so that, when a tank target is broadside and the front and rear ends of the tank touch both of the lines as shown in phantom in FIG. 7, the firearm is correctly elevated for the range. The lines 94 are graduated for finding the range when the front or rear end of a tank is the target.
Thus, firearm 12, which when collapsed is only 10% inches long, may be easily carried as a sidearm by in fantry troops and it is easily fired by hand, although carrying an anti-tank projectile of artillery capabilities, because of its recoilless operation. Firearm 12 is quickly readied for firing by opening covers 26 and 28 and extending flash deflector l8 and blast deflector 20. When blast deflector 20 is fully extended, button 78 is uncovered and released so that it may be rotated from the safe to the fire position. If firearm 12 is not discharged after extension to the ready-to-fire position, it may be made safe by telescoping inner section 22 over firing tube 16 sufficiently to cover and protect button 78 after the button is rotated to the safe position thereof.
When firearm 12 is fired, button 78 is depressed to move sear 66 to the firing pin release position wherein the sear is completely received by opening 58 and thereby firing pin 62 is freedto strike primer 60 with the sear being carried forwardly by the firing pin in such opening.
Firearm 12 is sighted on its target by rotating it until rear sight reticle 90 and the graduated lines 92 and 94 are in vertical relationship, as shown in FIG. 7, and then the elevation of the firearm is varied until the tank target is positioned between either the graduated lines 92, if the tank is broadside, or graduated lines 94, if the target is at the front or rear end of the tank. Thus, firearm 12 is correctly elevated to lob projectile 14 onto the target. By covers 26 and 28 being fabricated from transparent plastic material, the operator always has visual contact with the target as the sighting members can never obstruct the operator's view.
From the foregoing it is clearly apparent that there is provided herein an effective firearm which has artillery capabilities but which may be carried as a sidearm by its compact construction wherein the covers act as the sighting elements and the telescopic parts provides a safety for the trigger.
Although a particular embodiment of the invention has been described in detail herein, it is evident that many variations may be devised within the spirit and scope thereof and the following claims are intended to include such variations.
I claim:
1. A telescopic firearm including a firing tube for the discharge of a projectile, a blast deflector, a flash deflector for receiving said firing tube and blast deflector when telescoped thereinto, covers mounted by hinges on said flash deflector for closing the ends thereof, and a sight system incorporated in said covers.
2. The firearm as defined in claim 1 wherein said blast deflector is composed of a plurality of telescopic sections which are corrugated longitudinally for added strength and to relieve any excessive gas pressure produced therein.
3. The firearm as defined in claim 1 wherein said firing tube is provided with a firing mechanism including a trigger extending radially through said firing tube and said blast deflector is provided with longitudinal corrugations which when said blast deflector is partially telescoped on said firing tube straddles said trigger to prevent actuation thereof.
4. The firearm as defined in claim 1 wherein said firing tube is provided with a firing mechanism including a trigger extending radially through said firing tube and an actuating button rotatingly mounted on the outside of said trigger, said button being arcuately formed according to the radius of said firing tube so that when said button is disposed longitudinally, respective to said firing tube, said trigger is held against actuation through the contact of the ends of said button with the outside of said firing tube and when said button is rotated so as to be transversely disposed said trigger is freed for actuation, and wherein said blast deflector is provided with longitudinal corrugations disposed so as to straddle said button when longitudinally disposed and said blast deflector is partially telescoped to prevent rotation thereof from the longitudinal position and to guard said button against accidental actuation.
5. The firearm as defined in claim I wherein said sight system is established when said front and rear covers are swung open 180.
6. The firearm as defined in claim 1 wherein said front and rear covers are fabricaed from transparent material and said sight system includes a circlar reicle inscribed in said rear cover and pairs of graduated lines inscribed in said front cover, said graduated lines being arranged to indicate the elevation of the firearm according to the distance of a target relative thereto.
7. The firearm as defined in claim 1 wherein said hinges are mounted on said flash deflector apart and said hinges permit pivotal displacement of said front and rear covers to an open position for establishing said sight system 8. The firearm as defined in claim 7 wherein a circular reticle is inscribed on said rear cover adjacent the perimeter thereof and pairs of graduated lines are inscribed on said front cover to indicate the elevation of the firearm according to the distance of a target therefrom and wherein said reticle is located in a geometric plane passing through the longitudinal axis of said front and rear sights and said graduated lines are disposedsymmetrically to such geometric plane.

Claims (8)

1. A telescopic firearm including a firing tube for the discharge of a projectile, a blast deflector, a flash deflector for receiving said firing tube and blast deflector when telescoped thereinto, covers mounted by hinges on said flash deflector for closing the ends thereof, and a sight system incorporated in said covers.
2. The firearm as defined in claim 1 wherein said blast deflector is composed of a plurality of telescopic sections which are corrugated longitudinally for added strength and to relieve any excessive gas pressure produced therein.
3. The firearm as defined in claim 1 wherein said firing tube is provided with a firing mechanism including a trigger extending radially through said firing tube and said blast deflector is provided with longitudinal corrugations which when said blast deflector is partially telescoped on said firing tube straddles said trigger to prevent actuation thereof.
4. The firearm as defined in claim 1 wherein said firing tube is provided with a firing mechanism including a trigger extending radially through said firing tube and an actuating button rotatingly mounted on the outside of said trigger, said button being arcuately formed according to the radius of said firing tube so that when said button is disposed longitudinally, respective to said firing tube, said trigger is held against actuation through the contact of the ends of said button with the outside of said firing tube and when said button is rotated so as to be transversely disposed said trigger is freed for actuation, and wherein said blast deflector is provided with longitudinal corrugations disposed so as to straddle said button when longitudinally disposed and said blast deflector is partially telescoped to prevent rotation thereof from the longitudinal position and to guard said button against accidental actuation.
5. The firearm as defined in claim 1 wherein said sight system is established when said front and rear covers are swung open 180* .
6. The firearm as defined in claim 1 wherein said front and rear covers are fabricaed from transparent material and said sight system includes a circlar reicle inscribed in said rear cover and pairs of graduated lines inscribed in said front cover, said graduated lines being arranged to indicate the elevation of the firearm according to the distance of a target relative thereto.
7. The firearm as defined in claim 1 wherein said hinges are mounted on said flash deflector 90* apart and said hinges permit pivotal displacement of said front and rear covers 180* to an open position for establishing said sight system.
8. The firearm as defined in claim 7 wherein a circular reticle is inscribed on said rear cover adjacent the perimeter thereof and pairs of graduated lines are inscribed on said front cover to indicate the elevation of the firearm according to the distance of a target therefrom and wherein said reticle is located in a geometric plane passing through the longitudinal axis of said front and rear sights and said graduated lines are disposed symmetrically to such geometric plane.
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Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3946638A (en) * 1974-03-29 1976-03-30 The United States Of America As Represented By The Secretary Of The Army Low recoil anti-tank rocket launcher
US3961556A (en) * 1974-10-03 1976-06-08 The United States Of America As Represented By The Secretary Of The Army Rocket launcher telescoping tube locking mechanism
US4141275A (en) * 1977-07-14 1979-02-27 The United States Of America As Represented By The Secretary Of The Navy Afterburner recoilless rifle
US4153282A (en) * 1977-05-05 1979-05-08 The United States Of America As Represented By The Secretary Of The Army Coned joint for joining dissimilar diameter filament wound tubes
US4203347A (en) * 1978-04-10 1980-05-20 The Boeing Company Shock suppressing apparatus and method for a rocket launcher
EP0077482A1 (en) * 1981-10-20 1983-04-27 The Boeing Company Noise, flash and smoke suppressor apparatus and method for rocket launcher
EP0145696A1 (en) * 1983-08-16 1985-06-19 Vereinigte Edelstahlwerke Aktiengesellschaft (Vew) Projectile weapon, particularly an armour piercing weapon
US4531445A (en) * 1983-11-07 1985-07-30 N.I. Industries, Inc. Projectile launcher
US4970937A (en) * 1988-05-20 1990-11-20 British Aerospace Public Limited Company Anti-ice protection for projectiles
US5109750A (en) * 1990-06-13 1992-05-05 George Kayaian Closed-breech missile and weapon system
US5398588A (en) * 1993-02-16 1995-03-21 Hughes Aircraft Company Missile system with telescoping launch tube
US7013788B1 (en) * 2003-07-24 2006-03-21 The United States Of America Represented By The Secretary Of The Navy Launch tube with adjustable plenum
US20140224105A1 (en) * 2011-08-04 2014-08-14 James Y. Menefee, III Recoil attenuated payload launcher system
US8967046B2 (en) 2012-11-30 2015-03-03 Alliant Techsystems Inc. Gas generators, launch tubes including gas generators and related systems and methods
US10281248B2 (en) 2015-11-11 2019-05-07 Northrop Grumman Innovation Systems, Inc. Gas generators, launch tube assemblies including gas generators, and related systems and methods
CN110530204A (en) * 2019-07-17 2019-12-03 北京玻钢院复合材料有限公司 Entirety breaks through the directional separation part and directional separation structure of formula firing box sealing cover
US11473861B2 (en) * 2018-05-08 2022-10-18 Zsolt HEGYESHALMI Recoilless, slideless repeating magazine-fed weapon
US11959711B1 (en) * 2021-10-15 2024-04-16 The United States Of America As Represented By The Secretary Of The Army Recoilless gun and ammunition

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3946638A (en) * 1974-03-29 1976-03-30 The United States Of America As Represented By The Secretary Of The Army Low recoil anti-tank rocket launcher
US3961556A (en) * 1974-10-03 1976-06-08 The United States Of America As Represented By The Secretary Of The Army Rocket launcher telescoping tube locking mechanism
US4153282A (en) * 1977-05-05 1979-05-08 The United States Of America As Represented By The Secretary Of The Army Coned joint for joining dissimilar diameter filament wound tubes
US4141275A (en) * 1977-07-14 1979-02-27 The United States Of America As Represented By The Secretary Of The Navy Afterburner recoilless rifle
US4203347A (en) * 1978-04-10 1980-05-20 The Boeing Company Shock suppressing apparatus and method for a rocket launcher
EP0077482A1 (en) * 1981-10-20 1983-04-27 The Boeing Company Noise, flash and smoke suppressor apparatus and method for rocket launcher
EP0145696A1 (en) * 1983-08-16 1985-06-19 Vereinigte Edelstahlwerke Aktiengesellschaft (Vew) Projectile weapon, particularly an armour piercing weapon
US4531445A (en) * 1983-11-07 1985-07-30 N.I. Industries, Inc. Projectile launcher
US4970937A (en) * 1988-05-20 1990-11-20 British Aerospace Public Limited Company Anti-ice protection for projectiles
US5109750A (en) * 1990-06-13 1992-05-05 George Kayaian Closed-breech missile and weapon system
US5398588A (en) * 1993-02-16 1995-03-21 Hughes Aircraft Company Missile system with telescoping launch tube
US7013788B1 (en) * 2003-07-24 2006-03-21 The United States Of America Represented By The Secretary Of The Navy Launch tube with adjustable plenum
US20140224105A1 (en) * 2011-08-04 2014-08-14 James Y. Menefee, III Recoil attenuated payload launcher system
US8807004B1 (en) * 2011-08-04 2014-08-19 James Y. Menefee, III Recoil attenuated payload launcher system
US8967046B2 (en) 2012-11-30 2015-03-03 Alliant Techsystems Inc. Gas generators, launch tubes including gas generators and related systems and methods
US9605932B2 (en) 2012-11-30 2017-03-28 Orbital Atk, Inc. Gas generators, launch tubes including gas generators and related systems and methods
US10281248B2 (en) 2015-11-11 2019-05-07 Northrop Grumman Innovation Systems, Inc. Gas generators, launch tube assemblies including gas generators, and related systems and methods
US11473861B2 (en) * 2018-05-08 2022-10-18 Zsolt HEGYESHALMI Recoilless, slideless repeating magazine-fed weapon
CN110530204A (en) * 2019-07-17 2019-12-03 北京玻钢院复合材料有限公司 Entirety breaks through the directional separation part and directional separation structure of formula firing box sealing cover
US11959711B1 (en) * 2021-10-15 2024-04-16 The United States Of America As Represented By The Secretary Of The Army Recoilless gun and ammunition

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