US3915058A - Single barrel gun with a rotary operating mechanism - Google Patents

Single barrel gun with a rotary operating mechanism Download PDF

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Publication number
US3915058A
US3915058A US403121A US40312173A US3915058A US 3915058 A US3915058 A US 3915058A US 403121 A US403121 A US 403121A US 40312173 A US40312173 A US 40312173A US 3915058 A US3915058 A US 3915058A
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United States
Prior art keywords
gun
rotation
housing
aft
longitudinal axis
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.)
Expired - Lifetime
Application number
US403121A
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English (en)
Inventor
Lawrence R Folsom
Victor R Gardy
August J Haberstroh
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General Electric Co
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General Electric Co
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 General Electric Co filed Critical General Electric Co
Priority to US403121A priority Critical patent/US3915058A/en
Priority to IL45686A priority patent/IL45686A/xx
Priority to DE2446145A priority patent/DE2446145C2/de
Priority to DE19747432482U priority patent/DE7432482U/de
Priority to IT27877/74A priority patent/IT1022447B/it
Priority to CH1320174A priority patent/CH600286A5/xx
Priority to BE149139A priority patent/BE820620A/xx
Priority to NO743571A priority patent/NO142971C/no
Priority to FR7433227A priority patent/FR2246836B1/fr
Priority to ES430619A priority patent/ES430619A1/es
Priority to JP49113364A priority patent/JPS6237320B2/ja
Priority to SE7412493A priority patent/SE400639B/xx
Priority to NLAANVRAGE7413094,A priority patent/NL174984C/xx
Priority to GB43000/74A priority patent/GB1493376A/en
Priority to US05/533,188 priority patent/US3955300A/en
Application granted granted Critical
Publication of US3915058A publication Critical patent/US3915058A/en
Priority to US05/924,783 priority patent/US4328737A/en
Priority to US06/032,587 priority patent/US4257310A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A5/00—Mechanisms or systems operated by propellant charge energy for automatically opening the lock
    • F41A5/02—Mechanisms or systems operated by propellant charge energy for automatically opening the lock recoil-operated
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A9/00—Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
    • F41A9/29—Feeding of belted ammunition
    • F41A9/30—Sprocket-type belt transporters
    • F41A9/31—Sprocket-type belt transporters with cartridge stripping means

Definitions

  • This invention relates to operating mechanisms for single barrel guns, particularly to a rotary operating mechanism which may be recoil driven.
  • the feeder of such a gun is operated intermittently, and is driven only during a short period of the gun cycle, thereby putting high peak loads on the ammunition supply.
  • An externally powered rotary operating mechanism is shown by R. J. Gatling in U.S. Pat. No. 125,563 issued Apr. 9, 1877. More modern, conventional rotary operating mechanism are shown, for example, by H. McC. Otto in U.S. Pat. No. 2,849,921 issued Sept. 2, 1958; R. E. Chiabrandy in U.S. Pat. No. 3,407,701 issued Oct. 29, 1968; and R. E. Chiabrandy et al. in U.S. Pat. No. 3,380,343 issued Apr. 30, 1968.
  • a gas powered rotary operating mechanism is shown by R. F. Hudson in U.S. Pat. No. 1,786,207 issued Dec. 23, 1930.
  • a recoil operated feeder is shown in The Machine Gun by G. M. Chinn, Vol. IV, page 245, Department of the Navy, 1955.
  • a feature of this invention is the provision of a gun having a single barrel and a rotary operating mechanism which is symmetrical about the longitudinal axis of the gun barrel.
  • FIG. 1 is a longitudinal view in cross-section of a gun embodying this invention; taken along a plane through the gun barrel longitudinal axis;
  • FIG. 2 is a curve showing the relative displacements of the gun barrel and the gun bolt with respect to the cam angle of the rotary operator of the embodiment of FIG. 1;
  • FIG. 3 is a transverse view in cross-section of the embodiment of FIG. 1, taken along plane llI-III, looking aft, particularly showing the gun bolt;
  • FIG. 4 is a transverse view in cross-section of the embodiment of FIG. 1, taken along plane IVIV, looking forward, particularly showing the chamber;
  • FIG. 5 is a transverse view in cross-section of the embodiment of FIG. 1, taken along plane V-V of FIG. 6, rotated looking aft, particularly showing the bolt retracted, and the feeder mechanism;
  • FIG. 6 is a plan detail view of a portion of the embodiment of FIG. 1, taken along plane VI-VI particularly showing the feeder mechanism;
  • FIG. 7 is a transverse view in cross-section of the embodiment of FIG. 1, taken along plane VIIVII, particularly showing the gear train of the feeder mechanism;
  • FIG. 8 is a longitudinal view in cross-section of the gun bolt of FIG. 1, taken along a plane through the gun barrel longitudinal axis, particularly showing the firing pin mechanism;
  • FIG. 9 is a transverse view in cross-section of the embodiment of FIG. 1, taken along a plane IXIX, looking aft, particularly showing the sear;
  • FIGS. 10A and 10B are longitudinal and transverse views respectively of a modified embodiment of the head of the gun bolt in the locked position.
  • FIGS. 11A and 11B are longitudinal and transverse views respectively of the embodiment of FIG. 10A in the unlocked position.
  • FIG. 1 The embodiment of the invention shown in FIG. 1 comprises a single barrel, recoil driven, rotary operated machine gun.
  • the gun comprises a main housing 10 of substantially tubular shape, to which is fixed a forward housing 12 which is also of tubular shape.
  • the aft end of the forward housing includes an annular ring 14 providing an inner annulus l6, and outer annulus l8, and an aft annulus 20.
  • a back plate 22 is fixed to the aft end of the housing 10.
  • An aft rotor 24 of generally tubular shape is jour nalled for rotation about the gun longitudinal axis within the housing 10 by a forward radial bearing 26 and by a pair of aft thrust bearings 28 held by a bearing retainer ring 30.
  • a forward rotor 32 of generally tubular shape is journalled for rotation about the gun longitudinal axis within the housings 10 by a pair of forward thrust bearings 34 held by a retainer ring 36, and by an aft radial bearing 38 held by a retainer ring 40.
  • a connecting shaft 42 is joumalled, for rotation parallel to the gun longitudinal axis, to the housing 10 by a forward radial bearing 44 and an aft radial bearing 46.
  • the shaft includes a forward gear annulus 48 meshed with a gear annulus 50 on the forward rotor 32 and an aft gear annulus S2 meshed with a 32, annulus 54 on the aft rotor.
  • the shaft thus couples the front and rear rotors for concurrent rotation, and as will be described later, drives a feeder system and serves as a torsion-spring self starter.
  • a barrel extension is disposed within the housing 10 and is journalled for reciprocation by slides riding in tracks 64 in the housing.
  • the barrel extension includes a forward bore 66 for receiving the gun barrel 68 and an aft bore 70 for receiving the head 72 of the gun bolt 74.
  • the aft end 76 of the gun barrel is secured to the forward bore 66 by means of a plurality of interrupted threads 78. Alternatively, lugs and a latch may be utilized.
  • the forward portion 80 of the gun barrel extends into the forward housing 12.
  • An annular spring stop 82 is fixed to the forward end of the gun barrel.
  • a barrel return spring 84 is disposed about the forward end of the gun barrel and spaced therefrom by a sleeve 86, within the forward housing 12, between the spring stop 82 and the inner annulus 16.
  • a trunnion ring 88 is disposed on the forward housing 12 and journalled for reciprocation thereon in suitable tracks, not shown, and restrained by suitable buffer springs 90 fore and aft of the ring which are constrained between the outer annulus 18 and a lock ring 91 fixed forwardly on the forward housing.
  • the forward rotor 32 has two diametrically opposed cam rollers 92 and 94, which respectively ride in two overlapping helical cam tracks 96 and 98 in the barrel extension 60.
  • An annular cam track 100 overlaps the two helical tracks.
  • the gun bolt 74 includes the gun bolt head 72, and a substantially tubular body 102 terminating in an aft guide disc 104.
  • the aft guide disc slides within the bore 106 of the aft rotor 24.
  • the tubular body has a pair of slides 107 riding in the tracks 64, a transverse web 108, with a longitudinal bore 1 10, separating a forward bore 112 from an aft bore 114.
  • the head 72 has a forward portion 116 having a plurality of radially projecting locking lugs 118, a bolt face 120, a pair of diametrically spaced apart extractor lugs 122, and an aft portion 124 disposed within the bore 112 having a longitudinal aft bore 126, a longitudinal foward stepped bore 128 and a transverse slot 130.
  • a disc 132 is disposed in the bore 114 and has a stern 134 passing through the bore into the bore 126 of the head.
  • a pin 136 passes through transverse bores in the stem and body and through a slot in the head to fix these parts together while permitting some relative rotation of the head to the body.
  • a firing pin 138 is disposed in the bore 128 and has a transverse actuating arm 140 fixed thereto and passing outwardly through the slot 130 and a slot 142 in the body 114.
  • a helical firing pin spring 144 is disposed in the bore 126 and captured between the stem 134 and the firing pin 138.
  • a quasi-helical cam track 146 is provided on the external aft surface of the body 102.
  • a quasi-helical cam track 148 is provided at the external surface of the aft rotor 24 for its aft and forward dwell portions by a side wall 150 of a rib 152 and a side wall 151 respectively formed on the rotor and for the remainder portion by an aft side wall 153 and a side wall 154 of an insert 156 fixed to the inner wall of the housing.
  • a longitudinal slot 158 is provided in the wall of the aft rotor with longitudinal tracks 160.
  • a slide 162 is disposed in the slot with rails 164 guided by the tracks. The slide 162 has an aft cam follower roller 166 engaged in the aft rotor cam track 148, and a forward cam driver roller 168 engaged in the gun bolt cam track 146.
  • a recess 170 is provided in the external surface of the aft rotor and has a shoulder 172.
  • a solenoid 174 is fixed to the housing and has an armature 176 which is coupled through a slot to a dog 178 which is pivotally 5 mounted to the interior wall of the housing and is biased towards the rotor by a helical compression spring 180.
  • the dog may be provided as a toggle to reduce the force required of the solenoid.
  • the gun barrel 68 includes the rifled bore 182 and the chamber 184.
  • the barrel extension includes a cavity 186 adapted to receive the bolt head forward portion 116, and a plurality of grooves 188 to pass the locking lugs 118.
  • a post 190 has its aft end fixed to the back plate 22.
  • a helical bolt return spring 192 is disposed over the post 190 and into the bore 114 of the gun bolt, and is captured between the back plate 22 and the disc 132. In the battery, unlocked, disposition of the bolt head, the firing pin actuator arm abuts the aft face 194 of an inwardly directed projection 196 on the housing which serves as a sear, and the firing pin spring is compressed.
  • the gun bolt also has a pair of slides 107 extending from the body 102, which also ride in the tracks 64, and an actuating arm 200 extending transversely from the bolt head forward portion 1 16.
  • the actuating arm 200 has a cam following surface 202 which when in the battery unlocked disposition, as seen in FIG. 3, is acted upon by a counter-clockwise rotating cam 204 which is fixed on a shaft 206 and which rotates one revolution per gun cycle at a nonuniform velocity to swing the arm 200 clockwise into lock.
  • the arm 200 has an additional cam following surface 208 which when in the battery-locked disposition and traveling aft in recoil, is acted upon by a ramp surface 210 on a projection fixed to the housing to swing the arm 200 counter-clockwise into unlock.
  • the cam tracks 96/98, I46 and 148 do not have uniform pitch angles. To preclude the possibility of a cam roller and a cam track blocking rather than driving, the pitch angle of the cam track should be kept below 5 I", and preferably 45. Given a large enough aft rotor diameter, the pitch angle of the track 146 could be 0, i.e., a simple annulus. However, with a small diameter aft rotor, to keep down the pitch angle of the track 148, the track 146 is provided with a significant pitch angle. The effective pitch angle of the combination of the tracks 146 and 148 must then be considered with respect to the track 96/98.
  • the effective pitch angle of the combination of the tracks 146 and 148 must be identical to the pitch angle of the track 96/98. After the gun bolt is unlocked, the effective pitch angle of the combination of the tracks 146 and 148 is made relatively greater than the pitch angle of the track 96/98 to provide for an aftward movement of the gun bolt which is more rapid than the aftward movement of the barrel extension, i.e., acceleration of the gun bolt relative to the barrel extension.
  • the gun mechanism as so far described operates as follows: The gun is in battery with a round R1 locked in the chamber as shown in FIG. 1, and the solenoid 174 is energized. As the cam 204 drives the bolt head into its fully locked position, the firing pin actuator arm 140 rides off the sear surface 194 and the spring 144 drives the firing pin 138 to fire the round. The explosion causes the barrel 68 and the barrel extension 60 with the locked thereto gun bolt 74 to recoil aft. As the gun bolt 74 moves aft the cam surface 208 rides up the ramp surface 210, unlocking the bolt head.
  • the cam tracks 96 and 98 drive the cam follower rollers 92 and 94 respectively to rotate the forward rotor 32 and its gear annulus 50.
  • the annulus 50 drives the connecting shaft gear annulus 48, which through the shaft 42 rotates the shaft gear annulus S2, and thereby, the gear annulus 54 and the aft rotor 24.
  • the stationary cam track 148 drives the cam follower roller 166 aft, and thereby, the slide 162 and the cam driver roller 168.
  • the roller 168 drives the gun bolt cam track 146 aft, together with the gun bolt.
  • the slide 162 accelerates the aft movement of the gun bolt with respect to the barrel extension, as shown in FIG. 2.
  • the barrel return spring returns the barrel to battery before 180.
  • the fired cartridge case is transversely ejected. If another round is to be fired, as the rotors rotate through the gun bolt aft dwell which straddles 180, while the fired cartridge case is transversely ejected, a fresh cartridge is transversely injected.
  • the gun bolt return spring 192 drives the bolt forward with the fresh cartridge, to insert the bolt head 72 into the aft bore 70 and to chamber the cartridge.
  • the arm 140 abuts the surface 194 compressing the firing pin.
  • the shaft 206 rotates to swing the cam 204 to swing the arm 200 to rotate the bolt head into lock.
  • the solenoid 174 is de-energized so that the spring 180 biases the dog 178 to catch the shoulder 172 to halt rotation of the aft rotor.
  • the forward rotor which is coupled to the aft rotor by the connecting shaft 42 continues to rotate but decelerates responsive to its inertia and the torsional strength of the connecting shaft 42, with the barrel extension in battery.
  • the wedging angle of the cam tracks 96 and 98 is such as to prevent reverse movement of the rollers 92 and 94 respectively and reverse rotation of the forward rotor.
  • the system is thus halted in a charged condition with the connecting shaft in torsional strain.
  • Subsequent energization of the solenoid 174 results in an untwisting of the connecting shaft which accelerates the aft rotor, to permit the gun bolt return spring to drive the gun bolt into chamber and be locked.
  • the forward rotor is rotated by an external source of power, while the rollers 92 and 94 travel in the annular cam track 100.
  • the feeder injects one round of ammunition between the extractor lugs of the bolt during rear dwell of the gun bolt and ejects the previously fired case.
  • the feeder is driven by the connecting shaft 42 which is driven by the forward rotor 32.
  • the connecting shaft 42 has a first intermediate gear 201 and a second intermediate sun gear 202.
  • the gear 202 is meshed with a pair of planetary gears 204 which are respectively journalled on a spider 206 and are respectively meshed with a stationary annular gear 208.
  • the spider 206 has an annular sun gear 210 which is meshed with a pair of planetary gears 212 which are respectively joumalled on a spider 214 and are respectively meshed with the stationary annular gear 208.
  • This planetary system provides a l6:l reduction.
  • the spider 214 is integral with a tubular shaft 216 which is coaxial with the connecting shaft 42.
  • a forward stripper sprocket 218 and an aft stripper sprocket 220 are fixed to the shaft 216.
  • the stripper sprockets engage the leading round R2 in a train of linked ammunition, and draws the train past a link positioner 222, forward outer link guides 224, and 224A, aft outer link guides 226, and 226A, a forward stripper guide 228, and an aft stripper guide 230 to strip and eject each link seriation from the respective rounds of ammunition.
  • the stripper sprockets each have four cusps and, rotate at a substantially uniform velocity, one-fourth the rate of the g
  • the gear 201 is meshed with a reduction gear 232, which is fixed for rotation with an elliptical gear 234, which is meshed with an elliptical gear 236, which is fixed for rotation with an idler gear 238, which is meshed with a gear 240 which is fixed to the injector shaft 206.
  • the injector shaft thus rotates at a sinusoidal velocity once per gun cycle.
  • the shaft 206 as previously mentioned carries the cam 204.
  • the shaft 206 has fixed thereto a forward injector sprocket 242 and an aft injector sprocket 244.
  • the gear 201 is also meshed with an idler gear 246, which is meshed with a gear 248 which is fixed for rotation with an elliptical gear 250, which is meshed with an elliptical gear 252, which is fixed for rotation with a gear 254, which is meshed with a gear 256 which is fixed to an ejector shaft 258.
  • the shaft 258 has fixed thereto a forward retarder-ejector sprocket 260 and an aft retarder-ejector sprocket 262.
  • the stripper sprockets rotate counterclockwise at a substantially uniform velocity to continually pull the train of ammunition at a substantially uniform velocity into the feeder and to strip and eject the leading link.
  • the stripped round is guided on the inner surfaces of the stripper guides 228 and 230, and continuations thereof.
  • the stripper sprockets hand the round off into the cups of the now at substantial dwell injector sprockets 242 and 244 and the round is retained there by the distal ends of the now at substantial dwell retarder-ejector sprockets 260 and 262.
  • the retarder-ejector sprockets rotate counter-clockwise to sweep the fired case laterally across the bolt face out from the extractor lugs 122 and along eject guideways 264 and 266.
  • the injector sprockets rotate clockwise to advance the fresh round along the injector guideway continuations to and across the bolt face and into the extractor lugs 122, and then continue to rotate full cycle to receive the next hand off from the stripper sprockets.
  • the round is prevented from tilting on the bolt face by the trailing edge of the retarder-ejector sprockets, and as the bolt comes forward, these sprockets continue to rotate out of the way and to rotate full cycle to halt the next handed off round in the injector sprockets.
  • sequence of events of the gun cycle may be tabulated as follows:
  • ALTERNATIVE EMBODIMENT The invention may be embodied in an externally powered configuration. Conventionally, externally powered configurations have the advantage of continuing to cycle notwithstanding one or more misfires.
  • a rotating source of power 400 may be conveniently coupled to the gear annulus 50 of the forward rotor 32.
  • the pitch angle of the cam tracks 96 and 98 are selected to permit the cam rollers on the forward rotor to reciprocate the barrel extension.
  • the speed of the rotating source of power is selected to drive the gun at a rate which is within the natural, recoil operated, rate of the gun.
  • FIGS. 10A, 10B, 11A, and 113 may be incorporated into the gun bolt.
  • Two longitudinally extending diametrically spaced apart slots 300 and 302 are provided in the head 72, and two 2 shaped cam slots 304 and 306 are provided in the tubular body 102 which receive respective cam follower pins 308 anad 310, which are fixed to respective slides 312 and 314, which are respectively disposed in the slots 304 and 306.
  • the locked position of the head on the body shown in FIGS. 10A and 103, the slides are retracted within the bolt head.
  • the unlocked position shown in FIGS.
  • the distal ends of the slides project forwardly from the bolt face.
  • the slide 314 is slightly longer than the slide 312.
  • additional cam not shown, similar to the cam 204, is fixed to the shaft 206 adjacent the counter-battery position of the bolt head and serves to deflect the arm 200 to swing the bolt head into the locked orientation when the gun bolt is aft, prior to the injection of a fresh round to the face of the bolt.
  • the injector sprockets 242 and 244 then feed a round across the end of the now retracted slide 312 to the center of the bolt face, between the extractor lugs, while the previously fired cartridge case is ejected.
  • An additional ramp surface is provided slightly forward of the counter-battery position of the bolt head and serves to deflect the arm 200 as the bolt counter-recoils forwardly to swing the bolt head into the unlocked orientation, projecting the ends of the slides from the bolt face.
  • the end of the slide 314 emerges first to positively halt transverse travel of the round along the face of the bolt as the ejector sprockets 260 and 262 swing away from the round.
  • the slides are again retracted. After firing, during recoil, when the bolt is unlocked from the barrel extension the slides are again projected, capturing the fired cartridge case to the bolt face during recoil of the bolt to its counter-battery position.
  • a gun comprising:
  • a single gun barrel having a longitudinal axis, disposed within said housing and journalled for reciprocation along said longitudinal axis with respect to said housing;
  • an operating mechanism for said gun bolt journalled for rotation about said longitudinal axis said operating mechanism comprising tubular means journalled for rotation within said housing about said longitudinal axis, first coupling means interengaging said gun barrel and said tubular means whereby rectilinear aftward movement of said gun barrel causes rotation of said tubular means, and second coupling means interengaging said gun bolt and said tubular means whereby said rotation of said tubular means provides rectilinear aftward movement of said gun bolt which is accelerated with respect to the movement of said gun barrel, said first coupling means comprising a first quasi-helical cam track fixed to one of a first group consisting of said gun barrel and said tubular means, and a first cam roller fixed to the other of said group and interengaged with said first cam track, and said second coupling means comprises a second quasi-helical cam track fixed to said tubular means, a third cam track fixed to said gun bolt, and a slide, journalled for longitudinal reciprocation, having a second cam roller interengaged with said second cam track and
  • a gun comprising: a housing; a single gun barrel, having a longitudinal axis, disposed within said housing, and joumalled for reciprocation along said longitudinal axis with respect to said housing; a single gun bolt disposed within said housing and joumalled for reciprocation along said longitudinal axis; and an operating mechanism for said gun bolt joumalled for rotation about said longitudinal axis; said operating mechanism comprising tubular means joumalled for rotation within said housing about said longitudinal axis,
  • first coupling means interengaging said gun barrel and said tubular means whereby rectilinear aftward movement of said gun barrel causes rotation of said tubular means
  • second coupling means interengaging said gun bolt and said tubular means whereby said rotation of said tubular means provides rectilinear aftward movement of said gun bolt which is accelerated with respect to the movement of said gun barrel
  • said tubular means comprising a forward tubular means, engaged by said first coupling means
  • detent means for halting rotation of said aft tubular means
  • said first coupling means permitting rotation in a first direction and precluding rotation in a second direction, opposite to said first direction, of said forward tubular means when said detent means is effective to halt rotation of said aft tubular means whereby said forward tubular means decelerates, torsionally straining said shaft means.
  • a gun according to claim 3 further including:
  • a gun bolt return spring which is compressed by aftward movement of said gun bolt during an initial portion of the cycle of said gun, and which provides forward movement of said gun bolt during a subsequent portion of said cycle of said gun.
  • a gun comprising:
  • a single gun barrel having a longitudinal axis, disposed within said housing, and joumalled for reciprocation along said longitudinal axis with respect to said housing;
  • a single gun bolt disposed within said housing and joumalled for reciprocation along said longitudinal axis;
  • said operating mechanism comprising tubular means joumalled for rotation within said housing about said longitudinal axis
  • first coupling means interengaging said gun barrel and said tubular means whereby rectilinear aftward movement of said gun barrel causes rotation of said tubular means
  • tubular means comprising a forward tubular means, engaged by said first coupling means
  • detent means for halting rotation of said aft tubular means
  • said first coupling means permitting rotation in a first direction and precluding rotation in a second direction, opposite to said first direction, of said forward tubular means when said detent means is effective to halt rotation of said aft tubular means, whereby said forward tubular means decelerates, storing energy in said power transmission means.
  • a gun comprising:
  • a gun barrel having a longitudinal axis, disposed within said housing, and joumalled for reciprocation along said longitudinal axis with respect to said housing;
  • a gun bolt disposed within said housing and journalled for reciprocation along said longitudinal axis;
  • an operating mechanism comprising first means joumalled for rotation within said housing,
  • first coupling means interengaging said gun barrel and said first means whereby rectilinear aftward movement of said gun barrel causes rotation of said first means
  • second coupling means interengaging said gun bolt and said first means whereby said rotation of said first means provides rectilinear aftward movement of said gun bolt which is accelerated with respect to the movement of said gun barrel
  • said first means comprising a forward rotating means, engaged by said first coupling means
  • stop means for halting rotation of said aft rotating means
  • said first coupling means permitting rotation in a first direction and precluding rotation in a second direction, opposite to said first direction, of said forward rotating means when said stop means is effective to halt rotation of said aft rotating means, whereby said forward rotating means decelerates, storing energy in said power transmission means.
  • a gun comprisig:
  • a gun barrel having a longitudinal axis, disposed within said housing, and journalled for reciprocation along said longitudinal axis with respect to said housing;
  • a gun bolt disposed within said housing and journalled for reciprocation along said longitudinal axis;
  • an operating mechanism comprising first means journalled for rotation within said housing, first coupling means interengaging said gun barrel and said first means whereby rectilinear al'tward movement of said gun barrel causes rotation of said first means, said first means comprising a forward rotating means, engaged by said first coupling means, an aft rotating means, and power transmission means driven by said forward rotating means and driving said aft rotating means, and stop means for halting rotation of said aft rotating means, said first coupling means permitting rotation in a first direction and precluding rotation in a sec-.
  • a gun comprising: a housing; a gun barrel, having a longitudinal axis, disposed within said housing, and journalled for reciprocation along said longitudinal axis with respect to said housing; a gun bolt disposed within said housing and journalled for reciprocation along said longitudinal axis; an operating mechanism for said gun bolt comprising a forward tubular means journalled for rotation about said longitudinal axis,
  • first coupling means interengaging said gun barrel and said forward tubular means, so that rectilinear aftward movement of said gun barrel causes rotation of said aft tubular means
  • said first coupling means comprises a fist quasi-helical cam track fixed to one of a first group consisting of said gun barrel and said tubular means, and
  • a gun firing a round of ammunition comprising: a housing; a gun barrel, having a longitudinal axis, disposed within said housing, and journaled for reciprocation along said longitudinal axis with respect to said housing; a gun bolt disposed within said housing and journaled for reciprocation along said longitudinal axis; an operating mechanism for said gun bolt comprising a forward rotating means journaled for rotation about said gun barrel longitudinal axis,
  • an aft rotating means spaced from said forward rotating means by at least the length of a round of ammunition and journaled for rotation about said gun barrel longitudinal axis,
  • first coupling means interengaging said gun barrel and said forward rotating means so that rectilinear aftward movement of said gun barrel causes rotation of said aft rotating means
  • second coupling means interengaging said gun bolt and said aft rotating means, so that rotation of said aft rotating means causes rectilinear aftward movement of said gun bolt which is accelerated with respect to the movement of said gun barrel.
  • a gun according to claim 10 further including:
  • an external rotating source of power coupled to and driving one of said rotating means.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles (AREA)
  • Soil Working Implements (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Transmission Devices (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Forklifts And Lifting Vehicles (AREA)
US403121A 1973-10-03 1973-10-03 Single barrel gun with a rotary operating mechanism Expired - Lifetime US3915058A (en)

Priority Applications (17)

Application Number Priority Date Filing Date Title
US403121A US3915058A (en) 1973-10-03 1973-10-03 Single barrel gun with a rotary operating mechanism
IL45686A IL45686A (en) 1973-10-03 1974-09-20 Recoil operated single barrel gun with a rotary feeder operating mechanism
DE2446145A DE2446145C2 (de) 1973-10-03 1974-09-27 Munitionszubringer für eine Waffe mit in Waffenlängsrichtung hin- und herbewegtem Verschluß
DE19747432482U DE7432482U (de) 1973-10-03 1974-09-27 Einlaeufiges gewehr mit einem drehbetaetigungsmechanismus
IT27877/74A IT1022447B (it) 1973-10-03 1974-09-30 Arma a canna singola con meccanismo di azionamento rotant
CH1320174A CH600286A5 (de) 1973-10-03 1974-10-01
ES430619A ES430619A1 (es) 1973-10-03 1974-10-02 Perfeccionamientos introducidos en las escopetas de un solo"canon".
FR7433227A FR2246836B1 (de) 1973-10-03 1974-10-02
BE149139A BE820620A (fr) 1973-10-03 1974-10-02 Mitrailleuse a canon unique
NO743571A NO142971C (no) 1973-10-03 1974-10-02 Ammunisjonsmater for et skytevaapen.
SE7412493A SE400639B (sv) 1973-10-03 1974-10-03 Ammunitionsmatare for att vapen med ett fram och ater i vapnets lengdriktning rorligt slutstycke
NLAANVRAGE7413094,A NL174984C (nl) 1973-10-03 1974-10-03 Patroonaanvoerinrichting voor een geweer.
JP49113364A JPS6237320B2 (de) 1973-10-03 1974-10-03
GB43000/74A GB1493376A (en) 1973-10-03 1974-10-03 Ammunition feeder
US05/533,188 US3955300A (en) 1973-10-03 1974-12-16 Gun bolt
US05/924,783 US4328737A (en) 1973-10-03 1978-06-12 Ammunition feeder for a gun
US06/032,587 US4257310A (en) 1973-10-03 1979-04-23 Ammunition feeding mechanism for a gun

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US403121A US3915058A (en) 1973-10-03 1973-10-03 Single barrel gun with a rotary operating mechanism

Related Child Applications (3)

Application Number Title Priority Date Filing Date
US05533160 Division 1974-12-16
US05533189 Division 1974-12-16
US05/533,188 Division US3955300A (en) 1973-10-03 1974-12-16 Gun bolt

Publications (1)

Publication Number Publication Date
US3915058A true US3915058A (en) 1975-10-28

Family

ID=23594542

Family Applications (1)

Application Number Title Priority Date Filing Date
US403121A Expired - Lifetime US3915058A (en) 1973-10-03 1973-10-03 Single barrel gun with a rotary operating mechanism

Country Status (13)

Country Link
US (1) US3915058A (de)
JP (1) JPS6237320B2 (de)
BE (1) BE820620A (de)
CH (1) CH600286A5 (de)
DE (2) DE7432482U (de)
ES (1) ES430619A1 (de)
FR (1) FR2246836B1 (de)
GB (1) GB1493376A (de)
IL (1) IL45686A (de)
IT (1) IT1022447B (de)
NL (1) NL174984C (de)
NO (1) NO142971C (de)
SE (1) SE400639B (de)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4011790A (en) * 1975-07-28 1977-03-15 General Electric Company Recoil converter for self powered gun
US4062266A (en) * 1975-09-25 1977-12-13 Elmore Lester C Liquid propellant modular gun incorporating dual cam operation and internal water cooling
US4244270A (en) * 1978-07-03 1981-01-13 General Electric Company Feeder for a gun
FR2479966A1 (fr) * 1980-04-07 1981-10-09 Gen Electric Mitrailleuse du type gatling comportant un dispositif perfectionne de presentation des cartouches aux culasses
US4548120A (en) * 1983-12-16 1985-10-22 The United States Of America As Represented By The Secretary Of The Army Externally powered separate loaded ammunition cannon

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2706889A1 (de) * 1977-02-17 1978-08-31 Vollmer Werke Maschf Handfeuerwaffe fuer huelsenlose munition
DE3101541C2 (de) * 1981-01-20 1985-05-23 Rheinmetall GmbH, 4000 Düsseldorf Getriebe für einen Gurtzuführerantrieb eines Gasdruckladers

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US676995A (en) * 1900-08-18 1901-06-25 Georges Roth Automatic firearm.
US1410524A (en) * 1918-10-30 1922-03-21 Us Ordnance Co Breech closure
US2989900A (en) * 1960-06-09 1961-06-27 Donald P Grover Stopping and starting system
US3071043A (en) * 1957-09-17 1963-01-01 William D Mcthomas Recoil-operated multiple barrel gun

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Publication number Priority date Publication date Assignee Title
US125563A (en) * 1872-04-09 Improvement in revolving-battery gums
US1786207A (en) * 1927-12-12 1930-12-23 Automatic Guns Inc Machine gun
US2849921A (en) * 1954-04-02 1958-09-02 Company The Schenectady Trust Gatling gun
GB784100A (de) * 1954-05-25
US3380343A (en) * 1966-12-21 1968-04-30 Gen Electric Firing mechanism for high rate of fire multi-barrel automatic weapon
US3407701A (en) * 1967-07-17 1968-10-29 Gen Electric Gas drive for a rotating barrel gun

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US676995A (en) * 1900-08-18 1901-06-25 Georges Roth Automatic firearm.
US1410524A (en) * 1918-10-30 1922-03-21 Us Ordnance Co Breech closure
US3071043A (en) * 1957-09-17 1963-01-01 William D Mcthomas Recoil-operated multiple barrel gun
US2989900A (en) * 1960-06-09 1961-06-27 Donald P Grover Stopping and starting system

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4011790A (en) * 1975-07-28 1977-03-15 General Electric Company Recoil converter for self powered gun
US4062266A (en) * 1975-09-25 1977-12-13 Elmore Lester C Liquid propellant modular gun incorporating dual cam operation and internal water cooling
US4244270A (en) * 1978-07-03 1981-01-13 General Electric Company Feeder for a gun
FR2479966A1 (fr) * 1980-04-07 1981-10-09 Gen Electric Mitrailleuse du type gatling comportant un dispositif perfectionne de presentation des cartouches aux culasses
DE3113413A1 (de) * 1980-04-07 1982-01-21 General Electric Co., Schenectady, N.Y. "transportradanordnung fuer hochgeschwindigkeits-feuer-revolvierende batteriegeschuetze"
US4342253A (en) * 1980-04-07 1982-08-03 General Electric Company Sprocket arrangement in a high rate of fire revolving battery gun
US4548120A (en) * 1983-12-16 1985-10-22 The United States Of America As Represented By The Secretary Of The Army Externally powered separate loaded ammunition cannon

Also Published As

Publication number Publication date
JPS5078199A (de) 1975-06-25
NO142971C (no) 1980-11-19
NL7413094A (nl) 1975-04-07
IT1022447B (it) 1978-03-20
FR2246836A1 (de) 1975-05-02
SE7412493L (sv) 1975-04-04
NO743571L (de) 1975-04-28
FR2246836B1 (de) 1982-06-18
SE400639B (sv) 1978-04-03
JPS6237320B2 (de) 1987-08-12
BE820620A (fr) 1975-04-02
ES430619A1 (es) 1976-10-16
IL45686A0 (en) 1975-02-10
GB1493376A (en) 1977-11-30
DE7432482U (de) 1978-02-02
DE2446145A1 (de) 1975-04-10
CH600286A5 (de) 1978-06-15
DE2446145C2 (de) 1984-09-13
NO142971B (no) 1980-08-11
NL174984C (nl) 1984-09-03
IL45686A (en) 1979-10-31

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