EP0006491A2 - Dispositif pour supporter une installation d'armes sur un véhicule de combat - Google Patents

Dispositif pour supporter une installation d'armes sur un véhicule de combat Download PDF

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Publication number
EP0006491A2
EP0006491A2 EP79101774A EP79101774A EP0006491A2 EP 0006491 A2 EP0006491 A2 EP 0006491A2 EP 79101774 A EP79101774 A EP 79101774A EP 79101774 A EP79101774 A EP 79101774A EP 0006491 A2 EP0006491 A2 EP 0006491A2
Authority
EP
European Patent Office
Prior art keywords
intermediate frame
vehicle
frame
bearing
support
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.)
Granted
Application number
EP79101774A
Other languages
German (de)
English (en)
Other versions
EP0006491B1 (fr
EP0006491A3 (en
Inventor
Walter Ebner
Werner Kramis
Gustav Studer
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.)
Rheinmetall Air Defence AG
Original Assignee
Contraves AG
Oerlikon Contraves AG
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 Contraves AG, Oerlikon Contraves AG filed Critical Contraves AG
Publication of EP0006491A2 publication Critical patent/EP0006491A2/fr
Publication of EP0006491A3 publication Critical patent/EP0006491A3/xx
Application granted granted Critical
Publication of EP0006491B1 publication Critical patent/EP0006491B1/fr
Expired legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A23/00—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles
    • F41A23/34—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles on wheeled or endless-track vehicles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A23/00—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles
    • F41A23/56—Arrangements for adjusting the gun platform in the vertical or horizontal position

Definitions

  • the invention relates to a device for supporting an weapon system on a combat vehicle, in which combat vehicle the weapon system arranged on a platform and rotatable about a vertical axis, together with an intermediate frame, is mounted on the chassis frame of the vehicle via three support devices arranged at a distance from one another.
  • a mobile combat vehicle - US Pat. No. 3,946,640 - is known, in which a weapon system arranged on a platform and rotatably mounted about a vertical axis by means of a rotary bearing is mounted on the vehicle chassis via three articulated supports spaced apart from one another and an intermediate frame, the prevent articulated supports arranged between the chassis and the intermediate frame from transmitting the vehicle-side twists to the weapon system.
  • This combat vehicle has a relatively high center of gravity, which can have an adverse effect on the function of the weapon system, which is designed, for example, as a rocket launcher or machine gun, in extreme operating conditions.
  • the relatively large, unchangeable overall height of the entire combat vehicle limits the driving characteristics and transport options, but in particular the rail transport options.
  • wheeled or caterpillar vehicles to arrange a platform on the vehicle chassis frame which is designed to accommodate, for example, collapsible support parts for lifting and assembly platforms or for storing parts for shovel excavators or the like.
  • the platform of these vehicles is essentially supported by a Known three-point mounting on the chassis frame of the vehicle, one side of the bearing can be provided, for example, with pivotable articulated supports directed in the direction of travel of the vehicle or with largely freely movable ball-and-socket supports and the other side mechanical or hydraulic means for leveling the entire platform in relation to the chassis frame.
  • the invention has for its object to provide a combined device for supporting a weapon system mounted on a combat vehicle mentioned at the outset, which prevents transmission of the torsional, bending and stretching forces occurring to the weapon system when driving and / or shooting on the chassis frame, and by means of which, moreover, the weapon system can be brought into a position which is more favorable both for driving operation and in the loading dimension permissible for rail transport.
  • the support devices which are operatively connected to the intermediate frame and the chassis frame, for absorbing angular and sliding movements and in the direction of travel of the vehicle, viewed at least on one side with respect to the chassis frame for lowering and lifting the intermediate frame carrying the weapon system are trained.
  • the weapon system can be leveled and stabilized with respect to the combat vehicle by means of additional supports pivotably attached to the intermediate frame and standing on the ground, and the vehicle can also be lowered on the bow side in relation to the leveled weapon system in order to achieve maximum depression of the weapon.
  • the two oppositely arranged support devices are operatively connected to one another by a shaft rotatably driven about their longitudinal axis by means of a cylinder arranged in the intermediate frame.
  • the invention also assumes that the intermediate frame with the weapon system can be lowered or raised by a pivoting movement directed in the longitudinal direction of the vehicle and parallel to the chassis frame in relation to its starting position .
  • the two front support devices arranged opposite one another are likewise operatively connected to one another by a first shaft, the rear support device having a second shaft arranged parallel to the first shaft.
  • the two shafts are driven by a tension member driven intermittently by a cylinder.
  • 1, 5 and 12 show a side view of a combat vehicle in which the vehicle is generally designated 100, the chassis frame of the vehicle is 110 and a driver's cabin is 150, the driver's cabin being, for example, a removable cabin roof 160 having.
  • the chassis frame 110 which is designed, for example, as a trough, serves to receive and support an intermediate frame that can be lowered and raised again with respect to the chassis frame, which is arranged between the two side walls of the chassis frame and is, for example, box-shaped and designed to accommodate an azimuth pivot bearing 220 (not shown) .
  • a platform 210 is fastened on the rotary bearing 220, on which a weapon 200 designed as a machine gun and a cabin 250 are arranged and fastened by means not shown.
  • the platform 210 with the weapon 200 and cabin 250 arranged thereon can be rotated relative to the intermediate frame 90 about an essentially vertical axis X of the rotary bearing 220 in the direction of arrow P.
  • Fig. 2 shows a plan view of a section of the combat vehicle without a weapon and you can see the chassis frame 110 designed as a tub and spaced apart storage and support points A, B and C.
  • the storage and support points are on the one hand on the chassis frame 110 and on the other Intermediate frame 90 attached.
  • the two support and bearing points B and C are shown offset for a simplified illustration.
  • a lifting cylinder 120 is arranged corresponding to the bearing and support points A, B and C.
  • the lifting cylinders are provided with the cabin 250 for raising and lowering the intermediate frame 90, the platform 210 and the weapon 200 fastened on the platform and are dimensioned accordingly.
  • the bearing and support points A, B and C together form a three-point bearing, in which the two points B and C are arranged symmetrically to one another at one end and the point A is attached to the other end of the intermediate frame 90.
  • the two points B and C are arranged at an angle a, which is of the order of magnitude of approximately 120 ° to one another.
  • the intermediate frame 90 has a bearing surface formed by a side wall 91 and designated by 92 for receiving and fastening the essentially identical bearing and support points A, B and C at the appropriate location.
  • FIG. 3 the bearing and support point A, designated by a circle S in FIG. 1, is shown on a larger scale and in section as an exemplary embodiment, which is described in more detail below.
  • the bearing and support point essentially consists of a bearing pin 20 fastened to the intermediate frame 90, a housing 25 with an integrally formed support element 35, a pivotable spacer 40 articulated on the housing and a guide part 45 for the support element 35 which is fixedly connected to the chassis frame 110 of the bearing journal 20, an opening 93 is provided in the side wall 91 of the intermediate frame 90, in which the bearing journal 20, centered with a flange 21 on the contact surface 92 and fastened by means not shown, is centered with a shoulder 22.
  • the cylindrical part 23 of the bearing pin 20 is preferably closed by a cover 24.
  • the bearing pin 20 arranged coaxially in the housing 25 is mounted with its cylindrical part 23 in a joint ball 27 and the joint ball in a ball socket 26.
  • the ball socket 26 is secured in the housing 25 on one side by a first bushing 28 and on the other side by a second bushing 29 against axial displacement.
  • the socket 28 and the socket 29, which is preferably designed as a cover cap, are not included attached means attached to the housing 25.
  • the bearing and support points A, B and C are each protected on one side by the cover cap and on the other side by a sleeve 30 against contamination.
  • the sleeve 30 is fastened on the one hand to the flange 21 of the bearing journal 20 and on the other hand to the housing 25 by means not shown.
  • the tubular support element 35 molded onto the housing 25 is arranged coaxially in the guide part 45 and is guided at the upper end by a first inner bush 46 and at the lower end by a second inner bush 47.
  • the support element 35 has at least two guide grooves 38 which are distributed around the circumference and into which a bolt 49 mounted in the bushing 46 engages, as a result of which the support element 35 is secured against rotation.
  • a bushing 37 is inserted and firmly connected to the support element.
  • the bushing 37 has a threaded piece (not specified) and a guide part and serves to receive a tensioning screw 39.
  • the intermediate frame is made by means of the tensioning screw 39 which is operatively connected to the support element 35 and the housing 25 and a tensioning element 48 which is supported on the bushing 47 of the guide part 45 90, .. which is essentially distanced from the spacer 40 to the chassis frame 110, is pulled against the guide part 45 which is fixedly connected to the chassis frame, whereby the chassis frame 110 is essentially rigidly operatively connected to the intermediate frame 90.
  • FIG. 4 shows the bearing and support point A in a side view and one can see the housing 25, for example a polygon, the intermediate frame 90, the chassis frame 110 and the spacer 40.
  • the housing 25 for example a polygon, the intermediate frame 90, the chassis frame 110 and the spacer 40.
  • two tabs 31 are arranged at a distance from each other, between which a tab 43 attached to the spacer 40 is arranged and held by an axis 44.
  • the parts 31, 43 and 44 together form a schematically illustrated pivot bearing 50, by means of which the spacer 40, after a raster element 41, not shown, provided with a handle 33 and locked in the groove 38 of the support element 35 with a pin 34, is released and the clamping screw 39 is partially unscrewed and the intermediate frame is raised relative to the chassis frame by the lifting cylinder 120 by a corresponding amount to release a corresponding swivel radius - swiveled about the axis 44 along the swivel line 51 into the dash-dot position and by a manner not shown on the housing 25 attached and pivotable about an axis 32 pawl 42 is held in this position.
  • the intermediate frame 90 and thus also the platform 210 with the weapon 200 and the cabin 250 attached to it can be moved in the direction of the arrow 52 in FIG Fig. 4 dash-dotted position (only a portion of the intermediate frame 90 shown) can be lowered.
  • the housing 25 lies with its bearing surface 25 'on the upper edge of the inner bush 46 and the support element 35 with the clamping screw 39 and the clamping element 48 protrude from the underside of the chassis frame 110 (only partially shown in FIG. 4).
  • the lowering of the intermediate frame with the attached weapon system consisting of the parts 200, 210 and 250 is particularly necessary for rail transport.
  • the camp and bases A, B and C 3 and 4 show a first combined device for supporting the weapon system.
  • the bearing and support points A, B and C ensure the torsional, bending and elongation forces that occur when driving and shooting on the chassis frame not transferred to the weapon system.
  • the angular and sliding movements are taken up by the bearing pin 20, which is axially displaceably mounted in the joint ball, as is shown, for example, by the dashed-dotted section of the journal 20.
  • the intermediate frame 90 with the weapon system attached to it is deliberately not leveled compared to the vehicle which is inclined, for example, due to uneven terrain.
  • FIG. 5 and 6 show a first variant of an intermediate frame 94 and the mounting of the intermediate frame in connection with the combat vehicle according to FIG. 1 and the fighting vehicle shown in the firing position and with the cabin roof removed can be seen in which with platform 210 .
  • the intermediate frame 94 attached weapon system is leveled and stabilized by means of supports 15, 16 and 17 attached to the intermediate frame.
  • the parts 100, 110, 150, 200, 210, 220 and 250 correspond to the combat vehicle according to FIG. 1.
  • the supports 15, 16 and 17, not shown and described, are pivotally attached to the intermediate frame and hydraulically for driving the vehicle into the 5 dash-dotted position pivotable and lockable in this position by a device 18, not shown.
  • FIG. 6 shows a section of the combat vehicle without a weapon and one can see the chassis frame 110, the supports 15, 16 and 17 fastened to the intermediate frame, shown in the swung-out state, and bearing and support points A ', B arranged at a distance from one another 'and C', which are arranged essentially within the box-shaped intermediate frame 94, shown partly in section.
  • the two storage and support points B I and C ! are essentially the same, of which point C 'is described in more detail below.
  • the point C 'along the line E - F in FIG. 6 is shown in view and on a larger scale and one can see a shaft 65 which is arranged in the intermediate frame 94 transversely to the direction of travel of the vehicle and which is at least two apart from one another arranged bearing blocks 66 which are fastened to the intermediate frame by means not shown, are rotatably mounted.
  • the shaft 65 is actuated by a cylinder 64, shown schematically in FIG.
  • a bearing block 55 which is fixedly connected to the chassis frame 110 by means not shown, is arranged on each side and projects through an opening 54 provided in the intermediate frame 94 into the interior of the intermediate frame. In the upper area, the bearing block 55 has a recess 56 in which the bearing element 68 is guided to move back and forth by the rotary movement Y of the disk 60 or the shaft 65.
  • the bearing element 68 denoted by a circle D in FIG. 7, is shown on a larger scale and partly in section as an exemplary embodiment, and the disk 60, which is arranged at a distance from the bearing block 55, to which an axle pin 63 is attached eccentrically can be seen.
  • FIG. 8 and 8a show the bearing and support point C 'in a side view according to the line G - G in FIG. 7, the chassis frame 110 and intermediate frame 94 in the driving position in FIG. 8 and the chassis frame opposite in FIG. 8a the leveled intermediate frame is shown in the shooting position.
  • FIG. 10 and Fig. 11 the bearing and support point A 'for the intermediate frame 94, indicated by a circle T in Fig. 5, is shown on a larger scale in a view and a side view.
  • a first bearing block 70 is fastened to the chassis frame 110 and a second bearing block 75 is fastened to the intermediate frame 94 by means not shown in detail.
  • the two bearing blocks 70, 75 are operatively connected to one another by a swivel bracket 74.
  • the swivel bracket 74 is connected on the one hand by a first bolt 76 to the second bearing block 75 and on the other hand by a second bolt 71 to the first bearing block 70.
  • the two bolts 71 and 76 are each secured by a washer 72 and a split pin 73.
  • the intermediate frame 94 with the platform 210 and the weapon system attached to it are mechanically leveled and stabilized with respect to the vehicle by means of the supports 15, 16 and 17 standing on the ground.
  • the bearing and support points A ', B' and C 'according to the first variant have the effect that the torsional, bending and elongation forces which occur during driving as well as when shooting on the chassis frame are not transmitted to the weapon system.
  • a maximum depression of the weapon barrel of the weapon 200 which is shown in dash-dotted lines in FIG. 5, there is the possibility in this variant of lowering the vehicle 100 on the bow side with respect to the horizontal intermediate frame 94.
  • the lowering process is achieved by means of the two bearing and support points B 'and C' which are operatively connected to one another by the shaft 65 and are described in more detail below.
  • the shaft 65 with the disk 60 fastened thereon is rotated in the direction of the arrow Y (FIG. 7), so that that which is rotatably fastened to the disk 60 and in the recess 56 of the bearing block 55 inevitably guided bearing element 68 is moved outwards from the center (rest position according to FIG. 8) of the bearing block 55 and at the same time is moved down along the pivot line 57 running around the longitudinal axis of the shaft 65 and thus the vehicle is lowered on the bow side (FIG. 5).
  • the bearing block 55 is in a central position (dash-dotted) and shown in an end position, the middle position corresponding to a rotation of the shaft 65 of 90 ° and the end position of 180 °.
  • the width of the bearing block 55 is dimensioned such that the bearing element 68 is still sufficiently guided in the recess 56 in the central position.
  • the bearing and support point A 'shown in FIGS. 10 and 11 is designed with three degrees of freedom and, on the one hand, enables a movement in the longitudinal direction of the vehicle and shown in FIG. 10 by a pivot line 77 about the longitudinal axis of the transverse to the longitudinal direction of the vehicle arranged first bolt 76 and on the other hand a movement directed transversely to the longitudinal direction of the vehicle and shown in FIG. 11 by a pivot line 78 about the longitudinal axis of the bolt 71 arranged in the longitudinal direction of the vehicle.
  • FIGS. 12 and 13 show a second variant of an intermediate frame 95 and its mounting on the chassis frame 110 of the vehicle 100.
  • parts 100, 110 and 150 and parts 160, 200, 210, 220 and 250 (not shown) correspond to the combat vehicle according to FIG. 1.
  • the plan view according to FIG. 13 shows a section of the combat vehicle without a weapon, from which the arrangement of the storage and support points A ", B" and C "arranged at a distance from one another can be seen.
  • FIG. 14 shows the bearing and support point A "in a view in the direction of the arrow R in FIG. 12 with the box-shaped intermediate frame 95 shown in the lowered position, which at this point has a pocket 96 formed essentially from two opposite side walls 97, 97 ' Arranged in the pocket 96 is an actuating element 80, which is designed like a crankshaft and is operatively connected to the intermediate frame 95, and a bearing block 101 which is fastened to the chassis frame 110 by means not shown spaced and essentially parallel to each other and connected by a shaft 83 to each other disks 84, 84 'and a fixed to the disk 84' journal 85.
  • the shaft 83 connecting the two disks 84, 84 'to each other is eccentric to the center of the disk
  • the shaft 81 is in the side wall 97 and the bearing pin 8 5 rotatably mounted in the side wall 97 '.
  • FIGS. 15 and 15a show the bearing and support point A "in a side view along the line K - K in FIG. 14, the intermediate frame 95 being shown in a lowered position in FIG. 15 and in a raised position in FIG. 15a
  • Bearing block 101 is preferably fork-shaped for receiving and mounting a swivel part 102 and has a bore (not shown and designated in each fork part).
  • the swivel part 102 is mounted and used in the associated bore of the bearing block 101 with two bearing pins 103 attached to the side of the swivel part for the rotatable mounting of the crankshafts similarly designed actuating element 80 fastened shaft 83.
  • the two bearing and support points B “and C” are of substantially the same design and are arranged symmetrically to one another on the intermediate frame 95, of which the point C "is described in more detail below.
  • the point C" according to the line L - M in 13 is shown in a view and on a larger scale and one can see a shaft 105 which is arranged in the intermediate frame transversely to the direction of travel of the vehicle and which is rotatably mounted in two spaced-apart side walls 104, 104 'of the intermediate frame 95.
  • the two shafts 81 and 105 which are arranged transversely to the direction of travel of the vehicle and essentially parallel to one another, are supported by a cylinder 107, shown schematically in FIG 106 and, on the other hand, is operatively connected to the gear 82, which is connected in a rotationally fixed manner to the shaft 81, in accordance with the arrow direction Z shown in FIGS. 14 and 16.
  • a disk 86 connected to the shaft in a rotationally fixed manner, to each of which a bearing journal 87 is fastened eccentrically.
  • a bearing bracket 101 ' which is fastened to the chassis frame 110 by means which are not shown and which is designed to support a pivoting part 102'.
  • the bearing block 101 'and the swivel part 102' essentially correspond to the parts 101 and 102 according to the exemplary embodiment according to FIG. 14.
  • FIG. 17 and 17a show the bearing and support point C "in a side view along the line shown in FIG. 16 N - N, the intermediate frame 95 being shown in the lowered position in FIG. 17 and in the raised position in FIG. 17a.
  • the bearing and support points shown in FIGS. 14 to 17 enable, on the one hand, a movement oriented transversely to the longitudinal direction of the vehicle and shown in FIGS. 14 and 16 by a pivot line 89, 89 'by means of the pivoting parts mounted in the bearing blocks, for which purpose A corresponding distance is provided between the bearing blocks and the disks.
  • a movement oriented essentially in the longitudinal direction of the vehicle and represented by a pivot line III, III 'in FIGS. 15, 15a and 17, 17a is made possible by means of the shafts 81, 105 connected in parallel by the chain 108 and is a direct function of the chain slack.
  • the chain sag is mainly determined by the two tensioning wheels 109, 109 'mounted in the intermediate frame 95 in a manner not shown in detail.
  • the rear bearing and support point A "can be mechanically blocked by a wedge (not shown), which relieves the load on the chain 108.
  • the wedge is either up or down in pocket 96 inserted, for which purpose the two disks 84, 84 'are correspondingly flattened on one side (contact surface).

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
EP79101774A 1978-07-05 1979-06-05 Dispositif pour supporter une installation d'armes sur un véhicule de combat Expired EP0006491B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CH7319/78 1978-07-05
CH731978 1978-07-05

Publications (3)

Publication Number Publication Date
EP0006491A2 true EP0006491A2 (fr) 1980-01-09
EP0006491A3 EP0006491A3 (en) 1980-01-23
EP0006491B1 EP0006491B1 (fr) 1982-03-17

Family

ID=4323260

Family Applications (1)

Application Number Title Priority Date Filing Date
EP79101774A Expired EP0006491B1 (fr) 1978-07-05 1979-06-05 Dispositif pour supporter une installation d'armes sur un véhicule de combat

Country Status (3)

Country Link
US (1) US4317405A (fr)
EP (1) EP0006491B1 (fr)
DE (1) DE2962278D1 (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE507660C2 (sv) * 1996-12-02 1998-06-29 Bofors Ab Sätt och anordning för horisonten runt sidriktbar artilleripjäs
GB9822010D0 (en) * 1998-10-08 1999-10-20 Vickers Shipbuilding & Eng Improvements in or relating to self-propelled guns
DE10118637B4 (de) * 2001-04-12 2007-08-02 Rheinmetall Landsysteme Gmbh Schalldämpferlafette für Rohrwaffen
DE102012103353A1 (de) * 2012-04-17 2013-10-17 Krauss-Maffei Wegmann Gmbh & Co. Kg Verfahren zum Transport eines Fahrzeugs sowie Fahrzeug
US9309686B2 (en) * 2014-04-10 2016-04-12 Us Tower Corporation Multi-axial mast positioning system

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1395020A (en) * 1917-09-01 1921-10-25 Holt Mfg Co Anti-aircraft-gun mount
GB496332A (en) * 1936-12-02 1938-11-29 Insley Mfg Corp Improvements in or relating to excavators or cranes
US2500815A (en) * 1947-03-10 1950-03-14 Gerli Flying stage
US2815250A (en) * 1952-11-19 1957-12-03 Pitman Mfg Company Machine with elevatable and traveling carriage
GB787107A (en) * 1955-01-08 1957-12-04 James Maurice Newcombe Bond Improvements in and relating to earth working machines and cranes
US3168273A (en) * 1962-05-17 1965-02-02 Thomson Houston Comp Francaise Tripod structure
US3239169A (en) * 1963-12-02 1966-03-08 Automatic Motor Base Co Machinery support
US3464654A (en) * 1967-03-24 1969-09-02 Babcock & Wilcox Co Leveling construction for heavy machinery and instruments
US3689090A (en) * 1970-03-18 1972-09-05 July Nekhemievich Dunaevsky Excavator
US3946640A (en) * 1972-12-04 1976-03-30 Contraves Ag Mobile anti-aircraft device
DE2510785A1 (de) * 1975-03-08 1976-09-16 Phywe Ag Stellvorrichtung

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE71373C (de) * Firma FRANZ KATH-REINER's NACHFOLGER in München, Ostbahnhof Behandlung von Kaffeebohnen mit einem Extract aus Kaffee- oder Cacaoschalen während des Röstens
US652154A (en) * 1899-09-28 1900-06-19 James Armstrong Wilding Gun-carriage or other vehicle.
US709301A (en) * 1901-11-01 1902-09-16 Edwin Morris Capps Machine-gun.
DE2721906A1 (de) * 1977-05-14 1978-11-23 Rheinmetall Gmbh Vorrichtung zum verkantungsausgleich von steilfeuergeschuetzen o.dgl.

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1395020A (en) * 1917-09-01 1921-10-25 Holt Mfg Co Anti-aircraft-gun mount
GB496332A (en) * 1936-12-02 1938-11-29 Insley Mfg Corp Improvements in or relating to excavators or cranes
US2500815A (en) * 1947-03-10 1950-03-14 Gerli Flying stage
US2815250A (en) * 1952-11-19 1957-12-03 Pitman Mfg Company Machine with elevatable and traveling carriage
GB787107A (en) * 1955-01-08 1957-12-04 James Maurice Newcombe Bond Improvements in and relating to earth working machines and cranes
US3168273A (en) * 1962-05-17 1965-02-02 Thomson Houston Comp Francaise Tripod structure
US3239169A (en) * 1963-12-02 1966-03-08 Automatic Motor Base Co Machinery support
US3464654A (en) * 1967-03-24 1969-09-02 Babcock & Wilcox Co Leveling construction for heavy machinery and instruments
US3689090A (en) * 1970-03-18 1972-09-05 July Nekhemievich Dunaevsky Excavator
US3946640A (en) * 1972-12-04 1976-03-30 Contraves Ag Mobile anti-aircraft device
DE2510785A1 (de) * 1975-03-08 1976-09-16 Phywe Ag Stellvorrichtung

Also Published As

Publication number Publication date
EP0006491B1 (fr) 1982-03-17
DE2962278D1 (en) 1982-04-15
EP0006491A3 (en) 1980-01-23
US4317405A (en) 1982-03-02

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