[go: up one dir, main page]

US3035494A - Recoil adjusting device - Google Patents

Recoil adjusting device Download PDF

Info

Publication number
US3035494A
US3035494A US4829A US482960A US3035494A US 3035494 A US3035494 A US 3035494A US 4829 A US4829 A US 4829A US 482960 A US482960 A US 482960A US 3035494 A US3035494 A US 3035494A
Authority
US
United States
Prior art keywords
recoil
chamber
adjusting device
weapon
venturi openings
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
US4829A
Inventor
Musser C Walton
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to US4829A priority Critical patent/US3035494A/en
Application granted granted Critical
Publication of US3035494A publication Critical patent/US3035494A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • 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

Definitions

  • This invention r'elates to weapons which function upon firing to produce a rearward blast of gas whereby recoil of the weapon is minimized. More particularly, it provides means which are operable to adjust such recoil to any desired value.
  • recoilless weapons normally include a barrel which is perforated to emit the gases by which the recoil is neutralized. Surrounding this barrel is a chamber which receives these gases and discharges them through a plurality of venturi openings at the breech end of the weapon.
  • the recoil of the weapon is very sensitive to slight irregularities in the surface of the venturi openings. Due to difficulties in manufacture and to erosion during the use of the weapon, it is practically impossible to ensure that the venturi openings are such as to minimize recoil to the desired degree.
  • the present invention avoids this difficulty by the provision of a ring or baflie which may be advanced into the chamber to any desired extent.
  • FIG. 1 is a sectional view of a recoilless weapon with the recoil compensator in its extreme rear position
  • FIG. 2 is a similar view showing the recoil compensator somewhat advanced into the chamber
  • FIG. 3 is a cross-section taken on the line 3-3 of FIG. 1.
  • the recoilless weapon illustrated by these figures includes a barrel which has fixed to its breech end a chamber 11. Threaded into the rear end of the chamber 11 is a removable liner 12 which has a plurality of venturi openings 13. Threaded into the forward end of the member 12 is a conical ring 14 which may be adjusted longitudinally to different positions as indicated by FIG. 2.
  • the weapon illustrated by the various figures is adapted to fire a cartridge which includes a perforated casing 15 containing a propellant 16 and is closed at its forward end by a projectile 17, this cartridge being held in place by a breech member 18 of a well known type.
  • the conical member 14 is arranged to be adjusted longitudinally. This adjustment functions to change the area of the path of the gases from the cartridge to the venturi openings. It also lengthens the travel of the gas immediately adjacent the head of the cartridge. This results in higher etficiency since more of the powder is burnt.
  • the recoil compensator 14 functions somewhat in the nature of a bafiie, since the powder gases, in order to get through the restricted area between the compensator 14 and the chamber 11, have to experience a drop in' pressure. This reduces the pressure of the gases at the point where they are entering the venturi openings. Since the pressure at the entrance of the venturi openings is somewhat lower than in the chamber, the mass rate of flow through the venturi openings is reduced. This permits the venturi openings to function even after it has eroded to a slightly larger size, thus by adjustment of compensator 14 forward and backward, the recoil can be adjusted to zero or to any other desired value.
  • this invention more than provides replaceable or adjustable venturi openings, by reason of the fact that the member 14 may be adjusted forwardly to compensate for erosion or wear in the venturi openings, thus prolonging the useful life of those openings.
  • the forward and outer end portion of member 14 may be subject to erosion, nevertheless with forward adjustment its outer end may be brought closer to chamber wall 11 due to the slope of this wall.
  • This member 14 is an advantage for two reasons. It functions as a preliminary constriction although erosion may occur at the outer end of member 14 and the adjacent wall 11. When member 14 wears and it is adjusted forwardly it cooperates with a new and nearer wall portion 11 where erosion has not been as serious.
  • Another inherent advantage in member 14 which will be appreciated by those familiar with recoilless weapons is the fact that it functions to change the gas flow to an extent from laminar flow to turbulent flow, which latter counteracts the effect of erosion to a noticeable degree.
  • a recoilless type weapon comprising in combination, a barrel, means forming a chamber fixed to a breech end portion of said barrel for reception axially thereto, a perforate casing of propellant spaced radially from said chamber forming means and communicating with said barrel, a removable liner fixed within a rear end portion of said chamber forming means, said liner being provided therein with a plurality of equally angularly spaced venturi openings, a breech member for holding a round within said weapon, said liner axially positioning the rear end of said perforate casing of propellant, and a member having a cylindrical portion threaded within said liner and being outside said perforate casing of propellant, said member having a forwardly and radially outwardly flaring ring portion forming with a rearwardly flaring portion of said chamber forming means a preliminary constriction through which propellant gases pass prior to passing rearwardly through said venturi openings, a wall of said chamber forming means adjacent the outer end of said

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)

Description

May 1952. c w. MUSSER 3,035,494
RECOIL. ADJUSTING DEVICE Filed Jan. 26, 1960 Y1 VA VA W] Y] FIG. 2
FIG. 3
INVENTOR. C WALTON MUSSER L J. W
ATTORNEYS:
aired rates l atent 3,035,494 RECOIL ADJUSTING DEVICE C Walton Musser, Beverly, Mass., assignor to the United States of America as represented by the Secretary of the Army Filed Jan. 26, 1960, Ser. No. 4,829
1 Claim. (Cl. 89-1.7)
(Granted under Title 35, US. Code (1952), sec. 266) The invention described herein may be manufactured and used by or for the Government for governmental purposes Without the payment to me of any royalty thereon.
This invention r'elates to weapons which function upon firing to produce a rearward blast of gas whereby recoil of the weapon is minimized. More particularly, it provides means which are operable to adjust such recoil to any desired value.
As is well understood by those skilled in the art, recoilless weapons normally include a barrel which is perforated to emit the gases by which the recoil is neutralized. Surrounding this barrel is a chamber which receives these gases and discharges them through a plurality of venturi openings at the breech end of the weapon.
Experience has shown that the recoil of the weapon is very sensitive to slight irregularities in the surface of the venturi openings. Due to difficulties in manufacture and to erosion during the use of the weapon, it is practically impossible to ensure that the venturi openings are such as to minimize recoil to the desired degree. The present invention avoids this difficulty by the provision of a ring or baflie which may be advanced into the chamber to any desired extent.
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 claim.
Referring to the drawings:
FIG. 1 is a sectional view of a recoilless weapon with the recoil compensator in its extreme rear position,
FIG. 2 is a similar view showing the recoil compensator somewhat advanced into the chamber, and
FIG. 3 is a cross-section taken on the line 3-3 of FIG. 1.
The recoilless weapon illustrated by these figures includes a barrel which has fixed to its breech end a chamber 11. Threaded into the rear end of the chamber 11 is a removable liner 12 which has a plurality of venturi openings 13. Threaded into the forward end of the member 12 is a conical ring 14 which may be adjusted longitudinally to different positions as indicated by FIG. 2.
The weapon illustrated by the various figures is adapted to fire a cartridge which includes a perforated casing 15 containing a propellant 16 and is closed at its forward end by a projectile 17, this cartridge being held in place by a breech member 18 of a well known type.
As previously indicated, the conical member 14 is arranged to be adjusted longitudinally. This adjustment functions to change the area of the path of the gases from the cartridge to the venturi openings. It also lengthens the travel of the gas immediately adjacent the head of the cartridge. This results in higher etficiency since more of the powder is burnt.
In use the recoil compensator 14 functions somewhat in the nature of a bafiie, since the powder gases, in order to get through the restricted area between the compensator 14 and the chamber 11, have to experience a drop in' pressure. This reduces the pressure of the gases at the point where they are entering the venturi openings. Since the pressure at the entrance of the venturi openings is somewhat lower than in the chamber, the mass rate of flow through the venturi openings is reduced. This permits the venturi openings to function even after it has eroded to a slightly larger size, thus by adjustment of compensator 14 forward and backward, the recoil can be adjusted to zero or to any other desired value.
Those familiar with recoilless guns will understand that this invention more than provides replaceable or adjustable venturi openings, by reason of the fact that the member 14 may be adjusted forwardly to compensate for erosion or wear in the venturi openings, thus prolonging the useful life of those openings. As shown in the drawing even though the forward and outer end portion of member 14 may be subject to erosion, nevertheless with forward adjustment its outer end may be brought closer to chamber wall 11 due to the slope of this wall. This member 14 is an advantage for two reasons. It functions as a preliminary constriction although erosion may occur at the outer end of member 14 and the adjacent wall 11. When member 14 wears and it is adjusted forwardly it cooperates with a new and nearer wall portion 11 where erosion has not been as serious. Another inherent advantage in member 14 which will be appreciated by those familiar with recoilless weapons is the fact that it functions to change the gas flow to an extent from laminar flow to turbulent flow, which latter counteracts the effect of erosion to a noticeable degree.
I claim:
A recoilless type weapon comprising in combination, a barrel, means forming a chamber fixed to a breech end portion of said barrel for reception axially thereto, a perforate casing of propellant spaced radially from said chamber forming means and communicating with said barrel, a removable liner fixed within a rear end portion of said chamber forming means, said liner being provided therein with a plurality of equally angularly spaced venturi openings, a breech member for holding a round within said weapon, said liner axially positioning the rear end of said perforate casing of propellant, and a member having a cylindrical portion threaded within said liner and being outside said perforate casing of propellant, said member having a forwardly and radially outwardly flaring ring portion forming with a rearwardly flaring portion of said chamber forming means a preliminary constriction through which propellant gases pass prior to passing rearwardly through said venturi openings, a wall of said chamber forming means adjacent the outer end of said flaring ring portion having an oppositely directed slope from that of said ring portion threaded within said liner, whereby said ring member may be adjustably moved forwardly to provide compensation for wear in the venturi openings.
References Cited in the file of this patent UNITED STATES PATENTS 2,489,747 Burney Nov. 29, 1949 2,489,748 Burney Nov. 29, 1949 2,537,063 Kroeger et al. Jan. 9, 1951 2,598,256 Hickman May 27, 1952
US4829A 1960-01-26 1960-01-26 Recoil adjusting device Expired - Lifetime US3035494A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US4829A US3035494A (en) 1960-01-26 1960-01-26 Recoil adjusting device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US4829A US3035494A (en) 1960-01-26 1960-01-26 Recoil adjusting device

Publications (1)

Publication Number Publication Date
US3035494A true US3035494A (en) 1962-05-22

Family

ID=21712728

Family Applications (1)

Application Number Title Priority Date Filing Date
US4829A Expired - Lifetime US3035494A (en) 1960-01-26 1960-01-26 Recoil adjusting device

Country Status (1)

Country Link
US (1) US3035494A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3338133A (en) * 1965-10-06 1967-08-29 Andrew J Grandy Launching system
US4091709A (en) * 1976-07-26 1978-05-30 The United States Of America As Represented By The Secretary Of The Army Recoilless rifle nozzle
US4203347A (en) * 1978-04-10 1980-05-20 The Boeing Company Shock suppressing apparatus and method for a rocket launcher
US4944210A (en) * 1988-08-08 1990-07-31 Hughes Aircraft Company Missile launcher
US4962689A (en) * 1989-08-01 1990-10-16 Hughes Aircraft Company Gas generator missile launch system
US20100275763A1 (en) * 2006-12-22 2010-11-04 Saab Ab Nozzle
US10788284B1 (en) * 2019-05-09 2020-09-29 The United States Of America As Represented By The Secretary Of The Army Grounded and vehicular mounted weapons with improved recoil stability

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2489747A (en) * 1941-12-05 1949-11-29 Burney Charles Dennistoun Reduced recoil type gun
US2489748A (en) * 1942-05-07 1949-11-29 Burney Charles Dennistoun Controlled pressure gun
US2537063A (en) * 1949-02-02 1951-01-09 William J Kroeger Breech and firing mechanism for recoilless firearms
US2598256A (en) * 1945-04-21 1952-05-27 Us Sec War Recoilless gun

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2489747A (en) * 1941-12-05 1949-11-29 Burney Charles Dennistoun Reduced recoil type gun
US2489748A (en) * 1942-05-07 1949-11-29 Burney Charles Dennistoun Controlled pressure gun
US2598256A (en) * 1945-04-21 1952-05-27 Us Sec War Recoilless gun
US2537063A (en) * 1949-02-02 1951-01-09 William J Kroeger Breech and firing mechanism for recoilless firearms

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3338133A (en) * 1965-10-06 1967-08-29 Andrew J Grandy Launching system
US4091709A (en) * 1976-07-26 1978-05-30 The United States Of America As Represented By The Secretary Of The Army Recoilless rifle nozzle
US4203347A (en) * 1978-04-10 1980-05-20 The Boeing Company Shock suppressing apparatus and method for a rocket launcher
US4944210A (en) * 1988-08-08 1990-07-31 Hughes Aircraft Company Missile launcher
US4962689A (en) * 1989-08-01 1990-10-16 Hughes Aircraft Company Gas generator missile launch system
US20100275763A1 (en) * 2006-12-22 2010-11-04 Saab Ab Nozzle
US10788284B1 (en) * 2019-05-09 2020-09-29 The United States Of America As Represented By The Secretary Of The Army Grounded and vehicular mounted weapons with improved recoil stability

Similar Documents

Publication Publication Date Title
US3399597A (en) Silent firearm
US2351037A (en) Stabilizer for guns
US3490330A (en) Firearm,particularly light antitank weapon
JPS61110899A (en) Compensator for small arm operated by gas pressure
US3367055A (en) Shotgun muzzle device comprising a compensator and choke
US2801416A (en) Means for controlling the velocity of projectiles
US10557675B1 (en) Devices for restricting the flow of propellant gas in gas-actuated firearms
US3611867A (en) Emergency weapon for firing high-velocity grenade rounds
US3318033A (en) Grenade launching arrangement
US3459101A (en) High velocity weapon
JPS6183900A (en) Flash suppressor
US3726218A (en) Low velocity cartridge having total propellant ignition
US3988990A (en) Projectile
US3035494A (en) Recoil adjusting device
US20060011056A1 (en) Recoil reduction adapter
US2715858A (en) Regulator means for a firearm gas piston
US3396658A (en) Small arms cartridge
US3437039A (en) Multicharge cartridge for multibarrel automatic guns
US3326128A (en) Rockets and combinations of rockets and cases
US4553480A (en) No flash, very low noise howitzer round and tube
US2472111A (en) Recoilless firearm and ammunition therefor
US2681619A (en) Rocket projectile
US3152510A (en) Recoil controlling device
US2119169A (en) Gas-operated gun loading device
US3618250A (en) Launching arrangement for sub-caliber projectiles