EP0289538A1 - Dispositif de visee pour aligner l'axe de visee d'un appareil avec un point de mire - Google Patents

Dispositif de visee pour aligner l'axe de visee d'un appareil avec un point de mire

Info

Publication number
EP0289538A1
EP0289538A1 EP87906988A EP87906988A EP0289538A1 EP 0289538 A1 EP0289538 A1 EP 0289538A1 EP 87906988 A EP87906988 A EP 87906988A EP 87906988 A EP87906988 A EP 87906988A EP 0289538 A1 EP0289538 A1 EP 0289538A1
Authority
EP
European Patent Office
Prior art keywords
axis
movement
target
directional
axes
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.)
Withdrawn
Application number
EP87906988A
Other languages
German (de)
English (en)
Inventor
Ghert Meier
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
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 Oerlikon Contraves AG filed Critical Oerlikon Contraves AG
Publication of EP0289538A1 publication Critical patent/EP0289538A1/fr
Withdrawn legal-status Critical Current

Links

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
    • F41A27/00—Gun mountings permitting traversing or elevating movement, e.g. gun carriages
    • F41A27/06—Mechanical systems
    • F41A27/08—Bearings, e.g. trunnions; Brakes or blocking arrangements

Definitions

  • the invention relates to a device for aligning a target body, in particular a gun barrel, to a target point.
  • the type of device is derived from the preamble of patent claim 1.
  • the classic Feidflabgebut has directional means' with two directional coordinates and tracks a target point in the
  • the orientation of the plane in which the target axis is to be pivoted about the second axis is undetermined.
  • the orientation (Az i mut) can be any.
  • the direction of this axis thus represents a singularity of the gun's directional coordinates.
  • a small change in this target point results in a major change in the direction of the plane discussed above, ie the gun on the ground; in other words, a large rotation of the aiming means (on the ground) around the azimuth axis has to be carried out in order to follow a small movement in the region around the azimuth axis.
  • This "large” rotation is, depending on the speed of the movement of the target point, associated with a corresponding speed of rotation and acceleration of the weight of the gun on the ground.
  • the provision of the required service has consequences for the effort (costs) and the accuracy that can be achieved.
  • the singularity axis is slightly inclined to the zenith axis, i.e. no longer at right angles to the carriage level, is arranged on a rotatable base so that when the base rotates azimuth, the singularity axis moves around the zenith axis on the surface of a cone.
  • This type of wobble movement of the singularity axis to the flap plane improves the target behavior close to the zenith axis, but this inclination is not sufficient to optimally align the target axis to a target at every angle.
  • the configuration of the gun proposed there causes a difficult realization of the further requirements that are placed on a gun suitable for modern warfare must become.
  • the auxiliary operations must be installed under or next to the carriage shown, which either results in an undesirable (very high) overall height of the gun system or results in shadowing in the effective area, which is also undesirable in most cases (an exception) Naval guns, in which the gun can be "extended” as it were in the direction below deck).
  • a future gun In order to be able to successfully combat fast, agile, small targets such as guided missiles, a future gun must be able to meet the following conditions:
  • the invention is therefore based on the object of fundamentally improving a device of the type mentioned, so that with a comparatively simple, low structure, a diverse range of movement of its target body (measuring device, gun barrel, etc.) with optimal adaptation to structural conditions is guaranteed ⁇ tet.
  • the device should align one of the azimuth or. enable the axis corresponding to the singularity axis in a quick and simple manner in directions in which the target axis can follow a flying object with minimal load on the drives of the device.
  • the device has three axes of rotation, the first and the second, counting from the target body axis, forming a classic right axis system, and allowing a third axis of rotation between this directional axis system and the base to be pivoted such that the apparatus directivity movements can perform gulartician with enough 'angular distance of their Sin ⁇ , and that the first and third rotation axis are spaced from each other.
  • a preferred embodiment is characterized in that the device has two axes of rotation, a first and a third which can be placed in parallel, and are connected to an axis system by a second axis of rotation which is substantially perpendicular thereto, the two axes of rotation, the first and the third are arranged at a distance from one another, wherein an axis corresponding to the axis of singularity (that is the second axis of movement) can be pivoted over a large angular range and the distance is selected such that the orientation of the target axis body is impeded can be avoided by the structures on the gun.
  • the auxiliary systems can be arranged as required without shadowing between the target and the gun barrel (or measuring sensor). With the help of the mentioned distance between the third axis and the 'system, this can be moved so that it can aim over the casing of the gun, in which the necessary auxiliary systems are housed, without hindrance and the auxiliary systems also do not have to move become.
  • the conditions listed above for a future-oriented, modern gun are thus fulfilled.
  • Figures 1 to 4 each show a device schematically and perspectively shown in four movement positions. It is striking that in the proposed axis arrangement, the axis of rotation 9 (base axis), which is horizontally arranged on the base body, only requires a small range of rotation of less than 90 'in order to enable an adjustment for each target point (including the zenith range). This enables the overall device to be constructed in a very simple manner, since the indispensable additional units can be arranged in a housing 10 right next to the basic axis 9.
  • the base body 5 has, for example, a fixed bearing body which is arranged next to a housing which encloses the operating device (for example energy supply, straightening means such as radar and electronic devices, etc.). Due to the corresponding arrangement of the third movement axis 9 and the distance thereof to the crossing point (not necessarily intersection) of the first and second movement axes 7.8, the target axis body 2 can be turned over this housing in order to be aligned with a target point located behind the housing to become. For elimination of invalidity zones in the opposite ⁇ - _ direction j verur ⁇ second movement axis 8, the second movement axis about the third movement axis 9 can be lowered to a sufficient extent, that is to say, as shown in FIG. 3, below the horizontal. For sufficient removal of ineffectiveness zones in the entire straightening range, a mobility of the second support body through an angle of 90 "or less may be sufficient.
  • the operating device for example energy supply, straightening means such as radar and electronic devices, etc.
  • the heavier device parts such as the support body 4, which, for example, has to hold a supply of ammunition
  • the device parts 3 and 2 which represent the directional axis system for tracking
  • all movement stops - fen have a smaller movement component.
  • a lot of dynamism is required from axes 7 and 8, much less from axis 9, which only has to be brought into a fixed, selected position for certain combat positions. If it is moved to a new position, this usually does not happen during a tracking process, but when a new area sector is to be monitored.
  • the device according to the invention essentially consists of a target axis body 2, a first support body 3, a second support body 4 and a base body 5, which are connected to one another via three axes of rotation, such that the axis of rotation (basic axis) between the base body 5 and the second support body 4 and the axis of rotation (directional axis) between the target axis body 2 and the first support body 3 can be set parallel to one another and are at a distance from one another within which the common center of gravity of the device (or only the moving one) Parts?)
  • the target axis body corresponds to a weapon (gun barrel, laser, etc.), the first movable support body 3 to an upper mount and the second movable support body 4 to a lower mount.
  • the target body 2 or. the gun barrel around a first movement axis 7 in which is perpendicular to the target axis 6 in Direction of arrow X 'and moreover pivotable about a second axis of movement 8 running perpendicular to this axis of movement 7 in the direction of arrow Y in order to be aligned with a moving target body.
  • the second axis of movement 8 is directed at a constant angle, for example vertically or vertically.
  • the gun has a correspondingly upward-widening and ineffective zone in which the target axis is at too small an angle relative to the second movement axis in order to follow a missile by means of a sufficiently rapid rotary movement about this second movement axis 8 to be able to.
  • the respective ineffectiveness zone which is directed upward at an angle of, for example, 30 "with respect to the vertical in the direction of the second movement axis 8 can be pivoted away about a vertical axis on a circular path (not shown) at a constant angle of inclination.
  • the vertically upward area remains unchanged close to the ineffectiveness zone, which is prevented according to the present invention by mounting the second movable support body 4 around a fixed, horizontal, third movement axis 9, a basic axis, around the the support body 4 can be pivoted in the direction of the arrow X.
  • This third movement axis 9 is arranged at a distance A from an intersection point (preferably the intersection of the two axes) of the two axes 7, 8, which can be borrowed continuously change the second movement axis known as the singularity axis, for example iel also sloping downwards, as shown in Figure 3, and the crossing point (or Intersection) of the two axes 7, 8 including the target axis 2 moves on a not-shown th circular path at distance A up and down.
  • An upper position, shown in FIG. 2, of the first movement axis 7 and thus also of the target axis body 2 from the position which is particularly favorable for the target object detection and tracking, also enables the detection of target objects which are located behind or move past the raised housing 10 of the device .
  • the second movement axis 8 can also be inclined downward in order to detect target objects present in the vicinity and below the horizontal plane.
  • first movable support body and the fixed bearing body 12 are fork-shaped or in two parts in order to enclose the body to be supported, that is to say the target axle body 2 or the second movable support body 4, between two axle bearings.
  • the bearing about the third axis 9, that is, the bearing body 12, can also be integrated in the housing.
  • the defined alignment of the three axes of motion 7, 8, 9 relative to one another leads to a correspondingly simple design of operating devices to be provided in the housing 10 for the control of drives (not shown), and for the movement of the target axis body 2, the first support body 3 and the second support body 4 relative to one another or relative to the base body 5.
  • the base body 5 stands on three spindle columns 13, 14, 15, which enable the platform 11 of the base body 5 to be supported in a stable manner.
  • the device according to the invention can be used for the easy and quick alignment of a wide variety of devices which are to be aligned with an object and can therefore be referred to as a target axis body. These include, for example, laser devices, other optical devices, radar devices, or all devices whose optical or other axes are to be aligned with a target object.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

Le dispositif présente trois axes de rotation (7, 8, 9), où les premier (7) et deuxième (8) axes, considérés à partir de l'axe de visée, forment un système d'axes de pointage classique. Un troisième axe (9) disposé entre ce système et un bâti (5) du dispositif permet de tourner ce système par rapport à un axe singulier de façon que l'on puisse effectuer les mouvements de visée du dispositif avec une distance angulaire suffisante de son axe singulier, le premier axe (7) se trouvant à une distance (A) du troisième axe (9), ce qui permet une visée sans obstacle au-dessus d'un boîtier (10) contenant les appareils auxiliaires nécessaires.
EP87906988A 1986-11-03 1987-11-02 Dispositif de visee pour aligner l'axe de visee d'un appareil avec un point de mire Withdrawn EP0289538A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CH4347/86 1986-11-03
CH434786 1986-11-03

Publications (1)

Publication Number Publication Date
EP0289538A1 true EP0289538A1 (fr) 1988-11-09

Family

ID=4274402

Family Applications (1)

Application Number Title Priority Date Filing Date
EP87906988A Withdrawn EP0289538A1 (fr) 1986-11-03 1987-11-02 Dispositif de visee pour aligner l'axe de visee d'un appareil avec un point de mire

Country Status (5)

Country Link
US (1) US4953443A (fr)
EP (1) EP0289538A1 (fr)
JP (1) JPH01501245A (fr)
BR (1) BR8707523A (fr)
WO (1) WO1988003637A1 (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2662788B1 (fr) * 1990-05-31 1994-08-12 France Etat Armement Montage de tourelle et de son systeme d'observation deporte, sans angle mort.
FR2824896B1 (fr) * 2001-05-17 2003-08-15 Giat Ind Sa Systeme de pointage d'une arme
SE519151E5 (sv) * 2001-11-19 2013-07-30 Bae Systems Bofors Ab Vapensikte med siktessensorer avsett för fordon, fartyg eller motsvarande
US6820531B1 (en) * 2003-12-01 2004-11-23 Textron Systems Corporation Positioning system with continuous-range inclination and rotation angles
ITUB20151137A1 (it) * 2015-05-28 2016-11-28 Oto Melara Spa Sistema di supporto per arma da fuoco, in particolare destinato ad essere montato appeso ad una superficie superiore.

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1353499A (en) * 1919-01-29 1920-09-21 Internat Torpedo Boat Corp Gun-mount for boats
DE666317C (de) * 1935-04-12 1938-10-17 Rheinmetall Borsig Akt Ges Fussrichtmaschine fuer Geschuetze
CH196695A (fr) * 1936-12-31 1938-03-31 Sageb Societe Anonyme De Gesti Matériel d'artillerie.
GB548302A (en) * 1941-03-17 1942-10-06 Percy Smallwood Improvements in mountings for guns, searchlights and similar directional elements
NL79497C (fr) * 1946-10-23
US2762265A (en) * 1949-07-28 1956-09-11 Brev Aero Mechaniques S A Soc Gun mountings carried by movable supports
DE2037819C3 (de) * 1970-07-30 1975-02-13 Manfred 4000 Duesseldorf Graf Richtvorrichtung
SU763082A1 (ru) * 1977-07-01 1980-09-15 Предприятие П/Я Р-6930 Манипул тор модульного типа
US4367532A (en) * 1979-10-12 1983-01-04 Nordson Corporation Manually programmable robot with power-assisted motion during programming
US4326446A (en) * 1979-11-19 1982-04-27 The United States Of America As Represented By The Secretary Of The Army Linkage of actuating system for elevating gun mount
US4606695A (en) * 1984-05-18 1986-08-19 Kurt Manufacturing Company, Inc. Multiple axis robot arm
DE3436081A1 (de) * 1984-10-02 1986-04-10 Rheinmetall GmbH, 4000 Düsseldorf Einrichtung zum horizontieren einer drehbaren waffenplattform
DE3440041A1 (de) * 1984-11-02 1986-05-07 Rheinmetall GmbH, 4000 Düsseldorf Hochschwenkbare scheitellafettierung fuer das waffenrohr eines kampfpanzers

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO8803637A1 *

Also Published As

Publication number Publication date
US4953443A (en) 1990-09-04
WO1988003637A1 (fr) 1988-05-19
JPH01501245A (ja) 1989-04-27
BR8707523A (pt) 1989-02-21

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