首页> 外国专利> Rudder device for high-speed boats, with a cavitation reducing rudder, twisted, especially completely suspended

Rudder device for high-speed boats, with a cavitation reducing rudder, twisted, especially completely suspended

机译:用于高速船的舵装置,带有减少气蚀的舵,扭曲,尤其是完全悬挂

摘要

Rudder device for high-speed vessels with a twisted rudder, with cavitation reducer, comprising a rudder blade with a propeller (115) associated with the rudder blade and arranged on a driving axle (PA), as well as an axle of rudder (140) attached to the rudder blade (100), in which the rudder device (200) a) is formed by a rudder blade (100) that has a thin profile with a reduced thickness composed of two segments of shovel (10, 20) with the same height or with different heights, arranged one above another, with a lower blade segment (20) having a reduced height with respect to the height of the upper blade segment (10) and with edges of attack (11, 21) directed towards the propeller (115) that present a profile approximately semicircularly and that are positioned such that an attack flange (11) is laterally shifted to port (BB) or starboard (SB) and the other edge of attack (21) is offset laterally te starboard (SB) or port (BB) with respect to the medialongitudinal line (LML) of the rudder blade (100), and in which the surfaces of the side walls (12, 13; 22,23) of both rudder blade segments (10, 20) converge on a final edge (15) directed away from the propeller (115), a1) in which both leading edges (11, 21) and the edge end (15) extend downwards narrowing conically and reducing cross-sectional surfaces (30) from the upper zone (OB) to the lower zone (UB) of the rudder blade (100), a2) or where the final edge (15) extends rectilinearly and parallel to the axis (140) of the rudder and the two leading edges (11, 21) extend downwards narrowing conically and reducing the size of cross-sectional surfaces (30) from the upper zone (OB) to the lower zone (UB), a3) in which two rectilinear side wall segments (16; 17; 26, 27) have the same length in pairs and the cross sections between both segments of side wall (16, 17; 26, 27) have the same size and are symmetrically shaped, a4) in the that the distance between a side wall segment (18; 28) that extends in an arc-shaped way with respect to the longitudinal midline (LML) is greater than the distance between a lateral wall segment (19; 29) that extends very arched with respect to the longitudinal midline (LML) ), and the cross sections located on both sides of the longitudinal midline (LML) between the two lateral wall segments (18; 28) that extend in the form of a flat arc are formed asymmetrically deformed, and b) is formed by an axis of rudder (140) with at least one bearing which acts in functional synergy with the rudder blade (100), and b1) in which the shaft (140) of the rudder is arranged together with the limera tube (120), in the one that is removed, in the area of the greatest profile thickness (PD) or between it and the leading edges of the upper blade segment (10) and extends with its fixing device (145) at the end through the entire height of the upper shovel segment (10), b2) in which the limera tube ( 120), deeply sunk in the upper shovel segment (10), to choose (140) the rudder is equipped, as a cantilever arm, with a longitudinal internal hole (125) in the center to receive the rudder shaft (140) , b3) in which the cross section of the limera tube is made with thin walls and the delimiting tube (120) has a neck bearing (130) on the side of the inner wall to receive the axis (140) of the mirror, and b4 ) in which the shaft (140) of the rudder protrudes in its final zone (140b) with a section (140a) of the tube (120) and is connected at the end of this section (140a) with the upper blade segment ( 10), characterized in that c) the cross sections (31) of the upper (10) and lower (20) blade segments have in the area between the final edge (15) and the greater profile thickness (PD) of the blade of the rudder (100) a length (L) corresponding at least 1½ times the length (L1) of the cross sections (32) of l Upper (10) and lower (20) blade segments between the thickest area of the profile (PD) of the blade (100) and the leading edges (11, 21), c1) the upper blade segment (10 ) has a port side (BB) and the lower blade segment (20) has a starboard (SB) two side wall segments (18, 28) that extend in a flat arc from the leading edges (11, 21) in the direction at the end edge (15) with a length (L2) corresponding to the length (L'2) of the side wall segment (18) from the leading edges (11, 21) to the area of greater profile thickness (PD) more a length (L''2) corresponding at least 1/3 of the length (L'2), being arranged next to the side wall segment (18, 28) in the form of a flat arc or side wall segment (16, 26) rectilinear ending at the end edge, and c2) the upper blade segment (10) has starboard (SB) and the lower blade segment (20) port (BB) both segments of lateral wall (19, 29) strongly arched extending from the leading edges (11, 21) in the direction of the final edge (15) with a length (L3) that extends along a length (L'3) of the segment side wall (19) from the leading edges (11, 21) to the area of greater profile thickness (PD) plus a length (L''3) corresponding at least 1/3 of the length (L ' 3), the rectilinear side wall segment (17, 27) ending at the end edge (15) being disposed next to the side wall segment (19, 29).
机译:用于带有扭转舵的带有减气蚀作用的高速船舵装置,包括带有推进器(115)的舵叶,该推进器与舵叶相连并布置在驱动轴(PA)上,并且舵轴(140) )连接到舵叶(100),其中舵装置(200)a)由具有薄轮廓且厚度减小的舵叶(100)形成,该轮廓由两段铲子(10、20)和相同高度或不同高度,彼此叠置,下刀片部分(20)相对于上刀片部分(10)的高度减小,并且攻击边缘(11、21)朝向呈大致半圆形轮廓的螺旋桨(115)的位置使得攻击法兰(11)侧移到左舷(BB)或右舷(SB),而攻击的另一边缘(21)则横向偏向右舷(SB)或端口(BB)相对于产品的纵向中线(LML)舵叶片(100),其中侧壁(12、13;两个舵叶节段(10、20)的22,23)会聚在背离螺旋桨(115)的最终边缘(15)上,a1),两个前缘(11、21)和边缘端部(15)从舵叶(100)的上部区域(OB)到下部区域(UB)向下锥形收缩并减小横截面(30),或者最终边缘(15)直线延伸并平行于舵的轴(140)和两个前缘(11、21)向下延伸,呈圆锥形变窄,并减小了从上部区域(OB)到下部区域(UB)的横截面(30)的尺寸a3 ),其中两个直线形的侧壁段(16; 17; 26,27)成对地具有相同的长度,并且两个侧壁(16,17; 26,27)的段之间的横截面具有相同的尺寸并对称地成形,a4)在于,相对于纵向中线(LML)以弧形方式延伸的侧壁段(18; 28)之间的距离大于dist侧壁段之间的距离(19; 29)相对于纵向中线(LML)非常拱形地延伸,并且位于两个侧壁段(18; 28)之间的纵向中线(LML)两侧的横截面以a的形式延伸圆弧不对称变形而形成,并且b)由舵轴(140)形成,至少有一个轴承与舵叶(100)发挥功能协同作用,而b1)由舵轴(140)构成。方向舵与角膜缘管(120)一起布置,在被移除的那根管中,在最大轮廓厚度(PD)的区域内或在其与上叶片部分(10)的前缘之间,并随着其固定而延伸装置(145)穿过上铲段(1​​0)的整个高度b2),在其中,深沉在上铲段(1​​0)中的the骨管(120)选择方向舵(140)作为悬臂在中心处装有纵向内孔(125),以容纳舵轴(140), b3),其中角膜胶管的横截面是薄壁的,而定界管(120)在内壁的侧面上有一个颈部轴承(130),以容纳镜子的轴(140),b4 ),其中舵轴(140)在其最终区域(140b)中伸出管(120)的一部分(140a),并在该部分(140a)的末端与上叶片部分(10)连接),其特征在于c)上叶片(10)和下叶片(20)的横截面(31)在最终边缘(15)和叶片的较大轮廓厚度(PD)之间。方向舵(100)的长度(L)至少是截面的最厚区域(PD)之间的上叶片(10)和下叶片(20)的截面(32)的长度(L1)的1.5倍。叶片(100)和前缘(11、21),c1),上部叶片部分(10)具有左舷(BB),下部叶片部分(20)具有右舷(SB)两个侧壁部分( 18、28)从前缘(11、21)沿端缘(15)的方向以一条平弧线延伸,长度(L2)对应于从前缘开始的侧壁段(18)的长度(L'2)边缘(11、21)到轮廓厚度(PD)更大的区域,而长度(L''2)至少对应于长度(L'2)的1/3,并与侧壁段(18)相邻布置,28)呈圆弧形或侧壁段(16、26)的形式,在端部边缘处直线终止,并且c2)上部叶片段(10)具有右舷(SB),下部叶片段(20)的端口(BB)侧壁(19、29)的两个部分从前缘(11、21)沿最终边缘(15)的方向从前缘(11、21)强烈拱起,并沿长度(L'3)延伸段侧壁(19)的前缘(11),21)到更大轮廓厚度(PD)加上长度(L''3)的区域,该长度至少等于长度(L'3)的1/3,直线侧壁段(17、27)终止于端部边缘(15)紧邻侧壁段(19、29)设置。

著录项

  • 公开/公告号ES2385822T3

    专利类型

  • 公开/公告日2012-08-01

    原文格式PDF

  • 申请/专利权人 BECKER MARINE SYSTEMS GMBH & CO. KG;

    申请/专利号ES20080016049T

  • 发明设计人 LEHMANN DIRK;

    申请日2008-09-11

  • 分类号B63H25/38;

  • 国家 ES

  • 入库时间 2022-08-21 17:21:03

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号