Compact artillery

Information

  • Patent Grant
  • 6571676
  • Patent Number
    6,571,676
  • Date Filed
    Tuesday, December 4, 2001
    22 years ago
  • Date Issued
    Tuesday, June 3, 2003
    21 years ago
Abstract
A gun system has a two piece cannon assembly that is separated between a removable chamber instead of a traditional breech, and a projectile forcing cone. The chamber has a plug at one end that can accommodate any type of ignition system, and the other end is open and is attached to the barrel with a connection fitting. High pressure gases created by combustion of the propellant are sealed with a high-pressure gas compression seal at the interface between the chamber and the barrel. The connection fitting provides an attachment for a rear cannon bearing slide, which rides on rails attached to the main support structure, and also reacts any torque induced into the barrel from the actuation of the chamber/barrel locking collar. A turntable upon which are mounted two chamber elevating/support mechanisms and two projectile loader/rammer mechanisms is positioned around one of the main support structure legs.
Description




BACKGROUND OF THE INVENTION




There is a resurgence of interest in the US Navy in long range artillery as a replacement for missiles due to the cost savings involved. That is, even though the missile launcher is normally cheaper than a gun of similar caliber, each missile is much more expensive than the projectile and propellant for the gun and this soon outweighs the extra cost of the gun system.




To obtain greater range, the gun barrels must be longer or the chamber pressure must be greater. A combination of these two factors, together with optimum projectile design, provides the best opportunity for long range firings. However, the protrusion of the barrel above the deck is vulnerable to detection by enemy radar, hence it is of interest to reduce this to a minimum.




To maximize the length of barrel for a given protrusion of the barrel from the housing module, there should be a minimum of recoiled components behind the chamber/breech, and also, the recoil stroke should be as short as possible. The optimum space utilization is to have only enough room behind the back of the cannon assembly for recoiling. For this to be effected, the chamber must be separated from the barrel to allow for loading of the projectile and charge. This also allows a reduction in time between shots as the charge may be loaded at the same time as the projectile.




The gun described herein embodies the necessary features to allow for compact stowage as well as providing improved performance. A 5 inch caliber smooth bore barrel has been assumed, however the design can be readily scaled up or down.




SUMMARY OF THE INVENTION




The invention provides a gun system that incorporates a two piece cannon assembly that is separated between the chamber and the projectile forcing cone. The gun described has no traditional breech. It has a removable chamber instead which has a plug at one end that can accommodate any type of ignition system that may be required. The other end is open and is attached to the barrel with a connection fitting that is clamped to the barrel by a threaded collar. The high pressure gases created by the propellant combustion are sealed with a high-pressure gas compression seal at the interface between the chamber and the barrel. The lower side of the connection fitting has a locking collar screwed into it. The internal diameter of this locking collar has a bayonet feature or interrupted thread to suit the top end of the chamber. A torque plate, which extends out beyond the edge of the connection fitting, is attached to the lower face of the collar. A slot in the torque plate aligns with the pin of a slide actuator that is attached to a frame cross-member. When the cannon assembly is in battery position, the actuator pin is located inside the torque plate slot.




The connection fitting also provides the attachment for the rear cannon bearing slide which rides on rails attached to the main support structure. This also reacts any torque induced into the barrel from the actuation of the chamber/barrel locking collar.




To provide adequate clearance to the loading mechanism, the recoil cylinders are mounted in front of (above) the chamber/barrel connection fitting. The lower end of the cylinders are attached to the connection fitting. The structure necessary to support the front of the recoil cylinders and hence transmit the recoil force to the main support, provides a suitable mounting for the front barrel slide. The resultant extended “wheelbase” between the front and rear slides ensures improved shot repeatability.




A turntable upon which are mounted two chamber elevating/support mechanisms and two projectile loader/rammer mechanisms is positioned around one of the main support structure legs.











DESCRIPTION OF THE DRAWINGS




The invention and its many attendant objects and advantages will become more clear upon reading the following description of the preferred embodiment in conjunction with a review of the following drawings, wherein:





FIG. 1

is a perspective view of a gun assembly according to this invention;





FIG. 2

is a sectional side elevation of the gun assembly shown in

FIG. 1

;





FIG. 3

is a sectional front elevation of the gun assembly shown in

FIG. 1

;





FIG. 4

is an enlarged sectional elevation of the circled area shown in

FIG. 2

;





FIG. 5

is an enlarged sectional elevation of the circled area in

FIG. 3

;





FIG. 6

is an enlarged sectional elevation of the circled area in

FIG. 4

;





FIG. 7

is a sectional plan view along lines


7





7


in

FIG. 3

;





FIG. 8

is a sectional plan view along lines


8





8


in

FIG. 3

;





FIG. 9

is a sectional elevation of a recoil cylinder and an attached hydraulic schematic diagram of recoil energy recovery system;





FIG. 10

is a sectional elevation of a recoil cylinder configured to provided a self contained counterrecoil force; and





FIG. 11

is an elevation of the barrel shown in

FIG. 1

with the barrel sleeve removed to show cooling channels.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT




Turning now to the drawings, wherein like reference characters identify identical or corresponding parts, and more particularly to

FIGS. 1-3

thereof, a long range artillery cannon


30


is shown having an elongated barrel


32


mounted in a recoil mechanism


34


attached to a main support structure


36


over a chamber shuttle turntable system


38


.




The main support structure


36


includes two legs


40


and a cross head


42


attached to the front or upper end of the legs


40


. The cross head


42


has a central axial opening


44


that receives and guides the barrel


32


during the axial movement of recoil and recovery to battery position. The underside of the cross head


42


has a pair of lugs


46


for connection to the upper ends of piston rods


48


operation in cylinders


49


of the recoil mechanism


34


, as described in more detail below.




The chamber shuttle turntable system


38


has a turntable


50


that rotates around one of the support structure legs


40


, providing two functions. It supports the mechanisms


51


that locate and elevate the two chambers


52


and it also supports the rammer/loader mechanisms


55


that ram projectiles


58


into the barrel. It rotates at the appropriate time of the firing cycle to align a chamber


52


or a loader/rammer


55


with the rear of the barrel.




The attachment of a chamber


52


to the barrel is by means of a rotating locking collar


60


that is screwed into a rear barrel fitting


62


and locates the end of the chamber


52


with either a six-part segmented bayonet connection or interrupted grooves. The preferred configuration is with the interrupted grooves (see

FIG. 4

) as it provides a more even load distribution along the length of the connection and is more compact. It is rotated through the 30° necessary to fully connect by means of hydraulic cylinders


65


acting tangentially (see FIG.


7


). At the same time, axial force is maintained on the chamber by the lifting cylinders


68


(see

FIG. 5

) to ensure adequate seating of a high pressure seal


70


(see FIG.


6


). The hydraulic cylinders


65


that rotate the locking collar


60


are mounted to the static support structure and apply force to the collar


60


by means of a sliding pin


72


engaging with a slot in a torque plate


75


which is attached to the collar


60


(see FIG.


4


). During recoil, the pin


72


(which is non-recoiling) disengages from the slot in the torque plate


75


(which is recoiling) and then re-engages when the barrel returns to battery position. The chamber


52


is disengaged by reversing the above operations.




Sealing of Chamber Section to Barrel




The chamber


52


is designed to be loaded with a rigid combustible propellant charge case


78


incorporating the metallic high pressure sealing ring


70


clipped or molded into its down range end (see FIG.


6


). This sealing ring is therefore replaced at each shot. The sealing function is performed in two ways. The primary method of sealing is via the stub cartridge case thin wall sleeve design at each end of the ring which expands under the effect of the rising gas pressure to contact the barrel/chamber wall during firing. The secondary (back-up) method is via the conical sections of the ring which are compressed during the barrel/chamber connection to produce a seal/tube interface pressure sufficient to seal the gas pressure prior to it rising and energizing the seal. The forward extension of the seal ring also protects the conical barrel surface where the chamber diameter transitions down to the bore diameter and where the potential for gas erosion is at the maximum.




The geometry of the seal


70


, chamber


52


and barrel


32


are selected to ensure the seal


70


stays in the chamber when it is separated from the barrel. Prior to installing a new propelling charge, the old sealing ring


70


is removed and stored or discarded (the remainder of the propellant charge, including the case, having been fully consumed). The design of the sealing ring


70


facilitates easy removal after firing by means of a mechanical claw extractor being inserted into it and then expanded to lock in place. Incorporated with the extractor may be a compressed air supply to blow any dirt particles from the barrel/chamber sealing surfaces prior to insertion of the replacement charge.




Turntable




The turntable


50


is shown in

FIGS. 7 & 8

. The descriptions of the two types of mechanisms mounted to the turntable


50


are as follows:




Turntable chamber elevating/support—There are two alternatives for this attachment and these are as follows:




Alternative 1) A rotating locking collar in the rear barrel fitting-chamber does not rotate. The chamber


52


is located in the elevating/support mechanisms


51


in a non-rotating sliding sleeve


80


which supports it in between shots as well as guides it whilst being raised by hydraulic cylinders to mate with the rear face of the barrel. At the base of the chamber are castellated features


82


. At the base of the sliding sleeve is a rotating support ring which has a castellated internal diameter and is hydraulically actuated. The chamber castellations rest on the ring castellations whilst the chamber is being raised into position or is in the rest position between shots. After the chamber is attached to the barrel by means of the locking collar, the support ring is rotated such that the castellations are now out of phase with each other, thereby allowing the chamber clearance to recoil through the ring.




Alternative 2) The chamber section is rotated. An alternative method of effecting the connection between the chamber and the barrel is to directly mate the chamber to the connection fitting, instead of via a locking ring, by means of bayonet features or interrupted threads. The joint is then tightened by rotating the chamber. The high pressure seal may be compressed by either the action of the chamber torque resulting in axial force via the interrupted threads or helical profile on the bayonet interface, or more directly, by the hydraulic cylinders which raise and lower the chamber. The disadvantage of this method is that the acceleration/deceleration forces involved in rotating a heavy object such as the chamber requires additional support structure, energy input and time. This may be objectionable for high firing rates.




Turntable projectile loader/rammer—Projectiles are introduced into a support tube


84


of the loader/rammer


55


by means of a handling system (not described herein). Parallel to and alongside the support tube is a hydraulic cylinder


86


that has an arm


88


extending under the projectile base. This causes the projectile to be rammed into the lower end of the barrel such that a seal


90


on the projectile


58


is compressed into the barrel forcing cone. This keeps the projectile


58


from falling back down into the support tube when the loader/rammer


55


is withdrawn.




Cooling




The gun described herein has been designed with integrated active cooling. This is not a requirement of the overall design but does permit higher rates of fire by removing the heat from the areas where it is mainly generated, i.e., the barrel


32


, the chamber


52


, and recoil cylinders. The sketches show a thin wall sleeve


92


shrunk fitted around the barrel


32


. The barrel has axial grooves


95


machined in its exterior (see FIG.


11


). The assembly of the sleeve to the barrel creates passageways that contain the cooling fluid. The front barrel slide acts as the interface at which the cooling fluid is introduced and evacuated from the barrel.




Due to the fact that the chamber


52


is passed from one support medium to another, a continuous cooling fluid connection cannot be maintained to it. Hence coolant only flows when the chamber has been returned to its mount on the turntable and interfaces with the coolant connections (see FIGS.


5


and


7


). The duration which coolant flows to the chamber is slightly less than two shots.




The recoil cylinders


49


can either be wrapped with cooling jackets or, in the case of the energy recovery configuration, the fluid can be cooled during its passage to the external accumulators as described below.




Recoil




The most efficient and most common method of absorbing recoil energy is via the throttling of hydraulic fluid. Traditional recoil cylinder configurations can be adapted to function satisfactorily. However, if a traditional recoil cylinder is used, a counterrecoil cylinder is also required to return the gun to the battery position.




The following configuration has a counterrecoil as well as a recoil function and also provides the ability to extract hydraulic fluid energy from the recoil stroke which can be used to supplement overall system energy requirements to power functions such as breech locking and ammunition loading mechanism actuation. Where it is used for energy recovery, the removal of fluid during each recoil cycle also facilitates cooling via a heat exchanger. The fluid which has been heated by absorbing recoil energy is replaced with cool fluid from an external low pressure accumulator for each shot (see explanation below and hydraulic schematic). The recoil cylinder design and the hydraulic schematic for energy recovery is shown in FIG.


9


. Counterrecoil snubbing can be easily incorporated internally into this cylinder design.




Recoil energy recovery—The recoil cylinder


49


can be configured, together with an external high-pressure accumulator


97


and low pressure accumulator


99


, to recover hydraulic energy. During recoil, the barrel's imparted energy is absorbed by the throttling of the hydraulic fluid through the varying orifice produced between the outside of a recoil piston


100


and the bore of the cylinder extension


102


. The diameter of the bore


104


is varied along length thereof to ensure a constant and hence a minimum recoil force. This fluid is then forced through a check valve


106


where some energy is also absorbed by the compression of the nitrogen gas behind a floating piston


108


in the energy recovery accumulator inside the piston


100


. This gas volume is supplemented by an exterior gas cylinder


110


to minimize the gas pressure increase when it is compressed by the displaced recoil fluid. After recoil, stored energy, in the form of the pressurized fluid is transferred from the energy recovery accumulator to the high-pressure external accumulator


97


. Should this accumulator be fully charged, surplus fluid is dumped to the low pressure accumulator


99


via a bypass valve. The low-pressure external accumulator also provides the fluid pressure required to produce the retraction force in the cylinder to return the system to battery position. A high-pressure boost pump


112


is incorporated in the circuit to make up the difference between the hydraulic energy required for operation of all the systems and that which is supplied by the energy recovery. Pressure transducers


114


are placed appropriately in the system to ensure fail safe operation.




No energy recovery—Should energy recovery not be required, the recoil cylinder can also be simply configured to provided a self contained counterrecoil force using the integral floating piston


100


and compressed gas to retract the cylinder after recoiling—see FIG.


10


. After recoiling as described above, the compressed fluid passes back to the recoil chamber past the check valve and piston via an orifice. This produces the retraction force in the cylinder required to return the system to battery position. Cooling can be provided by an external water jacket around the cylinder.




In both cases, the cylinder rod


48


is attached to the gun support structure


42


and the cylinder


49


is attached to the recoiling components. This facilitates connections from the recoil piston to the exterior components for the two oil lines and one gas line necessary per cylinder and also permits bleeding of the system at the highest point.




The design of the recoil cylinder incorporates common existing technology and can therefore be designed for reliability. Also, the attachments to the support structure provide for very simple and quick replacement.




Stowage




Weapon stowage may be simply compacted by retracting the barrel the full recoil distance. This is achieved by pumping fluid out of the recoil cylinder and into a separate storage volume. Further retraction is possible by either a longer recoil cylinder or detachment of the recoil cylinder at one end and a separate system to raise and lower the weapon. In this case the chamber is detached from the barrel in the normal manner and the carousel rotated to an intermediate position to allow for clearance of the rear barrel connection fitting when retracted.




Maintenance




The most common major maintenance item is replacement of the barrel after it has developed unacceptable wear. Replacement is a relatively simple process, involving the removal of the front bearing slide and unscrewing the threaded retaining ring at the breech end. The tube can then be withdrawn through the hole in the front support structure.




Features, Advantages and Benefits

















Features




Advantages




Benefits




























1.0




The cannon is




1.1




The length of




1.1.1




Manufacturing -







separated between





barrel becomes





This assists the







the chamber and





shorter for a





manufacturing







projectile seat.





given cannon





process in a









assembly length.





number of ways.











During











manufacture, the











difficulty is











increased as the











length of











component











increases. This











applies to the











forging, heat











treatment,











exterior











machining,











interior boring











and autofrettage











processes. A











shorter barrel











would reduce











manufacturing











costs by











permitting











simpler











manufacturing











techniques.










1.1.2




Transportation -











A shorter barrel











permits trans-











portation of all











components in a











shorter container,











allowing deploy-











ment by smaller











vehicles/vessels.










1.1.3




Stowage - The











barrel may be











retracted during











stowage down to











the level of the











chamber inter-











face, thereby











reducing radar











signature.











Alternatively,











with the chamber











moved aside, the











barrel may be











retracted down to











the level of the











base of the gun











mount area,











further











reducing radar











signature.








1.2




Easy access to




1.2.1




Cleaning - Easier









the forcing cone





cleaning, and









area.





inspection of the











seal area during











operation.










1.2.2




Cooling -











Forced-air











cooling is











possible of both











the chamber and











forcing cone











areas.








1.3




A separate




1.3.1




Flexibility -









chamber and





This enables









barrel permits





many different









many variations





projectile/









of each to be





propellant









fitted to the





combinations to









same mount.





be fired.










1.3.2




Optimum material











selection - The











material used in











the manufacture











of a separate











barrel and











chamber can be











different and











specifically











selected to











suit their











particular











operational











requirements.








1.4




A separate barrel




1.4.1




Wear specific









allows for easy





components - The









replacement





barrel is the









during service.





primary part of a











gun that suffers











from wear.











The majority of











the other











components are











not replaced until











their fatigue lives











are reached.










1.4.2




Time saving -











Simplifying











replacement











reduces time out











of commission.






2.0




The chamber and




2.1




This allows




2.1.1




Compressed time







projectile loader/





simultaneous





budget - The gun







rammer are





loading of





can be fired at a







duplicated and





propellant in one





higher rate as it







positioned on a





chamber while





permits parallel







turntable such





the other is





functioning. Ie.,







that each of the





being attached to





The used metallic







chambers and





the gun for firing.





gas seal can be







each of the





This also applies





removed and the







loader/rammers





to the two





next round of







align with the





rammer/loader





propellant can be







barrel when the





stations that are





loaded into one







turntable is





positioned in





chamber while







indexed.





between the two





the other is being









chamber mounts.





attached to the











rear of the barrel.











Also, the next











projectile can











be positioned in











the loader/rammer











at the same time











as the other is











rammed, etc.










2.2.2




Fault bypass -











Should a fault











occur in any one











of the two











projectile











rammer/loaders or











chamber stations,











the gun can











continue firing











(albeit at a lower











rate) using the











remaining func-











tioning station.










2.2.3




Facilitate











cooling - The











chamber has











additional time











to cool in











between shots.






3.0




The connection




3.1




Protects transition




3.1.1




Increased barrel







between the





area between





life.







chamber and





chamber and




3.2.1




Reduced handling







barrel is protected





forcing cone from





requirements







by a short





effects of





when removing







metallic sleeve/





propellant gas





after shot.







seal. This is




3.2




Smaller than




3.3.1




More compact -







attached to the





cartridge case





A large diameter







rigid combustible




3.3




Permits a larger





chamber is bene-







cartridge case and





ratio of chamber





ficial as it reduces







is hence replaced





diameter to





the chamber







with each shot.





projectile





length for a given









diameter (the





volume, thereby









erosion effects





reducing the









in the transition





overall length of









area from





the gun. This in









propellant gas





turn reduces the









become more





amount of barrel









destructive as the





protrusion above









ratio increases).





deck.










3.3.2




Safer ignition -











Simplifies











obtaining efficient











and safe











propellant











ignition.











As the ratio of











L/D increases, so











does the difficulty











in ensuring even











ignition of the











propellant.






4.0




Accessible recoil




4.1




Easily replaceable




4.1.1




Time saving -







cylinders







Out of











commission time











reduced.










4.1.2




Performance











matching -











Different recoil











characteristics











may be incor-











porated for











different barrel/











chamber











combinations.














Method of Operation




The configuration of the gun with the turntable mounted chambers and loader/rammers permits some operations to be done in parallel. This facilitates a faster firing rate. The following table clarifies the operations during one complete firing cycle, starting from the recoil stroke.



















OPERATIONS DONE






OP #




FIRING CYCLE TIME BUDGET (GUN)




IN PARALLEL











1




RECOIL







2




COUNTERRECOIL






3




ROTATE CHAMBER SUPPORT RING







TO SUPPORT POSITION






4




UNLOAD CHAMBER #1 LOCK RING






5




UNLOCK CHAMBER #1 FROM







BARREL






6




LOWER CHAMBER #1






7




ROTATE CAROUSEL TO PROJECTILE




CONNECT COOL-







LOAD POSITION




ING TO CHAMBER








#1






8




RAM PROJECTILE INTO BARREL




REMOVE








CHAMBER #1








SEAL & CLEAN






9




RETRACT RAMMER




DISCONNECT








COOLING TO








CHAMBER #2






10 




ROTATE CAROUSEL







TO PROPELLANT







LOAD POSITION






11 




RAISE CHAMBER #2 TO BARREL




REPLENISH








CHAMBER #1 &








PROJECTILE TUBE






12 




LOCK CHAMBER #2 TO BARREL






13 




UNLOAD CHAMBER #2







SUPPORT RING






14 




ROTATE SUPPORT RING TO RECOIL







POSITION






15 




FIRE














Obviously, numerous modifications and variations of the preferred embodiment described above are possible and will become apparent to those skilled in the art in light of this specification. Moreover, many functions and advantages are described for the preferred embodiment, but in many uses of the invention, not all of these functions and advantages would be needed. Therefore, we contemplate the use of the invention using fewer than the complete set of noted features, process steps, benefits, functions and advantages. Moreover, several species and embodiments of the invention are disclosed herein, but not all are specifically claimed, although all are covered by generic claims. Nevertheless, it is our intention that each and every one of these species and embodiments, and the equivalents thereof, be encompassed and protected within the scope of the following claims, and no dedication to the public is intended by virtue of the lack of claims specific to any individual species. Accordingly, it is expressly intended that all these embodiments, species, modifications and variations, and the equivalents thereof, in all their combinations, are to be considered within the spirit and scope of the invention as defined in the following claims, wherein



Claims
  • 1. A gun assembly, comprising:a gun barrel and a separable chamber; said separable chamber includes a plug at one end that accommodates a propellant ignition system; said separable chamber having an open end opposite said one end, said open end having interrupted threads or bayonet fittings for connection to said barrel by way of rotating locking collar; a connection fitting having a continuous internal thread for threadedly engaging continuous external threads on said locking collar; said locking collar has internal bayonet features or interrupted thread to engage said interrupted threads or bayonet fittings at said open end of said chamber; a torque plate attached to a lower face of said collar and extending radially beyond said connection fitting; a slot in said torque plate aligned with a pin of a slide actuator attached to a frame cross-member; whereby said actuator pin is located inside the torque plate slot when said gun assembly is in a battery position and is disengaged from said slot during recoil to disengage said chamber from said barrel during recoil.
  • 2. A gun assembly as defined in claim 1, further comprising:a projectile propellant canister for use in said gun assembly having a consumable casing and a high pressure gas seal at an outer end thereof for providing a gas seal at the interface between said open end of said chamber and said gun barrel; whereby high pressure gases created by propellant combustion are sealed with said high-pressure gas compression seal at said interface between said chamber and said barrel.
  • 3. A gun assembly as defined in claim 1, further comprising:said connection fitting has an attachment for a rear cannon bearing slide which rides on rails attached to a main support structure; whereby any torque induced into said barrel from the actuation of said chamber/barrel is reacted into said locking collar.
  • 4. A gun assembly as defined in claim 1, further comprising:recoil cylinders mounted in front of said chamber/barrel connection fitting; said recoil cylinders having pistons with piston rods attached to said connection fitting; said recoil cylinders having front ends connected to a main gun support to support the front of said recoil cylinders and transmit recoil forces generated when said gun fires to said main support; whereby an extended “wheelbase” between the front and rear slides ensures improved shot repeatability.
  • 5. A gun assembly as defined in claim 1, further comprising:a turntable upon which are mounted two chamber elevating/support mechanisms and two projectile loader/rammer mechanisms is positioned around one of said main support structure legs.
Parent Case Info

This relates to U.S. Provisional Application 60/251,349 filed on Dec. 4, 2000. This invention pertains to long range artillery, and more particularly to artillery having a low profile and improved performance.

US Referenced Citations (8)
Number Name Date Kind
1234575 Schneider Jul 1917 A
1393057 Vollmer Oct 1921 A
2807195 Musser Sep 1957 A
2922338 Barbe Jan 1960 A
3755948 Heinicke Sep 1973 A
3877167 Keppeler Apr 1975 A
4690032 Stoner Sep 1987 A
5837920 Staiert et al. Nov 1998 A
Provisional Applications (1)
Number Date Country
60/251349 Dec 2000 US