CONFIGURABLE WEAPON STATION HAVING UNDER ARMOR RELOAD

Abstract

A vehicle-mounted weapon station is configurable to adjust the height of a rotational elevation axis thereof. The weapon station is provided with at least one fixed hanging ammunition container that is reloadable under the armored protection of the vehicle and the weapon station shell. The weapon station may have both electrically-powered and manually-powered drive systems for rotating a pedestal about an azimuth axis relative to the vehicle, and for rotating weaponry and operational units about the elevation axis, wherein the electrical and manual drive systems transmit power through the same output gear.

Claims

1-11. (canceled)

12. An electromechanical assembly comprising: a rotary interface defined by a first element and a second element, wherein the second element is rotatable about an main axis relative to the first element; a slip ring configured to transmit power and data across the rotary interface, the slip ring including a passageway extending through the slip ring across the rotary interface; and a first drive train having an input end, an output end, and a drive shaft between the input end and the output end, wherein the input end and output end are on opposite sides of the rotary interface and the drive shaft extends through the passageway; wherein the drive shaft is rotatable about a drive axis by applying torque to the input end of the first drive train, and the output end of the first drive train is driven by rotation of the drive shaft about the drive axis

13. The electromechanical assembly according to claim 12, wherein the output end of the drive train is drivably coupled to the second element to cause the second element to rotate relative to the first element by applying torque to the input end of the drive train.

14. The electromechanical assembly according to claim 12, further comprising at least one additional drive train having a corresponding drive shaft extending through the passageway.

15. The electromechanical assembly according to claim 12, wherein the drive shaft of the at least one additional drive train is coaxial with the drive shaft of the first drive train.

16. The electromechanical assembly according to claim 12, wherein the drive axis coincides with the main axis.

17. The electromechanical assembly according to claim 12, wherein the input end of the first drive train includes a crank handle connected to the drive shaft and manually operable to rotate the drive shaft.

18. The electromechanical assembly according to claim 17, wherein the output end of the first drive train is connected to a drive gear, wherein operation of the crank handle to rotate the drive shaft causes rotation of the drive gear.

19. A manned weapon station apparatus comprising: a pedestal adapted to be mounted on an armored vehicle for rotation relative to the armored vehicle about an azimuth axis; a yoke assembly carried by the pedestal, the yoke assembly being adapted to support at least one weapon for rotation relative to the pedestal about an elevation axis, the yoke assembly including a pair of laterally-spaced elevation yoke arms extending upward from the pedestal; and a personnel support platform suspended from the pedestal for rotation with the pedestal about the azimuth axis.

20. The manned weapon station apparatus according to claim 19, further comprising a slip ring configured to transmit power and data across a rotary interface between the pedestal and the armored vehicle, wherein the slip ring is mounted to the personnel support platform.

21. The manned weapon station apparatus according to claim 19, wherein the personnel support platform is suspended from the pedestal by at least one vertical structural member, and the manned weapon station apparatus further comprises a weapon control unit mounted on the at least one structural member.

22. The manned weapon station apparatus according to claim 19, wherein the personnel support platform is suspended from the pedestal by at least one vertical structural member, and the manned weapon station apparatus further comprises a seat mounted on the at least one structural member.

23. The manned weapon station apparatus according to claim 19, further comprising a periscope allowing a person within an interior compartment defined by the pedestal to view external objects.

24. The manned weapon station apparatus according to claim 19, wherein the pedestal includes a personnel hatch located between the pair of elevation yoke arms.

25. The manned weapon station apparatus according to claim 24, wherein the personnel hatch is hingedly mounted on the pedestal.

26. The manned weapon station apparatus according to claim 24, wherein the personnel hatch is slidably mounted on the pedestal.

27. The manned weapon station apparatus according to claim 24, wherein the personnel hatch is inclined relative to horizontal.

28. A cradle for supporting at least one weapon between a pair of yoke arms for rotation about an elevation axis, each of the pair of yoke arms including a respective hub rotatable about the elevation axis, wherein the cradle comprises: a pair of laterally-spaced mounting braces configured for respective removable attachment to the hubs of the pair of yoke arms; a support platform extending between the pair of mounting braces, wherein the support platform extends in a plane parallel to and offset from the elevation axis; wherein the support platform includes a first under-weapon mounting area upon which a weapon may be seated, the first under-weapon mounting area having an access opening; wherein the support platform includes an over-weapon mounting area from which a weapon may be suspended; wherein the cradle is attachable to the hubs in a first orientation such that the plane of the support platform is below the elevation axis for seating a weapon in the first under-weapon mounting area; wherein the cradle is attachable to the hubs in a second orientation such that the plane of the support platform is above the elevation axis for suspending a weapon from the over-weapon mounting area.

29. The cradle according to claim 28, wherein the support platform further includes a second under-weapon mounting area upon which a weapon may be seated, the second under-weapon mounting area having a corresponding access opening.

30. The cradle according to claim 29, wherein the over-weapon mounting area is between the access opening of the first under-weapon mounting area and the access opening of the second under-weapon mounting area.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0019] The nature and mode of operation of the present invention will now be more fully described in the following detailed description of the invention taken with the accompanying drawing figures, in which:

[0020] FIG. 1 is a perspective view of an RWS formed in accordance with an embodiment of the present invention, without any weapons or operational units installed thereon;

[0021] FIG. 2 is another perspective view of the RWS shown in FIG. 1, wherein the RWS is shown equipped with a central weapon cradle;

[0022] FIG. 3 is a further perspective view of the RWS shown in FIG. 1, viewing from underneath the RWS;

[0023] FIG. 4 is an exploded perspective view of the RWS shown in FIG. 1;

[0024] FIG. 5 is a perspective view of the RWS shown in FIG. 1, wherein a first pair of elevation yoke arms of the RWS has been replaced with a second, taller pair of yoke arms, and the RWS is shown equipped with a lateral weapon cradle;

[0025] FIG. 6 is another perspective view of the RWS shown in FIG. 5;

[0026] FIG. 7 is an exploded perspective view of an elevation yoke arm of the RWS shown in FIG. 5;

[0027] FIGS. 8-10 depict examples of various weapon configurations of the RWS as shown in FIG. 1, wherein shorter yoke arms are installed;

[0028] FIGS. 11-14 depict examples of various weapon configurations of the RWS as shown in FIG. 5, wherein taller yoke arms are installed;

[0029] FIG. 15 is a perspective view looking upward toward an inner compartment of the RWS pedestal, wherein a base plate of the pedestal and other structure are hidden to more clearly show ammunition containers of the RWS;

[0030] FIG. 16 is another perspective view looking upward toward an inner compartment of the RWS pedestal, wherein a slip ring of the RWS is hidden to more clearly show ammunition containers of the RWS;

[0031] FIG. 17 is a perspective view of an empty ammunition container of the RWS; and

[0032] FIG. 18 is a cross-sectional view of the ammunition container shown in FIG. 17, wherein the ammunition container is loaded with an ammunition belt.

[0033] FIG. 19 is an exploded perspective view of an RWS formed in accordance with another embodiment of the present invention, without any weapons or operational units installed thereon;

[0034] FIG. 20 is a perspective view of the RWS shown in FIG. 19 in a short configuration thereof;

[0035] FIG. 21 is a perspective view of the RWS shown in FIG. 19 in a tall configuration thereof;

[0036] FIG. 22 is a top plan view of a pedestal of the RWS shown in FIG. 19;

[0037] FIG. 23 is a perspective view of the RWS shown in FIG. 19 in its short configuration with weaponry and operational units mounted thereon;

[0038] FIG. 24 is a perspective view of the RWS shown in FIG. 19 in its tall configuration with weaponry and operational units mounted thereon;

[0039] FIG. 25 is a perspective view showing a drive system of the RWS shown in FIG. 19;

[0040] FIG. 26 is a bottom plan view of the drive system shown in FIG. 25;

[0041] FIG. 27 is a top perspective view of an alternative drive system incorporating a manual drive train;

[0042] FIG. 28 is a bottom perspective view of the alternative drive system shown in FIG. 27;

[0043] FIG. 29 is a bottom plan view of the alternative drive system shown in FIG. 27, wherein linkage arm covers are removed to reveal internal transmission structure;

[0044] FIG. 30 is a cross-sectioned perspective view of a slip ring and a portion of the manual drive train of the alternative drive system;

[0045] FIG. 31 is a perspective view of a manned weapon station formed in accordance with a further embodiment of the present invention, wherein the manned weapon station is based on the RWS shown in FIG. 19;

[0046] FIG. 32 is another perspective view of the manned weapon station shown in FIG. 31;

[0047] FIG. 33 is a perspective view of a weapon support cradle usable in an RWS of the present invention, wherein the cradle is shown in its non-inverted orientation;

[0048] FIG. 34 is a perspective view of the weapon support cradle shown in FIG. 33, wherein the cradle is shown in its inverted orientation;

[0049] FIG. 35 is a view similar to that of FIG. 33, wherein the non-inverted cradle is shown supporting weaponry seated upon a platform of the cradle;

[0050] FIG. 36 is perspective view of the weapon support cradle and weaponry shown in Fig. D3 as viewed from underneath the weapon support cradle; and

[0051] FIG. 37 is a view similar to that of FIG. 34, wherein the inverted cradle is shown supporting weaponry suspended from the cradle platform.

DETAILED DESCRIPTION OF THE INVENTION

[0052] FIGS. 1-4 depict a remote weapon station (RWS) 10 formed in accordance with an embodiment of the present invention, wherein RWS 10 is shown without any weapons, weapon cradles, or other operational units mounted thereon. RWS 10 generally comprises a base or pedestal 12 and a weapon support yoke 14 definable by a first pair of elevation yoke arms 14A, 14B. As will be understood by those skilled in the art, pedestal 12 is adapted to be mounted on an armored vehicle (not shown) so as to cover a hatch opening in a top deck of the armored vehicle and be rotatable relative to the armored vehicle about an azimuth axis AZ. For this purpose, pedestal 12 may include a base plate 16 to which an outer rotary bearing race 18 is attached, and a corresponding inner rotary bearing race 20 mountable to the armored vehicle. For example, inner race 20 may be bolted onto the top deck of the armored vehicle. Pedestal 12 further includes an armored shell 22 coupled to base plate 16. As seen in FIG. 3, pedestal 12 defines an interior compartment 24 that is accessible from within the armored vehicle. Shell 22 may include a pair of lateral hatches 23 at opposite lateral sides of pedestal 12, a pair of front hatches 25 at a front end of the pedestal, and/or a topside hatch 27.

[0053] Rotation of pedestal 12 about azimuth axis AZ may be driven by an azimuth drive assembly 26 fixed to an interior wall of shell 22. Azimuth drive assembly 26 includes a motor-driven output gear 28 meshing with inner gear teeth 30 of inner race 20. Azimuth drive assembly 26 may be commanded through an operator interface and control electronics (not shown) to control the angular position of pedestal 12 about azimuth axis AZ relative to the armored vehicle. A slip ring assembly 32 provides signal transmission to and from azimuth drive assembly 26 and other electronic units in pedestal 12 across the rotational interface.

[0054] In accordance with an aspect of the present invention, pedestal 12 includes a pair of laterally-spaced yoke arm attachment interfaces 34 for removable mounting of elevation yoke arms 14A, 14B. In the illustrated embodiment, each yoke arm attachment interface 34 includes a flat surface 36 on the exterior of shell 22, a plurality bolt holes 38 registering with bolt holes 40 on the corresponding yoke arm 14A, 14B, and a central opening 42 communicating with pedestal interior compartment 24. The pair of elevation yoke arms 14A, 14B are removably mounted on the pair of yoke arm attachment interfaces 34 using threaded fasteners 44 extending through aligned holes 38, 40. As a result, elevation yoke arms 14A, 14B move with pedestal 12 as the pedestal rotates about azimuth axis AZ. As shown in the depicted embodiment, topside hatch 27 may be located between the pair of yoke arm attachment interfaces 34, and may be inclined relative to attachment interfaces 34 so that spent ammunition casings slide down and do not accumulate on the topside hatch. RWS 10 includes a pair of elevation rotary bearings 46A, 46B respectively supported by elevation yoke arms 14A, 14B. Elevation rotary bearings 46A, 46B are aligned with each other to define a rotational elevation axis EL at a first height H1 above pedestal 12.

[0055] Reference is also made now to FIGS. 5-7. Apparatus for RWS 10 comprises a second pair of elevation yoke arms 14C, 14D configured for removable mounting on the pair of yoke arm attachment interfaces 34 of pedestal 12 for movement with the pedestal. The second pair of elevation yoke arms 14C, 14D are taller than the first pair of yoke arms 14A, 14B and can be selectively swapped with the first pair of elevation yoke arms 14A, 14B to support the pair of elevation rotary bearings 46A, 46B at a second height H2 above the pedestal greater than the first height Hl. In this manner, elevation axis EL is height-adjustable for replacing a mounted primary weapon with a different primary weapon.

[0056] As may be understood from FIGS. 4 and 7, RWS 10 additionally comprises an elevation drive motor 48 and an elevation drive hub 50 connected to the elevation drive motor 48 and supported by elevation rotary bearing 46A, wherein elevation drive hub 50 is rotatable about elevation axis EL by operation of elevation drive motor 48. Elevation drive motor 48 may be housed within the elevation yoke arm that houses drive hub 50 to keep drive motor 48 near drive hub 50 and reduce complexity of a connecting drive train assembly, however drive motor 48 may be located outside of the yoke arm without straying from the invention.

[0057] RWS 10 also comprises an elevation follower hub 52 supported by elevation rotary bearing 46B. Elevation drive hub 50 and elevation follower hub 52 are configured for removable mounting of at least one primary weapon thereto such that the primary weapon resides between the mounted pair of elevation yoke arms 14A, 14B or 14C, 14D and is rotatable about elevation axis EL by operation elevation drive motor 48. For example, hubs 50 and 52 may each include a bolt hole array used to removably mount a weapon cradle 56 (shown in FIG. 2) or to directly mount a primary weapon housing thereto. Weapon cradle 56 may be designed to support more than one weapon.

[0058] RWS 10 may further comprise a lateral hub 58 connected to elevation drive motor 48, wherein the lateral hub 58 is rotatable about elevation axis EL by operation of elevation drive motor 48. Lateral hub 58 is configured for removable mounting of a secondary weapon thereto, either directly or through a secondary or lateral weapon cradle 60, such that the mounted secondary weapon is rotatable about elevation axis EL by operation of the elevation drive motor 48.

[0059] Referring again to FIG. 4, RWS 10 may also comprise a sighting hub 62 and a corresponding sighting drive motor 64. In the embodiment shown, sighting hub 62 is supported by the same yoke arm (either 14 B or 14D) as elevation follower hub 52 for rotation about elevation axis EL. Sighting hub 62 is configured for removable mounting of a sighting unit thereto. Sighting hub 62 is rotatable about elevation axis EL by operation of sighting drive motor 64. Sighting drive motor 64 is operable independently of elevation drive motor 48, whereby sighting hub 62 and a mounted sighting unit are rotatable about the elevation axis EL independently of elevation drive hub 50 and any equipment or weapons mounted to drive hub 50.

[0060] Attention is now directed to FIGS. 4 and 7. In an aspect of the present invention, the second pair of elevation yoke arms 14C, 14D may be structurally similar to the first pair of elevation yoke arms 14A, 14B. When mounted to pedestal 12, each yoke arm 14A-14D includes a respective base 66S or 66T and a respective cap 68 removably attachable onto base 66. In the embodiment shown by the figures, the yoke arm bases 66T (tall) of the second pair of elevation yoke arms 14C, 14D are taller than the yoke arm bases 66S (short) of the first pair of elevation yoke arms 14A, 14B. Each base 66S or 66T is adapted for removable mounting to one of the yoke arm attachment interfaces 34 of pedestal 12. For example, each yoke arm base 66S or 66T may include bolt holes 40 registering with the bolt holes 38 of an associated yoke arm attachment interface 34. Caps 68 for yoke arms 14C, 14D may be identical to caps 68 for yoke arms 14A, 14B, or at least they may fit onto yoke arms 14A, 14B. Thus, the overall apparatus may require only a single pair of caps 68 for installation on the two bases 66 of the particular pair of yoke arms that currently mounted on pedestal 12 at a given time; the yoke arm bases 66S or 66T not in use at a given time do not require caps 68.

[0061] When RWS 10 is configured with taller yoke arms 14C, 14D, the overall height of the armored vehicle may prevent it from passing through locations where there are overhead obstructions. In order to temporarily lower the overall profile height of the armored vehicle, pedestal 12 may further include a pair of yoke arm pivot interfaces 70 spaced from the pair of yoke arm attachment interfaces 34, and the yoke arm bases 66T of the second pair of yoke arms 14C, 14D may include a pivot coupling 72 configured to mate with a corresponding pivot interface 70 of pedestal 12. For example, pivot interfaces 70 may have a pair of aligned circular pivot apertures 74 with which another pair of pivot apertures 76 in base 66T may be aligned, and a pair of pivot covers 78 securable into the aligned pivot apertures 74, 76. As a result, the second pair of yoke arms 14C, 14D may be pivoted relative to pedestal 12 when they are situated on, but not fixed to, yoke arm attachment interfaces 34. In this way, the armored vehicle can be provided with a lower profile for travel. The yoke arm pivot interfaces 70 may define a yoke arm pivot axis PA parallel to and behind elevation axis EL.

[0062] Changeover between the first pair of yoke arms 14A, 14B and the second pair of yoke arms 14C, 14D may be carried out by unbolting yoke arm caps 68 from the mounted yoke arm bases, removing the assembled bearings, hubs, and any drive motors housed by the mounted yoke arms, and unbolting the mounted yoke arm bases 66 from yoke arm attachment interfaces 34. The yoke arm bases 66 of the other pair of yoke arms are then bolted to the yoke arm attachment interfaces 34, the drive assemblies are reinstalled and aligned in the newly mounted yoke arm bases 66, and the caps 68 are bolted onto the newly mounted yoke arm bases 66. Transferring the same drive assemblies and bearings between the short and tall yoke arms avoids hardware cost and reduces the amount of additional hardware that must be stocked. It is also contemplated to provide dedicated drive assemblies within each yoke arm 14A-14D so that removal and replacement of the drive assemblies is not necessary. As will be appreciated, changeover may be accomplished quickly by trained mechanics at a military base, whereby the same armored vehicle may have one RWS configuration one day and a different RWS configuration the next.

[0063] FIGS. 8-10 illustrate various examples of weapon configurations of RWS 10 when the shorter pair of yoke arms 14A, 14B is installed on pedestal 12.

[0064] In FIG. 8, there is central weapon cradle 56 mounted between drive hub 50 and follower hub 52, and an M134 machine gun 100 mounted on central weapon cradle 56 as a primary weapon. A non-lethal equipment cradle 61 is coupled to lateral hub 58 and carries an acoustic hailer 102, an illuminator 104, and a grenade launcher 106. A sighting unit 108 is mounted on the opposite side of the RWS to sighting hub 62.

[0065] The configuration shown in FIG. 9 includes central weapon cradle 56 mounted between drive hub 50 and follower hub 52 to support an MK19 automatic grenade launcher 110 and an M2 machine gun 112. A javelin mount 114 is attached to lateral hub 58 and supports a javelin missile launcher 116. Sighting unit 108 is mounted on sighting hub 62.

[0066] As may be understood from FIGS. 8-9 and FIGS. 33-37, central weapon cradle 56 may be mounted to drive hub 50 and follower hub 52 in a non-inverted orientation (see FIGS. 9, 33, 35, and 36) and in an inverted orientation (see FIGS. 8, 34, and 37). Invertible cradle 56 comprises a pair of laterally-spaced mounting braces 56A, 56B configured for respective removable attachment to hubs 50, 52, and a support platform 56C extending between the pair of mounting braces 56A, 56B. Support platform 56C extends in a plane parallel to and offset from elevation axis EL. In the embodiment shown, support platform 56C includes a first under-weapon mounting area 57A upon which a weapon may be seated when cradle 56 is mounted in its non-inverted orientation, wherein the first under-weapon mounting area has an access opening 59A. Support platform 56C may further include a second under-weapon mounting area 57B upon which another weapon may be seated when cradle 56 is mounted in its non-inverted orientation, wherein the second under-weapon mounting area 57B has a corresponding access opening 59B. Access openings 59A and 59B are positioned and sized to allow spent ammunition casings to drop down away from the weapon mounted above. Support platform 56C also includes an over-weapon mounting area 57C from which a weapon may be suspended. In the embodiment shown, over-weapon mounting area 57C is between access openings 59A, 59B. When cradle 56 is mounted to hubs 50, 52 in its non-inverted orientation, the plane of support platform 56C is below elevation axis EL for seating a weapon in the first under-weapon mounting area 57A and/or in the second under-weapon mounting area 57B. When cradle 56 is mounted to hubs 50, 52 in its inverted orientation, the plane of support platform 56C is above elevation axis EL for suspending a weapon from the over-weapon mounting area 57C.

[0067] In FIG. 10, a TOW missile launcher 118 has a hub bracket for direct mounting to drive hub 50 and follower hub 52. Lateral cradle 60 supports an M240 machine gun 120. Sighting unit 108 is mounted on sighting hub 62.

[0068] FIGS. 11-14 show examples of other weapon configurations of RWS 10 when the taller pair of yoke arms 14C, 14D is installed on pedestal 12 replacing shorter yoke arms 14A, 14B.

[0069] In FIG. 11, a hellfire missile launch pod 122 has a hub bracket for direct mounting to drive hub 50 and follower hub 52. Lateral cradle 60 supports M240 machine gun 120. Again, sighting unit 108 is mounted on sighting hub 62.

[0070] The configuration of FIG. 12 is similar to that of FIG. 11, except the hellfire pod is replaced by an M230LF cradle 124 coupled to hubs 50 and 52 that carries an M230LF autocannon 126.

[0071] In FIG. 13, a pair of 30 mm ammunition boxes 128 are associated with opposite lateral sides of RWS 10, and an MK44 chain gun assembly 130 is mounted to hubs 50 and 52 as the primary weapon. Lateral cradle 60 supports M240 machine gun 120, and sighting unit 108 is mounted on sighting hub 62.

[0072] FIG. 14 shows TOW missile launcher 118 directly mounted to hubs 50 and 52 as the primary weapon. Lateral cradle 60 supports M240 machine gun 120, and sighting unit 108 is mounted on sighting hub 62.

[0073] The configurations shown in FIGS. 8 through 14 are intended as non-limiting examples. Of course, many other configurations involving other weapons and equipment are possible.

[0074] In another aspect of the present invention, RWS 10 enables reloading of ammunition under the armored protection of the vehicle and pedestal 12 without using space within the vehicle compartment and without the need for a conveyor mechanism. As best seen in FIGS. 15-18, RWS 10 comprises an ammunition container 80 having an ammunition storage portion 82 and an ammunition exit chute 84 leading from the storage portion 82, wherein the ammunition container 80 is fixed to pedestal 12 such that its storage portion 82 resides completely within interior compartment 24 of pedestal 12 and its exit chute 84 extends through shell 22 of pedestal 12. While it is preferred that storage portion 82 fit completely within interior compartment 24, an alternative wherein storage portion 82 is mostly within interior compartment 24 is also contemplated. Storage portion 82 of ammunition container 80 has a reload opening 86 by which the ammunition container may be reloaded with ammunition. A belt 88 of linked ammunition is fed from storage portion 82 through exit chute 84 to supply a weapon carried by the weapon support yoke 14, and the ammunition container is reloadable by onboard personnel under protection of the armored vehicle and the pedestal.

[0075] Ammunition container 80 may include a flange 90 on exit chute 84, whereby the ammunition container 80 may be fixed to shell 22 of pedestal 12 by threaded fasteners engaging the flange and the pedestal.

[0076] The storage portion 82 of ammunition container 80 may have a pair of side walls 92 connected by a front wall 93 and a top wall 94, wherein at least one of a bottom and a rear of storage portion 82 is open to provide the reload opening 86. Ammunition container 80 may take the form of a hanging ammo container configured with an open rear and a pair of inner support ledges 96 extending from side walls 92 to receive and suspend a folded ammunition belt 88 that is slid into the container through the rear reload opening 86. In the depicted embodiment, both the bottom and the rear of storage portion 82 are open to provide the reload opening 86, thereby allowing greater access during reloading. As best seen in FIG. 18, ledges 96 may have a slight dip or trough 97 to prevent unwanted sliding or shifting of the suspended ammunition belt 88 as the vehicle travels over uneven terrain. Support ledges 96 may be omitted if they would impede the feeding of a particular size of ammunition round.

[0077] As will be understood from the drawing figures, weapon support yoke 14 may be configured to support two weapons and RWS may comprise two ammunition containers 80 respectively associated with the two weapons. Those skilled in the art will understand that the dimensions and specific configuration of each ammunition container 80 may vary and will depend on the specific type of ammunition being fed. To allow an operator to reload either or both of the containers 80 from the same location, and to simplify location of a firing control unit 98 sensing ammunition status, the respective reload openings 86 of the two ammunition containers 80 may face a common reloading space 99 within interior compartment 24.

[0078] FIGS. 19-24 illustrate an RWS 210 formed in accordance with another embodiment of the present invention. In FIGS. 19-21, RWS 210 is shown without any weapons, weapon cradles, or other operational units mounted thereon. RWS 210 is similar to RWS 10 described above in that it comprises pedestal 12 including base plate 16, outer rotary bearing race 18, inner rotary bearing race 20, armored shell 22, and yoke arm attachment interfaces 34. As in the previous embodiment, pedestal 12 defines interior compartment 24 that is accessible from within the armored vehicle. RWS 210 may also comprise motorized elevation and azimuth drive systems as described above in connection with RWS 10. RWS 210 further comprises a pair of elevation yoke arms 214A, 214B supporting respective elevation rotary bearings 46A, 46B defining rotational elevation axis EL.

[0079] In the embodiment of FIGS. 19-24, elevation yoke arms 214A, 214B may be directly mounted on yoke arm attachment interfaces 34 to position elevation axis EL at a first height H1 (see FIGS. 20 and 23), and may also be indirectly mounted on yoke arm attachment interfaces 34 by way of a pair of spacers 215A, 215B to position elevation axis EL at a second height H2 different from first height H1 (see FIGS. 21 and 24). As may be understood, the bottom end of each elevation yoke arm 214A, 214B is configured to be removably mounted directly on the pair of yoke arm attachment interfaces 34, for example using threaded fasteners 44. The bottom end of each elevation yoke arm 214A, 214B is also configured for removable mounting on a respective attachment interface 234 at a top end of each spacer 215A, 215B using threaded fasteners 44. The bottom end of each spacer 215A, 215B is configured to be removably mounted directly on the pair of yoke arm attachment interfaces 34, for example using threaded fasteners 244. Thus, RWS 110 may be selectively configured in a short configuration as shown in FIGS. 20 and 23, or in a tall configuration as shown in FIGS. 21 and 24, depending upon whether spacers 215A, 215B are installed or not.

[0080] In the depicted embodiment, elevation yoke arm 214A is a driver elevation yoke arm that supports elevation drive motor 48, elevation rotary bearing 46A, and elevation drive hub 50, and elevation yoke arm 214B is a follower elevation yoke arm that supports elevation rotary bearing 46B and elevation follower hub 52. Advantageously, the elevation drive motor 48 may be coupled to the driver elevation yoke arm 214A and not coupled to the first spacer 215A, thereby facilitating selective installation and removal of spacer 215A to efficiently reconfigure RWS 210. First spacer 215A may be hollow as shown in FIG. 19 to freely receive drive hardware extending down from driver elevation yoke arm 214A.

[0081] In order to ensure axial alignment of elevation rotary bearings 46A, 46B in both the short and tall configurations, elevation rotary bearings 46A, 46B may be embodied as self-aligning ball bearings that are insensitive to slight misalignment of elevation drive hub 50 and elevation follower hub 52.

[0082] In an optional refinement of the invention, each of the first and second attachment interfaces 34 may define a plurality of different selectable attachment positions at which an elevation yoke arm 214A, 214B or a spacer 215A, 215B may be mounted on the attachment interface, whereby a longitudinal position (i.e. position fore to aft) of the elevation axis relative to the armored vehicle is adjustable. The attachment positions may be defined by providing further bolt holes 38 in each attachment interface 34. In another optional refinement of the invention, a lateral spacing between the driver elevation yoke arm 214A and the follower elevation yoke arm 214B differs depending upon whether or not the first spacer 215A and the second spacer 215B are installed. This may be achieved by configuring one or both spacers 215A, 215B such that its top-end attachment interface 234 defines an attachment location that is offset laterally (i.e. inboard or outboard) relative to the corresponding underlying attachment interface 34 on pedestal 12.

[0083] FIGS. 25 and 26 illustrate a basic automated drive system of RWS 210. The basic drive system comprises an electrically-powered azimuth drive motor 29 operable to rotate output gear 28. The output gear 28 meshes with inner gear teeth 30 of inner race 20, wherein output gear 28 functions as an azimuth drive gear rotatable by azimuth drive motor 29 to rotate pedestal 12 and yoke arms 214A, 214B about azimuth axis AZ. The basic drive system also comprises electrically-powered elevation drive motor 48 operable to rotate output gear 49. The output gear 49 meshes with a gear train coupled to drive hub 50 (not shown in FIGS. 25 and 26), wherein output gear 49 functions as an elevation drive gear rotatable by elevation drive motor 48 to drive rotation of elevation drive hub 50 about elevation axis EL. In the illustrated embodiment, azimuth drive gear 28 and elevation drive gear 49 travel with pedestal 12 in rotating relative to the armored vehicle about the azimuth axis AZ. Slip ring assembly 32 may be incorporated in the basic drive system to provide signal transmission to and from control electronics associated with azimuth drive motor 29, elevation drive motor 48, and other electronic units in pedestal 12 across the rotational interface defined between pedestal 12 and the armored vehicle upon which pedestal 12 is mounted. In FIG. 25, components of the basic automated drive system are shown floating in space because supporting structure has been hidden for sake of clarity. For example, elevation drive motor 48 and elevation drive gear 49 are actually supported by elevation yoke arm 214A (not shown), and slip ring assembly 32 may actually be supported by pedestal 12.

[0084] In an aspect of the present invention, the basic automated drive system described above with reference to FIGS. 25 and 26 may be enhanced in space-efficient fashion to enable manual operation of azimuth drive gear 28 and elevation drive gear 49 in the event of a loss of electrical power to drive motors 29 and 48. As shown in FIGS. 27-30, an azimuth drive train 250 and an elevation drive train 270 may be incorporated into the drive system to enable manual operation. As will be described in greater detail below, azimuth drive train 250 is manually operable to rotate azimuth drive gear 28 to thereby rotate pedestal 12 and elevation yoke arms 214A, 214B about azimuth axis AZ, and elevation drive train 270 is manually operable to rotate elevation drive gear 49 to thereby rotate elevation hub 50 about the elevation axis EL.

[0085] Azimuth drive train 250 may generally include a crank 252, a transmission arm 256, a first transmission belt 258, a primary drive shaft 260, a second transmission belt 262, a secondary drive shaft 266, and a motor-input gearbox 268.

[0086] Crank 252 may have a crank arm 253 and a handle 254. Crank arm 253 may be coupled at one end thereof to a first pulley 255, and handle 254 may be rotatably mounted at an opposite end of crank arm 253 to extend at a right angle relative to the longitudinal direction of crank arm 253. First pulley 255 may be rotatably mounted at a peripheral end of transmission arm 256 and connected by first transmission belt 258 to a second pulley 259. Second pulley 259 may be fixedly mounted to a bottom end of primary drive shaft 260. As will be understood, manual rotation of crank 252 will cause first pulley 255 to rotate, and this rotational motion is transmitted to second pulley 259 by first transmission belt 258, wherein primary drive shaft 260 is caused to rotate with second pulley 259. As best seen in FIG. 30, primary drive shaft 260 extends through a central axial passage 33 through slip ring assembly 32 and is rotatably mounted by a pair of rotary bearings 263 enabling primary drive shaft 260 to rotate relative to slip ring assembly 32. A third pulley 261 may be fixed to a top end of primary drive shaft 260 to rotate with primary drive shaft 260. Third pulley 261 may be connected by a second transmission belt 262 to a fourth pulley 264 fixedly mounted on secondary drive shaft 266, wherein rotation of third pulley 261 is transmitted to fourth pulley 264 by second transmission belt 262, thereby causing secondary drive shaft 266 to rotate. Secondary drive shaft 266 may be coupled to a manual input gearbox 268 associated with azimuth drive motor 29. Consequently, in a power outage situation, azimuth drive motor 29 may be powered manually to rotate azimuth drive gear 28 to achieve rotation of pedestal 12 about azimuth axis AZ relative to the armored vehicle.

[0087] Elevation drive train 270 is very similar to azimuth drive train 250 described above. Elevation drive train 270 may generally include a crank 272, a transmission arm 276, a first transmission belt 278, a primary drive shaft 280, a second transmission belt 282, a secondary drive shaft 286, and a motor-input gearbox 288.

[0088] Crank 272 may have a crank arm 273 and a handle 274, wherein crank arm 273 may be coupled at one end to a first pulley 275, and handle 274 may be rotatably mounted at an opposite end of crank arm 273 to extend at a right angle thereto. First pulley 275 may be rotatably mounted at a peripheral end of transmission arm 276 and connected by first transmission belt 278 to a second pulley 279 fixedly mounted to a bottom end of primary drive shaft 280. Thus, manual rotation of crank 272 will cause first pulley 275 to rotate, and this rotational motion is transmitted to second pulley 279 by first transmission belt 278. As a result, primary drive shaft 280 is caused to rotate with second pulley 259. As best seen in FIG. 30, primary drive shaft 280 of elevation drive train 270 extends through central axial passage 33 through slip ring assembly 32 by being coaxially nested to extend through primary drive shaft 260 of azimuth drive train 250, which is embodied as a tube sized to receive primary drive shaft 280. In the depicted embodiment, elevation primary drive shaft 280 is rotatably mounted within azimuth primary drive shaft 260 by a pair of rotary bearings 269 to enable shafts 260 and 280 to rotate independently of one another about a main axis of slip ring assembly 32 that may coincide with azimuth axis AZ. A third pulley 281 may be fixed to a top end of primary drive shaft 280 to rotate with primary drive shaft 280 and may be connected by a second transmission belt 282 to a fourth pulley 284 fixedly mounted on secondary drive shaft 286. Rotation of third pulley 281 is transmitted to fourth pulley 284 by second transmission belt 282, thereby causing secondary drive shaft 286 to rotate. Secondary drive shaft 286 may be coupled to a manual input gearbox 288 associated with elevation drive motor 48. Consequently, in a power outage situation, elevation drive motor 48 may be powered manually to rotate elevation drive gear 49 to achieve rotation of elevation drive hub 50 about elevation axis EL.

[0089] In an advantageous refinement, primary drive shaft 280 may be embodied as a hollow tube through which cables, for example fiber optic cables 290, may be routed from one side of the rotational interface to the other.

[0090] As shown in FIGS. 31 and 32, the present invention may also be embodied by a manned weapon station apparatus 310. Similar to the RWS embodiments described above, manned weapon station apparatus 310 comprises a pedestal 312 adapted to be mounted on an armored vehicle for rotation relative to the armored vehicle about an azimuth axis AZ, and a weapon support yoke 314 carried by pedestal 312 and having laterally-spaced elevation yoke arms 214A, 214B extending upward from the pedestal, with or without optional spacers 215A, 215B as described above. Pedestal 312 may include a topside hatch 327 between elevation yoke arms 214A, 214B to enable a person to enter or exit an interior compartment of the pedestal. The illustrated embodiment depicts hatch 327 as being connected to the pedestal by a hinge 328, however a hatch 327 may be made to slide along tracks to open and close if a hinged hatch does not have clearance relative to mounted weaponry. Topside hatch 327 may be inclined relative to horizontal so that spent ammunition casings slide down and do not accumulate on the topside hatch.

[0091] Manned weapon station apparatus 310 further comprises a personnel support platform 330 suspended from pedestal 12 for rotation with the pedestal about azimuth axis AZ. Personnel support platform 330 may be suspended from pedestal 312 by one or more vertical structural member 332. A weapon control unit 335 and a seat 337 may be mounted on the same or different structural members 332 for accommodating an operator. Manned weapon station apparatus 310 may further comprise a periscope 340 allowing the operator to view external objects from within the interior compartment of the pedestal 312.

[0092] Manned weapon station apparatus 310 may further comprise slip ring assembly 32 configured to transmit power and data across a rotary interface established between pedestal 312 and the armored vehicle. In the depicted embodiment, slip ring assembly 32 is mounted to the personnel support platform 320 in alignment with azimuth axis AZ. Alternatively, slip ring assembly 32 may be movably mounted to an inner wall of pedestal 12, for example by a pantograph arm or other mechanical arm that enables the slip ring assembly to be displaced within interior compartment 24. A user may then selectively align slip ring assembly 32 with azimuth axis AZ for pedestal rotations, or move slip ring assembly 32 out of the way for using topside hatch 327.

[0093] The description above relating to selective configuration of the height of elevation axis EL for RWS embodiments applies equally to the manned weapon station embodiment shown in FIGS. 31 and 32.

[0094] While the invention has been described in connection with exemplary embodiments, the detailed description is not intended to limit the scope of the invention to the particular forms set forth. The invention is intended to cover such alternatives, modifications and equivalents of the described embodiment as may be included within the spirit and scope of the invention.