US2956479A - Cascaded gun barrel - Google Patents

Cascaded gun barrel Download PDF

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US2956479A
US2956479A US718386A US71838658A US2956479A US 2956479 A US2956479 A US 2956479A US 718386 A US718386 A US 718386A US 71838658 A US71838658 A US 71838658A US 2956479 A US2956479 A US 2956479A
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barrel
pressure
cascaded
gun
gun barrel
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US718386A
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Musser C Walton
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    • 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
    • F41A21/00Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
    • 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

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  • This invention relates to recoilless rifles, and more especially to an improved arrangement of parts and method of operation whereby the weight of such rifles is greatly reduced.
  • Fig. 1 illustrates a preferred form of the invention
  • Fig. 2 is a curve indicating the relation between the travel of the projectile and pressure in the chamber.
  • the rifle of the present invention includes a member which is shaped to form a barrel, to form a chamber to the rear of the barrel and to form a venturi to the rear of the chamber.
  • a member 11 which is connected to the member 10 at its front and rear ends, the front connection being in the form of seals 12 and the rear connection being in the form of threads 13. Opening from the throat of the venturi into the space between the members 10 and 11 are a plurality of apertures 14.
  • the cartridge fired by the illustrated gun may be of the type wherein a propellant 15 surrounds a boom 17, is enclosed within a frangible or burnable casing 16 and extends between the fins 18 and the adapter 19 of the cartridge. Immediately ahead of the adapter 19 is the projectile.
  • the second factor is the shape of the curve on the Misses-Henky formula for calculating the required thickness of pressure vessels.
  • This curve shows a distinct upward trend particularly when 40% of the yield strength of the material is reached. From this 40% to 58% it changes rapidly, and at 58% the wall thickness would have to be infinite.
  • a recoilless gun having a barrel through which a projectile may be fired, a venturi nozzle at a rear end portion of said barrel and having a constricted throat portion in which the velocity of issuing gaseous prodncts of propellant combustion is increased and the pressure reduced, an outer substantially concentric tubular imperforate member encompassing said barrel but spaced radially therefrom and extending rearwardly substantially to said constricted throat portion, means closing the ends of the space between the outer member and barrel and forming a closed chamber between said barrel and outer tubular member, and a connection leading to said closed chamber from within a reduced pressure area part of the throat portion of said barrel whereby the closed chamber may be supplied with gas under reduced pressure as compared with that in the barrel without recourse to a separate source of pressure from that in said barrel and without use of a reducing valve possessing objectionable inertia.
  • a recoilless gun according to claim 1 in which said connection is made from said constricted throat portion where the reduction in pressure is substantially a maximum.

Description

Oct. 18, 1960 c w. MUSSER 2,956,479
CASCADED GUN BARREL Filed Feb. 2a, 1958 $IIIIIIIIIIIIIIII I |5,000 PEAK PRESSURE TRAVEL OF PROJECTILE PRESSURE AT PASSAGES ABOUT l2 CHAMBER PRESSURE.
FIG.2.
INVEN TOR. C WALTON MUSSER 9% a My; W W
United States Patent CASCADED GUN BARREL C Walton Musser, Beverly, Mass., assignor to the United States of America as represented by the Secretary of the Army Filed Feb. 28, 1958, Ser. No. 718,386
2 Claims. (Cl. 891.7):
(Granted under Title 35, US. Code (1952), see. 266) The invention described herein may be manufactured and used by or for the Government for governmental purposes without the payment of any royalty thereon.
This invention relates to recoilless rifles, and more especially to an improved arrangement of parts and method of operation whereby the weight of such rifles is greatly reduced.
It has been proposed heretofore to reduce the weight of a gun by the use of a cascaded barrel wherein a liquid under pressure is enclosed between the inner and outer cylinders of which the barrel is formed. The present invention retains this general type of barrel but difiers from the prior art gun in that the gas pressure incident to firing of the gun is utilized to reinforce the barrel. As hereinafter explained this result is achieved by providing, near the throat of the venturi, openings which conduct the gas from the chamber to the space between the inner and outer cylinders of the barrel. This has the very important advantage that it eliminates the need of a pump or other means for introducing a reinforc ing fluid and results in an inexpensive structure.
The invention will be better understood from the following description when considered in connection with the accompanying drawings and its scope is indicated by the appended claims.
Referring to the drawings:
Fig. 1 illustrates a preferred form of the invention, and
Fig. 2 is a curve indicating the relation between the travel of the projectile and pressure in the chamber.
Referring to Fig. 1, the rifle of the present invention includes a member which is shaped to form a barrel, to form a chamber to the rear of the barrel and to form a venturi to the rear of the chamber. Encircling the member 10 is a member 11 which is connected to the member 10 at its front and rear ends, the front connection being in the form of seals 12 and the rear connection being in the form of threads 13. Opening from the throat of the venturi into the space between the members 10 and 11 are a plurality of apertures 14.
The cartridge fired by the illustrated gun may be of the type wherein a propellant 15 surrounds a boom 17, is enclosed within a frangible or burnable casing 16 and extends between the fins 18 and the adapter 19 of the cartridge. Immediately ahead of the adapter 19 is the projectile.
In the operation of the rifle, burning of the propellant 15 generates in the chamber and in the region of the apertures 14 a gas under very high pressures. Flow of these gases through the venturi produces a pressure diflerential. Some of this gas at a lowered pressure level is forced through the apertures 14 into the space between the members 10 and 11 obviously enabling the inner cylinder 10 to withstand a higher pressure than it could without the exterior pressure applied to it by the gas.
For example, if the outer cylinder and the inner cylin- 2,956,479 Patented Oct. 18, 1960 der are both designed to withstand 15,000 lbs. pressure and if the space between the two cylinders is pressurized to 15,000 pounds (see Fig. 2), then 30,000 pounds may be applied to the inside of the inner cylinder. This results in a very considerable reduction in the required weight of the gun.
Two factors are involved in this weight reduction. In the first place, the side wall of a gun, when it becomes too thick, cannot be heat treated so as to obtain high physical strength without using special high alloy steels. In order to get high physical strength with ordinary alloy steels it is necessary to have the wall thickness relatively thin. Consequently with a thick walled chamber it may be possible to obtain only a fiber yield strength of 60,000 pounds per square inch. If this same wall with the same steel is made thinner, it can be heat treated to obtain a 150,000 pounds per square inch yield strength.
The second factor is the shape of the curve on the Misses-Henky formula for calculating the required thickness of pressure vessels. This curve shows a distinct upward trend particularly when 40% of the yield strength of the material is reached. From this 40% to 58% it changes rapidly, and at 58% the wall thickness would have to be infinite.
Under some conditions, combining these two factors into the cascaded barrel principle results in a weight saving of the order of 70%. This means that a barrel which would weigh 100,000 pounds if of solid construction, may be manufactured to Weigh only 30,000 pounds by utilizing the cascaded barrel principle.
While the pressure between the inner and outer cylinder could be produced by means other than those disclosed herein, all such other means lack the simplicity of structure and operation realized from the present invention which requires nothing more than the provision of an opening from the throat of the venturi to the space between the inner and outer cylinders.
I claim:
1. A recoilless gun having a barrel through which a projectile may be fired, a venturi nozzle at a rear end portion of said barrel and having a constricted throat portion in which the velocity of issuing gaseous prodncts of propellant combustion is increased and the pressure reduced, an outer substantially concentric tubular imperforate member encompassing said barrel but spaced radially therefrom and extending rearwardly substantially to said constricted throat portion, means closing the ends of the space between the outer member and barrel and forming a closed chamber between said barrel and outer tubular member, and a connection leading to said closed chamber from within a reduced pressure area part of the throat portion of said barrel whereby the closed chamber may be supplied with gas under reduced pressure as compared with that in the barrel without recourse to a separate source of pressure from that in said barrel and without use of a reducing valve possessing objectionable inertia.
2. A recoilless gun according to claim 1 in which said connection is made from said constricted throat portion where the reduction in pressure is substantially a maximum.
References Cited in the file of this patent UNITED STATES PATENTS 667,525 Huber Feb. 5, 1901 2,146,554 Rossmann Feb. 7, 1939 2,438,297 Pope Mar. 23, 1948 2,802,399 Little Aug. 13, 1957 FOREIGN PATENTS 490,182. Great Britain Aug. 10, 1938
US718386A 1958-02-28 1958-02-28 Cascaded gun barrel Expired - Lifetime US2956479A (en)

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3095813A (en) * 1961-07-05 1963-07-02 Henry S Lipinski Propellant container, plastic impregnated glass
US3216356A (en) * 1964-01-30 1965-11-09 Jr William F Kaufmann Projectile
US3827332A (en) * 1972-10-31 1974-08-06 D Lindsay Aircraft having recoilless rifle
US4073213A (en) * 1975-07-02 1978-02-14 Societe Anonyme Dite : Societe Europeenne De Propulsion Assembly for launching a projectile
EP0059012A2 (en) * 1981-02-19 1982-09-01 THE PROCTER & GAMBLE COMPANY Mouthwash compositions
FR2550856A1 (en) * 1983-08-17 1985-02-22 Messerschmitt Boelkow Blohm DEVICE FOR DYNAMICALLY STRENGTHENING HIGHLY SOLICITED STRUCTURES
US5054224A (en) * 1990-11-19 1991-10-08 The United States Of America As Represented By The Secretary Of The Army Apparatus and method for a composite polymer rifling disposable gun tube
US20100275763A1 (en) * 2006-12-22 2010-11-04 Saab Ab Nozzle

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US667525A (en) * 1900-06-08 1901-02-05 Carl Huber Internal-pressure-resistance cylinder.
GB490182A (en) * 1936-10-26 1938-08-10 Roberto Antona Traversi Improvements in or relating to gun barrels
US2146554A (en) * 1937-11-03 1939-02-07 Curtiss Wright Corp Cooling of machine guns
US2438297A (en) * 1944-04-05 1948-03-23 Winslow B Pope Recoilless gun
US2802399A (en) * 1953-11-30 1957-08-13 Steven M Little Rocket launcher

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US667525A (en) * 1900-06-08 1901-02-05 Carl Huber Internal-pressure-resistance cylinder.
GB490182A (en) * 1936-10-26 1938-08-10 Roberto Antona Traversi Improvements in or relating to gun barrels
US2146554A (en) * 1937-11-03 1939-02-07 Curtiss Wright Corp Cooling of machine guns
US2438297A (en) * 1944-04-05 1948-03-23 Winslow B Pope Recoilless gun
US2802399A (en) * 1953-11-30 1957-08-13 Steven M Little Rocket launcher

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3095813A (en) * 1961-07-05 1963-07-02 Henry S Lipinski Propellant container, plastic impregnated glass
US3216356A (en) * 1964-01-30 1965-11-09 Jr William F Kaufmann Projectile
US3827332A (en) * 1972-10-31 1974-08-06 D Lindsay Aircraft having recoilless rifle
US4073213A (en) * 1975-07-02 1978-02-14 Societe Anonyme Dite : Societe Europeenne De Propulsion Assembly for launching a projectile
EP0059012A2 (en) * 1981-02-19 1982-09-01 THE PROCTER & GAMBLE COMPANY Mouthwash compositions
EP0059012A3 (en) * 1981-02-19 1983-06-01 The Procter & Gamble Company Mouthwash compositions
FR2550856A1 (en) * 1983-08-17 1985-02-22 Messerschmitt Boelkow Blohm DEVICE FOR DYNAMICALLY STRENGTHENING HIGHLY SOLICITED STRUCTURES
US5054224A (en) * 1990-11-19 1991-10-08 The United States Of America As Represented By The Secretary Of The Army Apparatus and method for a composite polymer rifling disposable gun tube
US20100275763A1 (en) * 2006-12-22 2010-11-04 Saab Ab Nozzle

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