Shock absorbing mount for adjustable barrel

Information

  • Patent Grant
  • 6250198
  • Patent Number
    6,250,198
  • Date Filed
    Wednesday, August 11, 1999
    25 years ago
  • Date Issued
    Tuesday, June 26, 2001
    23 years ago
Abstract
Disclosed is a mount releasably attached to a launcher/spotting rifle assembly. The mount, when released, allows for the barrel of the spotting rifle of the launcher/spotting rifle assembly to be adjusted in a spherical manner, and when tightened, rigidly affixes the barrel to the launcher/spotting rifle assembly, while at the same time provides shock absorbing means which absorbs high stress from the firing shock typically created by the discharge of the launcher/spotting rifle assembly. The shock absorbing means acts to preserve the rigid and accurate attachment of the barrel to the launcher/spotting rifle assembly.
Description




BACKGROUND OF THE INVENTION




1. Field of the Invention




The present invention relates to firearm technology and, more particularly, to a releasable mount, which when loosened allows for spherical adjustment of the barrel of a spotting rifle and, which when tightened, firmly maintains the desired barrel orientation.




2. Description Of the Prior Art




Spotting rifles have means for adjusting the orientation of the barrel of the rifle so as to accurately position the barrel to bring to bear the fire power thereof onto a target. For such adjustment, the barrel needs to be allowed to pivot relative to the rifle, more particularly, relative to the receiver portion of the spotting rifle.




Spotting rifles are also used in conjunction with other firearms, such as a rocket launcher. In such applications, the rifle receiver is rigidly connected to the launch tube of the rocket launcher. Using the weapon is as follows: tracer rounds are fired from the spotting rifle until the gunner, controlling the rocket launcher, feels that he is accurately hitting the target. At this point, the gunner switches the weapon to launch mode and fires the rocket. The rocket and the spotting rounds have the same trajectory allowing the rocket launcher to hit the same target as the tracers.




Prior art spotting rifles used in conjunction with rocket launchers have allowed the barrel to pivot relative to the receiver portion of the spotting rifle, but did so without firmly securing the barrel to the receiver portion of the spotting rifle. Because the barrel was not firmly mounted, the barrel would “jump” when the spotting rifle was fired causing a large group, that is, scattering of bullets, onto the target. The prior art spotting rifles secured the barrel to the receiver portion by using set screws to improve the accuracy of the rifle and, thus, the rocket launcher, but it was determined that the set screws would back out of their capturing holes from the vibration caused by the firing of the spotting rifle and the rocket launcher. In addition, analysis was performed that showed high levels of stress were being encountered at the barrel/set screw interface which caused the loosening of the set screws from their capturing holes. It is desired that a releasable mount be provided which when loosened allows for the adjustment of the orientation of the barrel and, which when tightened, firmly maintains the orientation of the barrel during firing of the spotting rifle and the rocket launcher.




SUMMARY OF THE INVENTION




Accordingly, it is a primary object of the present invention to provide for mounting means such, when loosened, allows for the adjustment of a barrel of spotting rifle, and when tightened, maintains the desired orientation of the barrel, while at the same time absorbs high stress that normally occurs during the firing of the spotting rifle and also during the firing of the associated rocket launcher.




It is another object of the present invention to provide for mounting means that allows for spherical adjustment for the barrel of the spotting rifle so that the spotting rifle may be more effectively used with a rocket launcher.




It is yet another object of the present invention to provide for an adjustable means for the mounting of a barrel that has shock absorbing capabilities so as to maintain the desired orientation of the barrel of the spotting rifle.




It is a further object of the present invention to provide for adjustable mounting means that can be tightened and pinned to the receiver portion of the spotting rifle.




In accordance with these and other objects, the invention provides a firearm comprising a barrel, a receiver portion, a mount, and shock absorbing means. The barrel has first and second ends and serves as a discharge tube for the firearm. The receiver portion of the firearm has means for receiving and holding the second end of the barrel. The mount has means for releasably connecting to the receiver portion. The shock absorbing means is lodged in the mount and interposed between the barrel and the mount.











BRIEF DESCRIPTION OF THE DRAWINGS




The foregoing objects and advantages of the present invention will be more fully understood from the following detailed description having reference to the appended drawings wherein:





FIG. 1

is an overall view of the launcher/spotter rifle assembly of the present invention.





FIG. 2

is a sectional drawing illustrating the adjustable mount of the present invention; and





FIG. 3

is a section of the drawing taken along line


3





3


of

FIG. 2

, illustrating some of the details for connecting the adjustable mount to the launcher/spotter rifle assembly of FIG.


1


.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS




Referring to the drawings, wherein in the same reference number indicates the same element throughout, there is shown in

FIG. 1

an overall view of a typical launcher/spotter rifle assembly designated generally by the reference number


10


. The rocket launcher/spotter rifle assembly


10


has a handle


12


that is used in the operation of a trigger


14


. The launcher/spotter rifle assembly


10


further comprises a barrel


16


that is connected on the muzzle end thereof to a front bracket


18


of the launcher/spotter rifle assembly


10


by means of bore sighting adjustment device


20


, to be further described with reference to

FIG. 3

, and on the other end thereof to a receiver assembly


22


of the launcher/spotter rifle assembly


10


. The barrel


16


is connected to the receiver assembly


22


by means of a mount assembly


100


which is of particular importance to the present invention and may be further described with reference to FIG.


2


.





FIG. 2

illustrates the barrel


16


, which serves as the discharge tube for a spotting rifle of FIG.


1


and has a first or muzzle end (previously mentioned with regard to

FIG. 1

)


16


A and a second end (previously mentioned with regard to

FIG. 1

)


16


B, as well as having a centerline


24


along which is located a center


26


about which the barrel


16


is rotated in a spherical manner to be described. The spotting rifle is interchangeably referred to herein as simply a rifle or, more generally, as a firearm. Similarly, the launcher/spotter assembly


10


is sometimes referred to herein as a firearm. Although the practice of the invention is particularly suited for a spotting rifle operated in conjunction with a launcher both forming the launcher/spotter rifle assembly


10


, the practice of the invention is also applicable to other type firearms. The launcher/spotter assembly


10


further comprises the receiver portion


22


, having first and second ends


22


A and


22


B, respectively.




The mount assembly


100


of

FIG. 2

has a threaded insert


102


which interconnects the receiver portion


22


to a barrel clamp


104


of the mount assembly


100


. If desired, the threaded insert


102


can be eliminated if the receiver portion


22


is provided with external threads so that the barrel clamp


104


may threadly engage with the receiver portion


22


. The barrel clamp


104


has first and second ends


106


and


108


, with the first end


106


being threadedly engaged with the threaded insert


102


.




The mount assembly


100


further comprises a barrel bushing


110


which provides a shock absorbing means that is interposed between the barrel


16


and the barrel clamp


104


. In one preferred embodiment, the shock absorbing means


110


is a urethane compression spring preferably having a spring constant of about 12,000 lbs. per inch. If desired, materials other than urethane may be used for the preferred embodiment so long as the spring constant of 12,000 lbs. per inch or less is maintained. For other embodiments for totally different weapon systems, the barrel bushing


110


may require a higher or lower spring constant than the 12,000 lbs., per inch. For all embodiments, the stiffness of the barrel bushing


100


should be less than that of the surrounding steel.




The mount assembly


100


further preferably comprises a slide washer


112


and a barrel collar


114


. The slide washer


112


and the barrel collar


114


have faces


112


A and


114


A, respectively, that are curved in a complementary manner to each other. The faces


112


A and


114


A are spherically curved by means of their respective spherical radius relative to the center


26


of rotation of the barrel


16


.




The first end


16


A of the barrel


16


mates with the barrel sighting adjustment device


20


which is positioned inside of the front bracket


18


. The front bracket


18


and barrel sighting adjustment device


20


orient the barrel


16


which is rigidly fixed by the barrel clamp


104


. The sighting adjustment device


20


has set screws


20


A which may be further described with reference to

FIG. 3

which is a sectional view taken along line


3





3


of FIG.


2


.





FIG. 3

illustrates three set screws


20


A each connected to the first bracket


18


by means of respective self-locking helicoils


20


B. Each of the set screws


20


A is adjustable to orient the muzzel end


16


A to its desired line of sight.




Operation of Mount Assembly


100






In operation, and with reference to

FIGS. 2 and 3

, the mount assembly


100


is connected to the associated launcher/rifle assembly


10


via the threaded insert


102


. More particularly, the threaded insert


102


threads to the receiver portion


22


on one end and to the barrel clamp


104


on the other end. The barrel clamp


104


houses the clamp bushing


110


, the slide washer


112


and the barrel collar


114


. The second end


16


B of the barrel


16


has a spherical face


16


C which rests against a spherical face


22


C on the receiver portion


22


as shown in FIG.


2


. The barrel


16


is rigidly fixed by tightening the barrel clamp


104


.




The barrel


16


is adjusted by loosening the barrel clamp


104


which allows the barrel


16


to pivot spherically about the center of rotation


26


. Three set screws


20


A (shown most clearly in

FIG. 3

) which are mounted to the front bracket


18


at the muzzle end


16


A of the barrel


16


are adjusted to locate the barrel


16


based on bore sighting. The barrel clamp


104


is then tightened fixing the barrel


16


to the receiver portion


22


.




In actual operation, when the barrel


16


is firmly attached to the receiver portion


22


, the clamp bushing


110


, preferably in the form of an urethane spring, acts as the shock absorbing means to absorb the high stress from the firing shock typically created by the discharge of the launcher/spotter rifle assembly


10


.




It should now be appreciated that the practice of the present invention provides for the releasably attachable mount, which when loosened, allows for the spherical adjustment of the barrel of a spotting rifle and, which when attached, firmly mounts the adjustment means to the receiver portion of the launcher/spotter rifle assembly


10


, while at the same time has shock absorbing means which absorbs the high stress commonly created by the firing shock experience when discharging the launcher/spotter rifle assembly


10


.




Although the invention has been described relative to a specific embodiment thereof, there are numerous variations and modifications that will be readily apparent to those skilled in the art in light of the above teaching. It is, therefore, understood that within the scope of the appended claims, the invention may be practiced other than as specifically described.



Claims
  • 1. A firearm comprising:(a) a barrel having first and second ends; (b) a receiver portion of said firearm having means for receiving and holding said second end of said barrel; (c) a mount having means for releasably connecting to said receiver portion; and (d) shock absorbing means lodged in said mount and interposed between said barrel and said mount.
  • 2. The firearm according to claim 1, wherein said means for releasably connecting said mount to said receiver portion comprises threads on said mount and said receiver portion so as to provide threaded engagement therebetween.
  • 3. The firearm according to claim 1, wherein said shock absorbing means comprises a urethane spring.
  • 4. The firearm according to claim 1 further comprising a slide washer and a barrel collar interposed between said shock absorbing means and said barrel.
  • 5. The firearm according to claim 1 further comprises means for orienting said first end of said barrel.
  • 6. A firearm comprising:(a) a barrel having first and second ends and having a centerline; (b) a receiver portion of said firearm having means for receiving and holding said second end of said barrel; (c) a mount having means for releasably connecting to said receiver portion and means for orienting said barrel about said centerline in a spherical manner and (d) shock absorbing means lodged in said mount and interposed between said barrel and said mount.
ORIGIN OF THE INVENTION

The invention described herein was made in the performance of official duties by an employee of the Department of the Navy and may be manufactured, used, licensed by or for the Government for any governmental purpose without the payment of any royalty thereon.

US Referenced Citations (5)
Number Name Date Kind
3208178 Seiderman Sep 1965
3783738 Pelat Jan 1974
3877167 Keppler Apr 1975
5613308 Little Mar 1997
5655632 Valembois Aug 1997
Foreign Referenced Citations (3)
Number Date Country
704640 Apr 1941 DE
373517 Nov 1939 IT
86389 Oct 1955 NO