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    • 71. 发明专利
    • DK133024C
    • 1976-08-09
    • DK625570
    • 1970-12-09
    • TAMPELLA OY AB
    • ASIKAINEN N K
    • F41F1/06F41G1/50
    • A device for automatically setting the elevation angle of the aiming attachment of a grenade launcher in response to adjusting the range scale to the desired range. The range scale is on the surface of a casing mounted on the launcher tube for rotation adjustment. A sleeve extends over the scale indicia to protect the indicia and has a viewing window with a hairline to permit accurate adjustment of the range scale casing. A cam at the end face of the casing cooperates with a follower on the support shaft of the aiming device to adjust the angular setting of the aiming device in response to setting the range scale. The range scale casing is rotatably supported by a clamp sleeve which connects the bipod to the upper end of the launcher tube. With the aiming device angle preset by adjusting the range scale, it is a simple matter to adjust the bipod to position the launcher tube at an elevation angle to fire a projectile the required range.
    • 73. 发明专利
    • NL6803039A
    • 1968-05-27
    • NL6803039
    • 1968-03-04
    • F41A23/28F41A23/54F41A27/06F41F1/06F41G1/393F41G1/50
    • 930,446. Mortars. HOTCHKISS-BRANDT. June 22, 1961 [June 28, 1960], No. 22601/61. Class 92. Relates to mortars of the type in which the gun tube A, Figs. 1, 3, in the firing position, is supported by means of a ball swivel joint L on a base plate K and by a wheeled gun carriage. According to the invention an axle 3 is rotatably mounted in a tubular element 6 of the carriage and terminates in two support arms 69 carrying the stub axles of the wheels 2 whereby in rotating the axle 3, the position of the axis of the wheels 2 relative to the gun tube and consequently the elevational position of the gun tube is varied. The carriage comprises a collar B movable along the tube A by means of a device C which provides a fine setting for laying the mortar for elevation and the collar B is supported on a cradle D and can be moved transversely thereof by means of a device E for laying the mortar in azimuth. The collar B is pivoted at 26, Fig. 5, on the cradle D and is also conreacted thereto by an elastically yieldable device F to form a triangulated support system for the tube A. The device F can lengthen or shorten when the tube A tends to modify its angular position relative to the cradle D, e.g. upon firing owing to a rearward movement of the base plate K. The cradle D is mounted on the tubular element G for pivotal movement about an inclined axis W-W contained in the vertical longitudinal plane of symmetry of the carriage and is also connected to the element G by a device H, Fig. 3, whose length is adjustable for rendering the cradle D horizontal irrespective of the transverse inclination of the element G. A device N, Fig. 4, secures the tube A against movement relative to the cradle D when transporting and a device O fixes the base plate K to the tube A when transporting. A sleeve 72, Fig. 12, provided with outer fluting 72a is welded to the axle 3 and is keyed by inner fluting to a worm-wheel 73 meshing with a worm 74 rotatable by a hand wheel 75 to effect the rotation of the axle 3. When transporting the mortar, the teeth of the worm-wheel 73 and the worm 74 are relieved from stress by means of a sliding collar 82 spring-urged to a position to engage the fluting 72a and fluting 49a provided on the tubular element G and moved to and locked in the inoperative position by a hand lever 86. The part-spherical end L, Fig. 16, of the tube engages in a part-spherical socket 93 provided in a detachable plate 94 secured to the plate K. The torque to which the tube A is subjected by the projectile of it is rifled, is absorbed by a shaft 98 engaging in an oblong aperture 99 in the end L and in round apertures 100, Fig. 17, formed in two ears 101 integral with the plate 94. The shaft 98 is pivoted to the ball L by a screw 105 whose axis Z-Z is oblique and situated in the vertical plate P-P of symmetry of the base plate. The oblong shape of the aperture 99 combined with the diamond shape of the shaft 98 (see Fig. 17) permits movement of the gun tube about the axis Z-Z for purposes of laying the gun in azimuth. The sight M, Fig. 3, is mounted by means of a dovetail assembly on the end of an arm 107, Fig. 19, fixed to the collar B. Four studs 109 carried by the arm 107 extend through holes 110 in the collar B and are spring-urged against the gun tube A by a spring 111 which bears against a washer 112 carried by one end of a stud 113 whose other end bears by means of washers 114, 115 against the support arm 107. The stud 113 is slidable in a member 116 welded to the collar B. The female part 120 of the dovetail arrangement is mounted at the end of the arm 107 in such manner as to permit adjustment of the plane of sight so as to render it parallel with the plane of fire and to cause the angle of elevation of the sight to coincide with the actual angle of elevation of the gun tube A. The female part 120 is provided with a stem 121 which is pivotable owing to the provision of a portion of a ball 122 which has a centre Q and is mounted in a part-spherical socket formed on a cup 123 rigid with the arm 107, adjustment being affected by operating a screw 124.
    • 75. 发明专利
    • FR1190536A
    • 1959-10-13
    • FR1190536D
    • 1957-07-18
    • HOTCHKISS BRANDT
    • F41G1/30F41G1/50F41G3/14
    • 840,256. Sighting apparatus. HOTCHKISSBRANDT. July 14, 1958 [July 18, 1957], No. 22449/58. Class 92. An aiming device for a weapon with barrel A on a mount C and pivotable in azimulti on a baseplate B comprises in combination a sighting apparatus E with telescopic sight and a reference device X with a flat reflecting surface or equivalent means, which when observed through the sight, indicates if the line of sight W-W is perpendicular to it; the apparatus E being slidable on a slideway D fixed on the mount C and orientable to permit reduction of the plan distance between the line of sight W-W and the axis of the weapon V-V to a length equal or less than that of the reference device X when the firing direction is changed. The barrel, pivoted on a ball a to the base-plate B is clamped at c to a yoke e with traversing screw f on a tripod b. Slideway D is a hexagonal bar 2 connected to yoke e through a ball-andspring device 3 which absorbs firing and transit shocks whilst maintaining the bar rigidly in position at an angle u to the weapons axis and at 10-20 degrees to the horizontal to provide best conditions for mean elevation and to avoid obscuration of the reference device. The sight held in a socket on a bracket 4 releasably clamped astride the bar 2. The device X is a paralleloscope having elongated mirrors 47 and 48 inclined at 90 degrees to each other in a vertical plane and mounted so that parallel rays arriving along W-W remain parallel when reflected. The device is levelled on its stand 44 by a bubble 45 and is correctly oriented when a finger 49 that is perpendicular to the mirrors is directed towards the pivot a. The weapon is aimed by aligning graticules in the field of view of the telescope with the reflection of the flap 38 on the front of the telescope seen in the mirrors of the device X; or at night, the reflection of an electric lamp situated inside the sighting telescope (Figs. 6-8 not shown). As an alternative to the flaps, lamp and mirrors, the stand 44 may carry an array of rectangular plates all parallel to the finger 49 and fixed along the length of the support 46. When these plates are viewed exactly end-on from the telescope (Figs. 10 and 11 not shown), so that their sides are not seen, the line W-W is parallel to the finger 49.
    • 78. 发明申请
    • 도수운반형 포발사체를 위한 디지털 가늠자 및 그 제어방법
    • 数字式手持式手持式投影机及其控制方法
    • WO2016072547A1
    • 2016-05-12
    • PCT/KR2014/010913
    • 2014-11-13
    • 국방과학연구소
    • 이태규장석원이진승최재건문홍기
    • F41G1/46F41G1/50F41G3/14F41G11/00
    • F41G1/46F41G1/50F41G3/16F41G11/00G01C17/00G01C19/38
    • 본 발명은 도수운반형 포발사체를 위한 디지털 가늠자 및 그 제어방법에 관한 것이다. 본 발명의 일 실시 예에 따른 도수운반형 포발사체를 위한 디지털 가늠자는 관성센서패키지 (200) 및 수동회전장치(300)를 구비하는 도수운반형 포발사체를 위한 디지털 가늠자(100)에 있어서, 상기 관성센서패키지(200)는 자이로(210) 및 가속도계모듈(220)을 포함하는 것을 특징으로 한다. 본 발명에 따르면, 박격포와 같은 도수운반형 포발사체의 사격방향 측정장비를 저가의 중저급 자이로 1개를 이용하면서도 추정오차가 적은 도수운반형 포발사체를 위한 디지털 가늠자로 대체하여 포발사체의 정확하고 신속한 타격 및 운용성 개선이 가능하다. 또한 수동회전장치 이용에 따른 전자장비의 최소화에 의하여 환경에 대한 내구성을 증대되고, 도수운반형 포발사체를 위한 디지털 가늠자의 신속한 장탈착이 가능하여 포발사로 의한 고층격 등의 극한 환경에서 핵심부품을 보존할 수 있다.
    • 本发明涉及一种手持式炮弹的数字瞄准器及其控制方法。 根据本发明的实施例的用于手持式炮弹的数字瞄准器涉及具有惯性传感器封装(200)和手动旋转装置(300)的手持式炮弹的数字瞄准器(100) ),其中所述惯性传感器封装(200)包括陀螺仪(210)和加速度计模块(220)。 根据本发明,用于测量诸如砂浆的手持式炮弹射击的拍摄方向的设备可以用具有小的估计误差的手持型炮弹的数字瞄准器代替,同时使用一个低价 中低档陀螺仪,能够准确快速地射击炮弹,提高操作性。 此外,本发明可以通过根据手动旋转装置的使用使电子设备最小化来提高对环境的耐久性,并且允许快速安装或卸载手持式炮弹的数字瞄准具,以便能够保持 在极端环境中的关键组成部分,例如由于炮击而造成的高影响。
    • 80. 发明申请
    • VORRICHTUNG INSBESONDERE ZUR ERMITTLUNG DER NEIGUNG EINES WAFFENROHRES BEIM RICHTEN
    • 设备尤其是为确定武器管角在判断
    • WO2011057756A1
    • 2011-05-19
    • PCT/EP2010/006809
    • 2010-11-09
    • RHEINMETALL WAFFE MUNITION GMBHBORCHERT, RüdigerRADCZINSKY, Stefan
    • BORCHERT, RüdigerRADCZINSKY, Stefan
    • F41G1/44F41G1/50
    • F41G1/44F41G1/50
    • Die Erfindung betrifft eine an dem Waffenrohr (1) einer großkalibrigen Waffe, insbesondere eines Granatwerfers, befestigbare Vorrichtung (2; 2') insbesondere zur Ermittlung der Neigung des Waffenrohres (1) beim Richten. Um den Neigungswinkel des Waffenrohres (1) auf einfache Weise schnell und genau einstellen zu können, schlägt die Erfindung vor, dass die Vorrichtung (2; 2') mindestens ein einem Schlauchwaagenmesssystem entsprechendes Messsystem (4; 4') umfasst, welches aus zwei beabstandeten, sich in axialer Richtung des Waffenrohres (1) erstreckenden, rohrförmigen Teilen (6, 6'; 6") besteht, die ober- und unterseitig miteinander verbunden sind. Dabei sind die beiden kommunizierenden rohrförmigen Teile (6; 6'; 6") des Meßsystems (4; 4') teilweise mit einer ersten Flüssigkeit (7) gefüllt, wobei mindestens eines der beiden rohrförmigen Teile (6) einen durchsichtigen Bereich zur Beobachtung der Lage des Flüssigkeitsspiegels (9) aufweist, der an einer Messskala (10) abgelesen werden kann.
    • 本发明涉及一种向一个大口径武器的武器发射筒(1),特别是榴弹发射器,附着设备(2; 2“),特别是用于矫直期间确定枪管(1)的倾斜度。 由武器筒的倾斜角(1)被以简单的方式快速,准确地调整,本发明提出,所述装置(2; 2“)的至少一个对应于管刻度的测量系统的测量系统(4; 4”)包括,其中除了来自两个 在延伸的枪管(1)的管状部件的轴向方向(6,6“; 6“)。存在,这是顶侧和底侧彼此连接这里,两个连通管件(6; 6' ; 6" ) (9)从一个测量标度(10)读出部分填充有第一液体(7),其中,所述两个管状零件(6)中的至少一个具有用于观察液面的位置的透明区域;测量系统(4,4“) 可以。